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,- PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS O-ZERO ENGINEERING NOTE # 3823.11 5- EN-416 February 20, 1995 rev. 6/26/95: changes in italics
Transcript
Page 1: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

shy

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995 rev 62695 changes in italics

) ) )

sc~ ICS ((ZScDJ

[1-2 otJl(] 38 OD x 0049 N2 tubes

1 12 sch 105 pipe58 OD x 0049 He supply

j

I A Sch 105 He return 55

34 00 x 0065 He Cooldown return

He Cool downQuench Return x 0065 Cu Rod shield

Solenoid xfer ineMain Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

RE-I =-lljqr NIIT -r 5cAl_E

Plothd rue Fb 21 153829 CST 1995 by rucinki

~lGU~pound 1 N

) ) )

I

I

~

~ 00 x 0049 LN2 supply

p I ~ ~ 00 x 0065 Cu Rod shield o

~ Sch lOS pipe 450 00

II 5CH IDS ~lXLxO bull049~ N2 return

It bullbull =r O[) 0 Cj

~-oo-re-e35 He It

5e

1gtlt- 00 x O 049 He

VLPC transfer line

PRELIMINARY B ILDING TRANSFER LIN o SIGNS Russ Rucinski 22195

REII -jtqjqS tJor ro Sltteuro

Plott Tu feb 21 153732 CST Itt by rucinki

F GUJltE 2

0J

) )

SOlENOID PIPE SECTIONS~6Le i

LINE ~ pe$CflPTON DEi flDt 12

4 UIE SUPPL Y (HUTl) U-TUBE LHEDEWAR X-FER LINE

5 UIE SUPPLY XmiddotFERLINE U-TUBE U-TUBE

6 UIE SUPPLY (liUT1) U-TUBE X-FER LINE CONTROLOOWAR

7 UIE RETURN (HUTS) U-TUBE (DNTROL DEWAR X-FER LINE

8 LHE RETURN X-FER LINE U-TUBE U-TUBE

9 HE RETURN U-TUBE X-FER LINE X-FER LINEflPC)

10 LN2 SUPPLY U-TUBE LIN HEADER X-FER LINE

11 LN2 SUPPLY XmiddotFERLINE UmiddotTUBE TIE

12 LN2 SUPPL Y (SHIELD X-FER LINE TEE U-TUBE

13 LN2 SUPPLY (SHIELD) U-TUBE X-FER LINE CONTROL DEWAR

SUPPLY

_ 14 LN2 (INTERCEPT) X-FER LINE TIE U-TUBE

SUPPLY

_ 15 LN2 (INTERCEPT) U-TUBE XmiddotFERLINE CONTROL DEWAR

_L LN2 RETURN (SHIELD) U-TUBE (DNTROL DEWAR X-FER LIlltE

~7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE U-TUBE

18 LN2 RETURN (SHIELD) U-TUBE XmiddotFER LINE TEE -shyRETURN

19 LN2 (INTERCEPT) lImiddotTUBE CONTROL DEWAR X-FER LLltlO _ ---shy

RETURN

2_~__ IN2 (INTERrEPT) X-FER 111 ii-TIlliE lImiddotnlBE

RETURN

22 LN2 (INTERCEPT) UmiddotTUBE X-FER LINE TEE _

2_3 LN2 RETURN U-TUBE 1EE GN2 VENT HEADER

(COOLDOWNI

24 HE QUENCH) U-TUBE CONIROL DEWAR X-FER LINE -

(COOLDOWNI

25 HE QUENCH) X-FER LINE UmiddotTUBE U-TUIlE

(COOLDOWNI HEmOLDOWN

26 HE QUENCH) U-TUBE X-FER LINE RETURN

SUPPLY 27 HE (COOLDOWN) U-TUBE COOLr)OWNLINE _ JCiliLrr-E___

PIPE OR ruBE ItliIDi LIHiAB UE sect1m DlA ONI LENGTH IFTI ELBQWI

314 00 X 00S 068 5 2

SIS 00 X 049 0527 125 9

314 OD X 035 068 10 2

314 OD X 035 068 10 2

D~iO= 0 Concentric IM1 12S 9

314 00 X 03S 068 3 2

38 begt 1gt11 bull Z7

112 9 t ms ~ 3 2

~middotQDoLj t 1 1li1l9904I ~ 1 1

38 00 X 049 0277 124 9

112 00 x 035 043 10 2

318 00 X 049 0277 124 9

112 00 x 035 043 10 2--

112 00 x 035 043 iO 2

3S 00 X ()9 0277 125 9

liZ OD x 0)5 043 I-(-------- shy

li2 00 x 035 043 III 2---cshy --shy

18 OJ) X (149 0277 125 9

112 00 x 035 043 1 1

112 OD x 035 043 5 1

I S~H 10 bull (14 ~~ O5lshy 10 2

1 SC tC eo-l -3141 QD X 96S -~6i- 125 9

12S I1IO pound11 --3iImiddotGIH(~S- 06S 5 2

34 00 X()amp 068 5 _ 4

IED IIEU nmu

THRURUN IMHCtI ~

0 0 0

4 0 IDIVRTR

0 0 0

0 0 0

4 0 1 PVICV

0 0 0

0 0 0

0 0 0

2 I 1 PV

0 0 0

2 1 1 PV

0 0 0

0 0 ()

2 0 0

0 I ()

0 n I-shy --shy -------shy

2 n

0 1 0

0 0 0

0 0 0

_2 ~ 0 0 -----shy

0 0 ~-r---

0 0 10IVRTR

AI m

~~ (J~

til ~ Page

5 -

-

lHEOEWAR

H wesTHESUPPLY X-flRUNE a-WAY VALVE

H WEST HESlFPLY lJ1IJBE CHFEEDcoH

44 H wesTHESUPPLY X-flRUNE BAYONETcoH

45 H wesT HE SUPPLY x-FERUNE VALVE BOX

46 HE EMTHE SUPPLY X-flR UNE lJTUBE a-WAYVALVe

47 EMT HE SUPPLY X-flRUNE a-WAYVALVE

X-FBI UNE a-WAY VALVE Unee

CHFEEDCAN

X-flR IJNE BAYONET coH VALVE BOX

X-FER UNE VALVE BOX

UNE VIPC

RElUlN x-FERUNE a-WAYVALVE

57 H EMTHERETURN x-FERUNE a-WAY VALliE

5amp H wesT HE RElUlN X-FBI UNE VIPC

59 wesTHERElUlN X-FBIUNE IIALVEBOX

60 H wesTHERETUlN lJ1JBE BAYONETCAN

61 H wesTHE RElUlN X-flR UNE CH FEEDcoH

62 HE wesT HE RETURN XfER UNE a-WAY VALVE

63 H wesTHERETUlN X-flR UNE 3-WAY VALVe

RETUIN X-flR UNE a-WAY VALVE

X-FER UNE FER UNE

AHFEEDcoH

AHFEEDCAN

68 LN2 SUlPlY IIQ HEADER AHFEEDCAN

LN2 SUlPlY XfER UNE AH FEED CAN CHFEEDCAN

70 LN2 SUlPlY BAYONET CAN

71 LN2 SUlPlY X-ROR UNE BAYONET CAN VALVE BOX

LN2 SUPPLY XfERUNE VALve BOX VlPCWEST

73 LN2 SUPPLY XfER UNE VALVE BOX VLPCEAST

74 LN2 SUPPLY XfER UNE VtfC WEST VALVE BOX

75 LN2 SUlPlY XfER UNE VLPC EMT VALliE BOX

76 XfER UNE VALVE BOX BAYONET CAN

BAYONET CAN

CH

AHFEED

-0)( gaS _

II

fIIi ee M 885

0

-shy

12

47

24

2

2

123

12

47

24

47

24

24

24

24

2 o

o

o o

9

2 o

2 o

o

2

o

o

o

9 2

2 o

o

6

3

o o

o

2

o o

o

If

o 10V

o o

o o

o o

o

o

1011

o o

o o

o 1 PV

o

o o

1011

I CV

I CV

o I PV

o o

o

10V

2 I CV

ICV

I CV

o

o o

1 PV

I PV

o

o

o o

o

o

-

Page I

JCa

Solenoid Helium Steady State Pressure drops - Some preliminary calculations were done to estimate the steady state helium heat

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 The return pipe line 8 was looked

into further See appendix L It was determined that a 1 112 sch 10 pipe will be used

giving a hydraulic radius of1057 The total steady state pressure drop then is on the

order of01 psi for the piping Allowing all the pressure drops to occur across control

valves

Solenoid Nitroeen flowrates and pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cool down flowrate shall not exceed 5 gls

With the current selected pipe sizes nitrogen flow will less be than 5 gls until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gls

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix G

VLPC Helium CooJdown flowrates The LHe line sizes for the VLPC were determined by first calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc II of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

-

STEP VLPC TEMP

[K]

GAS TEMP IN rKl

GAS TEMP

OUTrKl

TIME [hrs]

MASS FLOW RATEREQD

[ws] 1 300 to 250 200 250 10 84 2 250 to 200 150 200 10 89 3 200 to 150 100 150 10 92 4 toO to 90 80 90 4 31

-

-------~- ----- ----- ------------------------- shy

17

- It was concluded that step 4s pressure drop would be about 36 times larger than step 1 IS

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet

temperature of 80K and an outlet temperature of 90K (refer to appendix D)

VLPC Helium Cool down Pressure drops A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 4

for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the

given pipe sizes and inletexit states The VLPC cooldown piping was first sized by

assuming a pressure drop of 95 psig an inlet temperature of 80K GHe and an outlet

temperature of 90K through the supply and return lines respectively Resistance

coefficients were calculated for four segments of the piping In the second step of the

calculation pressure drops were calculated for each segment taking into account the

change in density due to changes in pressure Summing the individual pressure drops

resulted in a rough estimated pressure drop of 591 psi These numbers are summarized

in table 9 for the initial supply size of318 OD and return size of112 OD tubes See

Appendix E for the raw calculations After looking at steady state pressure drops the

line sizes for the supply and return were increased to 112 OD and 518 OD respectively

Therefore pressure drops listed in Table 9 will be less

Table 9 VLPC Helium Cooldown piping pressure drop summary

for 318 supply amp 112 return sizes

PIPE SECTION PRESSURE DROP (PSIA)

Supply line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

-

-

15

- VLPC Helium Steady State Pressure drops

-

The expected pressure drop for 318 OD x 0035 wall supply tubing for a steady

state flow of5 gls and a transfer line heat load of lOW was conservatively estimated at

46 psi per 100ft This prompted the increase in size to 112 OD x 0049 wall tubing

The calculated pressure drop for the two phase supply would be 12 psi per 100ft

Backing offon the conservatism and figuring approx 200ft ofequivalent length a real

estimate ofthe supply pressure drop from the refrigerator to the VLPC cryostat is about 1

psi See Appendix H page H4

The expected pressure drop for the return 518 OD x 0049 wall tube with 5 gIs

65 K gas flowing is 06 psig Since the supply and return tubing accounts for less than 2

psi pressure drop there is approximiately 10 psi available across the control valve and

cryostat See Appendix H page H3

VLPC Nitro~en flowrates and pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 OD Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

~~~~~~ ~- ---~-~----~ --_ --------------------- shy

lC

- Table of Contents for the Appendices

Raw En2ineerin2 Calculations

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

Appendix L Solenoid steady state cales Helium return piping

-

-

-0 FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3B23115 SERIALmiddotCATEGORY

11 I PAGE

SUBJECT NAME

- (LPC Rl5~ RUCIf-Jst

CO t-J S f D ER ~-r~bf j -p ( e-e -t 0 S 1 A 1 S ~

CJ Svlt-CNoD Dc-gtICIr-J RE-POliL-r QC)fA1- - 270 VII ) 141601-1

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1 J vM(Jfpound(J5 Q1~o- = 180 tAJ bull

-

20 w

Sla DD 0 315 1AJA1-L id =- ~os ee = 4M 4middot (00437gt ~s)

D~ IT (305 )( OlS~ MN) ( I 72 k ~ 10- b Pec-S)

-41421 -f=oI3 l Z

(i) = I 3 AP 3 ~119j bull 0 ~ Ll -= L d Ii

(I 00 f-L~ K (0 Ii) 3 5 Sf

ItO ~ k

-

11

c_ bull OQ435 s -

--------_------------shy

I HZ 5- 3c-75pf1EN 01gtc f-1- (trCvLATlCIJ)

1r 1)7

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t-A 5Jh Z 0 i) gtlt a 0 lt-I~ AJJ I b5k -cb- O-1OZ1 cgtO(oz- gt 012 MI)~ L-= 200t-i roO9GM

v (m ) e --~ (z) (1r- DA )

-( il -J

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l) - - l lQ [ r) 2~

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( ( I ~ IS (82 amp8 ~gt1-= (~lt17 b lt013)( o elY) ( 4gt0 cr or) llaquo

2 5 b 8z (8 gt0 z 2-7 psi

--- --~----- ----~ - ~-~------ - -~- ---------shy

H-3 J I

-

r i~ - r- ~-t~ -shy6 -= 081 ~ Jfi L s __ O~ k

i -

e~ It~ Jo~ -1- 7Z 7lt alt ~- 5

N --=- 000 y~ Jias

j b5 1lt

Plt= 64 )-t

-

I L

SUBJECT NAME

- SUPPLlt( DATE(pZ 10 ~ IREVISION DATE

It-w FERMILAB

ENGINEERING NOTE SECTION PROJECT SERIAl-CATEGORY

3S23 I IS PAGE

rl4

3 III - (ImiddotTJ3~ T -z w TlANrrut l1-W -lo jr W -~ 1- I w mAlS L i rJ C

5~ I C ~ 1 1 ( LEA t 1=20M t-I-tlt ~1ClttA ampe i)wA-rt 10 LPC Clt-(os -rk-r

5TA-re(j)

t Ik- pewAn ~~-r L10

- L4 ~o ~

p 9 ( 5 i9 5 A $TAI

hl 1 Be J -

o Pz e M 16MPa = 95 fJ~(j ~L 11flP

-d- = ZYIl

Xl--= ~-~-Fo 158~119h 032 yj - kF ~f 1t--1I96

Afo()

S TIlO

Vft TtJ~ =- 6Po() 2 f5i

L~f-l E(t S P(2UbAb-Y ~~ v 1 VPltL-~( -ru ZfJO Ff

-

FERMILAB

ENGINEERING NOTE SECTION

RDIDcent PROJECT

He -y Fe12 SERIALmiddotCATEGORY

3S23IlS PAGE

LI SUBJECT 2-J

P HE RerulZJ =gt P toJ

50- e jJlH 0

NAME

DATE IREVISION DATE

5Z-hQ5 1

~iTATe Q)

P =I g A-rM

5Ar lGUID

1- 4l( 1lt

hjZ - 14 Bb lId

S-AIE hls 2 b35

S 1) sPec

~-IG CD P2 = I 2 MPoshy(z= _0

Y11Vd =30 b Jr

Mz I ~~

1 Sbil shy 1107

30 1-1107

s z lt3) 2 cent

P3 -=IZ ~ PA T Lj~IK

39 Yf ) = 5

~ HL 0 c( 3 ~ F-O

h middot07 J~ h~ 30 b-l~

)(~ 387

-

I

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)

FERMllAB

ENGINEERING NOTE SECTION PROJECT

Jle x Fampltt ( tlJ Ii

SERIAL-CATEGORY

38 Z- 3 bull Il $ PAGE

L2 SUBJECT

He NAME

IREVISION DATE DATE

5-30 -atS

IIFo(t 1i1 ~)( CQoj 0 bull 11 )t-I ~ ~) Afo-JO A Scu [0

P 1tJG IIJJ I cent 511 11 0D DI-f = L2

A

Ilz S CI-L 10 P IPG-) ID = I =gt82 I

t bull oS loJ

IS 35 00shy-I( 0 D J-- Felt -rtt IS S 12Gt

-

stlnput

000005

427 200

4 1211 2017 318 1323 000082 3876

-2 2 184 184 20

12 998

073 1000

shy

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

deltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 BakerXa BakerYa c M RsubL RsubG GasVel Liqvel

Output

accurate

turbulen 01906103

ft in ft

92387E-5 m2 gs kgm 3 kgm3 JlPa-s JlPa-s Nm

90430 0024496 kgS

137600 0015504 kgs 51012286 pam 16810555 Pam

14863285 psig

57405518 67244052

1 4281346 kgmA 3 kgmA 3

53412427 Nm JlPa-s

1210 8660 lbmhr-ft

1 1 17419928 82580072 1 0075104 ms 12568736 ms

Comment L3 Russ Rucinski 53095 Return He pipe for Solenoid 1 pipe w 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

model validity

flow type friction factor Must enter a guess pipe roughness Pipe inside diameter Length of pipe cross sectional area Total mass flow rate Liquid density density of the gas Liquid viscosity Gas Viscosity Surface tension of liquid quality = mdotGmdot Reynolds for liquid Mass flow rate for liquid Reynolds for gas Mass flow rate for gas AP1lL for the liquid AP1lL for the two phase

Total pressure drop for the pipe ~ 100 ~JGtcs 1b uu Stu

Lockhart-Martinelli parameter Lockhart-Martinelli parameter L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 Baker diagram dimensionless parameter density of air density of water Baker diagram dimensionless parameter Surface tension of water viscosity of water X - axis value for Baker plot Y-axis value for Baker plot

Volume fraction of liquid phase Volume fraction of gas phase Gas velocity Liquid velocity

000005 1057 200

4 1211 2017 318 1323 000082 3876

shy

2

25

184

316 20

12 998

073 1000

-

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

rdeltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 Bakerxa BakerYa c M RsubL RsubG GasVel LiqVel

Output Comment Russ Rucinski 53095 Return He pipe for Solenoid 1 12 pipe wi 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

accurate model validity

turbulen flow type 02260289 friction factor Must enter a guess

ft pipe roughness in Pipe inside diameter ft Length of pipe

00056612 m2 cross sectional area gls Total mass flow rate kgm 3 Liquid density kgm3 density of the gas JLPa-s Liquid viscosity JLPa-s Gas viscosity Nm Surface tension of liquid

quality = mdotGmdot 36530 Reynolds for liquid

0024496 kgls Mass flow rate for liquid 55580 Reynolds for gas

0015504 kgls Mass flow rate for gas

0650814 Palm LP I LU for the liquid 21275204 Palm LPLU for the two phase

01881077 psig 1 Total pressure drop for the pipe

57175294 Lockhart-Martinelli parameter 67767548 Lockhart-Martinelli parameter

L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719

1 4281346 Baker diagram dimensionless parameter kgm3 density of air kgm3 density of water

53412427 Baker diagram dimensionless parameter Nm Surface tension of water JLPa-s viscosity of water

1210 X - axis value for Baker 1410 lbmhr-ft Y-axis value for Baker

1 1 17490072 Volume fraction of liquid phase 82509928 Volume fraction of gas phase 16456003 ms Gas velocity 20429237 ms Liquid velocity

53095 middot

FERMILAB TWO PHASE HEUUM FLOW TESTS

) )

Russ KUCt~5~l

10 ~ 1 I UAUEOOV

11 ~7 I I I Flow Fath Flaw

~--- Annular Flow Wave Flow

------ Slug FlowI

A tf SIO ______

~gt

---IIMIR RIGIMI BOUNDARIII ~ G bull RCtPtC GAl OW RAlI -- ClFtC LIQUID now RAT ~l-III _lIN_

10 I I ~I gt bull I I

MaMIIow_

X 5SVI PI U bull MIddIt of IOIItnoId

1 10 VI PI bull bull Ex of IOIItnoId

18 VI PI 7 bull 1111111 of control dewarbull Figura 1 Baker diagram with Mamedov curves or two phase helium In horzonlal channels

[FttoJIA Djli El 38 23IlJ -Gt-J - 33 8 ]

r J1

01 10 10 10 ( 10 i ~ ~ 10 ~ ~ 10 L ~nG CAt 0 )V rPl

~ IMaIIon TIJampE

0J

PIPE

112 5C~ 10 f 5eCD

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995

Russ Rucinski and Steve Sakla ROOQJ Mech

Approved _________

-

n ~ middotrt -

Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

-------------~ ~~~--~~~~--

Ud

)

) ) f

J8 CO bull 0049 N2 tu~bullbull

58 CO bull 0049 He Supply 1 12 sch lOS pipe

l Sch lOS H return SS

J4 CO bull 0065 He Cool down return

He Cool downQuench Return 25 CO bull 0065 Cu Rod shield

Main Solenoid xfer ine Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

Potta 1 rb 21 153121 CST ~ by rwcnoi

~lGUJCE 1

N

)J

1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

i foE 9flIIy 1JTAlE rlTX6 AHFEEDCAN 112 00 X 049 0402 5 2 0 0 0

tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

I

bull VIJIC iliil-flH Ie FT I

I I i I bullbullOF IUlaWS IN 8 i I

I1Igel

I Ibull I

9 o 2 III J o en

L

FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

~I_ i 50 Uf-bln 3823 _ c NAME

Russ

ili2 -J-1 U ~io-pound lIJJoJ~l-c sc O~Il~ I-(JoTI CAJI60e Igt r_I Z S~ Z -n r Z Z Ilt r Zmiddot

J o N

(

N N

H

I

J

1 shy

c e-l ~w ~ UI

CIgt

~1

FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

~ )

-shy

~ M )

f ltgt0 ~O~ I 0 bull ~

If g -rI ~ t shy ~T

0

~ r

~ -a

-r

0 0

-Sci

bull~

~ ~

i-T

intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

-1(IL------- ~ ~l

-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

d (-10 ( ~raquo

839qYY --(Motte

25 lie SL 20

~ d51-

7 Sbull 2shy3 2 3 472

- ~

-- ---------- raquo

b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

1 EAIJgtltf lt FR61V tJ L c(Lflc lilA ~K

f~nr - ~- ALVMtJUM

SA 4 2otJ K 6~ oJ I 270 ~ amp-A5 our

h(7vr 1311~h lN ~ 1054 ~

-k-shy - - = A ATWO 1r (tgt15)(O4~[51))

o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

CaN-IIJfIIO vJ( 1--4 vt P~eAJ(1 of J-II TLJIi AJ ~fe~ AceA

A I) CDEFtIrL~ ib COOItgt()~J A-r (tATamp 0 5 ~A

o7b 10 T I ~ l

~tlcIio 60 it S ) ( lOS 5 ~ -q SJf) )l 3 CO os

STEP 3

S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

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(

It V

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ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

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1-lb-95 IREVIS10 OA TE

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PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

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V I r ~~~r ~fO ~ V

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-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

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I cto J _ ~ -F(3

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00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

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A V

SUBJECT

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FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

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A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

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FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

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115 W r 1

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NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

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SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

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K2

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lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 2: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

) ) )

sc~ ICS ((ZScDJ

[1-2 otJl(] 38 OD x 0049 N2 tubes

1 12 sch 105 pipe58 OD x 0049 He supply

j

I A Sch 105 He return 55

34 00 x 0065 He Cooldown return

He Cool downQuench Return x 0065 Cu Rod shield

Solenoid xfer ineMain Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

RE-I =-lljqr NIIT -r 5cAl_E

Plothd rue Fb 21 153829 CST 1995 by rucinki

~lGU~pound 1 N

) ) )

I

I

~

~ 00 x 0049 LN2 supply

p I ~ ~ 00 x 0065 Cu Rod shield o

~ Sch lOS pipe 450 00

II 5CH IDS ~lXLxO bull049~ N2 return

It bullbull =r O[) 0 Cj

~-oo-re-e35 He It

5e

1gtlt- 00 x O 049 He

VLPC transfer line

PRELIMINARY B ILDING TRANSFER LIN o SIGNS Russ Rucinski 22195

REII -jtqjqS tJor ro Sltteuro

Plott Tu feb 21 153732 CST Itt by rucinki

F GUJltE 2

0J

) )

SOlENOID PIPE SECTIONS~6Le i

LINE ~ pe$CflPTON DEi flDt 12

4 UIE SUPPL Y (HUTl) U-TUBE LHEDEWAR X-FER LINE

5 UIE SUPPLY XmiddotFERLINE U-TUBE U-TUBE

6 UIE SUPPLY (liUT1) U-TUBE X-FER LINE CONTROLOOWAR

7 UIE RETURN (HUTS) U-TUBE (DNTROL DEWAR X-FER LINE

8 LHE RETURN X-FER LINE U-TUBE U-TUBE

9 HE RETURN U-TUBE X-FER LINE X-FER LINEflPC)

10 LN2 SUPPLY U-TUBE LIN HEADER X-FER LINE

11 LN2 SUPPLY XmiddotFERLINE UmiddotTUBE TIE

12 LN2 SUPPL Y (SHIELD X-FER LINE TEE U-TUBE

13 LN2 SUPPLY (SHIELD) U-TUBE X-FER LINE CONTROL DEWAR

SUPPLY

_ 14 LN2 (INTERCEPT) X-FER LINE TIE U-TUBE

SUPPLY

_ 15 LN2 (INTERCEPT) U-TUBE XmiddotFERLINE CONTROL DEWAR

_L LN2 RETURN (SHIELD) U-TUBE (DNTROL DEWAR X-FER LIlltE

~7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE U-TUBE

18 LN2 RETURN (SHIELD) U-TUBE XmiddotFER LINE TEE -shyRETURN

19 LN2 (INTERCEPT) lImiddotTUBE CONTROL DEWAR X-FER LLltlO _ ---shy

RETURN

2_~__ IN2 (INTERrEPT) X-FER 111 ii-TIlliE lImiddotnlBE

RETURN

22 LN2 (INTERCEPT) UmiddotTUBE X-FER LINE TEE _

2_3 LN2 RETURN U-TUBE 1EE GN2 VENT HEADER

(COOLDOWNI

24 HE QUENCH) U-TUBE CONIROL DEWAR X-FER LINE -

(COOLDOWNI

25 HE QUENCH) X-FER LINE UmiddotTUBE U-TUIlE

(COOLDOWNI HEmOLDOWN

26 HE QUENCH) U-TUBE X-FER LINE RETURN

SUPPLY 27 HE (COOLDOWN) U-TUBE COOLr)OWNLINE _ JCiliLrr-E___

PIPE OR ruBE ItliIDi LIHiAB UE sect1m DlA ONI LENGTH IFTI ELBQWI

314 00 X 00S 068 5 2

SIS 00 X 049 0527 125 9

314 OD X 035 068 10 2

314 OD X 035 068 10 2

D~iO= 0 Concentric IM1 12S 9

314 00 X 03S 068 3 2

38 begt 1gt11 bull Z7

112 9 t ms ~ 3 2

~middotQDoLj t 1 1li1l9904I ~ 1 1

38 00 X 049 0277 124 9

112 00 x 035 043 10 2

318 00 X 049 0277 124 9

112 00 x 035 043 10 2--

112 00 x 035 043 iO 2

3S 00 X ()9 0277 125 9

liZ OD x 0)5 043 I-(-------- shy

li2 00 x 035 043 III 2---cshy --shy

18 OJ) X (149 0277 125 9

112 00 x 035 043 1 1

112 OD x 035 043 5 1

I S~H 10 bull (14 ~~ O5lshy 10 2

1 SC tC eo-l -3141 QD X 96S -~6i- 125 9

12S I1IO pound11 --3iImiddotGIH(~S- 06S 5 2

34 00 X()amp 068 5 _ 4

IED IIEU nmu

THRURUN IMHCtI ~

0 0 0

4 0 IDIVRTR

0 0 0

0 0 0

4 0 1 PVICV

0 0 0

0 0 0

0 0 0

2 I 1 PV

0 0 0

2 1 1 PV

0 0 0

0 0 ()

2 0 0

0 I ()

0 n I-shy --shy -------shy

2 n

0 1 0

0 0 0

0 0 0

_2 ~ 0 0 -----shy

0 0 ~-r---

0 0 10IVRTR

AI m

~~ (J~

til ~ Page

5 -

-

lHEOEWAR

H wesTHESUPPLY X-flRUNE a-WAY VALVE

H WEST HESlFPLY lJ1IJBE CHFEEDcoH

44 H wesTHESUPPLY X-flRUNE BAYONETcoH

45 H wesT HE SUPPLY x-FERUNE VALVE BOX

46 HE EMTHE SUPPLY X-flR UNE lJTUBE a-WAYVALVe

47 EMT HE SUPPLY X-flRUNE a-WAYVALVE

X-FBI UNE a-WAY VALVE Unee

CHFEEDCAN

X-flR IJNE BAYONET coH VALVE BOX

X-FER UNE VALVE BOX

UNE VIPC

RElUlN x-FERUNE a-WAYVALVE

57 H EMTHERETURN x-FERUNE a-WAY VALliE

5amp H wesT HE RElUlN X-FBI UNE VIPC

59 wesTHERElUlN X-FBIUNE IIALVEBOX

60 H wesTHERETUlN lJ1JBE BAYONETCAN

61 H wesTHE RElUlN X-flR UNE CH FEEDcoH

62 HE wesT HE RETURN XfER UNE a-WAY VALVE

63 H wesTHERETUlN X-flR UNE 3-WAY VALVe

RETUIN X-flR UNE a-WAY VALVE

X-FER UNE FER UNE

AHFEEDcoH

AHFEEDCAN

68 LN2 SUlPlY IIQ HEADER AHFEEDCAN

LN2 SUlPlY XfER UNE AH FEED CAN CHFEEDCAN

70 LN2 SUlPlY BAYONET CAN

71 LN2 SUlPlY X-ROR UNE BAYONET CAN VALVE BOX

LN2 SUPPLY XfERUNE VALve BOX VlPCWEST

73 LN2 SUPPLY XfER UNE VALVE BOX VLPCEAST

74 LN2 SUPPLY XfER UNE VtfC WEST VALVE BOX

75 LN2 SUlPlY XfER UNE VLPC EMT VALliE BOX

76 XfER UNE VALVE BOX BAYONET CAN

BAYONET CAN

CH

AHFEED

-0)( gaS _

II

fIIi ee M 885

0

-shy

12

47

24

2

2

123

12

47

24

47

24

24

24

24

2 o

o

o o

9

2 o

2 o

o

2

o

o

o

9 2

2 o

o

6

3

o o

o

2

o o

o

If

o 10V

o o

o o

o o

o

o

1011

o o

o o

o 1 PV

o

o o

1011

I CV

I CV

o I PV

o o

o

10V

2 I CV

ICV

I CV

o

o o

1 PV

I PV

o

o

o o

o

o

-

Page I

JCa

Solenoid Helium Steady State Pressure drops - Some preliminary calculations were done to estimate the steady state helium heat

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 The return pipe line 8 was looked

into further See appendix L It was determined that a 1 112 sch 10 pipe will be used

giving a hydraulic radius of1057 The total steady state pressure drop then is on the

order of01 psi for the piping Allowing all the pressure drops to occur across control

valves

Solenoid Nitroeen flowrates and pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cool down flowrate shall not exceed 5 gls

With the current selected pipe sizes nitrogen flow will less be than 5 gls until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gls

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix G

VLPC Helium CooJdown flowrates The LHe line sizes for the VLPC were determined by first calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc II of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

-

STEP VLPC TEMP

[K]

GAS TEMP IN rKl

GAS TEMP

OUTrKl

TIME [hrs]

MASS FLOW RATEREQD

[ws] 1 300 to 250 200 250 10 84 2 250 to 200 150 200 10 89 3 200 to 150 100 150 10 92 4 toO to 90 80 90 4 31

-

-------~- ----- ----- ------------------------- shy

17

- It was concluded that step 4s pressure drop would be about 36 times larger than step 1 IS

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet

temperature of 80K and an outlet temperature of 90K (refer to appendix D)

VLPC Helium Cool down Pressure drops A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 4

for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the

given pipe sizes and inletexit states The VLPC cooldown piping was first sized by

assuming a pressure drop of 95 psig an inlet temperature of 80K GHe and an outlet

temperature of 90K through the supply and return lines respectively Resistance

coefficients were calculated for four segments of the piping In the second step of the

calculation pressure drops were calculated for each segment taking into account the

change in density due to changes in pressure Summing the individual pressure drops

resulted in a rough estimated pressure drop of 591 psi These numbers are summarized

in table 9 for the initial supply size of318 OD and return size of112 OD tubes See

Appendix E for the raw calculations After looking at steady state pressure drops the

line sizes for the supply and return were increased to 112 OD and 518 OD respectively

Therefore pressure drops listed in Table 9 will be less

Table 9 VLPC Helium Cooldown piping pressure drop summary

for 318 supply amp 112 return sizes

PIPE SECTION PRESSURE DROP (PSIA)

Supply line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

-

-

15

- VLPC Helium Steady State Pressure drops

-

The expected pressure drop for 318 OD x 0035 wall supply tubing for a steady

state flow of5 gls and a transfer line heat load of lOW was conservatively estimated at

46 psi per 100ft This prompted the increase in size to 112 OD x 0049 wall tubing

The calculated pressure drop for the two phase supply would be 12 psi per 100ft

Backing offon the conservatism and figuring approx 200ft ofequivalent length a real

estimate ofthe supply pressure drop from the refrigerator to the VLPC cryostat is about 1

psi See Appendix H page H4

The expected pressure drop for the return 518 OD x 0049 wall tube with 5 gIs

65 K gas flowing is 06 psig Since the supply and return tubing accounts for less than 2

psi pressure drop there is approximiately 10 psi available across the control valve and

cryostat See Appendix H page H3

VLPC Nitro~en flowrates and pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 OD Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

~~~~~~ ~- ---~-~----~ --_ --------------------- shy

lC

- Table of Contents for the Appendices

Raw En2ineerin2 Calculations

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

Appendix L Solenoid steady state cales Helium return piping

-

-

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ENGINEERING NOTE SECTION PROJECT

3B23115 SERIALmiddotCATEGORY

11 I PAGE

SUBJECT NAME

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D~ IT (305 )( OlS~ MN) ( I 72 k ~ 10- b Pec-S)

-41421 -f=oI3 l Z

(i) = I 3 AP 3 ~119j bull 0 ~ Ll -= L d Ii

(I 00 f-L~ K (0 Ii) 3 5 Sf

ItO ~ k

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c_ bull OQ435 s -

--------_------------shy

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1r 1)7

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2 5 b 8z (8 gt0 z 2-7 psi

--- --~----- ----~ - ~-~------ - -~- ---------shy

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i -

e~ It~ Jo~ -1- 7Z 7lt alt ~- 5

N --=- 000 y~ Jias

j b5 1lt

Plt= 64 )-t

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SUBJECT NAME

- SUPPLlt( DATE(pZ 10 ~ IREVISION DATE

It-w FERMILAB

ENGINEERING NOTE SECTION PROJECT SERIAl-CATEGORY

3S23 I IS PAGE

rl4

3 III - (ImiddotTJ3~ T -z w TlANrrut l1-W -lo jr W -~ 1- I w mAlS L i rJ C

5~ I C ~ 1 1 ( LEA t 1=20M t-I-tlt ~1ClttA ampe i)wA-rt 10 LPC Clt-(os -rk-r

5TA-re(j)

t Ik- pewAn ~~-r L10

- L4 ~o ~

p 9 ( 5 i9 5 A $TAI

hl 1 Be J -

o Pz e M 16MPa = 95 fJ~(j ~L 11flP

-d- = ZYIl

Xl--= ~-~-Fo 158~119h 032 yj - kF ~f 1t--1I96

Afo()

S TIlO

Vft TtJ~ =- 6Po() 2 f5i

L~f-l E(t S P(2UbAb-Y ~~ v 1 VPltL-~( -ru ZfJO Ff

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FERMILAB

ENGINEERING NOTE SECTION

RDIDcent PROJECT

He -y Fe12 SERIALmiddotCATEGORY

3S23IlS PAGE

LI SUBJECT 2-J

P HE RerulZJ =gt P toJ

50- e jJlH 0

NAME

DATE IREVISION DATE

5Z-hQ5 1

~iTATe Q)

P =I g A-rM

5Ar lGUID

1- 4l( 1lt

hjZ - 14 Bb lId

S-AIE hls 2 b35

S 1) sPec

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Y11Vd =30 b Jr

Mz I ~~

1 Sbil shy 1107

30 1-1107

s z lt3) 2 cent

P3 -=IZ ~ PA T Lj~IK

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h middot07 J~ h~ 30 b-l~

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ENGINEERING NOTE SECTION PROJECT

Jle x Fampltt ( tlJ Ii

SERIAL-CATEGORY

38 Z- 3 bull Il $ PAGE

L2 SUBJECT

He NAME

IREVISION DATE DATE

5-30 -atS

IIFo(t 1i1 ~)( CQoj 0 bull 11 )t-I ~ ~) Afo-JO A Scu [0

P 1tJG IIJJ I cent 511 11 0D DI-f = L2

A

Ilz S CI-L 10 P IPG-) ID = I =gt82 I

t bull oS loJ

IS 35 00shy-I( 0 D J-- Felt -rtt IS S 12Gt

-

stlnput

000005

427 200

4 1211 2017 318 1323 000082 3876

-2 2 184 184 20

12 998

073 1000

shy

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

deltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 BakerXa BakerYa c M RsubL RsubG GasVel Liqvel

Output

accurate

turbulen 01906103

ft in ft

92387E-5 m2 gs kgm 3 kgm3 JlPa-s JlPa-s Nm

90430 0024496 kgS

137600 0015504 kgs 51012286 pam 16810555 Pam

14863285 psig

57405518 67244052

1 4281346 kgmA 3 kgmA 3

53412427 Nm JlPa-s

1210 8660 lbmhr-ft

1 1 17419928 82580072 1 0075104 ms 12568736 ms

Comment L3 Russ Rucinski 53095 Return He pipe for Solenoid 1 pipe w 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

model validity

flow type friction factor Must enter a guess pipe roughness Pipe inside diameter Length of pipe cross sectional area Total mass flow rate Liquid density density of the gas Liquid viscosity Gas Viscosity Surface tension of liquid quality = mdotGmdot Reynolds for liquid Mass flow rate for liquid Reynolds for gas Mass flow rate for gas AP1lL for the liquid AP1lL for the two phase

Total pressure drop for the pipe ~ 100 ~JGtcs 1b uu Stu

Lockhart-Martinelli parameter Lockhart-Martinelli parameter L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 Baker diagram dimensionless parameter density of air density of water Baker diagram dimensionless parameter Surface tension of water viscosity of water X - axis value for Baker plot Y-axis value for Baker plot

Volume fraction of liquid phase Volume fraction of gas phase Gas velocity Liquid velocity

000005 1057 200

4 1211 2017 318 1323 000082 3876

shy

2

25

184

316 20

12 998

073 1000

-

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

rdeltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 Bakerxa BakerYa c M RsubL RsubG GasVel LiqVel

Output Comment Russ Rucinski 53095 Return He pipe for Solenoid 1 12 pipe wi 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

accurate model validity

turbulen flow type 02260289 friction factor Must enter a guess

ft pipe roughness in Pipe inside diameter ft Length of pipe

00056612 m2 cross sectional area gls Total mass flow rate kgm 3 Liquid density kgm3 density of the gas JLPa-s Liquid viscosity JLPa-s Gas viscosity Nm Surface tension of liquid

quality = mdotGmdot 36530 Reynolds for liquid

0024496 kgls Mass flow rate for liquid 55580 Reynolds for gas

0015504 kgls Mass flow rate for gas

0650814 Palm LP I LU for the liquid 21275204 Palm LPLU for the two phase

01881077 psig 1 Total pressure drop for the pipe

57175294 Lockhart-Martinelli parameter 67767548 Lockhart-Martinelli parameter

L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719

1 4281346 Baker diagram dimensionless parameter kgm3 density of air kgm3 density of water

53412427 Baker diagram dimensionless parameter Nm Surface tension of water JLPa-s viscosity of water

1210 X - axis value for Baker 1410 lbmhr-ft Y-axis value for Baker

1 1 17490072 Volume fraction of liquid phase 82509928 Volume fraction of gas phase 16456003 ms Gas velocity 20429237 ms Liquid velocity

53095 middot

FERMILAB TWO PHASE HEUUM FLOW TESTS

) )

Russ KUCt~5~l

10 ~ 1 I UAUEOOV

11 ~7 I I I Flow Fath Flaw

~--- Annular Flow Wave Flow

------ Slug FlowI

A tf SIO ______

~gt

---IIMIR RIGIMI BOUNDARIII ~ G bull RCtPtC GAl OW RAlI -- ClFtC LIQUID now RAT ~l-III _lIN_

10 I I ~I gt bull I I

MaMIIow_

X 5SVI PI U bull MIddIt of IOIItnoId

1 10 VI PI bull bull Ex of IOIItnoId

18 VI PI 7 bull 1111111 of control dewarbull Figura 1 Baker diagram with Mamedov curves or two phase helium In horzonlal channels

[FttoJIA Djli El 38 23IlJ -Gt-J - 33 8 ]

r J1

01 10 10 10 ( 10 i ~ ~ 10 ~ ~ 10 L ~nG CAt 0 )V rPl

~ IMaIIon TIJampE

0J

PIPE

112 5C~ 10 f 5eCD

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995

Russ Rucinski and Steve Sakla ROOQJ Mech

Approved _________

-

n ~ middotrt -

Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

-------------~ ~~~--~~~~--

Ud

)

) ) f

J8 CO bull 0049 N2 tu~bullbull

58 CO bull 0049 He Supply 1 12 sch lOS pipe

l Sch lOS H return SS

J4 CO bull 0065 He Cool down return

He Cool downQuench Return 25 CO bull 0065 Cu Rod shield

Main Solenoid xfer ine Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

Potta 1 rb 21 153121 CST ~ by rwcnoi

~lGUJCE 1

N

)J

1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

i foE 9flIIy 1JTAlE rlTX6 AHFEEDCAN 112 00 X 049 0402 5 2 0 0 0

tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

I

bull VIJIC iliil-flH Ie FT I

I I i I bullbullOF IUlaWS IN 8 i I

I1Igel

I Ibull I

9 o 2 III J o en

L

FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

~I_ i 50 Uf-bln 3823 _ c NAME

Russ

ili2 -J-1 U ~io-pound lIJJoJ~l-c sc O~Il~ I-(JoTI CAJI60e Igt r_I Z S~ Z -n r Z Z Ilt r Zmiddot

J o N

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1 shy

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~1

FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

~ )

-shy

~ M )

f ltgt0 ~O~ I 0 bull ~

If g -rI ~ t shy ~T

0

~ r

~ -a

-r

0 0

-Sci

bull~

~ ~

i-T

intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

-1(IL------- ~ ~l

-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

d (-10 ( ~raquo

839qYY --(Motte

25 lie SL 20

~ d51-

7 Sbull 2shy3 2 3 472

- ~

-- ---------- raquo

b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

1 EAIJgtltf lt FR61V tJ L c(Lflc lilA ~K

f~nr - ~- ALVMtJUM

SA 4 2otJ K 6~ oJ I 270 ~ amp-A5 our

h(7vr 1311~h lN ~ 1054 ~

-k-shy - - = A ATWO 1r (tgt15)(O4~[51))

o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

CaN-IIJfIIO vJ( 1--4 vt P~eAJ(1 of J-II TLJIi AJ ~fe~ AceA

A I) CDEFtIrL~ ib COOItgt()~J A-r (tATamp 0 5 ~A

o7b 10 T I ~ l

~tlcIio 60 it S ) ( lOS 5 ~ -q SJf) )l 3 CO os

STEP 3

S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

~ 11 LE1 0o-lD)-S vJG ~e~ 771 ADD J(i~ w~ Fc~lJ vf J 50~~r--middotC

-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

- II gtlt 1( SvlfoVlS (2 fi_shyb w - ~PrD IP-t S vPlgto2---fShmiddott

30W 0 7- tz A- I Itt- 0 tv bull I () I( 5 1gt~fINI- pUs 130 w- Cc 15I4J Z 50 o

c A tJ 7 3_64- VII s~

1trcP1 jc ~---)-

rv - bullbull OF FXIEgt~ ( 2S 1 ~ CL- (_~

bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

2 ~ Zgt ~ IV - I (1 Of CH IA IJ amp- - J i_2soeW - l~ or- Ck Nt 13 INIttSq

- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 3: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

) ) )

I

I

~

~ 00 x 0049 LN2 supply

p I ~ ~ 00 x 0065 Cu Rod shield o

~ Sch lOS pipe 450 00

II 5CH IDS ~lXLxO bull049~ N2 return

It bullbull =r O[) 0 Cj

~-oo-re-e35 He It

5e

1gtlt- 00 x O 049 He

VLPC transfer line

PRELIMINARY B ILDING TRANSFER LIN o SIGNS Russ Rucinski 22195

REII -jtqjqS tJor ro Sltteuro

Plott Tu feb 21 153732 CST Itt by rucinki

F GUJltE 2

0J

) )

SOlENOID PIPE SECTIONS~6Le i

LINE ~ pe$CflPTON DEi flDt 12

4 UIE SUPPL Y (HUTl) U-TUBE LHEDEWAR X-FER LINE

5 UIE SUPPLY XmiddotFERLINE U-TUBE U-TUBE

6 UIE SUPPLY (liUT1) U-TUBE X-FER LINE CONTROLOOWAR

7 UIE RETURN (HUTS) U-TUBE (DNTROL DEWAR X-FER LINE

8 LHE RETURN X-FER LINE U-TUBE U-TUBE

9 HE RETURN U-TUBE X-FER LINE X-FER LINEflPC)

10 LN2 SUPPLY U-TUBE LIN HEADER X-FER LINE

11 LN2 SUPPLY XmiddotFERLINE UmiddotTUBE TIE

12 LN2 SUPPL Y (SHIELD X-FER LINE TEE U-TUBE

13 LN2 SUPPLY (SHIELD) U-TUBE X-FER LINE CONTROL DEWAR

SUPPLY

_ 14 LN2 (INTERCEPT) X-FER LINE TIE U-TUBE

SUPPLY

_ 15 LN2 (INTERCEPT) U-TUBE XmiddotFERLINE CONTROL DEWAR

_L LN2 RETURN (SHIELD) U-TUBE (DNTROL DEWAR X-FER LIlltE

~7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE U-TUBE

18 LN2 RETURN (SHIELD) U-TUBE XmiddotFER LINE TEE -shyRETURN

19 LN2 (INTERCEPT) lImiddotTUBE CONTROL DEWAR X-FER LLltlO _ ---shy

RETURN

2_~__ IN2 (INTERrEPT) X-FER 111 ii-TIlliE lImiddotnlBE

RETURN

22 LN2 (INTERCEPT) UmiddotTUBE X-FER LINE TEE _

2_3 LN2 RETURN U-TUBE 1EE GN2 VENT HEADER

(COOLDOWNI

24 HE QUENCH) U-TUBE CONIROL DEWAR X-FER LINE -

(COOLDOWNI

25 HE QUENCH) X-FER LINE UmiddotTUBE U-TUIlE

(COOLDOWNI HEmOLDOWN

26 HE QUENCH) U-TUBE X-FER LINE RETURN

SUPPLY 27 HE (COOLDOWN) U-TUBE COOLr)OWNLINE _ JCiliLrr-E___

PIPE OR ruBE ItliIDi LIHiAB UE sect1m DlA ONI LENGTH IFTI ELBQWI

314 00 X 00S 068 5 2

SIS 00 X 049 0527 125 9

314 OD X 035 068 10 2

314 OD X 035 068 10 2

D~iO= 0 Concentric IM1 12S 9

314 00 X 03S 068 3 2

38 begt 1gt11 bull Z7

112 9 t ms ~ 3 2

~middotQDoLj t 1 1li1l9904I ~ 1 1

38 00 X 049 0277 124 9

112 00 x 035 043 10 2

318 00 X 049 0277 124 9

112 00 x 035 043 10 2--

112 00 x 035 043 iO 2

3S 00 X ()9 0277 125 9

liZ OD x 0)5 043 I-(-------- shy

li2 00 x 035 043 III 2---cshy --shy

18 OJ) X (149 0277 125 9

112 00 x 035 043 1 1

112 OD x 035 043 5 1

I S~H 10 bull (14 ~~ O5lshy 10 2

1 SC tC eo-l -3141 QD X 96S -~6i- 125 9

12S I1IO pound11 --3iImiddotGIH(~S- 06S 5 2

34 00 X()amp 068 5 _ 4

IED IIEU nmu

THRURUN IMHCtI ~

0 0 0

4 0 IDIVRTR

0 0 0

0 0 0

4 0 1 PVICV

0 0 0

0 0 0

0 0 0

2 I 1 PV

0 0 0

2 1 1 PV

0 0 0

0 0 ()

2 0 0

0 I ()

0 n I-shy --shy -------shy

2 n

0 1 0

0 0 0

0 0 0

_2 ~ 0 0 -----shy

0 0 ~-r---

0 0 10IVRTR

AI m

~~ (J~

til ~ Page

5 -

-

lHEOEWAR

H wesTHESUPPLY X-flRUNE a-WAY VALVE

H WEST HESlFPLY lJ1IJBE CHFEEDcoH

44 H wesTHESUPPLY X-flRUNE BAYONETcoH

45 H wesT HE SUPPLY x-FERUNE VALVE BOX

46 HE EMTHE SUPPLY X-flR UNE lJTUBE a-WAYVALVe

47 EMT HE SUPPLY X-flRUNE a-WAYVALVE

X-FBI UNE a-WAY VALVE Unee

CHFEEDCAN

X-flR IJNE BAYONET coH VALVE BOX

X-FER UNE VALVE BOX

UNE VIPC

RElUlN x-FERUNE a-WAYVALVE

57 H EMTHERETURN x-FERUNE a-WAY VALliE

5amp H wesT HE RElUlN X-FBI UNE VIPC

59 wesTHERElUlN X-FBIUNE IIALVEBOX

60 H wesTHERETUlN lJ1JBE BAYONETCAN

61 H wesTHE RElUlN X-flR UNE CH FEEDcoH

62 HE wesT HE RETURN XfER UNE a-WAY VALVE

63 H wesTHERETUlN X-flR UNE 3-WAY VALVe

RETUIN X-flR UNE a-WAY VALVE

X-FER UNE FER UNE

AHFEEDcoH

AHFEEDCAN

68 LN2 SUlPlY IIQ HEADER AHFEEDCAN

LN2 SUlPlY XfER UNE AH FEED CAN CHFEEDCAN

70 LN2 SUlPlY BAYONET CAN

71 LN2 SUlPlY X-ROR UNE BAYONET CAN VALVE BOX

LN2 SUPPLY XfERUNE VALve BOX VlPCWEST

73 LN2 SUPPLY XfER UNE VALVE BOX VLPCEAST

74 LN2 SUPPLY XfER UNE VtfC WEST VALVE BOX

75 LN2 SUlPlY XfER UNE VLPC EMT VALliE BOX

76 XfER UNE VALVE BOX BAYONET CAN

BAYONET CAN

CH

AHFEED

-0)( gaS _

II

fIIi ee M 885

0

-shy

12

47

24

2

2

123

12

47

24

47

24

24

24

24

2 o

o

o o

9

2 o

2 o

o

2

o

o

o

9 2

2 o

o

6

3

o o

o

2

o o

o

If

o 10V

o o

o o

o o

o

o

1011

o o

o o

o 1 PV

o

o o

1011

I CV

I CV

o I PV

o o

o

10V

2 I CV

ICV

I CV

o

o o

1 PV

I PV

o

o

o o

o

o

-

Page I

JCa

Solenoid Helium Steady State Pressure drops - Some preliminary calculations were done to estimate the steady state helium heat

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 The return pipe line 8 was looked

into further See appendix L It was determined that a 1 112 sch 10 pipe will be used

giving a hydraulic radius of1057 The total steady state pressure drop then is on the

order of01 psi for the piping Allowing all the pressure drops to occur across control

valves

Solenoid Nitroeen flowrates and pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cool down flowrate shall not exceed 5 gls

With the current selected pipe sizes nitrogen flow will less be than 5 gls until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gls

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix G

VLPC Helium CooJdown flowrates The LHe line sizes for the VLPC were determined by first calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc II of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

-

STEP VLPC TEMP

[K]

GAS TEMP IN rKl

GAS TEMP

OUTrKl

TIME [hrs]

MASS FLOW RATEREQD

[ws] 1 300 to 250 200 250 10 84 2 250 to 200 150 200 10 89 3 200 to 150 100 150 10 92 4 toO to 90 80 90 4 31

-

-------~- ----- ----- ------------------------- shy

17

- It was concluded that step 4s pressure drop would be about 36 times larger than step 1 IS

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet

temperature of 80K and an outlet temperature of 90K (refer to appendix D)

VLPC Helium Cool down Pressure drops A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 4

for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the

given pipe sizes and inletexit states The VLPC cooldown piping was first sized by

assuming a pressure drop of 95 psig an inlet temperature of 80K GHe and an outlet

temperature of 90K through the supply and return lines respectively Resistance

coefficients were calculated for four segments of the piping In the second step of the

calculation pressure drops were calculated for each segment taking into account the

change in density due to changes in pressure Summing the individual pressure drops

resulted in a rough estimated pressure drop of 591 psi These numbers are summarized

in table 9 for the initial supply size of318 OD and return size of112 OD tubes See

Appendix E for the raw calculations After looking at steady state pressure drops the

line sizes for the supply and return were increased to 112 OD and 518 OD respectively

Therefore pressure drops listed in Table 9 will be less

Table 9 VLPC Helium Cooldown piping pressure drop summary

for 318 supply amp 112 return sizes

PIPE SECTION PRESSURE DROP (PSIA)

Supply line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

-

-

15

- VLPC Helium Steady State Pressure drops

-

The expected pressure drop for 318 OD x 0035 wall supply tubing for a steady

state flow of5 gls and a transfer line heat load of lOW was conservatively estimated at

46 psi per 100ft This prompted the increase in size to 112 OD x 0049 wall tubing

The calculated pressure drop for the two phase supply would be 12 psi per 100ft

Backing offon the conservatism and figuring approx 200ft ofequivalent length a real

estimate ofthe supply pressure drop from the refrigerator to the VLPC cryostat is about 1

psi See Appendix H page H4

The expected pressure drop for the return 518 OD x 0049 wall tube with 5 gIs

65 K gas flowing is 06 psig Since the supply and return tubing accounts for less than 2

psi pressure drop there is approximiately 10 psi available across the control valve and

cryostat See Appendix H page H3

VLPC Nitro~en flowrates and pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 OD Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

~~~~~~ ~- ---~-~----~ --_ --------------------- shy

lC

- Table of Contents for the Appendices

Raw En2ineerin2 Calculations

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

Appendix L Solenoid steady state cales Helium return piping

-

-

-0 FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3B23115 SERIALmiddotCATEGORY

11 I PAGE

SUBJECT NAME

- (LPC Rl5~ RUCIf-Jst

CO t-J S f D ER ~-r~bf j -p ( e-e -t 0 S 1 A 1 S ~

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1 J vM(Jfpound(J5 Q1~o- = 180 tAJ bull

-

20 w

Sla DD 0 315 1AJA1-L id =- ~os ee = 4M 4middot (00437gt ~s)

D~ IT (305 )( OlS~ MN) ( I 72 k ~ 10- b Pec-S)

-41421 -f=oI3 l Z

(i) = I 3 AP 3 ~119j bull 0 ~ Ll -= L d Ii

(I 00 f-L~ K (0 Ii) 3 5 Sf

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-

11

c_ bull OQ435 s -

--------_------------shy

I HZ 5- 3c-75pf1EN 01gtc f-1- (trCvLATlCIJ)

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t-A 5Jh Z 0 i) gtlt a 0 lt-I~ AJJ I b5k -cb- O-1OZ1 cgtO(oz- gt 012 MI)~ L-= 200t-i roO9GM

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-( il -J

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2 5 b 8z (8 gt0 z 2-7 psi

--- --~----- ----~ - ~-~------ - -~- ---------shy

H-3 J I

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r i~ - r- ~-t~ -shy6 -= 081 ~ Jfi L s __ O~ k

i -

e~ It~ Jo~ -1- 7Z 7lt alt ~- 5

N --=- 000 y~ Jias

j b5 1lt

Plt= 64 )-t

-

I L

SUBJECT NAME

- SUPPLlt( DATE(pZ 10 ~ IREVISION DATE

It-w FERMILAB

ENGINEERING NOTE SECTION PROJECT SERIAl-CATEGORY

3S23 I IS PAGE

rl4

3 III - (ImiddotTJ3~ T -z w TlANrrut l1-W -lo jr W -~ 1- I w mAlS L i rJ C

5~ I C ~ 1 1 ( LEA t 1=20M t-I-tlt ~1ClttA ampe i)wA-rt 10 LPC Clt-(os -rk-r

5TA-re(j)

t Ik- pewAn ~~-r L10

- L4 ~o ~

p 9 ( 5 i9 5 A $TAI

hl 1 Be J -

o Pz e M 16MPa = 95 fJ~(j ~L 11flP

-d- = ZYIl

Xl--= ~-~-Fo 158~119h 032 yj - kF ~f 1t--1I96

Afo()

S TIlO

Vft TtJ~ =- 6Po() 2 f5i

L~f-l E(t S P(2UbAb-Y ~~ v 1 VPltL-~( -ru ZfJO Ff

-

FERMILAB

ENGINEERING NOTE SECTION

RDIDcent PROJECT

He -y Fe12 SERIALmiddotCATEGORY

3S23IlS PAGE

LI SUBJECT 2-J

P HE RerulZJ =gt P toJ

50- e jJlH 0

NAME

DATE IREVISION DATE

5Z-hQ5 1

~iTATe Q)

P =I g A-rM

5Ar lGUID

1- 4l( 1lt

hjZ - 14 Bb lId

S-AIE hls 2 b35

S 1) sPec

~-IG CD P2 = I 2 MPoshy(z= _0

Y11Vd =30 b Jr

Mz I ~~

1 Sbil shy 1107

30 1-1107

s z lt3) 2 cent

P3 -=IZ ~ PA T Lj~IK

39 Yf ) = 5

~ HL 0 c( 3 ~ F-O

h middot07 J~ h~ 30 b-l~

)(~ 387

-

I

6P 14Sb

)

FERMllAB

ENGINEERING NOTE SECTION PROJECT

Jle x Fampltt ( tlJ Ii

SERIAL-CATEGORY

38 Z- 3 bull Il $ PAGE

L2 SUBJECT

He NAME

IREVISION DATE DATE

5-30 -atS

IIFo(t 1i1 ~)( CQoj 0 bull 11 )t-I ~ ~) Afo-JO A Scu [0

P 1tJG IIJJ I cent 511 11 0D DI-f = L2

A

Ilz S CI-L 10 P IPG-) ID = I =gt82 I

t bull oS loJ

IS 35 00shy-I( 0 D J-- Felt -rtt IS S 12Gt

-

stlnput

000005

427 200

4 1211 2017 318 1323 000082 3876

-2 2 184 184 20

12 998

073 1000

shy

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

deltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 BakerXa BakerYa c M RsubL RsubG GasVel Liqvel

Output

accurate

turbulen 01906103

ft in ft

92387E-5 m2 gs kgm 3 kgm3 JlPa-s JlPa-s Nm

90430 0024496 kgS

137600 0015504 kgs 51012286 pam 16810555 Pam

14863285 psig

57405518 67244052

1 4281346 kgmA 3 kgmA 3

53412427 Nm JlPa-s

1210 8660 lbmhr-ft

1 1 17419928 82580072 1 0075104 ms 12568736 ms

Comment L3 Russ Rucinski 53095 Return He pipe for Solenoid 1 pipe w 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

model validity

flow type friction factor Must enter a guess pipe roughness Pipe inside diameter Length of pipe cross sectional area Total mass flow rate Liquid density density of the gas Liquid viscosity Gas Viscosity Surface tension of liquid quality = mdotGmdot Reynolds for liquid Mass flow rate for liquid Reynolds for gas Mass flow rate for gas AP1lL for the liquid AP1lL for the two phase

Total pressure drop for the pipe ~ 100 ~JGtcs 1b uu Stu

Lockhart-Martinelli parameter Lockhart-Martinelli parameter L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 Baker diagram dimensionless parameter density of air density of water Baker diagram dimensionless parameter Surface tension of water viscosity of water X - axis value for Baker plot Y-axis value for Baker plot

Volume fraction of liquid phase Volume fraction of gas phase Gas velocity Liquid velocity

000005 1057 200

4 1211 2017 318 1323 000082 3876

shy

2

25

184

316 20

12 998

073 1000

-

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

rdeltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 Bakerxa BakerYa c M RsubL RsubG GasVel LiqVel

Output Comment Russ Rucinski 53095 Return He pipe for Solenoid 1 12 pipe wi 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

accurate model validity

turbulen flow type 02260289 friction factor Must enter a guess

ft pipe roughness in Pipe inside diameter ft Length of pipe

00056612 m2 cross sectional area gls Total mass flow rate kgm 3 Liquid density kgm3 density of the gas JLPa-s Liquid viscosity JLPa-s Gas viscosity Nm Surface tension of liquid

quality = mdotGmdot 36530 Reynolds for liquid

0024496 kgls Mass flow rate for liquid 55580 Reynolds for gas

0015504 kgls Mass flow rate for gas

0650814 Palm LP I LU for the liquid 21275204 Palm LPLU for the two phase

01881077 psig 1 Total pressure drop for the pipe

57175294 Lockhart-Martinelli parameter 67767548 Lockhart-Martinelli parameter

L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719

1 4281346 Baker diagram dimensionless parameter kgm3 density of air kgm3 density of water

53412427 Baker diagram dimensionless parameter Nm Surface tension of water JLPa-s viscosity of water

1210 X - axis value for Baker 1410 lbmhr-ft Y-axis value for Baker

1 1 17490072 Volume fraction of liquid phase 82509928 Volume fraction of gas phase 16456003 ms Gas velocity 20429237 ms Liquid velocity

53095 middot

FERMILAB TWO PHASE HEUUM FLOW TESTS

) )

Russ KUCt~5~l

10 ~ 1 I UAUEOOV

11 ~7 I I I Flow Fath Flaw

~--- Annular Flow Wave Flow

------ Slug FlowI

A tf SIO ______

~gt

---IIMIR RIGIMI BOUNDARIII ~ G bull RCtPtC GAl OW RAlI -- ClFtC LIQUID now RAT ~l-III _lIN_

10 I I ~I gt bull I I

MaMIIow_

X 5SVI PI U bull MIddIt of IOIItnoId

1 10 VI PI bull bull Ex of IOIItnoId

18 VI PI 7 bull 1111111 of control dewarbull Figura 1 Baker diagram with Mamedov curves or two phase helium In horzonlal channels

[FttoJIA Djli El 38 23IlJ -Gt-J - 33 8 ]

r J1

01 10 10 10 ( 10 i ~ ~ 10 ~ ~ 10 L ~nG CAt 0 )V rPl

~ IMaIIon TIJampE

0J

PIPE

112 5C~ 10 f 5eCD

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995

Russ Rucinski and Steve Sakla ROOQJ Mech

Approved _________

-

n ~ middotrt -

Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

-------------~ ~~~--~~~~--

Ud

)

) ) f

J8 CO bull 0049 N2 tu~bullbull

58 CO bull 0049 He Supply 1 12 sch lOS pipe

l Sch lOS H return SS

J4 CO bull 0065 He Cool down return

He Cool downQuench Return 25 CO bull 0065 Cu Rod shield

Main Solenoid xfer ine Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

Potta 1 rb 21 153121 CST ~ by rwcnoi

~lGUJCE 1

N

)J

1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

i foE 9flIIy 1JTAlE rlTX6 AHFEEDCAN 112 00 X 049 0402 5 2 0 0 0

tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

I

bull VIJIC iliil-flH Ie FT I

I I i I bullbullOF IUlaWS IN 8 i I

I1Igel

I Ibull I

9 o 2 III J o en

L

FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

~I_ i 50 Uf-bln 3823 _ c NAME

Russ

ili2 -J-1 U ~io-pound lIJJoJ~l-c sc O~Il~ I-(JoTI CAJI60e Igt r_I Z S~ Z -n r Z Z Ilt r Zmiddot

J o N

(

N N

H

I

J

1 shy

c e-l ~w ~ UI

CIgt

~1

FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

~ )

-shy

~ M )

f ltgt0 ~O~ I 0 bull ~

If g -rI ~ t shy ~T

0

~ r

~ -a

-r

0 0

-Sci

bull~

~ ~

i-T

intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

-1(IL------- ~ ~l

-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

d (-10 ( ~raquo

839qYY --(Motte

25 lie SL 20

~ d51-

7 Sbull 2shy3 2 3 472

- ~

-- ---------- raquo

b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

1 EAIJgtltf lt FR61V tJ L c(Lflc lilA ~K

f~nr - ~- ALVMtJUM

SA 4 2otJ K 6~ oJ I 270 ~ amp-A5 our

h(7vr 1311~h lN ~ 1054 ~

-k-shy - - = A ATWO 1r (tgt15)(O4~[51))

o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

CaN-IIJfIIO vJ( 1--4 vt P~eAJ(1 of J-II TLJIi AJ ~fe~ AceA

A I) CDEFtIrL~ ib COOItgt()~J A-r (tATamp 0 5 ~A

o7b 10 T I ~ l

~tlcIio 60 it S ) ( lOS 5 ~ -q SJf) )l 3 CO os

STEP 3

S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

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14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

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3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

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-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

- II gtlt 1( SvlfoVlS (2 fi_shyb w - ~PrD IP-t S vPlgto2---fShmiddott

30W 0 7- tz A- I Itt- 0 tv bull I () I( 5 1gt~fINI- pUs 130 w- Cc 15I4J Z 50 o

c A tJ 7 3_64- VII s~

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bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

2 ~ Zgt ~ IV - I (1 Of CH IA IJ amp- - J i_2soeW - l~ or- Ck Nt 13 INIttSq

- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 4: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

) )

SOlENOID PIPE SECTIONS~6Le i

LINE ~ pe$CflPTON DEi flDt 12

4 UIE SUPPL Y (HUTl) U-TUBE LHEDEWAR X-FER LINE

5 UIE SUPPLY XmiddotFERLINE U-TUBE U-TUBE

6 UIE SUPPLY (liUT1) U-TUBE X-FER LINE CONTROLOOWAR

7 UIE RETURN (HUTS) U-TUBE (DNTROL DEWAR X-FER LINE

8 LHE RETURN X-FER LINE U-TUBE U-TUBE

9 HE RETURN U-TUBE X-FER LINE X-FER LINEflPC)

10 LN2 SUPPLY U-TUBE LIN HEADER X-FER LINE

11 LN2 SUPPLY XmiddotFERLINE UmiddotTUBE TIE

12 LN2 SUPPL Y (SHIELD X-FER LINE TEE U-TUBE

13 LN2 SUPPLY (SHIELD) U-TUBE X-FER LINE CONTROL DEWAR

SUPPLY

_ 14 LN2 (INTERCEPT) X-FER LINE TIE U-TUBE

SUPPLY

_ 15 LN2 (INTERCEPT) U-TUBE XmiddotFERLINE CONTROL DEWAR

_L LN2 RETURN (SHIELD) U-TUBE (DNTROL DEWAR X-FER LIlltE

~7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE U-TUBE

18 LN2 RETURN (SHIELD) U-TUBE XmiddotFER LINE TEE -shyRETURN

19 LN2 (INTERCEPT) lImiddotTUBE CONTROL DEWAR X-FER LLltlO _ ---shy

RETURN

2_~__ IN2 (INTERrEPT) X-FER 111 ii-TIlliE lImiddotnlBE

RETURN

22 LN2 (INTERCEPT) UmiddotTUBE X-FER LINE TEE _

2_3 LN2 RETURN U-TUBE 1EE GN2 VENT HEADER

(COOLDOWNI

24 HE QUENCH) U-TUBE CONIROL DEWAR X-FER LINE -

(COOLDOWNI

25 HE QUENCH) X-FER LINE UmiddotTUBE U-TUIlE

(COOLDOWNI HEmOLDOWN

26 HE QUENCH) U-TUBE X-FER LINE RETURN

SUPPLY 27 HE (COOLDOWN) U-TUBE COOLr)OWNLINE _ JCiliLrr-E___

PIPE OR ruBE ItliIDi LIHiAB UE sect1m DlA ONI LENGTH IFTI ELBQWI

314 00 X 00S 068 5 2

SIS 00 X 049 0527 125 9

314 OD X 035 068 10 2

314 OD X 035 068 10 2

D~iO= 0 Concentric IM1 12S 9

314 00 X 03S 068 3 2

38 begt 1gt11 bull Z7

112 9 t ms ~ 3 2

~middotQDoLj t 1 1li1l9904I ~ 1 1

38 00 X 049 0277 124 9

112 00 x 035 043 10 2

318 00 X 049 0277 124 9

112 00 x 035 043 10 2--

112 00 x 035 043 iO 2

3S 00 X ()9 0277 125 9

liZ OD x 0)5 043 I-(-------- shy

li2 00 x 035 043 III 2---cshy --shy

18 OJ) X (149 0277 125 9

112 00 x 035 043 1 1

112 OD x 035 043 5 1

I S~H 10 bull (14 ~~ O5lshy 10 2

1 SC tC eo-l -3141 QD X 96S -~6i- 125 9

12S I1IO pound11 --3iImiddotGIH(~S- 06S 5 2

34 00 X()amp 068 5 _ 4

IED IIEU nmu

THRURUN IMHCtI ~

0 0 0

4 0 IDIVRTR

0 0 0

0 0 0

4 0 1 PVICV

0 0 0

0 0 0

0 0 0

2 I 1 PV

0 0 0

2 1 1 PV

0 0 0

0 0 ()

2 0 0

0 I ()

0 n I-shy --shy -------shy

2 n

0 1 0

0 0 0

0 0 0

_2 ~ 0 0 -----shy

0 0 ~-r---

0 0 10IVRTR

AI m

~~ (J~

til ~ Page

5 -

-

lHEOEWAR

H wesTHESUPPLY X-flRUNE a-WAY VALVE

H WEST HESlFPLY lJ1IJBE CHFEEDcoH

44 H wesTHESUPPLY X-flRUNE BAYONETcoH

45 H wesT HE SUPPLY x-FERUNE VALVE BOX

46 HE EMTHE SUPPLY X-flR UNE lJTUBE a-WAYVALVe

47 EMT HE SUPPLY X-flRUNE a-WAYVALVE

X-FBI UNE a-WAY VALVE Unee

CHFEEDCAN

X-flR IJNE BAYONET coH VALVE BOX

X-FER UNE VALVE BOX

UNE VIPC

RElUlN x-FERUNE a-WAYVALVE

57 H EMTHERETURN x-FERUNE a-WAY VALliE

5amp H wesT HE RElUlN X-FBI UNE VIPC

59 wesTHERElUlN X-FBIUNE IIALVEBOX

60 H wesTHERETUlN lJ1JBE BAYONETCAN

61 H wesTHE RElUlN X-flR UNE CH FEEDcoH

62 HE wesT HE RETURN XfER UNE a-WAY VALVE

63 H wesTHERETUlN X-flR UNE 3-WAY VALVe

RETUIN X-flR UNE a-WAY VALVE

X-FER UNE FER UNE

AHFEEDcoH

AHFEEDCAN

68 LN2 SUlPlY IIQ HEADER AHFEEDCAN

LN2 SUlPlY XfER UNE AH FEED CAN CHFEEDCAN

70 LN2 SUlPlY BAYONET CAN

71 LN2 SUlPlY X-ROR UNE BAYONET CAN VALVE BOX

LN2 SUPPLY XfERUNE VALve BOX VlPCWEST

73 LN2 SUPPLY XfER UNE VALVE BOX VLPCEAST

74 LN2 SUPPLY XfER UNE VtfC WEST VALVE BOX

75 LN2 SUlPlY XfER UNE VLPC EMT VALliE BOX

76 XfER UNE VALVE BOX BAYONET CAN

BAYONET CAN

CH

AHFEED

-0)( gaS _

II

fIIi ee M 885

0

-shy

12

47

24

2

2

123

12

47

24

47

24

24

24

24

2 o

o

o o

9

2 o

2 o

o

2

o

o

o

9 2

2 o

o

6

3

o o

o

2

o o

o

If

o 10V

o o

o o

o o

o

o

1011

o o

o o

o 1 PV

o

o o

1011

I CV

I CV

o I PV

o o

o

10V

2 I CV

ICV

I CV

o

o o

1 PV

I PV

o

o

o o

o

o

-

Page I

JCa

Solenoid Helium Steady State Pressure drops - Some preliminary calculations were done to estimate the steady state helium heat

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 The return pipe line 8 was looked

into further See appendix L It was determined that a 1 112 sch 10 pipe will be used

giving a hydraulic radius of1057 The total steady state pressure drop then is on the

order of01 psi for the piping Allowing all the pressure drops to occur across control

valves

Solenoid Nitroeen flowrates and pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cool down flowrate shall not exceed 5 gls

With the current selected pipe sizes nitrogen flow will less be than 5 gls until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gls

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix G

VLPC Helium CooJdown flowrates The LHe line sizes for the VLPC were determined by first calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc II of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

-

STEP VLPC TEMP

[K]

GAS TEMP IN rKl

GAS TEMP

OUTrKl

TIME [hrs]

MASS FLOW RATEREQD

[ws] 1 300 to 250 200 250 10 84 2 250 to 200 150 200 10 89 3 200 to 150 100 150 10 92 4 toO to 90 80 90 4 31

-

-------~- ----- ----- ------------------------- shy

17

- It was concluded that step 4s pressure drop would be about 36 times larger than step 1 IS

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet

temperature of 80K and an outlet temperature of 90K (refer to appendix D)

VLPC Helium Cool down Pressure drops A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 4

for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the

given pipe sizes and inletexit states The VLPC cooldown piping was first sized by

assuming a pressure drop of 95 psig an inlet temperature of 80K GHe and an outlet

temperature of 90K through the supply and return lines respectively Resistance

coefficients were calculated for four segments of the piping In the second step of the

calculation pressure drops were calculated for each segment taking into account the

change in density due to changes in pressure Summing the individual pressure drops

resulted in a rough estimated pressure drop of 591 psi These numbers are summarized

in table 9 for the initial supply size of318 OD and return size of112 OD tubes See

Appendix E for the raw calculations After looking at steady state pressure drops the

line sizes for the supply and return were increased to 112 OD and 518 OD respectively

Therefore pressure drops listed in Table 9 will be less

Table 9 VLPC Helium Cooldown piping pressure drop summary

for 318 supply amp 112 return sizes

PIPE SECTION PRESSURE DROP (PSIA)

Supply line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

-

-

15

- VLPC Helium Steady State Pressure drops

-

The expected pressure drop for 318 OD x 0035 wall supply tubing for a steady

state flow of5 gls and a transfer line heat load of lOW was conservatively estimated at

46 psi per 100ft This prompted the increase in size to 112 OD x 0049 wall tubing

The calculated pressure drop for the two phase supply would be 12 psi per 100ft

Backing offon the conservatism and figuring approx 200ft ofequivalent length a real

estimate ofthe supply pressure drop from the refrigerator to the VLPC cryostat is about 1

psi See Appendix H page H4

The expected pressure drop for the return 518 OD x 0049 wall tube with 5 gIs

65 K gas flowing is 06 psig Since the supply and return tubing accounts for less than 2

psi pressure drop there is approximiately 10 psi available across the control valve and

cryostat See Appendix H page H3

VLPC Nitro~en flowrates and pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 OD Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

~~~~~~ ~- ---~-~----~ --_ --------------------- shy

lC

- Table of Contents for the Appendices

Raw En2ineerin2 Calculations

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

Appendix L Solenoid steady state cales Helium return piping

-

-

-0 FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3B23115 SERIALmiddotCATEGORY

11 I PAGE

SUBJECT NAME

- (LPC Rl5~ RUCIf-Jst

CO t-J S f D ER ~-r~bf j -p ( e-e -t 0 S 1 A 1 S ~

CJ Svlt-CNoD Dc-gtICIr-J RE-POliL-r QC)fA1- - 270 VII ) 141601-1

es -r- I - bull C U R IL -bullbullrr Es j M e os AlE 70 vJ PEft- 0 ~~

+t-J(gt it-I2-I+APS p ACJOIOfJA-t 40 vJ Faa ~A)F~ ul-lE-s t

1 J vM(Jfpound(J5 Q1~o- = 180 tAJ bull

-

20 w

Sla DD 0 315 1AJA1-L id =- ~os ee = 4M 4middot (00437gt ~s)

D~ IT (305 )( OlS~ MN) ( I 72 k ~ 10- b Pec-S)

-41421 -f=oI3 l Z

(i) = I 3 AP 3 ~119j bull 0 ~ Ll -= L d Ii

(I 00 f-L~ K (0 Ii) 3 5 Sf

ItO ~ k

-

11

c_ bull OQ435 s -

--------_------------shy

I HZ 5- 3c-75pf1EN 01gtc f-1- (trCvLATlCIJ)

1r 1)7

) A

II f

t-A 5Jh Z 0 i) gtlt a 0 lt-I~ AJJ I b5k -cb- O-1OZ1 cgtO(oz- gt 012 MI)~ L-= 200t-i roO9GM

v (m ) e --~ (z) (1r- DA )

-( il -J

-~~---7- I )

v ~ v -2shybull 7 L- V

l) - - l lQ [ r) 2~

T

( ( I ~ IS (82 amp8 ~gt1-= (~lt17 b lt013)( o elY) ( 4gt0 cr or) llaquo

2 5 b 8z (8 gt0 z 2-7 psi

--- --~----- ----~ - ~-~------ - -~- ---------shy

H-3 J I

-

r i~ - r- ~-t~ -shy6 -= 081 ~ Jfi L s __ O~ k

i -

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N --=- 000 y~ Jias

j b5 1lt

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SUBJECT NAME

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It-w FERMILAB

ENGINEERING NOTE SECTION PROJECT SERIAl-CATEGORY

3S23 I IS PAGE

rl4

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5TA-re(j)

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p 9 ( 5 i9 5 A $TAI

hl 1 Be J -

o Pz e M 16MPa = 95 fJ~(j ~L 11flP

-d- = ZYIl

Xl--= ~-~-Fo 158~119h 032 yj - kF ~f 1t--1I96

Afo()

S TIlO

Vft TtJ~ =- 6Po() 2 f5i

L~f-l E(t S P(2UbAb-Y ~~ v 1 VPltL-~( -ru ZfJO Ff

-

FERMILAB

ENGINEERING NOTE SECTION

RDIDcent PROJECT

He -y Fe12 SERIALmiddotCATEGORY

3S23IlS PAGE

LI SUBJECT 2-J

P HE RerulZJ =gt P toJ

50- e jJlH 0

NAME

DATE IREVISION DATE

5Z-hQ5 1

~iTATe Q)

P =I g A-rM

5Ar lGUID

1- 4l( 1lt

hjZ - 14 Bb lId

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Mz I ~~

1 Sbil shy 1107

30 1-1107

s z lt3) 2 cent

P3 -=IZ ~ PA T Lj~IK

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)

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ENGINEERING NOTE SECTION PROJECT

Jle x Fampltt ( tlJ Ii

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38 Z- 3 bull Il $ PAGE

L2 SUBJECT

He NAME

IREVISION DATE DATE

5-30 -atS

IIFo(t 1i1 ~)( CQoj 0 bull 11 )t-I ~ ~) Afo-JO A Scu [0

P 1tJG IIJJ I cent 511 11 0D DI-f = L2

A

Ilz S CI-L 10 P IPG-) ID = I =gt82 I

t bull oS loJ

IS 35 00shy-I( 0 D J-- Felt -rtt IS S 12Gt

-

stlnput

000005

427 200

4 1211 2017 318 1323 000082 3876

-2 2 184 184 20

12 998

073 1000

shy

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

deltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 BakerXa BakerYa c M RsubL RsubG GasVel Liqvel

Output

accurate

turbulen 01906103

ft in ft

92387E-5 m2 gs kgm 3 kgm3 JlPa-s JlPa-s Nm

90430 0024496 kgS

137600 0015504 kgs 51012286 pam 16810555 Pam

14863285 psig

57405518 67244052

1 4281346 kgmA 3 kgmA 3

53412427 Nm JlPa-s

1210 8660 lbmhr-ft

1 1 17419928 82580072 1 0075104 ms 12568736 ms

Comment L3 Russ Rucinski 53095 Return He pipe for Solenoid 1 pipe w 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

model validity

flow type friction factor Must enter a guess pipe roughness Pipe inside diameter Length of pipe cross sectional area Total mass flow rate Liquid density density of the gas Liquid viscosity Gas Viscosity Surface tension of liquid quality = mdotGmdot Reynolds for liquid Mass flow rate for liquid Reynolds for gas Mass flow rate for gas AP1lL for the liquid AP1lL for the two phase

Total pressure drop for the pipe ~ 100 ~JGtcs 1b uu Stu

Lockhart-Martinelli parameter Lockhart-Martinelli parameter L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 Baker diagram dimensionless parameter density of air density of water Baker diagram dimensionless parameter Surface tension of water viscosity of water X - axis value for Baker plot Y-axis value for Baker plot

Volume fraction of liquid phase Volume fraction of gas phase Gas velocity Liquid velocity

000005 1057 200

4 1211 2017 318 1323 000082 3876

shy

2

25

184

316 20

12 998

073 1000

-

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

rdeltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 Bakerxa BakerYa c M RsubL RsubG GasVel LiqVel

Output Comment Russ Rucinski 53095 Return He pipe for Solenoid 1 12 pipe wi 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

accurate model validity

turbulen flow type 02260289 friction factor Must enter a guess

ft pipe roughness in Pipe inside diameter ft Length of pipe

00056612 m2 cross sectional area gls Total mass flow rate kgm 3 Liquid density kgm3 density of the gas JLPa-s Liquid viscosity JLPa-s Gas viscosity Nm Surface tension of liquid

quality = mdotGmdot 36530 Reynolds for liquid

0024496 kgls Mass flow rate for liquid 55580 Reynolds for gas

0015504 kgls Mass flow rate for gas

0650814 Palm LP I LU for the liquid 21275204 Palm LPLU for the two phase

01881077 psig 1 Total pressure drop for the pipe

57175294 Lockhart-Martinelli parameter 67767548 Lockhart-Martinelli parameter

L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719

1 4281346 Baker diagram dimensionless parameter kgm3 density of air kgm3 density of water

53412427 Baker diagram dimensionless parameter Nm Surface tension of water JLPa-s viscosity of water

1210 X - axis value for Baker 1410 lbmhr-ft Y-axis value for Baker

1 1 17490072 Volume fraction of liquid phase 82509928 Volume fraction of gas phase 16456003 ms Gas velocity 20429237 ms Liquid velocity

53095 middot

FERMILAB TWO PHASE HEUUM FLOW TESTS

) )

Russ KUCt~5~l

10 ~ 1 I UAUEOOV

11 ~7 I I I Flow Fath Flaw

~--- Annular Flow Wave Flow

------ Slug FlowI

A tf SIO ______

~gt

---IIMIR RIGIMI BOUNDARIII ~ G bull RCtPtC GAl OW RAlI -- ClFtC LIQUID now RAT ~l-III _lIN_

10 I I ~I gt bull I I

MaMIIow_

X 5SVI PI U bull MIddIt of IOIItnoId

1 10 VI PI bull bull Ex of IOIItnoId

18 VI PI 7 bull 1111111 of control dewarbull Figura 1 Baker diagram with Mamedov curves or two phase helium In horzonlal channels

[FttoJIA Djli El 38 23IlJ -Gt-J - 33 8 ]

r J1

01 10 10 10 ( 10 i ~ ~ 10 ~ ~ 10 L ~nG CAt 0 )V rPl

~ IMaIIon TIJampE

0J

PIPE

112 5C~ 10 f 5eCD

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995

Russ Rucinski and Steve Sakla ROOQJ Mech

Approved _________

-

n ~ middotrt -

Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

-------------~ ~~~--~~~~--

Ud

)

) ) f

J8 CO bull 0049 N2 tu~bullbull

58 CO bull 0049 He Supply 1 12 sch lOS pipe

l Sch lOS H return SS

J4 CO bull 0065 He Cool down return

He Cool downQuench Return 25 CO bull 0065 Cu Rod shield

Main Solenoid xfer ine Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

Potta 1 rb 21 153121 CST ~ by rwcnoi

~lGUJCE 1

N

)J

1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

i foE 9flIIy 1JTAlE rlTX6 AHFEEDCAN 112 00 X 049 0402 5 2 0 0 0

tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

I

bull VIJIC iliil-flH Ie FT I

I I i I bullbullOF IUlaWS IN 8 i I

I1Igel

I Ibull I

9 o 2 III J o en

L

FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

~I_ i 50 Uf-bln 3823 _ c NAME

Russ

ili2 -J-1 U ~io-pound lIJJoJ~l-c sc O~Il~ I-(JoTI CAJI60e Igt r_I Z S~ Z -n r Z Z Ilt r Zmiddot

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FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

~ )

-shy

~ M )

f ltgt0 ~O~ I 0 bull ~

If g -rI ~ t shy ~T

0

~ r

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-r

0 0

-Sci

bull~

~ ~

i-T

intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

-1(IL------- ~ ~l

-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

d (-10 ( ~raquo

839qYY --(Motte

25 lie SL 20

~ d51-

7 Sbull 2shy3 2 3 472

- ~

-- ---------- raquo

b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

1 EAIJgtltf lt FR61V tJ L c(Lflc lilA ~K

f~nr - ~- ALVMtJUM

SA 4 2otJ K 6~ oJ I 270 ~ amp-A5 our

h(7vr 1311~h lN ~ 1054 ~

-k-shy - - = A ATWO 1r (tgt15)(O4~[51))

o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

CaN-IIJfIIO vJ( 1--4 vt P~eAJ(1 of J-II TLJIi AJ ~fe~ AceA

A I) CDEFtIrL~ ib COOItgt()~J A-r (tATamp 0 5 ~A

o7b 10 T I ~ l

~tlcIio 60 it S ) ( lOS 5 ~ -q SJf) )l 3 CO os

STEP 3

S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

~ 11 LE1 0o-lD)-S vJG ~e~ 771 ADD J(i~ w~ Fc~lJ vf J 50~~r--middotC

-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

- II gtlt 1( SvlfoVlS (2 fi_shyb w - ~PrD IP-t S vPlgto2---fShmiddott

30W 0 7- tz A- I Itt- 0 tv bull I () I( 5 1gt~fINI- pUs 130 w- Cc 15I4J Z 50 o

c A tJ 7 3_64- VII s~

1trcP1 jc ~---)-

rv - bullbull OF FXIEgt~ ( 2S 1 ~ CL- (_~

bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

2 ~ Zgt ~ IV - I (1 Of CH IA IJ amp- - J i_2soeW - l~ or- Ck Nt 13 INIttSq

- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 5: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

5 -

-

lHEOEWAR

H wesTHESUPPLY X-flRUNE a-WAY VALVE

H WEST HESlFPLY lJ1IJBE CHFEEDcoH

44 H wesTHESUPPLY X-flRUNE BAYONETcoH

45 H wesT HE SUPPLY x-FERUNE VALVE BOX

46 HE EMTHE SUPPLY X-flR UNE lJTUBE a-WAYVALVe

47 EMT HE SUPPLY X-flRUNE a-WAYVALVE

X-FBI UNE a-WAY VALVE Unee

CHFEEDCAN

X-flR IJNE BAYONET coH VALVE BOX

X-FER UNE VALVE BOX

UNE VIPC

RElUlN x-FERUNE a-WAYVALVE

57 H EMTHERETURN x-FERUNE a-WAY VALliE

5amp H wesT HE RElUlN X-FBI UNE VIPC

59 wesTHERElUlN X-FBIUNE IIALVEBOX

60 H wesTHERETUlN lJ1JBE BAYONETCAN

61 H wesTHE RElUlN X-flR UNE CH FEEDcoH

62 HE wesT HE RETURN XfER UNE a-WAY VALVE

63 H wesTHERETUlN X-flR UNE 3-WAY VALVe

RETUIN X-flR UNE a-WAY VALVE

X-FER UNE FER UNE

AHFEEDcoH

AHFEEDCAN

68 LN2 SUlPlY IIQ HEADER AHFEEDCAN

LN2 SUlPlY XfER UNE AH FEED CAN CHFEEDCAN

70 LN2 SUlPlY BAYONET CAN

71 LN2 SUlPlY X-ROR UNE BAYONET CAN VALVE BOX

LN2 SUPPLY XfERUNE VALve BOX VlPCWEST

73 LN2 SUPPLY XfER UNE VALVE BOX VLPCEAST

74 LN2 SUPPLY XfER UNE VtfC WEST VALVE BOX

75 LN2 SUlPlY XfER UNE VLPC EMT VALliE BOX

76 XfER UNE VALVE BOX BAYONET CAN

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Page I

JCa

Solenoid Helium Steady State Pressure drops - Some preliminary calculations were done to estimate the steady state helium heat

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 The return pipe line 8 was looked

into further See appendix L It was determined that a 1 112 sch 10 pipe will be used

giving a hydraulic radius of1057 The total steady state pressure drop then is on the

order of01 psi for the piping Allowing all the pressure drops to occur across control

valves

Solenoid Nitroeen flowrates and pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cool down flowrate shall not exceed 5 gls

With the current selected pipe sizes nitrogen flow will less be than 5 gls until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gls

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix G

VLPC Helium CooJdown flowrates The LHe line sizes for the VLPC were determined by first calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc II of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

-

STEP VLPC TEMP

[K]

GAS TEMP IN rKl

GAS TEMP

OUTrKl

TIME [hrs]

MASS FLOW RATEREQD

[ws] 1 300 to 250 200 250 10 84 2 250 to 200 150 200 10 89 3 200 to 150 100 150 10 92 4 toO to 90 80 90 4 31

-

-------~- ----- ----- ------------------------- shy

17

- It was concluded that step 4s pressure drop would be about 36 times larger than step 1 IS

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet

temperature of 80K and an outlet temperature of 90K (refer to appendix D)

VLPC Helium Cool down Pressure drops A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 4

for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the

given pipe sizes and inletexit states The VLPC cooldown piping was first sized by

assuming a pressure drop of 95 psig an inlet temperature of 80K GHe and an outlet

temperature of 90K through the supply and return lines respectively Resistance

coefficients were calculated for four segments of the piping In the second step of the

calculation pressure drops were calculated for each segment taking into account the

change in density due to changes in pressure Summing the individual pressure drops

resulted in a rough estimated pressure drop of 591 psi These numbers are summarized

in table 9 for the initial supply size of318 OD and return size of112 OD tubes See

Appendix E for the raw calculations After looking at steady state pressure drops the

line sizes for the supply and return were increased to 112 OD and 518 OD respectively

Therefore pressure drops listed in Table 9 will be less

Table 9 VLPC Helium Cooldown piping pressure drop summary

for 318 supply amp 112 return sizes

PIPE SECTION PRESSURE DROP (PSIA)

Supply line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

-

-

15

- VLPC Helium Steady State Pressure drops

-

The expected pressure drop for 318 OD x 0035 wall supply tubing for a steady

state flow of5 gls and a transfer line heat load of lOW was conservatively estimated at

46 psi per 100ft This prompted the increase in size to 112 OD x 0049 wall tubing

The calculated pressure drop for the two phase supply would be 12 psi per 100ft

Backing offon the conservatism and figuring approx 200ft ofequivalent length a real

estimate ofthe supply pressure drop from the refrigerator to the VLPC cryostat is about 1

psi See Appendix H page H4

The expected pressure drop for the return 518 OD x 0049 wall tube with 5 gIs

65 K gas flowing is 06 psig Since the supply and return tubing accounts for less than 2

psi pressure drop there is approximiately 10 psi available across the control valve and

cryostat See Appendix H page H3

VLPC Nitro~en flowrates and pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 OD Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

~~~~~~ ~- ---~-~----~ --_ --------------------- shy

lC

- Table of Contents for the Appendices

Raw En2ineerin2 Calculations

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

Appendix L Solenoid steady state cales Helium return piping

-

-

-0 FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3B23115 SERIALmiddotCATEGORY

11 I PAGE

SUBJECT NAME

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It-w FERMILAB

ENGINEERING NOTE SECTION PROJECT SERIAl-CATEGORY

3S23 I IS PAGE

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ENGINEERING NOTE SECTION

RDIDcent PROJECT

He -y Fe12 SERIALmiddotCATEGORY

3S23IlS PAGE

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Jle x Fampltt ( tlJ Ii

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5-30 -atS

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-

stlnput

000005

427 200

4 1211 2017 318 1323 000082 3876

-2 2 184 184 20

12 998

073 1000

shy

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

deltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 BakerXa BakerYa c M RsubL RsubG GasVel Liqvel

Output

accurate

turbulen 01906103

ft in ft

92387E-5 m2 gs kgm 3 kgm3 JlPa-s JlPa-s Nm

90430 0024496 kgS

137600 0015504 kgs 51012286 pam 16810555 Pam

14863285 psig

57405518 67244052

1 4281346 kgmA 3 kgmA 3

53412427 Nm JlPa-s

1210 8660 lbmhr-ft

1 1 17419928 82580072 1 0075104 ms 12568736 ms

Comment L3 Russ Rucinski 53095 Return He pipe for Solenoid 1 pipe w 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

model validity

flow type friction factor Must enter a guess pipe roughness Pipe inside diameter Length of pipe cross sectional area Total mass flow rate Liquid density density of the gas Liquid viscosity Gas Viscosity Surface tension of liquid quality = mdotGmdot Reynolds for liquid Mass flow rate for liquid Reynolds for gas Mass flow rate for gas AP1lL for the liquid AP1lL for the two phase

Total pressure drop for the pipe ~ 100 ~JGtcs 1b uu Stu

Lockhart-Martinelli parameter Lockhart-Martinelli parameter L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 Baker diagram dimensionless parameter density of air density of water Baker diagram dimensionless parameter Surface tension of water viscosity of water X - axis value for Baker plot Y-axis value for Baker plot

Volume fraction of liquid phase Volume fraction of gas phase Gas velocity Liquid velocity

000005 1057 200

4 1211 2017 318 1323 000082 3876

shy

2

25

184

316 20

12 998

073 1000

-

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

rdeltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 Bakerxa BakerYa c M RsubL RsubG GasVel LiqVel

Output Comment Russ Rucinski 53095 Return He pipe for Solenoid 1 12 pipe wi 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

accurate model validity

turbulen flow type 02260289 friction factor Must enter a guess

ft pipe roughness in Pipe inside diameter ft Length of pipe

00056612 m2 cross sectional area gls Total mass flow rate kgm 3 Liquid density kgm3 density of the gas JLPa-s Liquid viscosity JLPa-s Gas viscosity Nm Surface tension of liquid

quality = mdotGmdot 36530 Reynolds for liquid

0024496 kgls Mass flow rate for liquid 55580 Reynolds for gas

0015504 kgls Mass flow rate for gas

0650814 Palm LP I LU for the liquid 21275204 Palm LPLU for the two phase

01881077 psig 1 Total pressure drop for the pipe

57175294 Lockhart-Martinelli parameter 67767548 Lockhart-Martinelli parameter

L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719

1 4281346 Baker diagram dimensionless parameter kgm3 density of air kgm3 density of water

53412427 Baker diagram dimensionless parameter Nm Surface tension of water JLPa-s viscosity of water

1210 X - axis value for Baker 1410 lbmhr-ft Y-axis value for Baker

1 1 17490072 Volume fraction of liquid phase 82509928 Volume fraction of gas phase 16456003 ms Gas velocity 20429237 ms Liquid velocity

53095 middot

FERMILAB TWO PHASE HEUUM FLOW TESTS

) )

Russ KUCt~5~l

10 ~ 1 I UAUEOOV

11 ~7 I I I Flow Fath Flaw

~--- Annular Flow Wave Flow

------ Slug FlowI

A tf SIO ______

~gt

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10 I I ~I gt bull I I

MaMIIow_

X 5SVI PI U bull MIddIt of IOIItnoId

1 10 VI PI bull bull Ex of IOIItnoId

18 VI PI 7 bull 1111111 of control dewarbull Figura 1 Baker diagram with Mamedov curves or two phase helium In horzonlal channels

[FttoJIA Djli El 38 23IlJ -Gt-J - 33 8 ]

r J1

01 10 10 10 ( 10 i ~ ~ 10 ~ ~ 10 L ~nG CAt 0 )V rPl

~ IMaIIon TIJampE

0J

PIPE

112 5C~ 10 f 5eCD

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995

Russ Rucinski and Steve Sakla ROOQJ Mech

Approved _________

-

n ~ middotrt -

Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

-------------~ ~~~--~~~~--

Ud

)

) ) f

J8 CO bull 0049 N2 tu~bullbull

58 CO bull 0049 He Supply 1 12 sch lOS pipe

l Sch lOS H return SS

J4 CO bull 0065 He Cool down return

He Cool downQuench Return 25 CO bull 0065 Cu Rod shield

Main Solenoid xfer ine Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

Potta 1 rb 21 153121 CST ~ by rwcnoi

~lGUJCE 1

N

)J

1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

i foE 9flIIy 1JTAlE rlTX6 AHFEEDCAN 112 00 X 049 0402 5 2 0 0 0

tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

I

bull VIJIC iliil-flH Ie FT I

I I i I bullbullOF IUlaWS IN 8 i I

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FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

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Russ

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J o N

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I

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c e-l ~w ~ UI

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FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

~ )

-shy

~ M )

f ltgt0 ~O~ I 0 bull ~

If g -rI ~ t shy ~T

0

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0 0

-Sci

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~ ~

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intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

-1(IL------- ~ ~l

-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

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FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

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o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

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S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

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(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

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kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

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~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

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3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

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tt3k~ ICft12 b ~ D (it IS

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o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

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AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

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N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

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b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

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bull (3 3) d I-

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PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

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375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

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PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

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NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

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(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 6: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

JCa

Solenoid Helium Steady State Pressure drops - Some preliminary calculations were done to estimate the steady state helium heat

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 The return pipe line 8 was looked

into further See appendix L It was determined that a 1 112 sch 10 pipe will be used

giving a hydraulic radius of1057 The total steady state pressure drop then is on the

order of01 psi for the piping Allowing all the pressure drops to occur across control

valves

Solenoid Nitroeen flowrates and pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cool down flowrate shall not exceed 5 gls

With the current selected pipe sizes nitrogen flow will less be than 5 gls until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gls

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix G

VLPC Helium CooJdown flowrates The LHe line sizes for the VLPC were determined by first calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc II of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

-

STEP VLPC TEMP

[K]

GAS TEMP IN rKl

GAS TEMP

OUTrKl

TIME [hrs]

MASS FLOW RATEREQD

[ws] 1 300 to 250 200 250 10 84 2 250 to 200 150 200 10 89 3 200 to 150 100 150 10 92 4 toO to 90 80 90 4 31

-

-------~- ----- ----- ------------------------- shy

17

- It was concluded that step 4s pressure drop would be about 36 times larger than step 1 IS

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet

temperature of 80K and an outlet temperature of 90K (refer to appendix D)

VLPC Helium Cool down Pressure drops A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 4

for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the

given pipe sizes and inletexit states The VLPC cooldown piping was first sized by

assuming a pressure drop of 95 psig an inlet temperature of 80K GHe and an outlet

temperature of 90K through the supply and return lines respectively Resistance

coefficients were calculated for four segments of the piping In the second step of the

calculation pressure drops were calculated for each segment taking into account the

change in density due to changes in pressure Summing the individual pressure drops

resulted in a rough estimated pressure drop of 591 psi These numbers are summarized

in table 9 for the initial supply size of318 OD and return size of112 OD tubes See

Appendix E for the raw calculations After looking at steady state pressure drops the

line sizes for the supply and return were increased to 112 OD and 518 OD respectively

Therefore pressure drops listed in Table 9 will be less

Table 9 VLPC Helium Cooldown piping pressure drop summary

for 318 supply amp 112 return sizes

PIPE SECTION PRESSURE DROP (PSIA)

Supply line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

-

-

15

- VLPC Helium Steady State Pressure drops

-

The expected pressure drop for 318 OD x 0035 wall supply tubing for a steady

state flow of5 gls and a transfer line heat load of lOW was conservatively estimated at

46 psi per 100ft This prompted the increase in size to 112 OD x 0049 wall tubing

The calculated pressure drop for the two phase supply would be 12 psi per 100ft

Backing offon the conservatism and figuring approx 200ft ofequivalent length a real

estimate ofthe supply pressure drop from the refrigerator to the VLPC cryostat is about 1

psi See Appendix H page H4

The expected pressure drop for the return 518 OD x 0049 wall tube with 5 gIs

65 K gas flowing is 06 psig Since the supply and return tubing accounts for less than 2

psi pressure drop there is approximiately 10 psi available across the control valve and

cryostat See Appendix H page H3

VLPC Nitro~en flowrates and pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 OD Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

~~~~~~ ~- ---~-~----~ --_ --------------------- shy

lC

- Table of Contents for the Appendices

Raw En2ineerin2 Calculations

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

Appendix L Solenoid steady state cales Helium return piping

-

-

-0 FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3B23115 SERIALmiddotCATEGORY

11 I PAGE

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It-w FERMILAB

ENGINEERING NOTE SECTION PROJECT SERIAl-CATEGORY

3S23 I IS PAGE

rl4

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RDIDcent PROJECT

He -y Fe12 SERIALmiddotCATEGORY

3S23IlS PAGE

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NAME

DATE IREVISION DATE

5Z-hQ5 1

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38 Z- 3 bull Il $ PAGE

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IREVISION DATE DATE

5-30 -atS

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A

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-

stlnput

000005

427 200

4 1211 2017 318 1323 000082 3876

-2 2 184 184 20

12 998

073 1000

shy

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

deltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 BakerXa BakerYa c M RsubL RsubG GasVel Liqvel

Output

accurate

turbulen 01906103

ft in ft

92387E-5 m2 gs kgm 3 kgm3 JlPa-s JlPa-s Nm

90430 0024496 kgS

137600 0015504 kgs 51012286 pam 16810555 Pam

14863285 psig

57405518 67244052

1 4281346 kgmA 3 kgmA 3

53412427 Nm JlPa-s

1210 8660 lbmhr-ft

1 1 17419928 82580072 1 0075104 ms 12568736 ms

Comment L3 Russ Rucinski 53095 Return He pipe for Solenoid 1 pipe w 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

model validity

flow type friction factor Must enter a guess pipe roughness Pipe inside diameter Length of pipe cross sectional area Total mass flow rate Liquid density density of the gas Liquid viscosity Gas Viscosity Surface tension of liquid quality = mdotGmdot Reynolds for liquid Mass flow rate for liquid Reynolds for gas Mass flow rate for gas AP1lL for the liquid AP1lL for the two phase

Total pressure drop for the pipe ~ 100 ~JGtcs 1b uu Stu

Lockhart-Martinelli parameter Lockhart-Martinelli parameter L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 Baker diagram dimensionless parameter density of air density of water Baker diagram dimensionless parameter Surface tension of water viscosity of water X - axis value for Baker plot Y-axis value for Baker plot

Volume fraction of liquid phase Volume fraction of gas phase Gas velocity Liquid velocity

000005 1057 200

4 1211 2017 318 1323 000082 3876

shy

2

25

184

316 20

12 998

073 1000

-

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

rdeltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 Bakerxa BakerYa c M RsubL RsubG GasVel LiqVel

Output Comment Russ Rucinski 53095 Return He pipe for Solenoid 1 12 pipe wi 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

accurate model validity

turbulen flow type 02260289 friction factor Must enter a guess

ft pipe roughness in Pipe inside diameter ft Length of pipe

00056612 m2 cross sectional area gls Total mass flow rate kgm 3 Liquid density kgm3 density of the gas JLPa-s Liquid viscosity JLPa-s Gas viscosity Nm Surface tension of liquid

quality = mdotGmdot 36530 Reynolds for liquid

0024496 kgls Mass flow rate for liquid 55580 Reynolds for gas

0015504 kgls Mass flow rate for gas

0650814 Palm LP I LU for the liquid 21275204 Palm LPLU for the two phase

01881077 psig 1 Total pressure drop for the pipe

57175294 Lockhart-Martinelli parameter 67767548 Lockhart-Martinelli parameter

L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719

1 4281346 Baker diagram dimensionless parameter kgm3 density of air kgm3 density of water

53412427 Baker diagram dimensionless parameter Nm Surface tension of water JLPa-s viscosity of water

1210 X - axis value for Baker 1410 lbmhr-ft Y-axis value for Baker

1 1 17490072 Volume fraction of liquid phase 82509928 Volume fraction of gas phase 16456003 ms Gas velocity 20429237 ms Liquid velocity

53095 middot

FERMILAB TWO PHASE HEUUM FLOW TESTS

) )

Russ KUCt~5~l

10 ~ 1 I UAUEOOV

11 ~7 I I I Flow Fath Flaw

~--- Annular Flow Wave Flow

------ Slug FlowI

A tf SIO ______

~gt

---IIMIR RIGIMI BOUNDARIII ~ G bull RCtPtC GAl OW RAlI -- ClFtC LIQUID now RAT ~l-III _lIN_

10 I I ~I gt bull I I

MaMIIow_

X 5SVI PI U bull MIddIt of IOIItnoId

1 10 VI PI bull bull Ex of IOIItnoId

18 VI PI 7 bull 1111111 of control dewarbull Figura 1 Baker diagram with Mamedov curves or two phase helium In horzonlal channels

[FttoJIA Djli El 38 23IlJ -Gt-J - 33 8 ]

r J1

01 10 10 10 ( 10 i ~ ~ 10 ~ ~ 10 L ~nG CAt 0 )V rPl

~ IMaIIon TIJampE

0J

PIPE

112 5C~ 10 f 5eCD

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995

Russ Rucinski and Steve Sakla ROOQJ Mech

Approved _________

-

n ~ middotrt -

Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

-------------~ ~~~--~~~~--

Ud

)

) ) f

J8 CO bull 0049 N2 tu~bullbull

58 CO bull 0049 He Supply 1 12 sch lOS pipe

l Sch lOS H return SS

J4 CO bull 0065 He Cool down return

He Cool downQuench Return 25 CO bull 0065 Cu Rod shield

Main Solenoid xfer ine Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

Potta 1 rb 21 153121 CST ~ by rwcnoi

~lGUJCE 1

N

)J

1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

i foE 9flIIy 1JTAlE rlTX6 AHFEEDCAN 112 00 X 049 0402 5 2 0 0 0

tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

I

bull VIJIC iliil-flH Ie FT I

I I i I bullbullOF IUlaWS IN 8 i I

I1Igel

I Ibull I

9 o 2 III J o en

L

FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

~I_ i 50 Uf-bln 3823 _ c NAME

Russ

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J o N

(

N N

H

I

J

1 shy

c e-l ~w ~ UI

CIgt

~1

FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

~ )

-shy

~ M )

f ltgt0 ~O~ I 0 bull ~

If g -rI ~ t shy ~T

0

~ r

~ -a

-r

0 0

-Sci

bull~

~ ~

i-T

intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

-1(IL------- ~ ~l

-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

d (-10 ( ~raquo

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25 lie SL 20

~ d51-

7 Sbull 2shy3 2 3 472

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-- ---------- raquo

b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

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f~nr - ~- ALVMtJUM

SA 4 2otJ K 6~ oJ I 270 ~ amp-A5 our

h(7vr 1311~h lN ~ 1054 ~

-k-shy - - = A ATWO 1r (tgt15)(O4~[51))

o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

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A I) CDEFtIrL~ ib COOItgt()~J A-r (tATamp 0 5 ~A

o7b 10 T I ~ l

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STEP 3

S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

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48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

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PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

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JS

t -= 0 0-5 ]7

I

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jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

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X-o ~1 OoS

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JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 7: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

17

- It was concluded that step 4s pressure drop would be about 36 times larger than step 1 IS

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet

temperature of 80K and an outlet temperature of 90K (refer to appendix D)

VLPC Helium Cool down Pressure drops A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 4

for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the

given pipe sizes and inletexit states The VLPC cooldown piping was first sized by

assuming a pressure drop of 95 psig an inlet temperature of 80K GHe and an outlet

temperature of 90K through the supply and return lines respectively Resistance

coefficients were calculated for four segments of the piping In the second step of the

calculation pressure drops were calculated for each segment taking into account the

change in density due to changes in pressure Summing the individual pressure drops

resulted in a rough estimated pressure drop of 591 psi These numbers are summarized

in table 9 for the initial supply size of318 OD and return size of112 OD tubes See

Appendix E for the raw calculations After looking at steady state pressure drops the

line sizes for the supply and return were increased to 112 OD and 518 OD respectively

Therefore pressure drops listed in Table 9 will be less

Table 9 VLPC Helium Cooldown piping pressure drop summary

for 318 supply amp 112 return sizes

PIPE SECTION PRESSURE DROP (PSIA)

Supply line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

-

-

15

- VLPC Helium Steady State Pressure drops

-

The expected pressure drop for 318 OD x 0035 wall supply tubing for a steady

state flow of5 gls and a transfer line heat load of lOW was conservatively estimated at

46 psi per 100ft This prompted the increase in size to 112 OD x 0049 wall tubing

The calculated pressure drop for the two phase supply would be 12 psi per 100ft

Backing offon the conservatism and figuring approx 200ft ofequivalent length a real

estimate ofthe supply pressure drop from the refrigerator to the VLPC cryostat is about 1

psi See Appendix H page H4

The expected pressure drop for the return 518 OD x 0049 wall tube with 5 gIs

65 K gas flowing is 06 psig Since the supply and return tubing accounts for less than 2

psi pressure drop there is approximiately 10 psi available across the control valve and

cryostat See Appendix H page H3

VLPC Nitro~en flowrates and pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 OD Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

~~~~~~ ~- ---~-~----~ --_ --------------------- shy

lC

- Table of Contents for the Appendices

Raw En2ineerin2 Calculations

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

Appendix L Solenoid steady state cales Helium return piping

-

-

-0 FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3B23115 SERIALmiddotCATEGORY

11 I PAGE

SUBJECT NAME

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It-w FERMILAB

ENGINEERING NOTE SECTION PROJECT SERIAl-CATEGORY

3S23 I IS PAGE

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ENGINEERING NOTE SECTION

RDIDcent PROJECT

He -y Fe12 SERIALmiddotCATEGORY

3S23IlS PAGE

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NAME

DATE IREVISION DATE

5Z-hQ5 1

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ENGINEERING NOTE SECTION PROJECT

Jle x Fampltt ( tlJ Ii

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38 Z- 3 bull Il $ PAGE

L2 SUBJECT

He NAME

IREVISION DATE DATE

5-30 -atS

IIFo(t 1i1 ~)( CQoj 0 bull 11 )t-I ~ ~) Afo-JO A Scu [0

P 1tJG IIJJ I cent 511 11 0D DI-f = L2

A

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t bull oS loJ

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-

stlnput

000005

427 200

4 1211 2017 318 1323 000082 3876

-2 2 184 184 20

12 998

073 1000

shy

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

deltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 BakerXa BakerYa c M RsubL RsubG GasVel Liqvel

Output

accurate

turbulen 01906103

ft in ft

92387E-5 m2 gs kgm 3 kgm3 JlPa-s JlPa-s Nm

90430 0024496 kgS

137600 0015504 kgs 51012286 pam 16810555 Pam

14863285 psig

57405518 67244052

1 4281346 kgmA 3 kgmA 3

53412427 Nm JlPa-s

1210 8660 lbmhr-ft

1 1 17419928 82580072 1 0075104 ms 12568736 ms

Comment L3 Russ Rucinski 53095 Return He pipe for Solenoid 1 pipe w 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

model validity

flow type friction factor Must enter a guess pipe roughness Pipe inside diameter Length of pipe cross sectional area Total mass flow rate Liquid density density of the gas Liquid viscosity Gas Viscosity Surface tension of liquid quality = mdotGmdot Reynolds for liquid Mass flow rate for liquid Reynolds for gas Mass flow rate for gas AP1lL for the liquid AP1lL for the two phase

Total pressure drop for the pipe ~ 100 ~JGtcs 1b uu Stu

Lockhart-Martinelli parameter Lockhart-Martinelli parameter L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 Baker diagram dimensionless parameter density of air density of water Baker diagram dimensionless parameter Surface tension of water viscosity of water X - axis value for Baker plot Y-axis value for Baker plot

Volume fraction of liquid phase Volume fraction of gas phase Gas velocity Liquid velocity

000005 1057 200

4 1211 2017 318 1323 000082 3876

shy

2

25

184

316 20

12 998

073 1000

-

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

rdeltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 Bakerxa BakerYa c M RsubL RsubG GasVel LiqVel

Output Comment Russ Rucinski 53095 Return He pipe for Solenoid 1 12 pipe wi 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

accurate model validity

turbulen flow type 02260289 friction factor Must enter a guess

ft pipe roughness in Pipe inside diameter ft Length of pipe

00056612 m2 cross sectional area gls Total mass flow rate kgm 3 Liquid density kgm3 density of the gas JLPa-s Liquid viscosity JLPa-s Gas viscosity Nm Surface tension of liquid

quality = mdotGmdot 36530 Reynolds for liquid

0024496 kgls Mass flow rate for liquid 55580 Reynolds for gas

0015504 kgls Mass flow rate for gas

0650814 Palm LP I LU for the liquid 21275204 Palm LPLU for the two phase

01881077 psig 1 Total pressure drop for the pipe

57175294 Lockhart-Martinelli parameter 67767548 Lockhart-Martinelli parameter

L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719

1 4281346 Baker diagram dimensionless parameter kgm3 density of air kgm3 density of water

53412427 Baker diagram dimensionless parameter Nm Surface tension of water JLPa-s viscosity of water

1210 X - axis value for Baker 1410 lbmhr-ft Y-axis value for Baker

1 1 17490072 Volume fraction of liquid phase 82509928 Volume fraction of gas phase 16456003 ms Gas velocity 20429237 ms Liquid velocity

53095 middot

FERMILAB TWO PHASE HEUUM FLOW TESTS

) )

Russ KUCt~5~l

10 ~ 1 I UAUEOOV

11 ~7 I I I Flow Fath Flaw

~--- Annular Flow Wave Flow

------ Slug FlowI

A tf SIO ______

~gt

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10 I I ~I gt bull I I

MaMIIow_

X 5SVI PI U bull MIddIt of IOIItnoId

1 10 VI PI bull bull Ex of IOIItnoId

18 VI PI 7 bull 1111111 of control dewarbull Figura 1 Baker diagram with Mamedov curves or two phase helium In horzonlal channels

[FttoJIA Djli El 38 23IlJ -Gt-J - 33 8 ]

r J1

01 10 10 10 ( 10 i ~ ~ 10 ~ ~ 10 L ~nG CAt 0 )V rPl

~ IMaIIon TIJampE

0J

PIPE

112 5C~ 10 f 5eCD

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995

Russ Rucinski and Steve Sakla ROOQJ Mech

Approved _________

-

n ~ middotrt -

Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

-------------~ ~~~--~~~~--

Ud

)

) ) f

J8 CO bull 0049 N2 tu~bullbull

58 CO bull 0049 He Supply 1 12 sch lOS pipe

l Sch lOS H return SS

J4 CO bull 0065 He Cool down return

He Cool downQuench Return 25 CO bull 0065 Cu Rod shield

Main Solenoid xfer ine Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

Potta 1 rb 21 153121 CST ~ by rwcnoi

~lGUJCE 1

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1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

i foE 9flIIy 1JTAlE rlTX6 AHFEEDCAN 112 00 X 049 0402 5 2 0 0 0

tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

I

bull VIJIC iliil-flH Ie FT I

I I i I bullbullOF IUlaWS IN 8 i I

I1Igel

I Ibull I

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FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

~I_ i 50 Uf-bln 3823 _ c NAME

Russ

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J o N

(

N N

H

I

J

1 shy

c e-l ~w ~ UI

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FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

~ )

-shy

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f ltgt0 ~O~ I 0 bull ~

If g -rI ~ t shy ~T

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intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

-1(IL------- ~ ~l

-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

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bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

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o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

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)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

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~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

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Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

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SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

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bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

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w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

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) 0middot 1 ltD ~~c Q ) -111 g

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I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

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)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

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~ Iojoo

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$$Hfi

Y shy~ V I

III ~fO Jo I TIl

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Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

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3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

~ 11 LE1 0o-lD)-S vJG ~e~ 771 ADD J(i~ w~ Fc~lJ vf J 50~~r--middotC

-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

- II gtlt 1( SvlfoVlS (2 fi_shyb w - ~PrD IP-t S vPlgto2---fShmiddott

30W 0 7- tz A- I Itt- 0 tv bull I () I( 5 1gt~fINI- pUs 130 w- Cc 15I4J Z 50 o

c A tJ 7 3_64- VII s~

1trcP1 jc ~---)-

rv - bullbull OF FXIEgt~ ( 2S 1 ~ CL- (_~

bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

2 ~ Zgt ~ IV - I (1 Of CH IA IJ amp- - J i_2soeW - l~ or- Ck Nt 13 INIttSq

- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 8: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

15

- VLPC Helium Steady State Pressure drops

-

The expected pressure drop for 318 OD x 0035 wall supply tubing for a steady

state flow of5 gls and a transfer line heat load of lOW was conservatively estimated at

46 psi per 100ft This prompted the increase in size to 112 OD x 0049 wall tubing

The calculated pressure drop for the two phase supply would be 12 psi per 100ft

Backing offon the conservatism and figuring approx 200ft ofequivalent length a real

estimate ofthe supply pressure drop from the refrigerator to the VLPC cryostat is about 1

psi See Appendix H page H4

The expected pressure drop for the return 518 OD x 0049 wall tube with 5 gIs

65 K gas flowing is 06 psig Since the supply and return tubing accounts for less than 2

psi pressure drop there is approximiately 10 psi available across the control valve and

cryostat See Appendix H page H3

VLPC Nitro~en flowrates and pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 OD Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

~~~~~~ ~- ---~-~----~ --_ --------------------- shy

lC

- Table of Contents for the Appendices

Raw En2ineerin2 Calculations

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

Appendix L Solenoid steady state cales Helium return piping

-

-

-0 FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3B23115 SERIALmiddotCATEGORY

11 I PAGE

SUBJECT NAME

- (LPC Rl5~ RUCIf-Jst

CO t-J S f D ER ~-r~bf j -p ( e-e -t 0 S 1 A 1 S ~

CJ Svlt-CNoD Dc-gtICIr-J RE-POliL-r QC)fA1- - 270 VII ) 141601-1

es -r- I - bull C U R IL -bullbullrr Es j M e os AlE 70 vJ PEft- 0 ~~

+t-J(gt it-I2-I+APS p ACJOIOfJA-t 40 vJ Faa ~A)F~ ul-lE-s t

1 J vM(Jfpound(J5 Q1~o- = 180 tAJ bull

-

20 w

Sla DD 0 315 1AJA1-L id =- ~os ee = 4M 4middot (00437gt ~s)

D~ IT (305 )( OlS~ MN) ( I 72 k ~ 10- b Pec-S)

-41421 -f=oI3 l Z

(i) = I 3 AP 3 ~119j bull 0 ~ Ll -= L d Ii

(I 00 f-L~ K (0 Ii) 3 5 Sf

ItO ~ k

-

11

c_ bull OQ435 s -

--------_------------shy

I HZ 5- 3c-75pf1EN 01gtc f-1- (trCvLATlCIJ)

1r 1)7

) A

II f

t-A 5Jh Z 0 i) gtlt a 0 lt-I~ AJJ I b5k -cb- O-1OZ1 cgtO(oz- gt 012 MI)~ L-= 200t-i roO9GM

v (m ) e --~ (z) (1r- DA )

-( il -J

-~~---7- I )

v ~ v -2shybull 7 L- V

l) - - l lQ [ r) 2~

T

( ( I ~ IS (82 amp8 ~gt1-= (~lt17 b lt013)( o elY) ( 4gt0 cr or) llaquo

2 5 b 8z (8 gt0 z 2-7 psi

--- --~----- ----~ - ~-~------ - -~- ---------shy

H-3 J I

-

r i~ - r- ~-t~ -shy6 -= 081 ~ Jfi L s __ O~ k

i -

e~ It~ Jo~ -1- 7Z 7lt alt ~- 5

N --=- 000 y~ Jias

j b5 1lt

Plt= 64 )-t

-

I L

SUBJECT NAME

- SUPPLlt( DATE(pZ 10 ~ IREVISION DATE

It-w FERMILAB

ENGINEERING NOTE SECTION PROJECT SERIAl-CATEGORY

3S23 I IS PAGE

rl4

3 III - (ImiddotTJ3~ T -z w TlANrrut l1-W -lo jr W -~ 1- I w mAlS L i rJ C

5~ I C ~ 1 1 ( LEA t 1=20M t-I-tlt ~1ClttA ampe i)wA-rt 10 LPC Clt-(os -rk-r

5TA-re(j)

t Ik- pewAn ~~-r L10

- L4 ~o ~

p 9 ( 5 i9 5 A $TAI

hl 1 Be J -

o Pz e M 16MPa = 95 fJ~(j ~L 11flP

-d- = ZYIl

Xl--= ~-~-Fo 158~119h 032 yj - kF ~f 1t--1I96

Afo()

S TIlO

Vft TtJ~ =- 6Po() 2 f5i

L~f-l E(t S P(2UbAb-Y ~~ v 1 VPltL-~( -ru ZfJO Ff

-

FERMILAB

ENGINEERING NOTE SECTION

RDIDcent PROJECT

He -y Fe12 SERIALmiddotCATEGORY

3S23IlS PAGE

LI SUBJECT 2-J

P HE RerulZJ =gt P toJ

50- e jJlH 0

NAME

DATE IREVISION DATE

5Z-hQ5 1

~iTATe Q)

P =I g A-rM

5Ar lGUID

1- 4l( 1lt

hjZ - 14 Bb lId

S-AIE hls 2 b35

S 1) sPec

~-IG CD P2 = I 2 MPoshy(z= _0

Y11Vd =30 b Jr

Mz I ~~

1 Sbil shy 1107

30 1-1107

s z lt3) 2 cent

P3 -=IZ ~ PA T Lj~IK

39 Yf ) = 5

~ HL 0 c( 3 ~ F-O

h middot07 J~ h~ 30 b-l~

)(~ 387

-

I

6P 14Sb

)

FERMllAB

ENGINEERING NOTE SECTION PROJECT

Jle x Fampltt ( tlJ Ii

SERIAL-CATEGORY

38 Z- 3 bull Il $ PAGE

L2 SUBJECT

He NAME

IREVISION DATE DATE

5-30 -atS

IIFo(t 1i1 ~)( CQoj 0 bull 11 )t-I ~ ~) Afo-JO A Scu [0

P 1tJG IIJJ I cent 511 11 0D DI-f = L2

A

Ilz S CI-L 10 P IPG-) ID = I =gt82 I

t bull oS loJ

IS 35 00shy-I( 0 D J-- Felt -rtt IS S 12Gt

-

stlnput

000005

427 200

4 1211 2017 318 1323 000082 3876

-2 2 184 184 20

12 998

073 1000

shy

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

deltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 BakerXa BakerYa c M RsubL RsubG GasVel Liqvel

Output

accurate

turbulen 01906103

ft in ft

92387E-5 m2 gs kgm 3 kgm3 JlPa-s JlPa-s Nm

90430 0024496 kgS

137600 0015504 kgs 51012286 pam 16810555 Pam

14863285 psig

57405518 67244052

1 4281346 kgmA 3 kgmA 3

53412427 Nm JlPa-s

1210 8660 lbmhr-ft

1 1 17419928 82580072 1 0075104 ms 12568736 ms

Comment L3 Russ Rucinski 53095 Return He pipe for Solenoid 1 pipe w 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

model validity

flow type friction factor Must enter a guess pipe roughness Pipe inside diameter Length of pipe cross sectional area Total mass flow rate Liquid density density of the gas Liquid viscosity Gas Viscosity Surface tension of liquid quality = mdotGmdot Reynolds for liquid Mass flow rate for liquid Reynolds for gas Mass flow rate for gas AP1lL for the liquid AP1lL for the two phase

Total pressure drop for the pipe ~ 100 ~JGtcs 1b uu Stu

Lockhart-Martinelli parameter Lockhart-Martinelli parameter L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 Baker diagram dimensionless parameter density of air density of water Baker diagram dimensionless parameter Surface tension of water viscosity of water X - axis value for Baker plot Y-axis value for Baker plot

Volume fraction of liquid phase Volume fraction of gas phase Gas velocity Liquid velocity

000005 1057 200

4 1211 2017 318 1323 000082 3876

shy

2

25

184

316 20

12 998

073 1000

-

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

rdeltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 Bakerxa BakerYa c M RsubL RsubG GasVel LiqVel

Output Comment Russ Rucinski 53095 Return He pipe for Solenoid 1 12 pipe wi 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

accurate model validity

turbulen flow type 02260289 friction factor Must enter a guess

ft pipe roughness in Pipe inside diameter ft Length of pipe

00056612 m2 cross sectional area gls Total mass flow rate kgm 3 Liquid density kgm3 density of the gas JLPa-s Liquid viscosity JLPa-s Gas viscosity Nm Surface tension of liquid

quality = mdotGmdot 36530 Reynolds for liquid

0024496 kgls Mass flow rate for liquid 55580 Reynolds for gas

0015504 kgls Mass flow rate for gas

0650814 Palm LP I LU for the liquid 21275204 Palm LPLU for the two phase

01881077 psig 1 Total pressure drop for the pipe

57175294 Lockhart-Martinelli parameter 67767548 Lockhart-Martinelli parameter

L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719

1 4281346 Baker diagram dimensionless parameter kgm3 density of air kgm3 density of water

53412427 Baker diagram dimensionless parameter Nm Surface tension of water JLPa-s viscosity of water

1210 X - axis value for Baker 1410 lbmhr-ft Y-axis value for Baker

1 1 17490072 Volume fraction of liquid phase 82509928 Volume fraction of gas phase 16456003 ms Gas velocity 20429237 ms Liquid velocity

53095 middot

FERMILAB TWO PHASE HEUUM FLOW TESTS

) )

Russ KUCt~5~l

10 ~ 1 I UAUEOOV

11 ~7 I I I Flow Fath Flaw

~--- Annular Flow Wave Flow

------ Slug FlowI

A tf SIO ______

~gt

---IIMIR RIGIMI BOUNDARIII ~ G bull RCtPtC GAl OW RAlI -- ClFtC LIQUID now RAT ~l-III _lIN_

10 I I ~I gt bull I I

MaMIIow_

X 5SVI PI U bull MIddIt of IOIItnoId

1 10 VI PI bull bull Ex of IOIItnoId

18 VI PI 7 bull 1111111 of control dewarbull Figura 1 Baker diagram with Mamedov curves or two phase helium In horzonlal channels

[FttoJIA Djli El 38 23IlJ -Gt-J - 33 8 ]

r J1

01 10 10 10 ( 10 i ~ ~ 10 ~ ~ 10 L ~nG CAt 0 )V rPl

~ IMaIIon TIJampE

0J

PIPE

112 5C~ 10 f 5eCD

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995

Russ Rucinski and Steve Sakla ROOQJ Mech

Approved _________

-

n ~ middotrt -

Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

-------------~ ~~~--~~~~--

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PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

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lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

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4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

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RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

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tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

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43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

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10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

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75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

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NAME

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intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

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14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

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~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

~ 11 LE1 0o-lD)-S vJG ~e~ 771 ADD J(i~ w~ Fc~lJ vf J 50~~r--middotC

-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

- II gtlt 1( SvlfoVlS (2 fi_shyb w - ~PrD IP-t S vPlgto2---fShmiddott

30W 0 7- tz A- I Itt- 0 tv bull I () I( 5 1gt~fINI- pUs 130 w- Cc 15I4J Z 50 o

c A tJ 7 3_64- VII s~

1trcP1 jc ~---)-

rv - bullbull OF FXIEgt~ ( 2S 1 ~ CL- (_~

bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

2 ~ Zgt ~ IV - I (1 Of CH IA IJ amp- - J i_2soeW - l~ or- Ck Nt 13 INIttSq

- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 9: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

lC

- Table of Contents for the Appendices

Raw En2ineerin2 Calculations

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

Appendix L Solenoid steady state cales Helium return piping

-

-

-0 FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3B23115 SERIALmiddotCATEGORY

11 I PAGE

SUBJECT NAME

- (LPC Rl5~ RUCIf-Jst

CO t-J S f D ER ~-r~bf j -p ( e-e -t 0 S 1 A 1 S ~

CJ Svlt-CNoD Dc-gtICIr-J RE-POliL-r QC)fA1- - 270 VII ) 141601-1

es -r- I - bull C U R IL -bullbullrr Es j M e os AlE 70 vJ PEft- 0 ~~

+t-J(gt it-I2-I+APS p ACJOIOfJA-t 40 vJ Faa ~A)F~ ul-lE-s t

1 J vM(Jfpound(J5 Q1~o- = 180 tAJ bull

-

20 w

Sla DD 0 315 1AJA1-L id =- ~os ee = 4M 4middot (00437gt ~s)

D~ IT (305 )( OlS~ MN) ( I 72 k ~ 10- b Pec-S)

-41421 -f=oI3 l Z

(i) = I 3 AP 3 ~119j bull 0 ~ Ll -= L d Ii

(I 00 f-L~ K (0 Ii) 3 5 Sf

ItO ~ k

-

11

c_ bull OQ435 s -

--------_------------shy

I HZ 5- 3c-75pf1EN 01gtc f-1- (trCvLATlCIJ)

1r 1)7

) A

II f

t-A 5Jh Z 0 i) gtlt a 0 lt-I~ AJJ I b5k -cb- O-1OZ1 cgtO(oz- gt 012 MI)~ L-= 200t-i roO9GM

v (m ) e --~ (z) (1r- DA )

-( il -J

-~~---7- I )

v ~ v -2shybull 7 L- V

l) - - l lQ [ r) 2~

T

( ( I ~ IS (82 amp8 ~gt1-= (~lt17 b lt013)( o elY) ( 4gt0 cr or) llaquo

2 5 b 8z (8 gt0 z 2-7 psi

--- --~----- ----~ - ~-~------ - -~- ---------shy

H-3 J I

-

r i~ - r- ~-t~ -shy6 -= 081 ~ Jfi L s __ O~ k

i -

e~ It~ Jo~ -1- 7Z 7lt alt ~- 5

N --=- 000 y~ Jias

j b5 1lt

Plt= 64 )-t

-

I L

SUBJECT NAME

- SUPPLlt( DATE(pZ 10 ~ IREVISION DATE

It-w FERMILAB

ENGINEERING NOTE SECTION PROJECT SERIAl-CATEGORY

3S23 I IS PAGE

rl4

3 III - (ImiddotTJ3~ T -z w TlANrrut l1-W -lo jr W -~ 1- I w mAlS L i rJ C

5~ I C ~ 1 1 ( LEA t 1=20M t-I-tlt ~1ClttA ampe i)wA-rt 10 LPC Clt-(os -rk-r

5TA-re(j)

t Ik- pewAn ~~-r L10

- L4 ~o ~

p 9 ( 5 i9 5 A $TAI

hl 1 Be J -

o Pz e M 16MPa = 95 fJ~(j ~L 11flP

-d- = ZYIl

Xl--= ~-~-Fo 158~119h 032 yj - kF ~f 1t--1I96

Afo()

S TIlO

Vft TtJ~ =- 6Po() 2 f5i

L~f-l E(t S P(2UbAb-Y ~~ v 1 VPltL-~( -ru ZfJO Ff

-

FERMILAB

ENGINEERING NOTE SECTION

RDIDcent PROJECT

He -y Fe12 SERIALmiddotCATEGORY

3S23IlS PAGE

LI SUBJECT 2-J

P HE RerulZJ =gt P toJ

50- e jJlH 0

NAME

DATE IREVISION DATE

5Z-hQ5 1

~iTATe Q)

P =I g A-rM

5Ar lGUID

1- 4l( 1lt

hjZ - 14 Bb lId

S-AIE hls 2 b35

S 1) sPec

~-IG CD P2 = I 2 MPoshy(z= _0

Y11Vd =30 b Jr

Mz I ~~

1 Sbil shy 1107

30 1-1107

s z lt3) 2 cent

P3 -=IZ ~ PA T Lj~IK

39 Yf ) = 5

~ HL 0 c( 3 ~ F-O

h middot07 J~ h~ 30 b-l~

)(~ 387

-

I

6P 14Sb

)

FERMllAB

ENGINEERING NOTE SECTION PROJECT

Jle x Fampltt ( tlJ Ii

SERIAL-CATEGORY

38 Z- 3 bull Il $ PAGE

L2 SUBJECT

He NAME

IREVISION DATE DATE

5-30 -atS

IIFo(t 1i1 ~)( CQoj 0 bull 11 )t-I ~ ~) Afo-JO A Scu [0

P 1tJG IIJJ I cent 511 11 0D DI-f = L2

A

Ilz S CI-L 10 P IPG-) ID = I =gt82 I

t bull oS loJ

IS 35 00shy-I( 0 D J-- Felt -rtt IS S 12Gt

-

stlnput

000005

427 200

4 1211 2017 318 1323 000082 3876

-2 2 184 184 20

12 998

073 1000

shy

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

deltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 BakerXa BakerYa c M RsubL RsubG GasVel Liqvel

Output

accurate

turbulen 01906103

ft in ft

92387E-5 m2 gs kgm 3 kgm3 JlPa-s JlPa-s Nm

90430 0024496 kgS

137600 0015504 kgs 51012286 pam 16810555 Pam

14863285 psig

57405518 67244052

1 4281346 kgmA 3 kgmA 3

53412427 Nm JlPa-s

1210 8660 lbmhr-ft

1 1 17419928 82580072 1 0075104 ms 12568736 ms

Comment L3 Russ Rucinski 53095 Return He pipe for Solenoid 1 pipe w 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

model validity

flow type friction factor Must enter a guess pipe roughness Pipe inside diameter Length of pipe cross sectional area Total mass flow rate Liquid density density of the gas Liquid viscosity Gas Viscosity Surface tension of liquid quality = mdotGmdot Reynolds for liquid Mass flow rate for liquid Reynolds for gas Mass flow rate for gas AP1lL for the liquid AP1lL for the two phase

Total pressure drop for the pipe ~ 100 ~JGtcs 1b uu Stu

Lockhart-Martinelli parameter Lockhart-Martinelli parameter L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 Baker diagram dimensionless parameter density of air density of water Baker diagram dimensionless parameter Surface tension of water viscosity of water X - axis value for Baker plot Y-axis value for Baker plot

Volume fraction of liquid phase Volume fraction of gas phase Gas velocity Liquid velocity

000005 1057 200

4 1211 2017 318 1323 000082 3876

shy

2

25

184

316 20

12 998

073 1000

-

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

rdeltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 Bakerxa BakerYa c M RsubL RsubG GasVel LiqVel

Output Comment Russ Rucinski 53095 Return He pipe for Solenoid 1 12 pipe wi 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

accurate model validity

turbulen flow type 02260289 friction factor Must enter a guess

ft pipe roughness in Pipe inside diameter ft Length of pipe

00056612 m2 cross sectional area gls Total mass flow rate kgm 3 Liquid density kgm3 density of the gas JLPa-s Liquid viscosity JLPa-s Gas viscosity Nm Surface tension of liquid

quality = mdotGmdot 36530 Reynolds for liquid

0024496 kgls Mass flow rate for liquid 55580 Reynolds for gas

0015504 kgls Mass flow rate for gas

0650814 Palm LP I LU for the liquid 21275204 Palm LPLU for the two phase

01881077 psig 1 Total pressure drop for the pipe

57175294 Lockhart-Martinelli parameter 67767548 Lockhart-Martinelli parameter

L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719

1 4281346 Baker diagram dimensionless parameter kgm3 density of air kgm3 density of water

53412427 Baker diagram dimensionless parameter Nm Surface tension of water JLPa-s viscosity of water

1210 X - axis value for Baker 1410 lbmhr-ft Y-axis value for Baker

1 1 17490072 Volume fraction of liquid phase 82509928 Volume fraction of gas phase 16456003 ms Gas velocity 20429237 ms Liquid velocity

53095 middot

FERMILAB TWO PHASE HEUUM FLOW TESTS

) )

Russ KUCt~5~l

10 ~ 1 I UAUEOOV

11 ~7 I I I Flow Fath Flaw

~--- Annular Flow Wave Flow

------ Slug FlowI

A tf SIO ______

~gt

---IIMIR RIGIMI BOUNDARIII ~ G bull RCtPtC GAl OW RAlI -- ClFtC LIQUID now RAT ~l-III _lIN_

10 I I ~I gt bull I I

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18 VI PI 7 bull 1111111 of control dewarbull Figura 1 Baker diagram with Mamedov curves or two phase helium In horzonlal channels

[FttoJIA Djli El 38 23IlJ -Gt-J - 33 8 ]

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01 10 10 10 ( 10 i ~ ~ 10 ~ ~ 10 L ~nG CAt 0 )V rPl

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112 5C~ 10 f 5eCD

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995

Russ Rucinski and Steve Sakla ROOQJ Mech

Approved _________

-

n ~ middotrt -

Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

-------------~ ~~~--~~~~--

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J8 CO bull 0049 N2 tu~bullbull

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l Sch lOS H return SS

J4 CO bull 0065 He Cool down return

He Cool downQuench Return 25 CO bull 0065 Cu Rod shield

Main Solenoid xfer ine Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

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1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

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tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

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SUBJECT

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ENGINEERING NOTE

FIGURES

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ENGINEERING NOTE SECTION PROJECT

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SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

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intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

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i bull I rI -j r

I

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I I

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bull

bull iii

bull iii

-I

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--

--

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UR

E 7

~-----------------~

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bull

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l

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I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

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PROJeCT SERIAl-CATEGORY

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SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

~ 11 LE1 0o-lD)-S vJG ~e~ 771 ADD J(i~ w~ Fc~lJ vf J 50~~r--middotC

-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

- II gtlt 1( SvlfoVlS (2 fi_shyb w - ~PrD IP-t S vPlgto2---fShmiddott

30W 0 7- tz A- I Itt- 0 tv bull I () I( 5 1gt~fINI- pUs 130 w- Cc 15I4J Z 50 o

c A tJ 7 3_64- VII s~

1trcP1 jc ~---)-

rv - bullbull OF FXIEgt~ ( 2S 1 ~ CL- (_~

bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

2 ~ Zgt ~ IV - I (1 Of CH IA IJ amp- - J i_2soeW - l~ or- Ck Nt 13 INIttSq

- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 10: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

-0 FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3B23115 SERIALmiddotCATEGORY

11 I PAGE

SUBJECT NAME

- (LPC Rl5~ RUCIf-Jst

CO t-J S f D ER ~-r~bf j -p ( e-e -t 0 S 1 A 1 S ~

CJ Svlt-CNoD Dc-gtICIr-J RE-POliL-r QC)fA1- - 270 VII ) 141601-1

es -r- I - bull C U R IL -bullbullrr Es j M e os AlE 70 vJ PEft- 0 ~~

+t-J(gt it-I2-I+APS p ACJOIOfJA-t 40 vJ Faa ~A)F~ ul-lE-s t

1 J vM(Jfpound(J5 Q1~o- = 180 tAJ bull

-

20 w

Sla DD 0 315 1AJA1-L id =- ~os ee = 4M 4middot (00437gt ~s)

D~ IT (305 )( OlS~ MN) ( I 72 k ~ 10- b Pec-S)

-41421 -f=oI3 l Z

(i) = I 3 AP 3 ~119j bull 0 ~ Ll -= L d Ii

(I 00 f-L~ K (0 Ii) 3 5 Sf

ItO ~ k

-

11

c_ bull OQ435 s -

--------_------------shy

I HZ 5- 3c-75pf1EN 01gtc f-1- (trCvLATlCIJ)

1r 1)7

) A

II f

t-A 5Jh Z 0 i) gtlt a 0 lt-I~ AJJ I b5k -cb- O-1OZ1 cgtO(oz- gt 012 MI)~ L-= 200t-i roO9GM

v (m ) e --~ (z) (1r- DA )

-( il -J

-~~---7- I )

v ~ v -2shybull 7 L- V

l) - - l lQ [ r) 2~

T

( ( I ~ IS (82 amp8 ~gt1-= (~lt17 b lt013)( o elY) ( 4gt0 cr or) llaquo

2 5 b 8z (8 gt0 z 2-7 psi

--- --~----- ----~ - ~-~------ - -~- ---------shy

H-3 J I

-

r i~ - r- ~-t~ -shy6 -= 081 ~ Jfi L s __ O~ k

i -

e~ It~ Jo~ -1- 7Z 7lt alt ~- 5

N --=- 000 y~ Jias

j b5 1lt

Plt= 64 )-t

-

I L

SUBJECT NAME

- SUPPLlt( DATE(pZ 10 ~ IREVISION DATE

It-w FERMILAB

ENGINEERING NOTE SECTION PROJECT SERIAl-CATEGORY

3S23 I IS PAGE

rl4

3 III - (ImiddotTJ3~ T -z w TlANrrut l1-W -lo jr W -~ 1- I w mAlS L i rJ C

5~ I C ~ 1 1 ( LEA t 1=20M t-I-tlt ~1ClttA ampe i)wA-rt 10 LPC Clt-(os -rk-r

5TA-re(j)

t Ik- pewAn ~~-r L10

- L4 ~o ~

p 9 ( 5 i9 5 A $TAI

hl 1 Be J -

o Pz e M 16MPa = 95 fJ~(j ~L 11flP

-d- = ZYIl

Xl--= ~-~-Fo 158~119h 032 yj - kF ~f 1t--1I96

Afo()

S TIlO

Vft TtJ~ =- 6Po() 2 f5i

L~f-l E(t S P(2UbAb-Y ~~ v 1 VPltL-~( -ru ZfJO Ff

-

FERMILAB

ENGINEERING NOTE SECTION

RDIDcent PROJECT

He -y Fe12 SERIALmiddotCATEGORY

3S23IlS PAGE

LI SUBJECT 2-J

P HE RerulZJ =gt P toJ

50- e jJlH 0

NAME

DATE IREVISION DATE

5Z-hQ5 1

~iTATe Q)

P =I g A-rM

5Ar lGUID

1- 4l( 1lt

hjZ - 14 Bb lId

S-AIE hls 2 b35

S 1) sPec

~-IG CD P2 = I 2 MPoshy(z= _0

Y11Vd =30 b Jr

Mz I ~~

1 Sbil shy 1107

30 1-1107

s z lt3) 2 cent

P3 -=IZ ~ PA T Lj~IK

39 Yf ) = 5

~ HL 0 c( 3 ~ F-O

h middot07 J~ h~ 30 b-l~

)(~ 387

-

I

6P 14Sb

)

FERMllAB

ENGINEERING NOTE SECTION PROJECT

Jle x Fampltt ( tlJ Ii

SERIAL-CATEGORY

38 Z- 3 bull Il $ PAGE

L2 SUBJECT

He NAME

IREVISION DATE DATE

5-30 -atS

IIFo(t 1i1 ~)( CQoj 0 bull 11 )t-I ~ ~) Afo-JO A Scu [0

P 1tJG IIJJ I cent 511 11 0D DI-f = L2

A

Ilz S CI-L 10 P IPG-) ID = I =gt82 I

t bull oS loJ

IS 35 00shy-I( 0 D J-- Felt -rtt IS S 12Gt

-

stlnput

000005

427 200

4 1211 2017 318 1323 000082 3876

-2 2 184 184 20

12 998

073 1000

shy

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

deltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 BakerXa BakerYa c M RsubL RsubG GasVel Liqvel

Output

accurate

turbulen 01906103

ft in ft

92387E-5 m2 gs kgm 3 kgm3 JlPa-s JlPa-s Nm

90430 0024496 kgS

137600 0015504 kgs 51012286 pam 16810555 Pam

14863285 psig

57405518 67244052

1 4281346 kgmA 3 kgmA 3

53412427 Nm JlPa-s

1210 8660 lbmhr-ft

1 1 17419928 82580072 1 0075104 ms 12568736 ms

Comment L3 Russ Rucinski 53095 Return He pipe for Solenoid 1 pipe w 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

model validity

flow type friction factor Must enter a guess pipe roughness Pipe inside diameter Length of pipe cross sectional area Total mass flow rate Liquid density density of the gas Liquid viscosity Gas Viscosity Surface tension of liquid quality = mdotGmdot Reynolds for liquid Mass flow rate for liquid Reynolds for gas Mass flow rate for gas AP1lL for the liquid AP1lL for the two phase

Total pressure drop for the pipe ~ 100 ~JGtcs 1b uu Stu

Lockhart-Martinelli parameter Lockhart-Martinelli parameter L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 Baker diagram dimensionless parameter density of air density of water Baker diagram dimensionless parameter Surface tension of water viscosity of water X - axis value for Baker plot Y-axis value for Baker plot

Volume fraction of liquid phase Volume fraction of gas phase Gas velocity Liquid velocity

000005 1057 200

4 1211 2017 318 1323 000082 3876

shy

2

25

184

316 20

12 998

073 1000

-

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

rdeltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 Bakerxa BakerYa c M RsubL RsubG GasVel LiqVel

Output Comment Russ Rucinski 53095 Return He pipe for Solenoid 1 12 pipe wi 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

accurate model validity

turbulen flow type 02260289 friction factor Must enter a guess

ft pipe roughness in Pipe inside diameter ft Length of pipe

00056612 m2 cross sectional area gls Total mass flow rate kgm 3 Liquid density kgm3 density of the gas JLPa-s Liquid viscosity JLPa-s Gas viscosity Nm Surface tension of liquid

quality = mdotGmdot 36530 Reynolds for liquid

0024496 kgls Mass flow rate for liquid 55580 Reynolds for gas

0015504 kgls Mass flow rate for gas

0650814 Palm LP I LU for the liquid 21275204 Palm LPLU for the two phase

01881077 psig 1 Total pressure drop for the pipe

57175294 Lockhart-Martinelli parameter 67767548 Lockhart-Martinelli parameter

L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719

1 4281346 Baker diagram dimensionless parameter kgm3 density of air kgm3 density of water

53412427 Baker diagram dimensionless parameter Nm Surface tension of water JLPa-s viscosity of water

1210 X - axis value for Baker 1410 lbmhr-ft Y-axis value for Baker

1 1 17490072 Volume fraction of liquid phase 82509928 Volume fraction of gas phase 16456003 ms Gas velocity 20429237 ms Liquid velocity

53095 middot

FERMILAB TWO PHASE HEUUM FLOW TESTS

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Russ KUCt~5~l

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112 5C~ 10 f 5eCD

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995

Russ Rucinski and Steve Sakla ROOQJ Mech

Approved _________

-

n ~ middotrt -

Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

-------------~ ~~~--~~~~--

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J8 CO bull 0049 N2 tu~bullbull

58 CO bull 0049 He Supply 1 12 sch lOS pipe

l Sch lOS H return SS

J4 CO bull 0065 He Cool down return

He Cool downQuench Return 25 CO bull 0065 Cu Rod shield

Main Solenoid xfer ine Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

Potta 1 rb 21 153121 CST ~ by rwcnoi

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1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

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tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

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SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

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FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

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intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

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I

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bull

bull iii

bull iii

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E 7

~-----------------~

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bull

ex t

l

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14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

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FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

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NAME

CATE IREVISION CATE

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---

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FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

~ 11 LE1 0o-lD)-S vJG ~e~ 771 ADD J(i~ w~ Fc~lJ vf J 50~~r--middotC

-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

- II gtlt 1( SvlfoVlS (2 fi_shyb w - ~PrD IP-t S vPlgto2---fShmiddott

30W 0 7- tz A- I Itt- 0 tv bull I () I( 5 1gt~fINI- pUs 130 w- Cc 15I4J Z 50 o

c A tJ 7 3_64- VII s~

1trcP1 jc ~---)-

rv - bullbull OF FXIEgt~ ( 2S 1 ~ CL- (_~

bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

2 ~ Zgt ~ IV - I (1 Of CH IA IJ amp- - J i_2soeW - l~ or- Ck Nt 13 INIttSq

- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 11: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

I HZ 5- 3c-75pf1EN 01gtc f-1- (trCvLATlCIJ)

1r 1)7

) A

II f

t-A 5Jh Z 0 i) gtlt a 0 lt-I~ AJJ I b5k -cb- O-1OZ1 cgtO(oz- gt 012 MI)~ L-= 200t-i roO9GM

v (m ) e --~ (z) (1r- DA )

-( il -J

-~~---7- I )

v ~ v -2shybull 7 L- V

l) - - l lQ [ r) 2~

T

( ( I ~ IS (82 amp8 ~gt1-= (~lt17 b lt013)( o elY) ( 4gt0 cr or) llaquo

2 5 b 8z (8 gt0 z 2-7 psi

--- --~----- ----~ - ~-~------ - -~- ---------shy

H-3 J I

-

r i~ - r- ~-t~ -shy6 -= 081 ~ Jfi L s __ O~ k

i -

e~ It~ Jo~ -1- 7Z 7lt alt ~- 5

N --=- 000 y~ Jias

j b5 1lt

Plt= 64 )-t

-

I L

SUBJECT NAME

- SUPPLlt( DATE(pZ 10 ~ IREVISION DATE

It-w FERMILAB

ENGINEERING NOTE SECTION PROJECT SERIAl-CATEGORY

3S23 I IS PAGE

rl4

3 III - (ImiddotTJ3~ T -z w TlANrrut l1-W -lo jr W -~ 1- I w mAlS L i rJ C

5~ I C ~ 1 1 ( LEA t 1=20M t-I-tlt ~1ClttA ampe i)wA-rt 10 LPC Clt-(os -rk-r

5TA-re(j)

t Ik- pewAn ~~-r L10

- L4 ~o ~

p 9 ( 5 i9 5 A $TAI

hl 1 Be J -

o Pz e M 16MPa = 95 fJ~(j ~L 11flP

-d- = ZYIl

Xl--= ~-~-Fo 158~119h 032 yj - kF ~f 1t--1I96

Afo()

S TIlO

Vft TtJ~ =- 6Po() 2 f5i

L~f-l E(t S P(2UbAb-Y ~~ v 1 VPltL-~( -ru ZfJO Ff

-

FERMILAB

ENGINEERING NOTE SECTION

RDIDcent PROJECT

He -y Fe12 SERIALmiddotCATEGORY

3S23IlS PAGE

LI SUBJECT 2-J

P HE RerulZJ =gt P toJ

50- e jJlH 0

NAME

DATE IREVISION DATE

5Z-hQ5 1

~iTATe Q)

P =I g A-rM

5Ar lGUID

1- 4l( 1lt

hjZ - 14 Bb lId

S-AIE hls 2 b35

S 1) sPec

~-IG CD P2 = I 2 MPoshy(z= _0

Y11Vd =30 b Jr

Mz I ~~

1 Sbil shy 1107

30 1-1107

s z lt3) 2 cent

P3 -=IZ ~ PA T Lj~IK

39 Yf ) = 5

~ HL 0 c( 3 ~ F-O

h middot07 J~ h~ 30 b-l~

)(~ 387

-

I

6P 14Sb

)

FERMllAB

ENGINEERING NOTE SECTION PROJECT

Jle x Fampltt ( tlJ Ii

SERIAL-CATEGORY

38 Z- 3 bull Il $ PAGE

L2 SUBJECT

He NAME

IREVISION DATE DATE

5-30 -atS

IIFo(t 1i1 ~)( CQoj 0 bull 11 )t-I ~ ~) Afo-JO A Scu [0

P 1tJG IIJJ I cent 511 11 0D DI-f = L2

A

Ilz S CI-L 10 P IPG-) ID = I =gt82 I

t bull oS loJ

IS 35 00shy-I( 0 D J-- Felt -rtt IS S 12Gt

-

stlnput

000005

427 200

4 1211 2017 318 1323 000082 3876

-2 2 184 184 20

12 998

073 1000

shy

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

deltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 BakerXa BakerYa c M RsubL RsubG GasVel Liqvel

Output

accurate

turbulen 01906103

ft in ft

92387E-5 m2 gs kgm 3 kgm3 JlPa-s JlPa-s Nm

90430 0024496 kgS

137600 0015504 kgs 51012286 pam 16810555 Pam

14863285 psig

57405518 67244052

1 4281346 kgmA 3 kgmA 3

53412427 Nm JlPa-s

1210 8660 lbmhr-ft

1 1 17419928 82580072 1 0075104 ms 12568736 ms

Comment L3 Russ Rucinski 53095 Return He pipe for Solenoid 1 pipe w 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

model validity

flow type friction factor Must enter a guess pipe roughness Pipe inside diameter Length of pipe cross sectional area Total mass flow rate Liquid density density of the gas Liquid viscosity Gas Viscosity Surface tension of liquid quality = mdotGmdot Reynolds for liquid Mass flow rate for liquid Reynolds for gas Mass flow rate for gas AP1lL for the liquid AP1lL for the two phase

Total pressure drop for the pipe ~ 100 ~JGtcs 1b uu Stu

Lockhart-Martinelli parameter Lockhart-Martinelli parameter L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 Baker diagram dimensionless parameter density of air density of water Baker diagram dimensionless parameter Surface tension of water viscosity of water X - axis value for Baker plot Y-axis value for Baker plot

Volume fraction of liquid phase Volume fraction of gas phase Gas velocity Liquid velocity

000005 1057 200

4 1211 2017 318 1323 000082 3876

shy

2

25

184

316 20

12 998

073 1000

-

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

rdeltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 Bakerxa BakerYa c M RsubL RsubG GasVel LiqVel

Output Comment Russ Rucinski 53095 Return He pipe for Solenoid 1 12 pipe wi 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

accurate model validity

turbulen flow type 02260289 friction factor Must enter a guess

ft pipe roughness in Pipe inside diameter ft Length of pipe

00056612 m2 cross sectional area gls Total mass flow rate kgm 3 Liquid density kgm3 density of the gas JLPa-s Liquid viscosity JLPa-s Gas viscosity Nm Surface tension of liquid

quality = mdotGmdot 36530 Reynolds for liquid

0024496 kgls Mass flow rate for liquid 55580 Reynolds for gas

0015504 kgls Mass flow rate for gas

0650814 Palm LP I LU for the liquid 21275204 Palm LPLU for the two phase

01881077 psig 1 Total pressure drop for the pipe

57175294 Lockhart-Martinelli parameter 67767548 Lockhart-Martinelli parameter

L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719

1 4281346 Baker diagram dimensionless parameter kgm3 density of air kgm3 density of water

53412427 Baker diagram dimensionless parameter Nm Surface tension of water JLPa-s viscosity of water

1210 X - axis value for Baker 1410 lbmhr-ft Y-axis value for Baker

1 1 17490072 Volume fraction of liquid phase 82509928 Volume fraction of gas phase 16456003 ms Gas velocity 20429237 ms Liquid velocity

53095 middot

FERMILAB TWO PHASE HEUUM FLOW TESTS

) )

Russ KUCt~5~l

10 ~ 1 I UAUEOOV

11 ~7 I I I Flow Fath Flaw

~--- Annular Flow Wave Flow

------ Slug FlowI

A tf SIO ______

~gt

---IIMIR RIGIMI BOUNDARIII ~ G bull RCtPtC GAl OW RAlI -- ClFtC LIQUID now RAT ~l-III _lIN_

10 I I ~I gt bull I I

MaMIIow_

X 5SVI PI U bull MIddIt of IOIItnoId

1 10 VI PI bull bull Ex of IOIItnoId

18 VI PI 7 bull 1111111 of control dewarbull Figura 1 Baker diagram with Mamedov curves or two phase helium In horzonlal channels

[FttoJIA Djli El 38 23IlJ -Gt-J - 33 8 ]

r J1

01 10 10 10 ( 10 i ~ ~ 10 ~ ~ 10 L ~nG CAt 0 )V rPl

~ IMaIIon TIJampE

0J

PIPE

112 5C~ 10 f 5eCD

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995

Russ Rucinski and Steve Sakla ROOQJ Mech

Approved _________

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Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

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4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

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RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

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43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

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lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

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intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

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14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

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~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

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L- e 10 J

l- I eo -0shy II

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10 F-I J

5 ~

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FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

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)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

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(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

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$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

~ 11 LE1 0o-lD)-S vJG ~e~ 771 ADD J(i~ w~ Fc~lJ vf J 50~~r--middotC

-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

- II gtlt 1( SvlfoVlS (2 fi_shyb w - ~PrD IP-t S vPlgto2---fShmiddott

30W 0 7- tz A- I Itt- 0 tv bull I () I( 5 1gt~fINI- pUs 130 w- Cc 15I4J Z 50 o

c A tJ 7 3_64- VII s~

1trcP1 jc ~---)-

rv - bullbull OF FXIEgt~ ( 2S 1 ~ CL- (_~

bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

2 ~ Zgt ~ IV - I (1 Of CH IA IJ amp- - J i_2soeW - l~ or- Ck Nt 13 INIttSq

- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 12: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

H-3 J I

-

r i~ - r- ~-t~ -shy6 -= 081 ~ Jfi L s __ O~ k

i -

e~ It~ Jo~ -1- 7Z 7lt alt ~- 5

N --=- 000 y~ Jias

j b5 1lt

Plt= 64 )-t

-

I L

SUBJECT NAME

- SUPPLlt( DATE(pZ 10 ~ IREVISION DATE

It-w FERMILAB

ENGINEERING NOTE SECTION PROJECT SERIAl-CATEGORY

3S23 I IS PAGE

rl4

3 III - (ImiddotTJ3~ T -z w TlANrrut l1-W -lo jr W -~ 1- I w mAlS L i rJ C

5~ I C ~ 1 1 ( LEA t 1=20M t-I-tlt ~1ClttA ampe i)wA-rt 10 LPC Clt-(os -rk-r

5TA-re(j)

t Ik- pewAn ~~-r L10

- L4 ~o ~

p 9 ( 5 i9 5 A $TAI

hl 1 Be J -

o Pz e M 16MPa = 95 fJ~(j ~L 11flP

-d- = ZYIl

Xl--= ~-~-Fo 158~119h 032 yj - kF ~f 1t--1I96

Afo()

S TIlO

Vft TtJ~ =- 6Po() 2 f5i

L~f-l E(t S P(2UbAb-Y ~~ v 1 VPltL-~( -ru ZfJO Ff

-

FERMILAB

ENGINEERING NOTE SECTION

RDIDcent PROJECT

He -y Fe12 SERIALmiddotCATEGORY

3S23IlS PAGE

LI SUBJECT 2-J

P HE RerulZJ =gt P toJ

50- e jJlH 0

NAME

DATE IREVISION DATE

5Z-hQ5 1

~iTATe Q)

P =I g A-rM

5Ar lGUID

1- 4l( 1lt

hjZ - 14 Bb lId

S-AIE hls 2 b35

S 1) sPec

~-IG CD P2 = I 2 MPoshy(z= _0

Y11Vd =30 b Jr

Mz I ~~

1 Sbil shy 1107

30 1-1107

s z lt3) 2 cent

P3 -=IZ ~ PA T Lj~IK

39 Yf ) = 5

~ HL 0 c( 3 ~ F-O

h middot07 J~ h~ 30 b-l~

)(~ 387

-

I

6P 14Sb

)

FERMllAB

ENGINEERING NOTE SECTION PROJECT

Jle x Fampltt ( tlJ Ii

SERIAL-CATEGORY

38 Z- 3 bull Il $ PAGE

L2 SUBJECT

He NAME

IREVISION DATE DATE

5-30 -atS

IIFo(t 1i1 ~)( CQoj 0 bull 11 )t-I ~ ~) Afo-JO A Scu [0

P 1tJG IIJJ I cent 511 11 0D DI-f = L2

A

Ilz S CI-L 10 P IPG-) ID = I =gt82 I

t bull oS loJ

IS 35 00shy-I( 0 D J-- Felt -rtt IS S 12Gt

-

stlnput

000005

427 200

4 1211 2017 318 1323 000082 3876

-2 2 184 184 20

12 998

073 1000

shy

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

deltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 BakerXa BakerYa c M RsubL RsubG GasVel Liqvel

Output

accurate

turbulen 01906103

ft in ft

92387E-5 m2 gs kgm 3 kgm3 JlPa-s JlPa-s Nm

90430 0024496 kgS

137600 0015504 kgs 51012286 pam 16810555 Pam

14863285 psig

57405518 67244052

1 4281346 kgmA 3 kgmA 3

53412427 Nm JlPa-s

1210 8660 lbmhr-ft

1 1 17419928 82580072 1 0075104 ms 12568736 ms

Comment L3 Russ Rucinski 53095 Return He pipe for Solenoid 1 pipe w 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

model validity

flow type friction factor Must enter a guess pipe roughness Pipe inside diameter Length of pipe cross sectional area Total mass flow rate Liquid density density of the gas Liquid viscosity Gas Viscosity Surface tension of liquid quality = mdotGmdot Reynolds for liquid Mass flow rate for liquid Reynolds for gas Mass flow rate for gas AP1lL for the liquid AP1lL for the two phase

Total pressure drop for the pipe ~ 100 ~JGtcs 1b uu Stu

Lockhart-Martinelli parameter Lockhart-Martinelli parameter L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 Baker diagram dimensionless parameter density of air density of water Baker diagram dimensionless parameter Surface tension of water viscosity of water X - axis value for Baker plot Y-axis value for Baker plot

Volume fraction of liquid phase Volume fraction of gas phase Gas velocity Liquid velocity

000005 1057 200

4 1211 2017 318 1323 000082 3876

shy

2

25

184

316 20

12 998

073 1000

-

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

rdeltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 Bakerxa BakerYa c M RsubL RsubG GasVel LiqVel

Output Comment Russ Rucinski 53095 Return He pipe for Solenoid 1 12 pipe wi 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

accurate model validity

turbulen flow type 02260289 friction factor Must enter a guess

ft pipe roughness in Pipe inside diameter ft Length of pipe

00056612 m2 cross sectional area gls Total mass flow rate kgm 3 Liquid density kgm3 density of the gas JLPa-s Liquid viscosity JLPa-s Gas viscosity Nm Surface tension of liquid

quality = mdotGmdot 36530 Reynolds for liquid

0024496 kgls Mass flow rate for liquid 55580 Reynolds for gas

0015504 kgls Mass flow rate for gas

0650814 Palm LP I LU for the liquid 21275204 Palm LPLU for the two phase

01881077 psig 1 Total pressure drop for the pipe

57175294 Lockhart-Martinelli parameter 67767548 Lockhart-Martinelli parameter

L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719

1 4281346 Baker diagram dimensionless parameter kgm3 density of air kgm3 density of water

53412427 Baker diagram dimensionless parameter Nm Surface tension of water JLPa-s viscosity of water

1210 X - axis value for Baker 1410 lbmhr-ft Y-axis value for Baker

1 1 17490072 Volume fraction of liquid phase 82509928 Volume fraction of gas phase 16456003 ms Gas velocity 20429237 ms Liquid velocity

53095 middot

FERMILAB TWO PHASE HEUUM FLOW TESTS

) )

Russ KUCt~5~l

10 ~ 1 I UAUEOOV

11 ~7 I I I Flow Fath Flaw

~--- Annular Flow Wave Flow

------ Slug FlowI

A tf SIO ______

~gt

---IIMIR RIGIMI BOUNDARIII ~ G bull RCtPtC GAl OW RAlI -- ClFtC LIQUID now RAT ~l-III _lIN_

10 I I ~I gt bull I I

MaMIIow_

X 5SVI PI U bull MIddIt of IOIItnoId

1 10 VI PI bull bull Ex of IOIItnoId

18 VI PI 7 bull 1111111 of control dewarbull Figura 1 Baker diagram with Mamedov curves or two phase helium In horzonlal channels

[FttoJIA Djli El 38 23IlJ -Gt-J - 33 8 ]

r J1

01 10 10 10 ( 10 i ~ ~ 10 ~ ~ 10 L ~nG CAt 0 )V rPl

~ IMaIIon TIJampE

0J

PIPE

112 5C~ 10 f 5eCD

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995

Russ Rucinski and Steve Sakla ROOQJ Mech

Approved _________

-

n ~ middotrt -

Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

-------------~ ~~~--~~~~--

Ud

)

) ) f

J8 CO bull 0049 N2 tu~bullbull

58 CO bull 0049 He Supply 1 12 sch lOS pipe

l Sch lOS H return SS

J4 CO bull 0065 He Cool down return

He Cool downQuench Return 25 CO bull 0065 Cu Rod shield

Main Solenoid xfer ine Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

Potta 1 rb 21 153121 CST ~ by rwcnoi

~lGUJCE 1

N

)J

1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

i foE 9flIIy 1JTAlE rlTX6 AHFEEDCAN 112 00 X 049 0402 5 2 0 0 0

tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

I

bull VIJIC iliil-flH Ie FT I

I I i I bullbullOF IUlaWS IN 8 i I

I1Igel

I Ibull I

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FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

~I_ i 50 Uf-bln 3823 _ c NAME

Russ

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J o N

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I

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FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

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intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

-1(IL------- ~ ~l

-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

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FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

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o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

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---

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FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

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SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

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~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

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~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

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(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

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~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

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II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

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$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

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~

~

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14 5ze 14 w

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use

I 9 WATT

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( I )

(i 0)

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3 B w) L 3~ s~

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3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

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-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

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c A tJ 7 3_64- VII s~

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bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

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- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 13: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

SUBJECT NAME

- SUPPLlt( DATE(pZ 10 ~ IREVISION DATE

It-w FERMILAB

ENGINEERING NOTE SECTION PROJECT SERIAl-CATEGORY

3S23 I IS PAGE

rl4

3 III - (ImiddotTJ3~ T -z w TlANrrut l1-W -lo jr W -~ 1- I w mAlS L i rJ C

5~ I C ~ 1 1 ( LEA t 1=20M t-I-tlt ~1ClttA ampe i)wA-rt 10 LPC Clt-(os -rk-r

5TA-re(j)

t Ik- pewAn ~~-r L10

- L4 ~o ~

p 9 ( 5 i9 5 A $TAI

hl 1 Be J -

o Pz e M 16MPa = 95 fJ~(j ~L 11flP

-d- = ZYIl

Xl--= ~-~-Fo 158~119h 032 yj - kF ~f 1t--1I96

Afo()

S TIlO

Vft TtJ~ =- 6Po() 2 f5i

L~f-l E(t S P(2UbAb-Y ~~ v 1 VPltL-~( -ru ZfJO Ff

-

FERMILAB

ENGINEERING NOTE SECTION

RDIDcent PROJECT

He -y Fe12 SERIALmiddotCATEGORY

3S23IlS PAGE

LI SUBJECT 2-J

P HE RerulZJ =gt P toJ

50- e jJlH 0

NAME

DATE IREVISION DATE

5Z-hQ5 1

~iTATe Q)

P =I g A-rM

5Ar lGUID

1- 4l( 1lt

hjZ - 14 Bb lId

S-AIE hls 2 b35

S 1) sPec

~-IG CD P2 = I 2 MPoshy(z= _0

Y11Vd =30 b Jr

Mz I ~~

1 Sbil shy 1107

30 1-1107

s z lt3) 2 cent

P3 -=IZ ~ PA T Lj~IK

39 Yf ) = 5

~ HL 0 c( 3 ~ F-O

h middot07 J~ h~ 30 b-l~

)(~ 387

-

I

6P 14Sb

)

FERMllAB

ENGINEERING NOTE SECTION PROJECT

Jle x Fampltt ( tlJ Ii

SERIAL-CATEGORY

38 Z- 3 bull Il $ PAGE

L2 SUBJECT

He NAME

IREVISION DATE DATE

5-30 -atS

IIFo(t 1i1 ~)( CQoj 0 bull 11 )t-I ~ ~) Afo-JO A Scu [0

P 1tJG IIJJ I cent 511 11 0D DI-f = L2

A

Ilz S CI-L 10 P IPG-) ID = I =gt82 I

t bull oS loJ

IS 35 00shy-I( 0 D J-- Felt -rtt IS S 12Gt

-

stlnput

000005

427 200

4 1211 2017 318 1323 000082 3876

-2 2 184 184 20

12 998

073 1000

shy

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

deltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 BakerXa BakerYa c M RsubL RsubG GasVel Liqvel

Output

accurate

turbulen 01906103

ft in ft

92387E-5 m2 gs kgm 3 kgm3 JlPa-s JlPa-s Nm

90430 0024496 kgS

137600 0015504 kgs 51012286 pam 16810555 Pam

14863285 psig

57405518 67244052

1 4281346 kgmA 3 kgmA 3

53412427 Nm JlPa-s

1210 8660 lbmhr-ft

1 1 17419928 82580072 1 0075104 ms 12568736 ms

Comment L3 Russ Rucinski 53095 Return He pipe for Solenoid 1 pipe w 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

model validity

flow type friction factor Must enter a guess pipe roughness Pipe inside diameter Length of pipe cross sectional area Total mass flow rate Liquid density density of the gas Liquid viscosity Gas Viscosity Surface tension of liquid quality = mdotGmdot Reynolds for liquid Mass flow rate for liquid Reynolds for gas Mass flow rate for gas AP1lL for the liquid AP1lL for the two phase

Total pressure drop for the pipe ~ 100 ~JGtcs 1b uu Stu

Lockhart-Martinelli parameter Lockhart-Martinelli parameter L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 Baker diagram dimensionless parameter density of air density of water Baker diagram dimensionless parameter Surface tension of water viscosity of water X - axis value for Baker plot Y-axis value for Baker plot

Volume fraction of liquid phase Volume fraction of gas phase Gas velocity Liquid velocity

000005 1057 200

4 1211 2017 318 1323 000082 3876

shy

2

25

184

316 20

12 998

073 1000

-

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

rdeltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 Bakerxa BakerYa c M RsubL RsubG GasVel LiqVel

Output Comment Russ Rucinski 53095 Return He pipe for Solenoid 1 12 pipe wi 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

accurate model validity

turbulen flow type 02260289 friction factor Must enter a guess

ft pipe roughness in Pipe inside diameter ft Length of pipe

00056612 m2 cross sectional area gls Total mass flow rate kgm 3 Liquid density kgm3 density of the gas JLPa-s Liquid viscosity JLPa-s Gas viscosity Nm Surface tension of liquid

quality = mdotGmdot 36530 Reynolds for liquid

0024496 kgls Mass flow rate for liquid 55580 Reynolds for gas

0015504 kgls Mass flow rate for gas

0650814 Palm LP I LU for the liquid 21275204 Palm LPLU for the two phase

01881077 psig 1 Total pressure drop for the pipe

57175294 Lockhart-Martinelli parameter 67767548 Lockhart-Martinelli parameter

L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719

1 4281346 Baker diagram dimensionless parameter kgm3 density of air kgm3 density of water

53412427 Baker diagram dimensionless parameter Nm Surface tension of water JLPa-s viscosity of water

1210 X - axis value for Baker 1410 lbmhr-ft Y-axis value for Baker

1 1 17490072 Volume fraction of liquid phase 82509928 Volume fraction of gas phase 16456003 ms Gas velocity 20429237 ms Liquid velocity

53095 middot

FERMILAB TWO PHASE HEUUM FLOW TESTS

) )

Russ KUCt~5~l

10 ~ 1 I UAUEOOV

11 ~7 I I I Flow Fath Flaw

~--- Annular Flow Wave Flow

------ Slug FlowI

A tf SIO ______

~gt

---IIMIR RIGIMI BOUNDARIII ~ G bull RCtPtC GAl OW RAlI -- ClFtC LIQUID now RAT ~l-III _lIN_

10 I I ~I gt bull I I

MaMIIow_

X 5SVI PI U bull MIddIt of IOIItnoId

1 10 VI PI bull bull Ex of IOIItnoId

18 VI PI 7 bull 1111111 of control dewarbull Figura 1 Baker diagram with Mamedov curves or two phase helium In horzonlal channels

[FttoJIA Djli El 38 23IlJ -Gt-J - 33 8 ]

r J1

01 10 10 10 ( 10 i ~ ~ 10 ~ ~ 10 L ~nG CAt 0 )V rPl

~ IMaIIon TIJampE

0J

PIPE

112 5C~ 10 f 5eCD

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995

Russ Rucinski and Steve Sakla ROOQJ Mech

Approved _________

-

n ~ middotrt -

Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

-------------~ ~~~--~~~~--

Ud

)

) ) f

J8 CO bull 0049 N2 tu~bullbull

58 CO bull 0049 He Supply 1 12 sch lOS pipe

l Sch lOS H return SS

J4 CO bull 0065 He Cool down return

He Cool downQuench Return 25 CO bull 0065 Cu Rod shield

Main Solenoid xfer ine Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

Potta 1 rb 21 153121 CST ~ by rwcnoi

~lGUJCE 1

N

)J

1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

i foE 9flIIy 1JTAlE rlTX6 AHFEEDCAN 112 00 X 049 0402 5 2 0 0 0

tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

I

bull VIJIC iliil-flH Ie FT I

I I i I bullbullOF IUlaWS IN 8 i I

I1Igel

I Ibull I

9 o 2 III J o en

L

FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

~I_ i 50 Uf-bln 3823 _ c NAME

Russ

ili2 -J-1 U ~io-pound lIJJoJ~l-c sc O~Il~ I-(JoTI CAJI60e Igt r_I Z S~ Z -n r Z Z Ilt r Zmiddot

J o N

(

N N

H

I

J

1 shy

c e-l ~w ~ UI

CIgt

~1

FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

~ )

-shy

~ M )

f ltgt0 ~O~ I 0 bull ~

If g -rI ~ t shy ~T

0

~ r

~ -a

-r

0 0

-Sci

bull~

~ ~

i-T

intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

-1(IL------- ~ ~l

-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

d (-10 ( ~raquo

839qYY --(Motte

25 lie SL 20

~ d51-

7 Sbull 2shy3 2 3 472

- ~

-- ---------- raquo

b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

1 EAIJgtltf lt FR61V tJ L c(Lflc lilA ~K

f~nr - ~- ALVMtJUM

SA 4 2otJ K 6~ oJ I 270 ~ amp-A5 our

h(7vr 1311~h lN ~ 1054 ~

-k-shy - - = A ATWO 1r (tgt15)(O4~[51))

o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

CaN-IIJfIIO vJ( 1--4 vt P~eAJ(1 of J-II TLJIi AJ ~fe~ AceA

A I) CDEFtIrL~ ib COOItgt()~J A-r (tATamp 0 5 ~A

o7b 10 T I ~ l

~tlcIio 60 it S ) ( lOS 5 ~ -q SJf) )l 3 CO os

STEP 3

S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

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S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

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$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

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use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

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3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

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115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

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-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

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b 4 - v 1 iJg~S

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1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

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- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 14: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

-

FERMILAB

ENGINEERING NOTE SECTION

RDIDcent PROJECT

He -y Fe12 SERIALmiddotCATEGORY

3S23IlS PAGE

LI SUBJECT 2-J

P HE RerulZJ =gt P toJ

50- e jJlH 0

NAME

DATE IREVISION DATE

5Z-hQ5 1

~iTATe Q)

P =I g A-rM

5Ar lGUID

1- 4l( 1lt

hjZ - 14 Bb lId

S-AIE hls 2 b35

S 1) sPec

~-IG CD P2 = I 2 MPoshy(z= _0

Y11Vd =30 b Jr

Mz I ~~

1 Sbil shy 1107

30 1-1107

s z lt3) 2 cent

P3 -=IZ ~ PA T Lj~IK

39 Yf ) = 5

~ HL 0 c( 3 ~ F-O

h middot07 J~ h~ 30 b-l~

)(~ 387

-

I

6P 14Sb

)

FERMllAB

ENGINEERING NOTE SECTION PROJECT

Jle x Fampltt ( tlJ Ii

SERIAL-CATEGORY

38 Z- 3 bull Il $ PAGE

L2 SUBJECT

He NAME

IREVISION DATE DATE

5-30 -atS

IIFo(t 1i1 ~)( CQoj 0 bull 11 )t-I ~ ~) Afo-JO A Scu [0

P 1tJG IIJJ I cent 511 11 0D DI-f = L2

A

Ilz S CI-L 10 P IPG-) ID = I =gt82 I

t bull oS loJ

IS 35 00shy-I( 0 D J-- Felt -rtt IS S 12Gt

-

stlnput

000005

427 200

4 1211 2017 318 1323 000082 3876

-2 2 184 184 20

12 998

073 1000

shy

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

deltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 BakerXa BakerYa c M RsubL RsubG GasVel Liqvel

Output

accurate

turbulen 01906103

ft in ft

92387E-5 m2 gs kgm 3 kgm3 JlPa-s JlPa-s Nm

90430 0024496 kgS

137600 0015504 kgs 51012286 pam 16810555 Pam

14863285 psig

57405518 67244052

1 4281346 kgmA 3 kgmA 3

53412427 Nm JlPa-s

1210 8660 lbmhr-ft

1 1 17419928 82580072 1 0075104 ms 12568736 ms

Comment L3 Russ Rucinski 53095 Return He pipe for Solenoid 1 pipe w 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

model validity

flow type friction factor Must enter a guess pipe roughness Pipe inside diameter Length of pipe cross sectional area Total mass flow rate Liquid density density of the gas Liquid viscosity Gas Viscosity Surface tension of liquid quality = mdotGmdot Reynolds for liquid Mass flow rate for liquid Reynolds for gas Mass flow rate for gas AP1lL for the liquid AP1lL for the two phase

Total pressure drop for the pipe ~ 100 ~JGtcs 1b uu Stu

Lockhart-Martinelli parameter Lockhart-Martinelli parameter L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 Baker diagram dimensionless parameter density of air density of water Baker diagram dimensionless parameter Surface tension of water viscosity of water X - axis value for Baker plot Y-axis value for Baker plot

Volume fraction of liquid phase Volume fraction of gas phase Gas velocity Liquid velocity

000005 1057 200

4 1211 2017 318 1323 000082 3876

shy

2

25

184

316 20

12 998

073 1000

-

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

rdeltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 Bakerxa BakerYa c M RsubL RsubG GasVel LiqVel

Output Comment Russ Rucinski 53095 Return He pipe for Solenoid 1 12 pipe wi 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

accurate model validity

turbulen flow type 02260289 friction factor Must enter a guess

ft pipe roughness in Pipe inside diameter ft Length of pipe

00056612 m2 cross sectional area gls Total mass flow rate kgm 3 Liquid density kgm3 density of the gas JLPa-s Liquid viscosity JLPa-s Gas viscosity Nm Surface tension of liquid

quality = mdotGmdot 36530 Reynolds for liquid

0024496 kgls Mass flow rate for liquid 55580 Reynolds for gas

0015504 kgls Mass flow rate for gas

0650814 Palm LP I LU for the liquid 21275204 Palm LPLU for the two phase

01881077 psig 1 Total pressure drop for the pipe

57175294 Lockhart-Martinelli parameter 67767548 Lockhart-Martinelli parameter

L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719

1 4281346 Baker diagram dimensionless parameter kgm3 density of air kgm3 density of water

53412427 Baker diagram dimensionless parameter Nm Surface tension of water JLPa-s viscosity of water

1210 X - axis value for Baker 1410 lbmhr-ft Y-axis value for Baker

1 1 17490072 Volume fraction of liquid phase 82509928 Volume fraction of gas phase 16456003 ms Gas velocity 20429237 ms Liquid velocity

53095 middot

FERMILAB TWO PHASE HEUUM FLOW TESTS

) )

Russ KUCt~5~l

10 ~ 1 I UAUEOOV

11 ~7 I I I Flow Fath Flaw

~--- Annular Flow Wave Flow

------ Slug FlowI

A tf SIO ______

~gt

---IIMIR RIGIMI BOUNDARIII ~ G bull RCtPtC GAl OW RAlI -- ClFtC LIQUID now RAT ~l-III _lIN_

10 I I ~I gt bull I I

MaMIIow_

X 5SVI PI U bull MIddIt of IOIItnoId

1 10 VI PI bull bull Ex of IOIItnoId

18 VI PI 7 bull 1111111 of control dewarbull Figura 1 Baker diagram with Mamedov curves or two phase helium In horzonlal channels

[FttoJIA Djli El 38 23IlJ -Gt-J - 33 8 ]

r J1

01 10 10 10 ( 10 i ~ ~ 10 ~ ~ 10 L ~nG CAt 0 )V rPl

~ IMaIIon TIJampE

0J

PIPE

112 5C~ 10 f 5eCD

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995

Russ Rucinski and Steve Sakla ROOQJ Mech

Approved _________

-

n ~ middotrt -

Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

-------------~ ~~~--~~~~--

Ud

)

) ) f

J8 CO bull 0049 N2 tu~bullbull

58 CO bull 0049 He Supply 1 12 sch lOS pipe

l Sch lOS H return SS

J4 CO bull 0065 He Cool down return

He Cool downQuench Return 25 CO bull 0065 Cu Rod shield

Main Solenoid xfer ine Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

Potta 1 rb 21 153121 CST ~ by rwcnoi

~lGUJCE 1

N

)J

1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

i foE 9flIIy 1JTAlE rlTX6 AHFEEDCAN 112 00 X 049 0402 5 2 0 0 0

tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

I

bull VIJIC iliil-flH Ie FT I

I I i I bullbullOF IUlaWS IN 8 i I

I1Igel

I Ibull I

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FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

~I_ i 50 Uf-bln 3823 _ c NAME

Russ

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J o N

(

N N

H

I

J

1 shy

c e-l ~w ~ UI

CIgt

~1

FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

~ )

-shy

~ M )

f ltgt0 ~O~ I 0 bull ~

If g -rI ~ t shy ~T

0

~ r

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-r

0 0

-Sci

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~ ~

i-T

intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

-1(IL------- ~ ~l

-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

d (-10 ( ~raquo

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bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

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o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

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S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

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(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

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k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

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f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

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t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

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bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

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3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

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-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

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-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

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It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

- II gtlt 1( SvlfoVlS (2 fi_shyb w - ~PrD IP-t S vPlgto2---fShmiddott

30W 0 7- tz A- I Itt- 0 tv bull I () I( 5 1gt~fINI- pUs 130 w- Cc 15I4J Z 50 o

c A tJ 7 3_64- VII s~

1trcP1 jc ~---)-

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bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

2 ~ Zgt ~ IV - I (1 Of CH IA IJ amp- - J i_2soeW - l~ or- Ck Nt 13 INIttSq

- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 15: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

6P 14Sb

)

FERMllAB

ENGINEERING NOTE SECTION PROJECT

Jle x Fampltt ( tlJ Ii

SERIAL-CATEGORY

38 Z- 3 bull Il $ PAGE

L2 SUBJECT

He NAME

IREVISION DATE DATE

5-30 -atS

IIFo(t 1i1 ~)( CQoj 0 bull 11 )t-I ~ ~) Afo-JO A Scu [0

P 1tJG IIJJ I cent 511 11 0D DI-f = L2

A

Ilz S CI-L 10 P IPG-) ID = I =gt82 I

t bull oS loJ

IS 35 00shy-I( 0 D J-- Felt -rtt IS S 12Gt

-

stlnput

000005

427 200

4 1211 2017 318 1323 000082 3876

-2 2 184 184 20

12 998

073 1000

shy

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

deltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 BakerXa BakerYa c M RsubL RsubG GasVel Liqvel

Output

accurate

turbulen 01906103

ft in ft

92387E-5 m2 gs kgm 3 kgm3 JlPa-s JlPa-s Nm

90430 0024496 kgS

137600 0015504 kgs 51012286 pam 16810555 Pam

14863285 psig

57405518 67244052

1 4281346 kgmA 3 kgmA 3

53412427 Nm JlPa-s

1210 8660 lbmhr-ft

1 1 17419928 82580072 1 0075104 ms 12568736 ms

Comment L3 Russ Rucinski 53095 Return He pipe for Solenoid 1 pipe w 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

model validity

flow type friction factor Must enter a guess pipe roughness Pipe inside diameter Length of pipe cross sectional area Total mass flow rate Liquid density density of the gas Liquid viscosity Gas Viscosity Surface tension of liquid quality = mdotGmdot Reynolds for liquid Mass flow rate for liquid Reynolds for gas Mass flow rate for gas AP1lL for the liquid AP1lL for the two phase

Total pressure drop for the pipe ~ 100 ~JGtcs 1b uu Stu

Lockhart-Martinelli parameter Lockhart-Martinelli parameter L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 Baker diagram dimensionless parameter density of air density of water Baker diagram dimensionless parameter Surface tension of water viscosity of water X - axis value for Baker plot Y-axis value for Baker plot

Volume fraction of liquid phase Volume fraction of gas phase Gas velocity Liquid velocity

000005 1057 200

4 1211 2017 318 1323 000082 3876

shy

2

25

184

316 20

12 998

073 1000

-

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

rdeltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 Bakerxa BakerYa c M RsubL RsubG GasVel LiqVel

Output Comment Russ Rucinski 53095 Return He pipe for Solenoid 1 12 pipe wi 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

accurate model validity

turbulen flow type 02260289 friction factor Must enter a guess

ft pipe roughness in Pipe inside diameter ft Length of pipe

00056612 m2 cross sectional area gls Total mass flow rate kgm 3 Liquid density kgm3 density of the gas JLPa-s Liquid viscosity JLPa-s Gas viscosity Nm Surface tension of liquid

quality = mdotGmdot 36530 Reynolds for liquid

0024496 kgls Mass flow rate for liquid 55580 Reynolds for gas

0015504 kgls Mass flow rate for gas

0650814 Palm LP I LU for the liquid 21275204 Palm LPLU for the two phase

01881077 psig 1 Total pressure drop for the pipe

57175294 Lockhart-Martinelli parameter 67767548 Lockhart-Martinelli parameter

L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719

1 4281346 Baker diagram dimensionless parameter kgm3 density of air kgm3 density of water

53412427 Baker diagram dimensionless parameter Nm Surface tension of water JLPa-s viscosity of water

1210 X - axis value for Baker 1410 lbmhr-ft Y-axis value for Baker

1 1 17490072 Volume fraction of liquid phase 82509928 Volume fraction of gas phase 16456003 ms Gas velocity 20429237 ms Liquid velocity

53095 middot

FERMILAB TWO PHASE HEUUM FLOW TESTS

) )

Russ KUCt~5~l

10 ~ 1 I UAUEOOV

11 ~7 I I I Flow Fath Flaw

~--- Annular Flow Wave Flow

------ Slug FlowI

A tf SIO ______

~gt

---IIMIR RIGIMI BOUNDARIII ~ G bull RCtPtC GAl OW RAlI -- ClFtC LIQUID now RAT ~l-III _lIN_

10 I I ~I gt bull I I

MaMIIow_

X 5SVI PI U bull MIddIt of IOIItnoId

1 10 VI PI bull bull Ex of IOIItnoId

18 VI PI 7 bull 1111111 of control dewarbull Figura 1 Baker diagram with Mamedov curves or two phase helium In horzonlal channels

[FttoJIA Djli El 38 23IlJ -Gt-J - 33 8 ]

r J1

01 10 10 10 ( 10 i ~ ~ 10 ~ ~ 10 L ~nG CAt 0 )V rPl

~ IMaIIon TIJampE

0J

PIPE

112 5C~ 10 f 5eCD

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995

Russ Rucinski and Steve Sakla ROOQJ Mech

Approved _________

-

n ~ middotrt -

Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

-------------~ ~~~--~~~~--

Ud

)

) ) f

J8 CO bull 0049 N2 tu~bullbull

58 CO bull 0049 He Supply 1 12 sch lOS pipe

l Sch lOS H return SS

J4 CO bull 0065 He Cool down return

He Cool downQuench Return 25 CO bull 0065 Cu Rod shield

Main Solenoid xfer ine Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

Potta 1 rb 21 153121 CST ~ by rwcnoi

~lGUJCE 1

N

)J

1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

i foE 9flIIy 1JTAlE rlTX6 AHFEEDCAN 112 00 X 049 0402 5 2 0 0 0

tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

I

bull VIJIC iliil-flH Ie FT I

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FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

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Russ

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I

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FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

~ )

-shy

~ M )

f ltgt0 ~O~ I 0 bull ~

If g -rI ~ t shy ~T

0

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0 0

-Sci

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intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

-1(IL------- ~ ~l

-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

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FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

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o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

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S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

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(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

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~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

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3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

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tt3k~ ICft12 b ~ D (it IS

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o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

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AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

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N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

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b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

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dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

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PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

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It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

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ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

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JS

t -= 0 0-5 ]7

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jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

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K2

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It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 16: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

stlnput

000005

427 200

4 1211 2017 318 1323 000082 3876

-2 2 184 184 20

12 998

073 1000

shy

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

deltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 BakerXa BakerYa c M RsubL RsubG GasVel Liqvel

Output

accurate

turbulen 01906103

ft in ft

92387E-5 m2 gs kgm 3 kgm3 JlPa-s JlPa-s Nm

90430 0024496 kgS

137600 0015504 kgs 51012286 pam 16810555 Pam

14863285 psig

57405518 67244052

1 4281346 kgmA 3 kgmA 3

53412427 Nm JlPa-s

1210 8660 lbmhr-ft

1 1 17419928 82580072 1 0075104 ms 12568736 ms

Comment L3 Russ Rucinski 53095 Return He pipe for Solenoid 1 pipe w 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

model validity

flow type friction factor Must enter a guess pipe roughness Pipe inside diameter Length of pipe cross sectional area Total mass flow rate Liquid density density of the gas Liquid viscosity Gas Viscosity Surface tension of liquid quality = mdotGmdot Reynolds for liquid Mass flow rate for liquid Reynolds for gas Mass flow rate for gas AP1lL for the liquid AP1lL for the two phase

Total pressure drop for the pipe ~ 100 ~JGtcs 1b uu Stu

Lockhart-Martinelli parameter Lockhart-Martinelli parameter L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 Baker diagram dimensionless parameter density of air density of water Baker diagram dimensionless parameter Surface tension of water viscosity of water X - axis value for Baker plot Y-axis value for Baker plot

Volume fraction of liquid phase Volume fraction of gas phase Gas velocity Liquid velocity

000005 1057 200

4 1211 2017 318 1323 000082 3876

shy

2

25

184

316 20

12 998

073 1000

-

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

rdeltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 Bakerxa BakerYa c M RsubL RsubG GasVel LiqVel

Output Comment Russ Rucinski 53095 Return He pipe for Solenoid 1 12 pipe wi 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

accurate model validity

turbulen flow type 02260289 friction factor Must enter a guess

ft pipe roughness in Pipe inside diameter ft Length of pipe

00056612 m2 cross sectional area gls Total mass flow rate kgm 3 Liquid density kgm3 density of the gas JLPa-s Liquid viscosity JLPa-s Gas viscosity Nm Surface tension of liquid

quality = mdotGmdot 36530 Reynolds for liquid

0024496 kgls Mass flow rate for liquid 55580 Reynolds for gas

0015504 kgls Mass flow rate for gas

0650814 Palm LP I LU for the liquid 21275204 Palm LPLU for the two phase

01881077 psig 1 Total pressure drop for the pipe

57175294 Lockhart-Martinelli parameter 67767548 Lockhart-Martinelli parameter

L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719

1 4281346 Baker diagram dimensionless parameter kgm3 density of air kgm3 density of water

53412427 Baker diagram dimensionless parameter Nm Surface tension of water JLPa-s viscosity of water

1210 X - axis value for Baker 1410 lbmhr-ft Y-axis value for Baker

1 1 17490072 Volume fraction of liquid phase 82509928 Volume fraction of gas phase 16456003 ms Gas velocity 20429237 ms Liquid velocity

53095 middot

FERMILAB TWO PHASE HEUUM FLOW TESTS

) )

Russ KUCt~5~l

10 ~ 1 I UAUEOOV

11 ~7 I I I Flow Fath Flaw

~--- Annular Flow Wave Flow

------ Slug FlowI

A tf SIO ______

~gt

---IIMIR RIGIMI BOUNDARIII ~ G bull RCtPtC GAl OW RAlI -- ClFtC LIQUID now RAT ~l-III _lIN_

10 I I ~I gt bull I I

MaMIIow_

X 5SVI PI U bull MIddIt of IOIItnoId

1 10 VI PI bull bull Ex of IOIItnoId

18 VI PI 7 bull 1111111 of control dewarbull Figura 1 Baker diagram with Mamedov curves or two phase helium In horzonlal channels

[FttoJIA Djli El 38 23IlJ -Gt-J - 33 8 ]

r J1

01 10 10 10 ( 10 i ~ ~ 10 ~ ~ 10 L ~nG CAt 0 )V rPl

~ IMaIIon TIJampE

0J

PIPE

112 5C~ 10 f 5eCD

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995

Russ Rucinski and Steve Sakla ROOQJ Mech

Approved _________

-

n ~ middotrt -

Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

-------------~ ~~~--~~~~--

Ud

)

) ) f

J8 CO bull 0049 N2 tu~bullbull

58 CO bull 0049 He Supply 1 12 sch lOS pipe

l Sch lOS H return SS

J4 CO bull 0065 He Cool down return

He Cool downQuench Return 25 CO bull 0065 Cu Rod shield

Main Solenoid xfer ine Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

Potta 1 rb 21 153121 CST ~ by rwcnoi

~lGUJCE 1

N

)J

1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

i foE 9flIIy 1JTAlE rlTX6 AHFEEDCAN 112 00 X 049 0402 5 2 0 0 0

tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

I

bull VIJIC iliil-flH Ie FT I

I I i I bullbullOF IUlaWS IN 8 i I

I1Igel

I Ibull I

9 o 2 III J o en

L

FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

~I_ i 50 Uf-bln 3823 _ c NAME

Russ

ili2 -J-1 U ~io-pound lIJJoJ~l-c sc O~Il~ I-(JoTI CAJI60e Igt r_I Z S~ Z -n r Z Z Ilt r Zmiddot

J o N

(

N N

H

I

J

1 shy

c e-l ~w ~ UI

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FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

~ )

-shy

~ M )

f ltgt0 ~O~ I 0 bull ~

If g -rI ~ t shy ~T

0

~ r

~ -a

-r

0 0

-Sci

bull~

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i-T

intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

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0~--

i i

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i bull I rI -j r

I

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bullII i

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I

l

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bull

bull iii

bull iii

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-_

-

--

--

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UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

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shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

d (-10 ( ~raquo

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~ d51-

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- ~

-- ---------- raquo

b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

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h(7vr 1311~h lN ~ 1054 ~

-k-shy - - = A ATWO 1r (tgt15)(O4~[51))

o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

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S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

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k-wlPlf K) ( 0 )~ (0 Ioq~

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3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

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o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

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N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

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-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

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14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

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LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

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CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

~ 11 LE1 0o-lD)-S vJG ~e~ 771 ADD J(i~ w~ Fc~lJ vf J 50~~r--middotC

-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

- II gtlt 1( SvlfoVlS (2 fi_shyb w - ~PrD IP-t S vPlgto2---fShmiddott

30W 0 7- tz A- I Itt- 0 tv bull I () I( 5 1gt~fINI- pUs 130 w- Cc 15I4J Z 50 o

c A tJ 7 3_64- VII s~

1trcP1 jc ~---)-

rv - bullbull OF FXIEgt~ ( 2S 1 ~ CL- (_~

bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

2 ~ Zgt ~ IV - I (1 Of CH IA IJ amp- - J i_2soeW - l~ or- Ck Nt 13 INIttSq

- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 17: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

000005 1057 200

4 1211 2017 318 1323 000082 3876

shy

2

25

184

316 20

12 998

073 1000

-

valid

flow f epsilon D L A mdot rhoL rhog muL muG sigmaL x ReL mdotL ReG mdotG dpdLL dpdLTP

rdeltaP

phiL X m n CG CL C lambda rhoair rhoH20 sigh sigmaH2 muH20 Bakerxa BakerYa c M RsubL RsubG GasVel LiqVel

Output Comment Russ Rucinski 53095 Return He pipe for Solenoid 1 12 pipe wi 58 tube inside

Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

accurate model validity

turbulen flow type 02260289 friction factor Must enter a guess

ft pipe roughness in Pipe inside diameter ft Length of pipe

00056612 m2 cross sectional area gls Total mass flow rate kgm 3 Liquid density kgm3 density of the gas JLPa-s Liquid viscosity JLPa-s Gas viscosity Nm Surface tension of liquid

quality = mdotGmdot 36530 Reynolds for liquid

0024496 kgls Mass flow rate for liquid 55580 Reynolds for gas

0015504 kgls Mass flow rate for gas

0650814 Palm LP I LU for the liquid 21275204 Palm LPLU for the two phase

01881077 psig 1 Total pressure drop for the pipe

57175294 Lockhart-Martinelli parameter 67767548 Lockhart-Martinelli parameter

L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719 L-M constant Look up in Table 719

1 4281346 Baker diagram dimensionless parameter kgm3 density of air kgm3 density of water

53412427 Baker diagram dimensionless parameter Nm Surface tension of water JLPa-s viscosity of water

1210 X - axis value for Baker 1410 lbmhr-ft Y-axis value for Baker

1 1 17490072 Volume fraction of liquid phase 82509928 Volume fraction of gas phase 16456003 ms Gas velocity 20429237 ms Liquid velocity

53095 middot

FERMILAB TWO PHASE HEUUM FLOW TESTS

) )

Russ KUCt~5~l

10 ~ 1 I UAUEOOV

11 ~7 I I I Flow Fath Flaw

~--- Annular Flow Wave Flow

------ Slug FlowI

A tf SIO ______

~gt

---IIMIR RIGIMI BOUNDARIII ~ G bull RCtPtC GAl OW RAlI -- ClFtC LIQUID now RAT ~l-III _lIN_

10 I I ~I gt bull I I

MaMIIow_

X 5SVI PI U bull MIddIt of IOIItnoId

1 10 VI PI bull bull Ex of IOIItnoId

18 VI PI 7 bull 1111111 of control dewarbull Figura 1 Baker diagram with Mamedov curves or two phase helium In horzonlal channels

[FttoJIA Djli El 38 23IlJ -Gt-J - 33 8 ]

r J1

01 10 10 10 ( 10 i ~ ~ 10 ~ ~ 10 L ~nG CAt 0 )V rPl

~ IMaIIon TIJampE

0J

PIPE

112 5C~ 10 f 5eCD

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995

Russ Rucinski and Steve Sakla ROOQJ Mech

Approved _________

-

n ~ middotrt -

Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

-------------~ ~~~--~~~~--

Ud

)

) ) f

J8 CO bull 0049 N2 tu~bullbull

58 CO bull 0049 He Supply 1 12 sch lOS pipe

l Sch lOS H return SS

J4 CO bull 0065 He Cool down return

He Cool downQuench Return 25 CO bull 0065 Cu Rod shield

Main Solenoid xfer ine Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

Potta 1 rb 21 153121 CST ~ by rwcnoi

~lGUJCE 1

N

)J

1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

i foE 9flIIy 1JTAlE rlTX6 AHFEEDCAN 112 00 X 049 0402 5 2 0 0 0

tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

I

bull VIJIC iliil-flH Ie FT I

I I i I bullbullOF IUlaWS IN 8 i I

I1Igel

I Ibull I

9 o 2 III J o en

L

FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

~I_ i 50 Uf-bln 3823 _ c NAME

Russ

ili2 -J-1 U ~io-pound lIJJoJ~l-c sc O~Il~ I-(JoTI CAJI60e Igt r_I Z S~ Z -n r Z Z Ilt r Zmiddot

J o N

(

N N

H

I

J

1 shy

c e-l ~w ~ UI

CIgt

~1

FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

~ )

-shy

~ M )

f ltgt0 ~O~ I 0 bull ~

If g -rI ~ t shy ~T

0

~ r

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-r

0 0

-Sci

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intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

-1(IL------- ~ ~l

-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

d (-10 ( ~raquo

839qYY --(Motte

25 lie SL 20

~ d51-

7 Sbull 2shy3 2 3 472

- ~

-- ---------- raquo

b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

1 EAIJgtltf lt FR61V tJ L c(Lflc lilA ~K

f~nr - ~- ALVMtJUM

SA 4 2otJ K 6~ oJ I 270 ~ amp-A5 our

h(7vr 1311~h lN ~ 1054 ~

-k-shy - - = A ATWO 1r (tgt15)(O4~[51))

o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

CaN-IIJfIIO vJ( 1--4 vt P~eAJ(1 of J-II TLJIi AJ ~fe~ AceA

A I) CDEFtIrL~ ib COOItgt()~J A-r (tATamp 0 5 ~A

o7b 10 T I ~ l

~tlcIio 60 it S ) ( lOS 5 ~ -q SJf) )l 3 CO os

STEP 3

S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

~ 11 LE1 0o-lD)-S vJG ~e~ 771 ADD J(i~ w~ Fc~lJ vf J 50~~r--middotC

-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

- II gtlt 1( SvlfoVlS (2 fi_shyb w - ~PrD IP-t S vPlgto2---fShmiddott

30W 0 7- tz A- I Itt- 0 tv bull I () I( 5 1gt~fINI- pUs 130 w- Cc 15I4J Z 50 o

c A tJ 7 3_64- VII s~

1trcP1 jc ~---)-

rv - bullbull OF FXIEgt~ ( 2S 1 ~ CL- (_~

bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

2 ~ Zgt ~ IV - I (1 Of CH IA IJ amp- - J i_2soeW - l~ or- Ck Nt 13 INIttSq

- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 18: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

53095 middot

FERMILAB TWO PHASE HEUUM FLOW TESTS

) )

Russ KUCt~5~l

10 ~ 1 I UAUEOOV

11 ~7 I I I Flow Fath Flaw

~--- Annular Flow Wave Flow

------ Slug FlowI

A tf SIO ______

~gt

---IIMIR RIGIMI BOUNDARIII ~ G bull RCtPtC GAl OW RAlI -- ClFtC LIQUID now RAT ~l-III _lIN_

10 I I ~I gt bull I I

MaMIIow_

X 5SVI PI U bull MIddIt of IOIItnoId

1 10 VI PI bull bull Ex of IOIItnoId

18 VI PI 7 bull 1111111 of control dewarbull Figura 1 Baker diagram with Mamedov curves or two phase helium In horzonlal channels

[FttoJIA Djli El 38 23IlJ -Gt-J - 33 8 ]

r J1

01 10 10 10 ( 10 i ~ ~ 10 ~ ~ 10 L ~nG CAt 0 )V rPl

~ IMaIIon TIJampE

0J

PIPE

112 5C~ 10 f 5eCD

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995

Russ Rucinski and Steve Sakla ROOQJ Mech

Approved _________

-

n ~ middotrt -

Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

-------------~ ~~~--~~~~--

Ud

)

) ) f

J8 CO bull 0049 N2 tu~bullbull

58 CO bull 0049 He Supply 1 12 sch lOS pipe

l Sch lOS H return SS

J4 CO bull 0065 He Cool down return

He Cool downQuench Return 25 CO bull 0065 Cu Rod shield

Main Solenoid xfer ine Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

Potta 1 rb 21 153121 CST ~ by rwcnoi

~lGUJCE 1

N

)J

1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

i foE 9flIIy 1JTAlE rlTX6 AHFEEDCAN 112 00 X 049 0402 5 2 0 0 0

tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

I

bull VIJIC iliil-flH Ie FT I

I I i I bullbullOF IUlaWS IN 8 i I

I1Igel

I Ibull I

9 o 2 III J o en

L

FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

~I_ i 50 Uf-bln 3823 _ c NAME

Russ

ili2 -J-1 U ~io-pound lIJJoJ~l-c sc O~Il~ I-(JoTI CAJI60e Igt r_I Z S~ Z -n r Z Z Ilt r Zmiddot

J o N

(

N N

H

I

J

1 shy

c e-l ~w ~ UI

CIgt

~1

FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

~ )

-shy

~ M )

f ltgt0 ~O~ I 0 bull ~

If g -rI ~ t shy ~T

0

~ r

~ -a

-r

0 0

-Sci

bull~

~ ~

i-T

intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

-1(IL------- ~ ~l

-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

d (-10 ( ~raquo

839qYY --(Motte

25 lie SL 20

~ d51-

7 Sbull 2shy3 2 3 472

- ~

-- ---------- raquo

b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

1 EAIJgtltf lt FR61V tJ L c(Lflc lilA ~K

f~nr - ~- ALVMtJUM

SA 4 2otJ K 6~ oJ I 270 ~ amp-A5 our

h(7vr 1311~h lN ~ 1054 ~

-k-shy - - = A ATWO 1r (tgt15)(O4~[51))

o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

CaN-IIJfIIO vJ( 1--4 vt P~eAJ(1 of J-II TLJIi AJ ~fe~ AceA

A I) CDEFtIrL~ ib COOItgt()~J A-r (tATamp 0 5 ~A

o7b 10 T I ~ l

~tlcIio 60 it S ) ( lOS 5 ~ -q SJf) )l 3 CO os

STEP 3

S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

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PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

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000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

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ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

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PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

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K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 19: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

PIPE SIZING

FOR

SOLENOIDVLPC

CRYOGENIC SYSTEMS

O-ZERO ENGINEERING NOTE 382311 5- EN-416

February 20 1995

Russ Rucinski and Steve Sakla ROOQJ Mech

Approved _________

-

n ~ middotrt -

Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

-------------~ ~~~--~~~~--

Ud

)

) ) f

J8 CO bull 0049 N2 tu~bullbull

58 CO bull 0049 He Supply 1 12 sch lOS pipe

l Sch lOS H return SS

J4 CO bull 0065 He Cool down return

He Cool downQuench Return 25 CO bull 0065 Cu Rod shield

Main Solenoid xfer ine Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

Potta 1 rb 21 153121 CST ~ by rwcnoi

~lGUJCE 1

N

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1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

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tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

I

bull VIJIC iliil-flH Ie FT I

I I i I bullbullOF IUlaWS IN 8 i I

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FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

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Russ

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FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

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i-T

intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

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i i

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i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

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I

bull

ex t

l

--l

J ~ --

I

r-shy

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I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

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I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

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FERMILAB SECTION

ENGINEERING NOTE SUSJECT

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PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

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II-qmiddot11

raeao

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NAME

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PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

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SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

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1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

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AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

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(aO5) ( 0100)

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SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

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7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

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o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

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PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

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FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

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D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

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VLt

NAME -shy

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~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

~ 11 LE1 0o-lD)-S vJG ~e~ 771 ADD J(i~ w~ Fc~lJ vf J 50~~r--middotC

-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

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SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

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jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

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It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 20: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

Introduction The addition of a solenoid magnet and VLPC detectors are two of a number of

upgrades which will occur at the D-Zero detector in the near future Both of these

upgrades will require cryogenic services for their operation The purpose of this

engineering note is to document the pipetube size choices made for these cryogenic

services This was done by calculating the required flow rates to cool down the magnet

and VLPCs over a reasonable length of time and to determine the required piping sizes

for a given allowable pressure drop The pressure drops for steady state conditions also

are addressed The cool down requirements drove the pipe size decision The raw

engineering calculations that were done for this project are included as an appendix to

this note The body of this document discusses the methods and results of the

calculations As a quick summary Figures 1 and 2 show the size selections Tables 1

and 2 give a more detailed size and description of each section of Solenoid and VLPC

transfer line

YLPC DetectorlCaostat Description The main detecting component of the VLPC detector is the VLPC (Visible Light

Photon Counter) chip These chips have an optimum performance at a temperature of

about 65K which will be maintained through the use of a cryostat Two cryostats named

east and west will be used to maintain the cold temperatures of the chips through the use

of liquid helium Liquid nitrogen will be used to intercept some of the heat leak coming

in to the cryostat These cryogens will be supplied to the cryostat via a vacuum jacketed

transfer line and u-tubes The transfer lines begin at the LHe refrigerator location near

the southeast comer of the D-Zero cleanroom The VLPC supply and return lines share a

common vacuum jacketed line These lines will originate at the valve box on the

refrigerator side and will run along the south wall see figure 4 The building side route

for the VLPC line follows the same path as the solenoid see figure 5 The detector side

VLPC piping can be seen in figure 6 For more description see the DO engineering note

Cryogenic Line routing Refrigerator to VLPC Cryostats and Solenoid DO note 3823115-EN-413

Solenoid MaIDet Description The solenoid magnet will provide a 2 tesla magnetic field in the inner bore of the

- central calorimeter It will operate at approximately 49K which will be obtained by

means of indirect cooling from liquid helium As with the VLPC cryostat liquid nitrogen

-------------~ ~~~--~~~~--

Ud

)

) ) f

J8 CO bull 0049 N2 tu~bullbull

58 CO bull 0049 He Supply 1 12 sch lOS pipe

l Sch lOS H return SS

J4 CO bull 0065 He Cool down return

He Cool downQuench Return 25 CO bull 0065 Cu Rod shield

Main Solenoid xfer ine Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

Potta 1 rb 21 153121 CST ~ by rwcnoi

~lGUJCE 1

N

)J

1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

i foE 9flIIy 1JTAlE rlTX6 AHFEEDCAN 112 00 X 049 0402 5 2 0 0 0

tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

I

bull VIJIC iliil-flH Ie FT I

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FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

~I_ i 50 Uf-bln 3823 _ c NAME

Russ

ili2 -J-1 U ~io-pound lIJJoJ~l-c sc O~Il~ I-(JoTI CAJI60e Igt r_I Z S~ Z -n r Z Z Ilt r Zmiddot

J o N

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I

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FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

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f ltgt0 ~O~ I 0 bull ~

If g -rI ~ t shy ~T

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intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

-1(IL------- ~ ~l

-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

d (-10 ( ~raquo

839qYY --(Motte

25 lie SL 20

~ d51-

7 Sbull 2shy3 2 3 472

- ~

-- ---------- raquo

b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

1 EAIJgtltf lt FR61V tJ L c(Lflc lilA ~K

f~nr - ~- ALVMtJUM

SA 4 2otJ K 6~ oJ I 270 ~ amp-A5 our

h(7vr 1311~h lN ~ 1054 ~

-k-shy - - = A ATWO 1r (tgt15)(O4~[51))

o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

CaN-IIJfIIO vJ( 1--4 vt P~eAJ(1 of J-II TLJIi AJ ~fe~ AceA

A I) CDEFtIrL~ ib COOItgt()~J A-r (tATamp 0 5 ~A

o7b 10 T I ~ l

~tlcIio 60 it S ) ( lOS 5 ~ -q SJf) )l 3 CO os

STEP 3

S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

~ 11 LE1 0o-lD)-S vJG ~e~ 771 ADD J(i~ w~ Fc~lJ vf J 50~~r--middotC

-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

- II gtlt 1( SvlfoVlS (2 fi_shyb w - ~PrD IP-t S vPlgto2---fShmiddott

30W 0 7- tz A- I Itt- 0 tv bull I () I( 5 1gt~fINI- pUs 130 w- Cc 15I4J Z 50 o

c A tJ 7 3_64- VII s~

1trcP1 jc ~---)-

rv - bullbull OF FXIEgt~ ( 2S 1 ~ CL- (_~

bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

2 ~ Zgt ~ IV - I (1 Of CH IA IJ amp- - J i_2soeW - l~ or- Ck Nt 13 INIttSq

- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 21: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

Ud

)

) ) f

J8 CO bull 0049 N2 tu~bullbull

58 CO bull 0049 He Supply 1 12 sch lOS pipe

l Sch lOS H return SS

J4 CO bull 0065 He Cool down return

He Cool downQuench Return 25 CO bull 0065 Cu Rod shield

Main Solenoid xfer ine Solenoid xfer ine

PRELIMINARY BUILDING TRANSFER LINE DESIGNS Russ Rucinski 22195

Potta 1 rb 21 153121 CST ~ by rwcnoi

~lGUJCE 1

N

)J

1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

i foE 9flIIy 1JTAlE rlTX6 AHFEEDCAN 112 00 X 049 0402 5 2 0 0 0

tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

I

bull VIJIC iliil-flH Ie FT I

I I i I bullbullOF IUlaWS IN 8 i I

I1Igel

I Ibull I

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FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

~I_ i 50 Uf-bln 3823 _ c NAME

Russ

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J o N

(

N N

H

I

J

1 shy

c e-l ~w ~ UI

CIgt

~1

FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

~ )

-shy

~ M )

f ltgt0 ~O~ I 0 bull ~

If g -rI ~ t shy ~T

0

~ r

~ -a

-r

0 0

-Sci

bull~

~ ~

i-T

intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

-1(IL------- ~ ~l

-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

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bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

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o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

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S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

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(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

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3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

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i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

~ 11 LE1 0o-lD)-S vJG ~e~ 771 ADD J(i~ w~ Fc~lJ vf J 50~~r--middotC

-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

- II gtlt 1( SvlfoVlS (2 fi_shyb w - ~PrD IP-t S vPlgto2---fShmiddott

30W 0 7- tz A- I Itt- 0 tv bull I () I( 5 1gt~fINI- pUs 130 w- Cc 15I4J Z 50 o

c A tJ 7 3_64- VII s~

1trcP1 jc ~---)-

rv - bullbull OF FXIEgt~ ( 2S 1 ~ CL- (_~

bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

2 ~ Zgt ~ IV - I (1 Of CH IA IJ amp- - J i_2soeW - l~ or- Ck Nt 13 INIttSq

- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 22: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

)J

1AISLE SOLENOID PIPE SECTIONSi

lIEEamp PIPampORtuBE 1IIIIIIII LIHiAB LQE lIEEamp llftI

LINE fIJIIQ lIm ffI1M 12 DlA liN LENBTH IFTI IiIImisect THRURUN IlIWJgj YAJnI

4 WE SUPPLY (HUTJ) UmiddotTIlBE WE DEWAR XmiddotFERLINE 314 aD x 035 068 5 2 0 0 0

5 WE SUPPLY XmiddotF6RLINE lJmiddotTIlBE UmiddotTIlBE Sl8 00 X 049 0527 125 I 4 0 IDIVRTR

c- IL WE SUPPLY (HUT) UmiddotTIlBE X-FERLINE alN11IOL OOWAR 314 on X 035 068 10 2 0 0 0

1 WE RETIlRN (HUT5) UmiddotTUBE OlNIROLOOWAR XmiddotF6R LINE 314 00 X 035 068 10 2 0 0 0

8 WE REnJRN XmiddotF6R LINE UmiddotTIlBE lJmiddotTUBE COllcanlric 0427 125 9 4 0 I PVI CV _

9 HE RETURN UmiddotTIlBE XmiddotF6R LINE XmiddotF6R LINE (VLPC) 314 00 X 035 068 J 2 0 0 0

1-- 1L LN2 SUPPLY UmiddotTUBE UNHEADEIl XmiddotFERLINE 112 aD x 035 043 3 2 0 0 0

C-- LN2 SUPPLY XmiddotF6R LINE UmiddotTUBE TEE 112 00 X 049 0402 I I 0 0 0

12 LN2 SUPPLY (SHIELD XmiddotFERLINE TEE UmiddotTIlBE 318 00 X 049 0277 124 9 2 I I PV

11 LN2 SUPPLY (SHIELD UmiddotTUBE XmiddotF6R LINE ltDNTROLOOWAR 112 00 I 035 043 10 2 0 0 ()

SUPPLY

14 LN2 (INTERCEIT) XmiddotIFR LINE (EE UmiddotTIlBE liS 00 X 049 0277 ----shy

124 9 2 I I~

SUPPLY

_ 15 LN2 (INTERCEIT) UmiddotTUBE XmiddotFER LINE ltDNTROIllWAR 12 00 bull035 043 10 2 0 shy ()shy

1bull LN2 RETURN (SHIELD) VmiddotmiddotruBE UlNTROL DEWAR XmiddotFER LINE 112 00 x 035 043 In 2

1 7 LN2 RETURN (SHIELD) XmiddotFER LINE UmiddotTUBE UmiddotTUBE 3g aD x 049 0271 125 ~ 2 shyl LN2 RETURN (SHIELD) UmiddotTUBE XmiddotFER LINE TEE 112 00 x 035 043 I I 0

RETURN

lJl_ LN2 (INTERCEIT) VmiddotTUOIO (l)N1ROLDIWAR XmiddotFER LINE 12 OD x JlJ5 (Imiddotn I 2 () 1-- -- _ -f------shy -----shy__ shy

RETURN

2Q LN2 (INTERCEPT) XmiddotFERII IImiddotnlIlC 11111111 _ 1amp OD X gtl9 gt277_1--__ 1 gtl --1

1- _ middotmiddotcmiddot _

RETURN

n LN2 (INTERCEIT) UmiddotTUBF XmiddotFER LINE 1Et 112 OD bull035 043 1 I n I

23 LN2 RETURN UmiddotTUBE TEE GNi VENT HEADER 12 00 x 035 043 5 I 0 0 0

(COOLOOWNI

_ bull24 HE QUENCH) ITtJBE CONTROL DEWAR XmiddotFER LINE 34 00 X oJ5 068 _~___ 11J 2 (I - - shy(COOLOOWNI

~ HE QUENCH) XmiddotFERLINE UmiddotTUBE U-TUSE 314 00 X 065 062 125 9_ ~ (COOLOOWNI HEltDOLOOWN

--~~ QUENCII) UmiddotTUBE XmiddotFER LINE RETURN 314 00 X 0)5 068 _5_ 2 poundI II shy -bull _shySUPPLY

27 HE I(ltDOLOOWN) UmiddotTUBE COOLOOWN LINE XmiddotFER LINE 34 OD X illS 068 5 4 q 1 IlIRIK

~ Page 1

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

i foE 9flIIy 1JTAlE rlTX6 AHFEEDCAN 112 00 X 049 0402 5 2 0 0 0

tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

I

bull VIJIC iliil-flH Ie FT I

I I i I bullbullOF IUlaWS IN 8 i I

I1Igel

I Ibull I

9 o 2 III J o en

L

FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

~I_ i 50 Uf-bln 3823 _ c NAME

Russ

ili2 -J-1 U ~io-pound lIJJoJ~l-c sc O~Il~ I-(JoTI CAJI60e Igt r_I Z S~ Z -n r Z Z Ilt r Zmiddot

J o N

(

N N

H

I

J

1 shy

c e-l ~w ~ UI

CIgt

~1

FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

~ )

-shy

~ M )

f ltgt0 ~O~ I 0 bull ~

If g -rI ~ t shy ~T

0

~ r

~ -a

-r

0 0

-Sci

bull~

~ ~

i-T

intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

-1(IL------- ~ ~l

-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

d (-10 ( ~raquo

839qYY --(Motte

25 lie SL 20

~ d51-

7 Sbull 2shy3 2 3 472

- ~

-- ---------- raquo

b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

1 EAIJgtltf lt FR61V tJ L c(Lflc lilA ~K

f~nr - ~- ALVMtJUM

SA 4 2otJ K 6~ oJ I 270 ~ amp-A5 our

h(7vr 1311~h lN ~ 1054 ~

-k-shy - - = A ATWO 1r (tgt15)(O4~[51))

o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

CaN-IIJfIIO vJ( 1--4 vt P~eAJ(1 of J-II TLJIi AJ ~fe~ AceA

A I) CDEFtIrL~ ib COOItgt()~J A-r (tATamp 0 5 ~A

o7b 10 T I ~ l

~tlcIio 60 it S ) ( lOS 5 ~ -q SJf) )l 3 CO os

STEP 3

S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

~ 11 LE1 0o-lD)-S vJG ~e~ 771 ADD J(i~ w~ Fc~lJ vf J 50~~r--middotC

-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

- II gtlt 1( SvlfoVlS (2 fi_shyb w - ~PrD IP-t S vPlgto2---fShmiddott

30W 0 7- tz A- I Itt- 0 tv bull I () I( 5 1gt~fINI- pUs 130 w- Cc 15I4J Z 50 o

c A tJ 7 3_64- VII s~

1trcP1 jc ~---)-

rv - bullbull OF FXIEgt~ ( 2S 1 ~ CL- (_~

bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

2 ~ Zgt ~ IV - I (1 Of CH IA IJ amp- - J i_2soeW - l~ or- Ck Nt 13 INIttSq

- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 23: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

5 LtampU

flel gil Dlill DIII~ 11Ii11~m ~ nR~j~N =CMLINI t IIIUD inPJ iEI3IIM III IIU --fIl VAVES

i foE 9flIIy 1JTAlE rlTX6 AHFEEDCAN 112 00 X 049 0402 5 2 0 0 0

tL lHE 9flIIy 1JTAlE LHeoewM AH FEED CAN liZ 00 X 049 0402 5 2 0 0 0

40 HIli wesTHE SUP Y XFEfllJlE 1JTAlE )WAY VAlVE 318 00 )( 035 0305 2 I I 0 0 tIE ~_IE__ -shy - 3oW~~e t t amp

tt foE WEST HE SUP Y XFEfl UIE )WAYVALVE lJTAlE 318 00 X 035 o lOS 123 9 3 0 1011

43 foE WEST HE SUPY 1JTAlE CHFEEDCAN BAYONET CAN 318 00 X 035 0305 12 2 0 0 0

44 HE WEST HESUOPLY XFEfl UIE BAYONET CAN VAVEBOX 318 00 X 035 0l05 41 8 I 0 0

45 foE WEST HESUOPLY XFEfllJlE VAVEBOX VIJC 318 00 X 035 0305 H 2 0 0 0

48 HE EtIIT HE SUOPLY XFEfllJlE 1JTAE a-WAY VAlVE 318 00 X 035 0305 2 0 1 I 0

47 foE EAST HE SUOPLY XFEfllJlE 1JTAlE WAY VALVE 318 00 X 035 0305 2 a 0 1 0

48 HE EtIIT HE SUOPLY XFEfl UNE WIltYVAlVe UoTAlE 318 00 X 035 0305 123 9 3 a IOV

411 HE EtIIT HE SUOPLY UoTAlE CHFElDCAN BAVONETCAN 318 00 X 035 0305 12 2 0 0 0

50 HIli EtIIT HE SUOPLY XFEfllJlE BAVONET CAN VALVE BOX 318 00 X 035 0305 41 8 1 0 0

51 HIli EASTHE9flIIY X-FlRUNE VAlVE BOX VIJC 318 00)( 035 0305 24 2 0 0 0

52 HE EAST HE AIlJRN XFEflJJNE vUC VAlVE BOX 318 00 X035 0305 24 a a I pv

53 HE EAST HE AIlJRN XFEfl UNE VAlVE BOX BAYONET CAN 318 00 X 035 0305 41 8 a 0 0

5 HE EAST HE RETURN lJTAlE BAYONET CAN CHFEEDCAN 38 00 )(035 0305 12 2 0 0 0

55 HE EAST HE AIlJRN XFEfllJlE CHFEEDCAN JrWAYVALVE 318 00 )( 035 0305 123 fI 3 1 1011

VJ UNE (COOIJlOWN 51 HE EtIIT HE AIlJRN XFEfl LINE 3-WAYVAlVE AErUIN) 38 00 )( 035 0305 2 2 t t CV

57 HE EtIIT HE AIlJRN KFEflLINE JrWAYVIltLVE JUNE VALVE BOlO 318 00 X 035 0305 2 2 2 1 t cv

5amp HE WESTHERElUlN XFEfl LINE VIJC VAlVE BOX 318 00 X 035 0305 24 I 0 0 1 PV

58 foE wesrHERElUlN XFEflLINE YALVEBOX BAVONET CAN 318 00 X 035 0305 47 8 0 0 0

80 HE WESTHERElUlN lUll BAVONET CAN CHFElDCAN 38 OD X 035 0305 12 2 0 0 0

81 foE _HE AIlJRN XFEfllJlE CHFEEDCAN 3-WAYIAlVE 318 00 X 035 0305 123 fI 2 a 10V

VJ UNE (COOIJlOWN 82 HE WEST HERElUlN XFEflUNE 3-WAYVALVE AEruIN) 38 00 K 035 0305 2 2 0 2 1 CII

as HE wesrHERElUlN XFEflLINE JoWAY VAlVE V UNEJVALVE BO~l 318 00 K 035 0305 1 I a 2 ICV

84 HE WEST HE AIlJRN XFEflUNE 3-WAYVALVE lB 318 00 X035 0305 1 1 1 2 1 ell

1JME FIION SOL xmiddot 81i HE IEIAI XFEflLINE FERUE lB In 00 x 049 0402 I 1 2 1 0

OOOLDOWN RINRN 8e HE IEIAI tJ-TAlE Ali IlIO CAN LINE 112 00 X 049 0402 5 2 0 0 Q

87 HE IEIAI lUll Ali IlIO CAN VALveBQ)( 34 00 x 035 088 4 0 0 0 0

8amp LN2 9flIIy tJ-TAlE LN2 HEAtlEII AH FEED CAN 38 00 X 049 0277 3 2 0 0 0

ao LN2 9flIIV XFEflLINE Ali IlIOCAN CHFEEOCAN 318 00 X 049 0217 125 9 2 0 I 0

10 LN2 9flIIV tJ-TAlE CHFEEDCAN BAVONET CAN 3t 00 X 049 0277 12 2 0 0 0

Ii LN2 9flIIV KFEflLINE IIIVONETCAN VALVE BOX 31t 00 X 049 0277 47 II 1 0 0

n LN2 9flIIY XFEflUNE VALVEBQ)( VlJCwesr 31S 00 X 049 0277 24 3 I 1 1 py

lJ LN2 9flIIY XFEflLINE IIALVEIIOX VUCEAST 3Ilt OD X 049 0277 24 3 I I 1 py

7 LN2 9flIIY XFEflLINE VlJlCWEST VALVE BOX 318 OD X 049 0277 24 0 0 1 0

75 LN2 SlRlY XFEfl LINE VlJlCEAST IIAlVEBOX 38 OD X G49 0277 2 1 1 0 0

It_ LN2 9flIIY XFEflLINE VALVEBQ)( BAVONET CAN 318 00 X 049 0277 47 II I 0 0

77 LN2 IEIAI UoTAlE BAVONET CAN CHFEEOCAN 3S OD X 049 0277 12 2 0 0 0

78_ LN2 IEIAI XFEflLINE CHFEEDCNi AHFEEOCAN 3S OD X 049 0271 125 I 2 0 0

7Q LN~ IEIAI lUll AHFlEDCAN GN2 VENT HEIltOEA 3S OD X 049 0277 5 2 0 0 0

I

bull VIJIC iliil-flH Ie FT I

I I i I bullbullOF IUlaWS IN 8 i I

I1Igel

I Ibull I

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L

FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

~I_ i 50 Uf-bln 3823 _ c NAME

Russ

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J o N

(

N N

H

I

J

1 shy

c e-l ~w ~ UI

CIgt

~1

FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

~ )

-shy

~ M )

f ltgt0 ~O~ I 0 bull ~

If g -rI ~ t shy ~T

0

~ r

~ -a

-r

0 0

-Sci

bull~

~ ~

i-T

intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

-1(IL------- ~ ~l

-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

d (-10 ( ~raquo

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25 lie SL 20

~ d51-

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b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

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f~nr - ~- ALVMtJUM

SA 4 2otJ K 6~ oJ I 270 ~ amp-A5 our

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-k-shy - - = A ATWO 1r (tgt15)(O4~[51))

o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

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A I) CDEFtIrL~ ib COOItgt()~J A-r (tATamp 0 5 ~A

o7b 10 T I ~ l

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STEP 3

S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

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I

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3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

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(it 1tf~J I uO 05 J cent )

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r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

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K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 24: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

I Ibull I

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FIGURE 4

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

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3823 II S

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NAME

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intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

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14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

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PROJECT SERIALmiddotCATEGOIIY PAGE

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USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

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NAME

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PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

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Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

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SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

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SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

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ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

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1-lb-95 IREVIS10 OA TE

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PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

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PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

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DATE jREVIS10N DATE i Cl - I - ~-l-

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FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

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PAGE

-1_

DATE REVISION DATE ic - 17- -14

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A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

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DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

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10 - 2 () - 91

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NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

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SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

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lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 25: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

SUBJECT

FERMILA8 SECTION

ENGINEERING NOTE

FIGURES

PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES

~I_ i 50 Uf-bln 3823 _ c NAME

Russ

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FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

~ )

-shy

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f ltgt0 ~O~ I 0 bull ~

If g -rI ~ t shy ~T

0

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intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

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-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

d (-10 ( ~raquo

839qYY --(Motte

25 lie SL 20

~ d51-

7 Sbull 2shy3 2 3 472

- ~

-- ---------- raquo

b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

1 EAIJgtltf lt FR61V tJ L c(Lflc lilA ~K

f~nr - ~- ALVMtJUM

SA 4 2otJ K 6~ oJ I 270 ~ amp-A5 our

h(7vr 1311~h lN ~ 1054 ~

-k-shy - - = A ATWO 1r (tgt15)(O4~[51))

o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

CaN-IIJfIIO vJ( 1--4 vt P~eAJ(1 of J-II TLJIi AJ ~fe~ AceA

A I) CDEFtIrL~ ib COOItgt()~J A-r (tATamp 0 5 ~A

o7b 10 T I ~ l

~tlcIio 60 it S ) ( lOS 5 ~ -q SJf) )l 3 CO os

STEP 3

S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

~ 11 LE1 0o-lD)-S vJG ~e~ 771 ADD J(i~ w~ Fc~lJ vf J 50~~r--middotC

-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

- II gtlt 1( SvlfoVlS (2 fi_shyb w - ~PrD IP-t S vPlgto2---fShmiddott

30W 0 7- tz A- I Itt- 0 tv bull I () I( 5 1gt~fINI- pUs 130 w- Cc 15I4J Z 50 o

c A tJ 7 3_64- VII s~

1trcP1 jc ~---)-

rv - bullbull OF FXIEgt~ ( 2S 1 ~ CL- (_~

bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

2 ~ Zgt ~ IV - I (1 Of CH IA IJ amp- - J i_2soeW - l~ or- Ck Nt 13 INIttSq

- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 26: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

FIGURE 6

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

-1-(0 lJT111TIES

SERIAL-CATEGORY

3823 II S

SUBJECT

LIN E D Rpo I Nc O~ PIPlrJ6

NAME

DATE REVISION OA TE

l2-S-q

~ )

-shy

~ M )

f ltgt0 ~O~ I 0 bull ~

If g -rI ~ t shy ~T

0

~ r

~ -a

-r

0 0

-Sci

bull~

~ ~

i-T

intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

-1(IL------- ~ ~l

-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

d (-10 ( ~raquo

839qYY --(Motte

25 lie SL 20

~ d51-

7 Sbull 2shy3 2 3 472

- ~

-- ---------- raquo

b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

1 EAIJgtltf lt FR61V tJ L c(Lflc lilA ~K

f~nr - ~- ALVMtJUM

SA 4 2otJ K 6~ oJ I 270 ~ amp-A5 our

h(7vr 1311~h lN ~ 1054 ~

-k-shy - - = A ATWO 1r (tgt15)(O4~[51))

o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

CaN-IIJfIIO vJ( 1--4 vt P~eAJ(1 of J-II TLJIi AJ ~fe~ AceA

A I) CDEFtIrL~ ib COOItgt()~J A-r (tATamp 0 5 ~A

o7b 10 T I ~ l

~tlcIio 60 it S ) ( lOS 5 ~ -q SJf) )l 3 CO os

STEP 3

S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

~ 11 LE1 0o-lD)-S vJG ~e~ 771 ADD J(i~ w~ Fc~lJ vf J 50~~r--middotC

-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

- II gtlt 1( SvlfoVlS (2 fi_shyb w - ~PrD IP-t S vPlgto2---fShmiddott

30W 0 7- tz A- I Itt- 0 tv bull I () I( 5 1gt~fINI- pUs 130 w- Cc 15I4J Z 50 o

c A tJ 7 3_64- VII s~

1trcP1 jc ~---)-

rv - bullbull OF FXIEgt~ ( 2S 1 ~ CL- (_~

bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

2 ~ Zgt ~ IV - I (1 Of CH IA IJ amp- - J i_2soeW - l~ or- Ck Nt 13 INIttSq

- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 27: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

intercepts will be used Along with liquid helium the liquid nitrogen will be supplied via 9 a vacuum jacketed transfer line and u-tubes These line will essentially follow the same

path as the VLPC piping (figure 4) in the assembly hall A line drawing of the solenoid

building side transfer line can be seen in figure 5 Via u-tubes the transfer line connects

to the control dewar mounted on the detector The routing path on the detector is

described in chapter 5 of the solenoid design report (Fermilab-TM-1886) and is also

shown graphically in figure 7 The helium supply and return lines in the transfer line will

consist of two concentric pipes The supply line will run inside the return line to make

use of the enthalpy of the return cold gas Preliminary Flow schematics for both the

VLPC and solenoid piping (FNAL Drg 38231 15-ME-317223) are shown in figures 8

thru 10

Solenoid Helium Cooldowp Oowrates The LHe line sizes for the solenoid were determined by first calculating the

required flow rates during cooldown These calculations are shown in Solenoid

Cooldown amp Flow Rates Etc of appendix A and are summarized in Table 3 A

cooldown rate of 5 Klhr was used in these calculations It should be noted that it is

planned to limit the actual rate to 2 Klhr

Table 3 SOLENOID COOLDOWN FLOW RATES

STEP SOLENOID TEMP

[K

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [hrs)

DELTAH COLD MASS

[J1

MASSFLO~IRATEREQD

pound2s] 1 300 to 250 200 250 10 642E+07 69 2 250 to 200 150 200 10 605E+07 65 3 200 to 150 100 150 10 544E+07 58 4 100 to 90 80 90 4 6S9E+06 88

The mass flow rates of steps 1amp4 were the largest The largest pressure drop of the steps

was determined by noting that APa fL~2 The corresponding pressure drops were pd

ratioed to determine which was larger It was concluded that step Is pressure drop would

be about 26 times larger than step 4s Therefore the cooldown lines should be sized for

a flow rate of 7 gls with an inlet temperature of 200K and an outlet temperature of 300K

(refer to appendix A)

------

------

--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1

0~--

i i

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-t--h-~

i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

+m

-_

-

--

--

-shy----------------------------~

I

FIG

UR

E 7

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

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FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

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o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

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---

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ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

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ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

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P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

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AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

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~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

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(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

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SUBJECL

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o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

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AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

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o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

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PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

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PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

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o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

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A V

SUBJECT

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VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

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1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

~ 11 LE1 0o-lD)-S vJG ~e~ 771 ADD J(i~ w~ Fc~lJ vf J 50~~r--middotC

-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

- II gtlt 1( SvlfoVlS (2 fi_shyb w - ~PrD IP-t S vPlgto2---fShmiddott

30W 0 7- tz A- I Itt- 0 tv bull I () I( 5 1gt~fINI- pUs 130 w- Cc 15I4J Z 50 o

c A tJ 7 3_64- VII s~

1trcP1 jc ~---)-

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- 2 lttr

- Car TI~

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At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 28: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

------

------

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0~--

i i

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i bull I rI -j r

I

I (~

I I

I I I~

~J Ii L i

1 -

Ibull

bullII i

~ I

I

l

-bull

bull

bull iii

bull iii

-I

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-_

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--

--

-shy----------------------------~

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UR

E 7

~-----------------~

-----t----

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bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

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shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

d (-10 ( ~raquo

839qYY --(Motte

25 lie SL 20

~ d51-

7 Sbull 2shy3 2 3 472

- ~

-- ---------- raquo

b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

1 EAIJgtltf lt FR61V tJ L c(Lflc lilA ~K

f~nr - ~- ALVMtJUM

SA 4 2otJ K 6~ oJ I 270 ~ amp-A5 our

h(7vr 1311~h lN ~ 1054 ~

-k-shy - - = A ATWO 1r (tgt15)(O4~[51))

o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

CaN-IIJfIIO vJ( 1--4 vt P~eAJ(1 of J-II TLJIi AJ ~fe~ AceA

A I) CDEFtIrL~ ib COOItgt()~J A-r (tATamp 0 5 ~A

o7b 10 T I ~ l

~tlcIio 60 it S ) ( lOS 5 ~ -q SJf) )l 3 CO os

STEP 3

S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

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3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

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o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

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PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

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II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

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Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

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bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

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375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

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SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

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-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

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ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 29: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

~-----------------~

-----t----

I

bull

ex t

l

--l

J ~ --

I

r-shy

-=shy

~ u ~

shy~-~ 0shy-

1-shy

I bull II

I Ii

iI J t=

4 ~

I

r

v uJ Cl J ~

L1

IbullbullI Imiddotaf

I bullbulli bull

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

d (-10 ( ~raquo

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25 lie SL 20

~ d51-

7 Sbull 2shy3 2 3 472

- ~

-- ---------- raquo

b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

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SA 4 2otJ K 6~ oJ I 270 ~ amp-A5 our

h(7vr 1311~h lN ~ 1054 ~

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o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

CaN-IIJfIIO vJ( 1--4 vt P~eAJ(1 of J-II TLJIi AJ ~fe~ AceA

A I) CDEFtIrL~ ib COOItgt()~J A-r (tATamp 0 5 ~A

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STEP 3

S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

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3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

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LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

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13V ENGINEERING NOTE NAMESUBJECT

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DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

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ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

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PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

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K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 30: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

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14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

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FERMILAB SECTION

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App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

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NAME

CATE IREVISION CATE

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ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

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NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

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Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

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1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

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= S h-rt5Ul

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w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

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(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

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~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

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SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

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6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

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f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

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t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

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DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

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FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

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SERIAlmiddotCATEGORY

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PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

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A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

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FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

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115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

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NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

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1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

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SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

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K2

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It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 31: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

14 For comparison D-Zero engineering note 3823111-EN-359 documents more complex

calculations for a cooldown rate of 2K1hr The highest mass flow for this cooldown rate

was 44 gls as shown in 38231 1 1-EN-359 (See table 4 below) Therefore the flow rate

of 7 gls used to size the cooldown lines will be a conservative number

Table 4 Helium Flow Results

Step I Inlet Exit bull Temperature Temperature

rKelvin rKelvin1

Inlet I Exit Enthalpy Enthalpy

rJal IJal

I i I

Inlet I Exit Pressure I Pressure IDsial I IDsial

=I ralsl

1 115 215 925 1444 I 89 I 5 12

2 I 125 225 665 1184 i 11 5 12 3 I 80 115 431 924 I 65 5 11 4 I 80 I 125 431 665 I 11 5 19 5 80 I 95I 431 509 I 138 5 44 6 46 I 80 302 431 I 7 5 23 7 46 I 60 302 321 I 1 5 21 8 46 i 45 302 249 I 1 5 i 33 9 46 I 35 302 191 1 5 38 10 46 I 215 j 302 158 i 1 5 44 1 1 I 46 225 I

12 46 i 175 302 302

132 7 5 41 105 7 5 55

13 I 46 I 125 302 186 1 5 I 67 14 46 815 302 580 I 1 5 I 83 15 46 6 302 418 i 7 5 104

Solenoid Helium CooldowD Pressure drops The fIrSt step in performing these calculations was to generate a list of the various

piping sections along with their corresponding lengths and number of elbows tees and

valves Each pipe section was given a number See table 1 for a listing of the solenoid

pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given

pipe sizes and inletexit states The solenoid cooldown piping was fIrSt sized by

assuming a pressure drop of 95 psig an inlet temperature of 200K GHe and an outlet

temperature of 300K through the supply and return lines respectively Resistance

coefficients were calculated for each piping section and for the solenoid Each coefficient

was converted to correspond to an inner diameter of 068 in since the Lds of each

section were not all the same In the second step of the calculation pressure drops were

calculated for each individual pipe section taking into account the change in density due

to changes in pressure Summing the individual pressure drops resulted in a total

pressure drop of 363 psi These numbers are summarized in table 5

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

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b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

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o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

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)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

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FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

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1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

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(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

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-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

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Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

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4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

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bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

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ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

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SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

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-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

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III) c)I 5U~i vI ~o Q

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115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

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-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

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Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

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c A tJ 7 3_64- VII s~

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bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

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At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 32: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

ISTable 5 Solenoid Helium Cooldown piping pressure drop summary

PIPE SECTION

INLET TEMP

(K)

OUfLET TEMP(K)

INLET PRESS (PSIA)

OUfLET PRESS (PSIA)

MASS FLOW (GIS)

RESISTANCE COEFFICIENT (K)

PRESSURE DROP (PSIA)

LINE 27 200 200 1147 11458 7 122 012 LINE 5 200 200 11458 10788 7 19492 67 LINE 6 200 200 10788 10769 7 52 019

SOLENOID 200 300 10769 8609 7 4302 216 LINE 24 300 300 8609 8572 7 544 037 LINE 25 300 300 8572 7961 7 9084 611 LINE 26 300 300 7961 7935 7 341 026

COOLDOWN RETIJRN 300 300 7935 7838 7 13 097

TOTAL DELTAP = 363 psi

It was estimated that using the total acceptable pressure drop of 95 psi 200 K in 300 K out that the maximum cooldown flow rate obtainable would be 113 gfs

Comparison to COF pipe sizes A simple comparison to COFs pipe sizes was made

The calculations are in appendix C The O-Zero solenoid cold mass is one-fourth that of

CDFs The cooldown rate for both solenoids will be the same so O-zero will only need

one-fourth the mass flow rate during cooldown For the same allowable pressure drop at one-fourth the flow the CDF pipe sizes could be reduced by 033 O-Zeros pipe sizes are compared to this number and are found to be larger

Table 6 Comparison to CDF sizes

LINE SECTION dcop 033dcop do-Zero

He supply 100 00 033 0625 00 He return 100 00 33 075 00 LN2 supply 05 00 17 0375 00 N2 return 0625 00 21 0375 00

--~~~~-------------

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

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25 lie SL 20

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b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

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h(7vr 1311~h lN ~ 1054 ~

-k-shy - - = A ATWO 1r (tgt15)(O4~[51))

o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

CaN-IIJfIIO vJ( 1--4 vt P~eAJ(1 of J-II TLJIi AJ ~fe~ AceA

A I) CDEFtIrL~ ib COOItgt()~J A-r (tATamp 0 5 ~A

o7b 10 T I ~ l

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STEP 3

S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

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1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

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Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

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3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

~ 11 LE1 0o-lD)-S vJG ~e~ 771 ADD J(i~ w~ Fc~lJ vf J 50~~r--middotC

-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

- II gtlt 1( SvlfoVlS (2 fi_shyb w - ~PrD IP-t S vPlgto2---fShmiddott

30W 0 7- tz A- I Itt- 0 tv bull I () I( 5 1gt~fINI- pUs 130 w- Cc 15I4J Z 50 o

c A tJ 7 3_64- VII s~

1trcP1 jc ~---)-

rv - bullbull OF FXIEgt~ ( 2S 1 ~ CL- (_~

bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

2 ~ Zgt ~ IV - I (1 Of CH IA IJ amp- - J i_2soeW - l~ or- Ck Nt 13 INIttSq

- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 33: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

Solenoid Helium Steady State Pressure drops G Some preliminary calculations were done to estimate the steady state helium hear

loads flowrates and pressure drops expected for each section of piping See appendices

I J and K The total pressure drop from the tubing sizes were on the order of 32 psi as

shown in the summary table in appendix K page K12 Essentially all this pressure drop

occurred in the long return pipe line 8 The pressure drop was based on line 8 being

a concentric tube with hydraulic radius of 0347 This calculation was never given a

fInal check or revised because it was decided that the cooldown process determined the

required pipe sizes It should be noted that the current size selection (Table I and figure

1) give line 8 a larger hydraulic radius of 0427 Therefore the helium steady state

pipe pressure drops will be negligible

Solenoid Njtrsmen flowrates apd pressure drops The nitrogen flowrate requirements for cooldown and steady state are considered

in calculations in appendix F The maximum pressure drop allowed for the nitrogen

circuit inlet to outlet is 30 psi based on the current storage dewar operating pressure Per

the Solenoid bid spec the required nitrogen cooldown flowrate shall not exceed 5 gjs

With the current selected pipe sizes nitrogen flow will less be than 5 gjs until the return

piping fluid is less than 150 K This means initially we may cannot deliver the full 5 gjs

I feel this is acceptable however The pressure drop for steady state nitrogen

requirements is expected to be less than 1 psi (with control valves full open) See

appendix O

YLPC Helium CooldoWD Dowtates The LHe line sizes for the VLPC were determined by fIrst calculating the required

flow rates during cooldown These calculations are shown in VLPC Cooldown amp Flow

Rates Etc of appendix D and are summarized in Table 7 A cooldown rate of 5 Klhr

was used in these calculations

Table 7 VLPC COOLDOWN FLOW RATES

STEP VLPC TEMP

[K]

GAS TEMP IN[K]

GAS TEMP

OUT[K]

TIME [brs]

MASS FLOW RATEREQD

leis] 1 30000 250 200 250 10 84 2 250 to 200 150 200 10 89 3 20000 150 100 150 10 92 4 100 to 90 80 90 4 31

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

d (-10 ( ~raquo

839qYY --(Motte

25 lie SL 20

~ d51-

7 Sbull 2shy3 2 3 472

- ~

-- ---------- raquo

b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

1 EAIJgtltf lt FR61V tJ L c(Lflc lilA ~K

f~nr - ~- ALVMtJUM

SA 4 2otJ K 6~ oJ I 270 ~ amp-A5 our

h(7vr 1311~h lN ~ 1054 ~

-k-shy - - = A ATWO 1r (tgt15)(O4~[51))

o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

CaN-IIJfIIO vJ( 1--4 vt P~eAJ(1 of J-II TLJIi AJ ~fe~ AceA

A I) CDEFtIrL~ ib COOItgt()~J A-r (tATamp 0 5 ~A

o7b 10 T I ~ l

~tlcIio 60 it S ) ( lOS 5 ~ -q SJf) )l 3 CO os

STEP 3

S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

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k-wlPlf K) ( 0 )~ (0 Ioq~

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3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

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LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

4~ G - -l- 7utc 3 vJ

~ I - 4 3 [ f 3 - 125 I=-t lt A) 100 F-t I -Z S -wshy

-t H 1- -Ofgt D F ~N 5 - 3 Sf ee 5 J 3 4 N4

t O bb W 1 lE

+ 3 UJs-eelt-r- ~N ~4N -r 1 VA-tvE Of--J tGC- --J

1J ccf

qJ Z 5PPt-t AsSvlE 4 SeH Os p(fgtpound

(J5 E 5 U -Tu ~ - Z f WI

III) c)I 5U~i vI ~o Q

~2) ASSUME Pr 5i_qtrT2G5 4- rs- HE-A LOp-pound) 10 E (lADmiddot SMEo

115 W r 1

25 w r I) 12S 1- 05 ~ 1315 32 W 1012S w ~

125 W rsshy II( 12

SEE

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB (tJ (rL7pound)RDDz) Jo ENGINEERING NOTE JfPc t SuI JOltgt 3823 S

NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE

i 0 -z) lt4

- L

---13) -1 ~PE 5r~ )

r) 32 WU---J~~ bull f 01-1 t

II lt-1 -shyI t- r 125 W T I C ltJ -T I 32W 2- 0 D ~ x

J3S IlaquoV gt lt3) C

~

~ 11 LE1 0o-lD)-S vJG ~e~ 771 ADD J(i~ w~ Fc~lJ vf J 50~~r--middotC

-0 SHIfD 11r-~ z vJ t- 718 -+ 2808 ~ 1(31 yJ f seuro~ SAfN ~)t- c -s)

f 2 I) w -+ ITV A IZb vJ

COromiddot-v middotu

~I~) I-I~A1 LP() = ~ I JiP-11V f r R rot or v-7v6f

It1V1i-middotoBvl= 13w

Va - ~eL (2)

VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN

I

324 IZ8vJ - Jf v-7v~ts

- SHrpoundirgt 5TNj)middotO~ )12 vV ) r laquoON D- 1 J

- II gtlt 1( SvlfoVlS (2 fi_shyb w - ~PrD IP-t S vPlgto2---fShmiddott

30W 0 7- tz A- I Itt- 0 tv bull I () I( 5 1gt~fINI- pUs 130 w- Cc 15I4J Z 50 o

c A tJ 7 3_64- VII s~

1trcP1 jc ~---)-

rv - bullbull OF FXIEgt~ ( 2S 1 ~ CL- (_~

bull Gl5 - CA w-(un V A-5V-Lvshy

b 4 - v 1 iJg~S

_ ~ rY_ ~jfPrJ2 w - HI~f() 0 - or-F S

1( 7 - fLIro 11 S) fp ampfl-1i 3 aW - INN pound(l ~ crr~( ~ fJ G i-OS

2 ~ Zgt ~ IV - I (1 Of CH IA IJ amp- - J i_2soeW - l~ or- Ck Nt 13 INIttSq

- 2 lttr

- Car TI~

- IJ l() ec~

At V

SUBJECT

FEAMILAB SECTION

ENGINEERING NOTE 50 LEr-gta D

1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~

ft laquoA1 LOW e tgtNit fib fI bull I ~-c f

PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S

JLPc $Qtfamp~D W33B2~115

NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

S-ATE ltplt-lt$_ I AffG-JOlx _~~~_________LI__

~eI~ p PI ~

7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy

JS

t -= 0 0-5 ]7

I

oo(~r (~)( ~)G~~J-l) ~

jY - ooogt -tL d~

0-shyd3gt- y L~]jOf b~

Re 2 lou dk f~ ~-~J J~ 0010 J

RG ~ Zt1u(gt ( Oo~ ~ f)( O U 0 -~d (O-~) -Lf= 10-t

K2

I 4 I kI -cl k fl ( -9) f cft - 5lJ~Sl - 0 I~r(l

It it 73 I - S it J(~I

X-o ~1 OoS

J ~ I()( 7 1lt-(gt r-1 Zftfq(~-gt

JJ ~ - 10 ~ I 511( tI fA -S

lr Cdey oh~

(1-lt= 30r 4-r c) elb-gt$)

Pz c Jr 1 fl()

lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

Page 34: PIPE SIZING: FOR SOLENOID/VLPC CRYOGENIC SYSTEMS

It was concluded that step 4s pressure drop would be about 36 times larger than step 1so

Therefore the cooldown lines were sized for a flow rate of 31 gls with an inlet temperature of 80K and an outlet temperature of 90K (refer to appendix D)

YLPC Helium Cooldowp Pressure drQPs A list of the various piping sections along with their corresponding lengths and

number of elbows tees and valves Each pipe section was given a number See table 2 for a listing of the VLPC pipe sections

Pressure drops due to friction valves tees bends etc were then calculated for the given pipe sizes and inletexit states The VLPC cooldown piping was fIrst sized by assuming a pressure drop of 95 psig an inlet temperature of 80K OHe and an outlet temperature of 90K through the supply and return lines respectively Resistance coefficients were calculated for four segments of the piping In the second step of the calculation pressure

drops were calculated for each segment taking into account the change in density due to changes in pressure Summing the individual pressure drops resulted in a rough

estimated pressure drop of 591 psi These numbers are summarized in table 8 See Appendix E for the raw calculations

Table 8 VLPC Helium Cooldown piping pressure drop summary

PIPE SECTION PRESSURE DROP (PSIA)

Suoolv line 38 044 West supply lines + VLPC cryostat 274

West return lines 281 Return line 66 32

Total Delta P = 591 psi

YLPC Helium Steady State Pressure drops The expected pressure drop for 38 OD x 0035 wall tubing is less than 01 psi

per 100 feet of tubing See appenix H No further calculations were done

YLPe NjtroBO Oowrates aod pressure drops The nitrogen tube sizes were chosen from a practical size standpoint It is

impractical to go to a size smaller than 38 00 Based on experience with the solenoid

nitrogen calculations I conclude that pressure drop in the VLPC nitrogen piping will be

negligible for the required flowrates No formal calculations were done

19 Table of Contents for the Appendices

Raw Enldoeering Calculatioos

Appendix A Solenoid Cooldown and Flowrates etc

Appendix B Estimated flowrate thru Solenoid cooldown piping and delta P

Appendix C Solenoid pipe size Comparison to CDF

Appendix D Calculation to determine VLPC Cooldown and flow rates required

Appendix E VLPC Piping Total pressure drop in cooldown phase

Appendix F Delta P for Solenoid LN2 transfer line

Appendix G Solenoid transfer line steady state conditions

Appendix H VLPC LHe line sizing for steady state conditions

Appendix I Heat loads for Solenoid amp VLPC transfer lines

Appendix J Steady state heat loads to solenoid transfer line

Appendix K Solenoid steady state cales Helium piping

I

SECTION PROJECT SERIAl-CATEGORY PlloeFEAMILAB

R D I Dcent LMlt IltE~flf ~2~ 115 AIo ENGINEERING NOTE NIIME

SU8JECT APPEJJO A- 50L-eNOID COOIDOvl tV if F=tow Z A 1e S etc OilTE IREVISION Oil TE

I I - l I i PIIgt( 1- C c~uI) amp-f SSo loA 1 11- 1+

14 Co 0 k~_ ~5iIE A LUMJuM (V~(ol fpoundtot-) cr f WE oJ 0 II A

d (-10 ( ~raquo

839qYY --(Motte

25 lie SL 20

~ d51-

7 Sbull 2shy3 2 3 472

- ~

-- ---------- raquo

b bull

bull b 20 50

FERMILAB SECTION

ENGINEERING NOTE SUSJECT

App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc

PROJECT SERIALmiddotCATEGOIIY PAGE

U~ AeFflltIlJ 3823 115 ~ 2 NAME

USs Ruc I 0] S(I DATE IREVISION DATE

II-qmiddot11

raeao

~e p i- 30 I +1J 270 k IN 10 HOWtS

6 HC4tO - At 6h J 4 b 0 1lt [ I 70 1 ~ - I 2 b t ~ 7 [ ~~ ]11

1 EAIJgtltf lt FR61V tJ L c(Lflc lilA ~K

f~nr - ~- ALVMtJUM

SA 4 2otJ K 6~ oJ I 270 ~ amp-A5 our

h(7vr 1311~h lN ~ 1054 ~

-k-shy - - = A ATWO 1r (tgt15)(O4~[51))

o seCTION PROJECT SERIAlmiddotCATEGORY PAGEFERMILAB LJ4e REffeIr A33823115ENGINEERING NOTE

NAME

CATE IREVISION CATE

II-Io-a~

ltdNu p -Jt(

90 ( J3 ~)tJQ kshyh ~ -- - =- 780 ~ d ( Cq~ ) aZS1 I J MZ L

CaN-IIJfIIO vJ( 1--4 vt P~eAJ(1 of J-II TLJIi AJ ~fe~ AceA

A I) CDEFtIrL~ ib COOItgt()~J A-r (tATamp 0 5 ~A

o7b 10 T I ~ l

~tlcIio 60 it S ) ( lOS 5 ~ -q SJf) )l 3 CO os

STEP 3

S Ai (CO c-AS IJ I 0 1( (rA cJ i

k~ - 53 S I l) ~ovr til 1C S lJ~ ~f~7IIO -r CILl_ S~~J~

)Y thp = Qo t1f$) L1Q51- 5 lS ~) (~5) -= t

---

o RDtxgt

FERMILAB

ENGINEERING NOTE seCTION

PROJeCT SERIAl-CATEGORY

LH poundfFtel 38 23 II 5 PAGE

~4 SUBJECT APPEJ DI t

SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE

I 1 - I 0 - Ttj

ReQuleeD MASS = -0 r-J R 1Es A 4E ampOIJC ALOV 6 $AM~ OREL70JAJ ~ME $7pound1gtgt gt1$ g 50ill(Z~5 -00 cCO-AJ

NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS

cRiATt Dva 10 INt~ASeo CaOLDOtlJ RA1e

COIJ$ e- fL VA -1 I vpound AT ()r 6-A5 ~ 50 ItC

I 00 t 70 q0 K bull

Sotpound~O(o 5 M P I 0 ~ I 71 10 k

A 4ltl 4 1-I-1e~ FOtt 1115 So TIP

ALL lJ 13 J] OoOj - t7BS 10 J~Coo 11100 IQ 177(p 7- ZS(i r t~ ltc 0 J J

~A- 80 K GAS oJ J ClfO ~ GA5 QuT

IaJ = 4 31Z ~d- hov-r = 4S3z l~

~SBt)lIOr [Pi ~ YlRe bull - I - B ~ amp

~ Q - ( HlfS1l +~3 2 )6 - 3r+~) 3bQJs ========

Q - ~S ec 10 r s = 4 S7 W 4 HeS II 3amp00 ~

CHeCK c ampJCJ1i~ c~ F CltfAJl

1~ JN(Jo 001 3 Reo P

Re 2 Z 00 ~ o ~

J 1-1 K ( 06ZIa) 0 8 lIit~ )A ~ B5PQ~ =- ooB5 cr ( bull 27~~) (Oill ~ 11o4t)

Re Z~OO [ - -= 8xtC cretiN) (oooeSep)

P b8

SECTION PROJECT SERIAL-CATEGORY PAGEFERMILAB

Ue ~fltI6l 3823 (5 A5o ENGINEERING NOTE NAMESUBJpoundCT ADPampJfh)( A

Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI

1-10 -ltt-l

0 ~ C 0=5 w~o2gt (SloI)(OZSif ~11)

111 PIlL s-rtfgt 5 vvE HAVpound (J Ui-l7Y fJI 1-IpoundIltr

A LeA pN () i(JV V E c-r I CN Coe I C -41 r F6trshy

A

---- WE lJEeD 70 ~ze alol-lgtO(VN -IIJpoundlt fQt A CcE1A8(shy

AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11

J

~NP 7= q ~~

1 -= 80 t IJ ) 100 Ilt oiJi [1poundP 5 J

bull f) fA~ jJIJ( W~(ampl ttP I ampamp 8~ ( f41f S1

o shy+ L Wl Z

6P 0( ~~ampJ S-

~I W J bull Sltsad shy

AP161 ~W~ ~I -f = O~

= S h-rt5Ul

~Ps~- (O(1)7 ( 018) -- -APS~ 1 Olamp (q)1 ( 018

w Tt- ) - 200 K

ACe

SPECDIC BEAT ENlJIALPY of ALUMINUM

Sources of Data

G1auque W F and Meade P F J Am Chem Soc El 1897-1901 (1941) Maler C G and Anderaon C T J Chem Phys 2 513-27 (1934) Phlllip_ ll E Lov Temperature PhyB1cs and ChemI_trc UDiv W1scons1n Press (1958)

Other Hererences

Belm U AIm Physik Beib11ltter 2 178 (1901) Goodman B B Compt rend ~44 2899 (1957) Gr1rtiths l E G and Gr1ttithS-E Phil Trans Boy Soc London~ 557 (1914) Kolt J A and Keesom W H Phys1cs ~ 835 (1937) Koret F AIm Physlk (4) Jsect 49 (1911) llerut W AnD Physik (4) Jsect 395 (1911) llerut W and Lindemann F A Z Elektrochem 17 817 (1911) llerut W and Schven F Sltzber kgl preus_Akad Wias 355 (1914) R1cbards T W and Jackson F G Z physik Chell 70 414 (1910) Schmitz B E Proc Boy Soc (London) 72 177 (19031 TUdeD w A Proc Boy Soc (London) tr 220 (1903)

Table ot Selected Values

Temp OK JpoK

H

JfJII

1 0000 10 1 000 051 0000 025 2 000 108 000 105 3 000 176 000 246

4 000 261 000 463 6 000 50 001 21 8 000 88 002 6

10 001 4 004 9

15 004 0 018 20 008 9 048 25 017 5 112 30 031 5 232

35 051 5 436 middot140 077 5 755 50 142 185

Temp OK

Cp Jp_oK

H

JfJII

60 0214 364 70 287 615 80 middot357 937 90 422 1325

100 481 1776 120 580 284 llMl 654 lMl7 1(0 713 544

180 760 692 200 797 848 220 826 1010 2lMl 849 1178

260 869 1350 280 886 152middot5 300 902 1704

Supereonduct1ng

Reprinted from WADD TECH REPORT 60-56

VIII-A-l

r FERMILABA va ENGINEERING NOTE

SECTION SERIALmiddotCATllGORY PAGE

61 SUBJECT shy

e-X~Allip rwJ ~TE 71tpoundL

c~IIDO (tO~AJ ~PltJr l He) ( ~ f- I

IDATE REVISION DATE

- f- 95

K=- 30~ ~ Cfomiddot e Ibow~ (~J-l~)

COCXOCJRtlIAV) 11)(

r -) (ttF~t4 (

( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)

~ --zo~ ~ Te ~ 41tfll Qv~ (PJ A middotZf)

k - b11 d~ ------4gt VQl~~ I ~1ft(IA1 ~ (efJ -z11o ttE-IfCJlA-N~J lCt)l Q

~~ kgt(~yt ---) Cotuu~iw J- K be be0A dJ~(elA-t die-MIller rtid C-~ ~-s)

fOuT bull OOl-cPmiddot

~E IN -= Z2~1ishy Z2l00 (02lt5)( O1- 1~~O --- t= QOZ-t

(aO5) ( 0100)

I(WDlTl ZZ=roO (LIt0(C OIl) ~ 3150

(0 I 01) ( a 0 )

SECTION

lWjocent 38l~ HS FERMILAB

ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE

SUBJECT

E JIIftIIIEI) 0 KATeuro 7 mev(

~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE

-7middot S

011 df (

1

120 (0 ott) ~ 8lt1 ( O 081)

l -=shy Ifamp f4) 12 ~r bOvgtI) d= 0 c t i CcLt f-euro 1) Lshy 11ltamp f-I) 2shy vo-Iv~~ Cv=3~) d= O5iI~ (Sb~~oJ) L ~ ~ I +t) d 7 083 i (~u bcoo Qr)

kc ~ ~ fshy 12 ( gto) 00 zs (~~J + 12 (~) Co Oz~ 1_

(

K~IOiOI tfCo4- rr +-ampt 2q1~

~

A SECTION PROJECT SERIAl-CA rEOORY PAGEFERMILAB )cent vf(I~)E ~al~middotS12J)~centV ENGINEERING NOTE 12gt3

SUBJECL

e~l4~ -7vN R~ 7 ~ NAME

5n~ S1kJf1 c~~ - CATE REVISION CATE I~tVol~ GclDvwIII v(P1tV( (14c ) ~ 6)

1-1175

-25 G2ri I 0 Co ~ 9081 IOCl)

kl~~ ~ ~ (DO~~) l~l~l) ~f~1

k-wlPlf K) ( 0 )~ (0 Ioq~

I

o SEAIAImiddotCATEGQAv PGEFERMIlA8

3823 1 5 BIENGINEERING NOTE SUBJECT

Cs7ltf1HlT) t-lOW e~n T hICJ(

swNOIJ) (ltX1U~N YIPIN I 1f1e) ~ Ij

tt3k~ ICft12 b ~ D (it IS

6- 3 2 (Iqqz)( 02)( 03) -

oc~i

~ II1 O ~ - o oS O - S Ho f ( o TtS 1-1~c) 2 00 tc) yenIf I 0 IfJ +-~

i_5(2-1 r~ ( Jzt ( 3f~3gt 01 ftJ~

(it 1tf~J I uO 05 J cent )

~ifo - 3lt2( 51(0 4-) (O~t) OmiddotJ1 fgta () ~If

LII-E

r-

t~Y$ 3toz(3t)1 )(OOit)( 019 ) - IC r=-id Ocif

o PROJeCT SERIAI-cATEGORY PAGEFERMI LAB

7JrI ultI2fI)shy 3B23middot S B5ENGINEERING NOTE

kz1 -= S 11 0 ( 300 k 05 j 11a)

o~( 1 ~~ )( 22) C 3 flgts D ~ S 01 I CDgt

~ Pl 3 - (s 11) ( a 051) (0 u) o ~ e1 ocS-1 f)

~~r 3 lt Z (0 iC1 ) ( () (581) ( 0 2JpL) ~ f) 8 1

IREVISION DATEDATE

-17-95

AD _ 3 lt2 (3 10 ( 0 cst) ( OUJ lt-) U 2lt shy

O j 8 Of

motlr ~ 0051 4

AV~ 3102 (I~) ( 00$1) (OZ7) Qt ell~ amptOif

tR f11tc b 3 f~J I ~ LeS gt ~ IITJrnv-It75LiT Ik~ tiF cPt lex)

PP~ s~ frte c~ M~ VlL (5 C7~ 7ifr9rJ 10 ~6 Pr~pTI~ rhttllAJ 6P~ wz JIK Eill

N - w~ fAPI = +0 Jis 95 III ~~6 ~ 3-32

o seCTIONFERMILAB

ENGINEERING NOTE NAMESUBJeCT

Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~

3-1gQS

8e A ssUIVeuro D - T co Q 1-pound)0 ru r-J FIll- cCS ~ A - ~ lt)

CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~

U51i~1) - 0 TAIltS A coMPAP-A6LE loooC- A -ri-C

SI2-eS 1iS(() rota CCF Af-)C 1~5~ c~SEl F=otL ucent

Ac~lI( C-DoCOWt-J FtOIltl iZAT=~ A ~e

-ri-trElMjIIllr c utO ~A~S bull

II

b~ CCSlev aroL7 Tal-f ) TLo - 19 S

fr6crgt ~- aQC-- tftCND 1)11 A

F__ ~ C(lA-Je 1~ IJI~ eM amp0

-T L wz 6P bL l d I

Co ~P~l tV V -rt-6

~ OS ~L

14- ~gt T~A-)-r~ -~~ t=co (1 p e F-ott cent va I e E 14 AlKSS bull~ ~fSIO (ampo(L C b ~ S 1(1 C t1

dIt

- d-P~ [[~r- (I)J

bull (3 3) d I-

bullbull

PROJECT SERlAl-CATEGOAV PAGEFERMILAB Up(~

IcNS~ Ltloit 3Bz3 S C2o ENGINEERING NOTE SUBJECT

OATE JAEVISION DATE

3-15-1S

33 dco r- prJO p c-c Dltigt D (A cIltIIZlt

A -E I -r ~ -rA amp - E ~ e LOu

LINe )~no

_He S~L--

---- He ~ET~1lN

I--l sw polll1

LNZ 1te1U It tJ

dcDf

II

IDO 0 1)

IODOD

7 0 0 0

bZS OD

33d coT

33

3~

1

21 M

d Dcent

It

102S OP

OSlf PA1c GQQ~J1 4viItJ (IJ

5-01 STA1e R~-rvltJ

ismiddotOD- 1ft

375 00 1 D ttM~~c -z 375 00

CAN ~ Ito M T~ AampN T)oc~) -4 E

PIPE-- S I -zES 1Sxc~eO -r~e Co~~A~~

c~F So Z E N r C ~ ~-r I 0 E t) O-l -r1- ~ 15trS~

OF 11~ 4shy 0 Pc -shy O-rH-E=-A p~~E~ MeoF

BEI~G Ea UA(I-

PAGEA V

FERMI LAB

ENGINEERING NOTE SECTION PROJECT

3823 f( Dishy

-

Xgt 0 011 ~ rYICljM-4Jshy

~1)c (t-qOG kU~~)( 0 blqb ~) -- ltIi 5 31 IV

L COffltl Pgtlvc Ilt ------ji ~Tccll

A G - ( omiddot oz1 W l ( -Ii C~gt~)

tf C~~)

amp 135~ ~t

o

SECTION PROJECT SEtIALmiddotCATEGORY PAGEFERMI LAB ~l)

D1f)t6ENGINEERING NOTE SUBJECT

DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy

c ~J(E9 17-1-1 R t Co ~SI(1

1shy

2BgtW

_ ~~~W

It - 1051 J ~Qul- ~N j -Z 180

rA ~d - Z 1)5 O~ 084 7~ amp -z (lt) 1 _ 2gte-

hf~~d -- AIf] (G-lVPC -l~ ( Ffc~ G- z~w - A 6T lt--O2t5b) I So~)

1pound P tIAJuI)

Doz~ ee~

KEb - 22loO M fid

(i) 22100 (OOcqJ( O02=J)

(dCJI )( O~TS)

A V

SUBJECT

FERMllAB

ENGINEERING NOTE PROJECT SERIALmiddotCATEGOFW PAGE

VLt

NAME -shy

lt5J2---E ~PK_(9 DATE j ~EVSION OA TE

-ltl-17 ~ -2b-~S RN2shy

CE4ampO IZN 72 bull ~ J~ I t

( 7 ) k7 Q r - 12 1 J i-=t5 ( 2 kJ

~ ( -1( _1lt )(SOk ~ Z~991 kJ v

(1-15102 +- Z~9I)k- ( ~ ) +-Ie ~ 3100gt

h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~

(055 -173i ~

t~ to2shy- IN bt =- ~IW ISgtf3 1tI-Ic

( 0 z yen) -) (3i)Ilt ) -

b~ l D ~~ a~)l O~)l z~o~~ ) - o o~ -fSgt

1 ~ T(~gt Z2T-oO (~o1)loos-) i~~1sS

(001) ( o r)

1s c t NVlI)= (0()2)) (1~~5) COCo) z-b1S

amp h = C~15)( OII~) _ 3~i M~-k )j MJ oa (LCV bull 1 9~ -r fJ bull ~q 1J

N -1 t~eo middoti~J

( 0 ~1-5~) ( o OZ-51 wyylt-J

SECTIONft FERMILA8

V ENGINEERING NOTE SUBJECT

PIlOJECT SERIALmiddotCATEGOIlY PAGE

3823 1( 5 NAME

5C-u-v ~Cu4

C -IC( rar) I zq I rz rlt1It lt1lt

shy

It z l~o9 kj6 JJ5S~~ 35 ~ - XSc ~) - v

S~ 25 Z381 N d-QT~ ( 1411 ~ -r 21JOfgt - V -+- 2~W - 2A~ IV( 3(pov)10 bK

100 k ( I-c ISU kI I

k~ 535 I ~~ Out 793 v3 2 3fgt shy

~ (11amp - c(~ 1gt - OQZ1

(K~ - S~SII) J _ 23~q

A (ft 2)(~ ltV -

(o2rnrl)( 50-)

~ eG- ZZToU (0 o~)( 0 O~~)- 1003b

(0011 ) lt o ~rs)

ill IIS D bull ~

AJO(O02~)(foo~8) (0lt) = 323

- X ( ~) ~-lnil-- it - 3z ~ J 008( tn-Ie- _ 2n c M1_1I

(0 ~5A(oQsLf 1Vl2)

SECTION PROJECT SERIAlmiddotCATEGORY P4GEFEAMILA8 (1)

362 3 II 5 D 5DcentENGINEERING NOTE SUBJECT NAME _

5 RI-E 5 -iLa shyDATE lEVSIOl( DATEr tLcJlJ

I - 2Z -91 amp-2b -is ~ C l-4~ z-ffdL K- R R I C lt 1-1

00 Ilt ae 25 (r

k=shy~ S7 1 d ( 0 amp - f l) lt-i = G2 3gt ~ k-shy

(J53tt~(212 _-)(01lt) 3111shy

1513Z~2 Z-S

(b23lI + ~1gt1) k ( yen ) + -IKw 11~11-W 1 ~ 3(o()~

$50 1lt ( I~ c )

- - 4 ~I ~ v ~ h(Jllt - h 3 l 1 157~ 3l)~~ A

~r~bJ ~ Iigt61- 7j- J~ (L)

( Irl2- -I~t)~ 151 3

~rlltd 12)t W ~ 1011 ic

D (0 l H-1lID Ie)

S f t - 2 L l~~ ~ - (~zJt)X ()o11 I~)( )IOaV--1 shy

Oqb Qel) Zz rOO (O~ltis)( 6 Otl ~ 3~j3

((fod) Co 1-s)

shy

ofb C3

~ (SZ lt) d 0(( ~)-= SJt ~_Ilt (tJ3t51~(D0291 l

V A SECTION PROJECT SERIAL CATEGORY PAGEFERMI LAB

Ki-j 38Z3 115 D~ i) i4ENGINEERING NOTE VL~ NAMESUBJECT

SJYE SCU-1

C 1-1( Cta() I L

7l f2 lt1 ltV lt1lt4J

-e T~ 22poundk

J (J -f) jH~

I ~S k ) 111 iltVS ~

13 If r WL~ (oo~)( O~C)( 111)i I I1 _=

( 60ZJ ( )l( O1~) 31

I

I bull

( ON C(t)S 10)

f~5 -poundr ~r1 Claquo(ctekb~ -==-fc k ) 90 K 0cA f

Pru (ItLC((fi17~N5 wt12 ~ PeL C~Yo~rnr f5fJSS

bull

SPECIFIC EEAT EN1~Y of COPPER

(10 0 to 300 OK)

Sources of Octa

Do~kery 5 M Cen J R~search A 59-66 (1937)

Ac-e S end Kards E J Che1 Soc Japan 62 312-15 (1941) =~-l U 1rn oysik u Chell1 (3) 66 237-44 (1598)

-3-cscn H L Clisholm H M eld Docerty S M Con J ReSearch sect 252-303 (1933) Uen A ald ~erth H Z anorg allgell1 Coell 188 Sclenck Fcst shysc~ri~t 1~2-72 (1930) Gi-que W F and lmiddot~esds P F J Am Chell Soc 03 lS97-901 (1941) Keesom W H and Onnes H K Co~s Fnys Lab Univ Leidel No 147a 3 (1915) Koref F k~ Foysik ~ 49-73 (19~)

rie-nst w S1tzber kgl preuss Akad Wiss 262 (1910) ernst W 51tber kgl preuss Akad Wiss 306 (19~)

iierlst W and L1nderampln F AmiddotZ Elektrochem 17 817 (19~)

Schimpff H Z phj~ik Chem 71 257 (1910)

Table ot Selected Values

Temp

lC

10 15 20 25

30 40 50 60

70 ao 90

Cp -- OK

fool -

0000 86 0027 001 7 016

021

060

099

137

173

205

232

11

Jp

00024 0101 034 middot090

195

61 140 258

413 602 822

Temp

lC

100 l20 140 160

lao 200 220 240

260 2ao 300

Cp r- u l

0254 288 313 332

346

356

364

371

376

381

386

11

Jem 106 161 221 285

353 424 496 569

644 720 796

Reprinted -on ~o) TECH REORT 60-36

VIII-B-4

FERMILAS

ENGINEERING NOTE F SUBJECT

I~ 3gt8 ~ bGgt fN huve fiCiN vckltgt or 62 14 becav~ ~Iow ) srlif vtto Eaiw~+ vut III1elt

( te fet fo cL~ 36 Z 3 - II S - H~ - 31121 3 ~ 2 I) ~ ~) VrelAeuro clr()~ (Cccu[u-tlV) ~JII be ~f-poundY~J -poundr o~kr ~tOQ

D~ fu Vl c l~lt (fcs+ k)~~f) ~I~p- bo tfil hAve rWieJ t V~+l )b( vd gt I C(VI d ~ v~ cot-~tt~

VU)( ~rr-JiM ll~ ~ct+t ~ 64

E Il-lc w gt ~ s_tt1

fl~~IIM Au fll6e ~11es JIS dtgt)( Qqq VJshy

bull 2 7 1

028

---_ --- shy

-UIC I~ 441 6V )

116 384 490 574 680 975 609 654 i) ) Armco

(997S~ pure) 7870 447 727 207 956 806 651 531 422 323 287 314 215 384 490 574 680 975 609 654

Carbon steels 7854 434 6OS 171 567 480 392 300Plain carbon

__ (Mn Silt 487 559 685 1169

Si OIIt) 7832 434 639 188 581 4118 392 3U

487 559 685 1168 AlSI1010

149 498 440 374 293Carbon- silicon 7817 446 519 501 582 699 971(Mn sIlt

Ollt lt Si 06~)

8131 434 4LO 116 422 397 350 276 487 559 685 1090

Carbon- manganeseshysilicon (l~ lt Mn 16S~ 01 lt Si s 061raquo

JCr- JMo- Si 7822 444 377 109 3K2 367 333 269 (018 C 065 Cr 492 575 688 969 023 Mo 061gt Si)

I Cr-Mo 7858 442 423 122 420 391 345 214 (016 CI Cr 492 575 688 969 054 Mo 0391gt Si)

1 Cr-V 7836 443 489 141 468 421 363 2112 (021gt C 1021gt Cr 492 575 688 969 0151gt V)

Stainless steels AISl102 8055 480 is1 391 173 200 228 254

512 559 58S 606 AISI304 1670 7900 477 149 395 92 126 166 198 226 254 280 317

272 402 515 557 582 611 640 682 t-ISl 316 8238 468 134 348 152 183 2Ll 242

504 550 576 602 AISI347 7978 480 142 311 158 189 219 241 ~

513 559 585 606 1 Lead 601 11340 129 353 241 397 367 340 314

11

~ Mqnesium 923 1740 1024 156 816

118

169

125

1S9

132

153

142

149 146 )0

Molybdenum

Nickel Pure

2894

1128

10240

8900

2S1

444

138

907

537

230

649

179 141

164

934

143 224

107

1074

134 261

802

1170

126 275

656

1267

118 285

676

112 295

718

105 308

762

98 330

826

90 380

86 459 Ir

I 232 383 485 592 530 562 594 616 0

Nichrome (80pound Ni 201gt Cr)

1672 8400 420 12 34 14 480

16 525

21 545

a 1

lnoonel X-1SO 1665 8510 439 117 3l 87 103 135 170 205 240 276 310 ~

(73 NiISIgt Cr a 611gt Fe)

Niobium 2741 8570 265 537 236 552 188

372

526 249

473

552 274

510

582 2113

546

613 292

626

644 301

675 310

72 I 324

79 I 341

~ e ii

Palladium 1821 12020 244 718 245 765 716 736 797 869 942 102 110 ~ Platinum

Pure 2045 21450 133 716 251

168

775 100

227

726 125

251

7l8 136

261

732 141

271

756 146

281

787 152

291

826 157

307

895 165

994 179

tj J)

FERMI LABIt V ENGINEERING NOTE

SUBJECT

1( SCi I c1f ( cjil

SECTION

~DJDcent PlOJECT

LPC RJo SftlL I) E$

SElIALCATEGORY

R~ Co 2-cdJ

L sf+ 1 01f1 -tltJ b e 10 bull 102

klt r~ + 2(~O~) ~ 0 024(2-) +shy deg[0024) -(7 00z1 d bull tilt

( bull Zo1 lt

KJ 502 40~)middot ~5

---WE~T Vtic suPfc- -E_S - 40 4f2f3- -1-1 SVLPC

L- -= 2 -t I Z IL +4-7 2 -+ Ie 2 Z~

t 00-lt k ~ O Oc (_-21 J- 2 S 2 1 --r (+10 e1bs)- 14- 11 Z+ G+ 2 +shy 6 3S

t I=C

PAGE

) EfL1~~ ~tgtJc J c 0

S1 (~)-7)

-z~2 -+- 21 b + 1 ft ze 4

A SECTION PROJECT SERIALmiddotCATEGORY PAGEFERMIlA8 VI-Pc 3

TJUgt oJ ltF rcA -IC 823 r-) E3V ENGINEERING NOTE

NAME

V-PC PIP r~( ~C~~-IIJ Dus~ KWCfoJS-

L-ra -= 2 tf + 4 -+- IZ+- I z3 + Z = lOe ~

- (ZO~)-t bull o-ze K -f D C26 oz

Ke 20 ( a 0)( 029) = 1(0middot8

1 _ - 70 ( 0 -z i) I I 11tl- - ampshy

VAlt-es ~ I Crrrut -I--3e G 10) I )lvE~ VMJe oC S 0 ) I C1olEC1oL JA(ue

i 641 (Uca )44 eLl1 CLf- + 100 (OZS) S e + l za 15

Ks ( ZO )1 -+ (ffO)

~ I t Ie + 11 + 31 9lt ~c

1lt 502 Olgtr

V A PROJECT SERIAL-CATEGORY PAGEFERMILAB -J-Pc

~I JltF6L 3823 liSENGINEERING NOTE E4I bullbullC NAMESUBJECT

PIP IIJ P 1l5S R uc iJ S r DATE REVISION DAEI

3-23-15

-shy 11(WeST VtJC (2pound r iJ 4 N

~ 31 ~s I~ - 5 ll f-- - =shy yt1 ~

100deg8 gtt

T hL3~ F 75 f

7lt-rT(JLV LII~ bb

- -t3 2OC -Pi5 ~ bull 0+ 3 5-om bull 3 I 5 SIII

bP ~ 3 b7 (501) Cmiddot oY 1 )(311 -t~ ) -II LL9g 3 Z ~

l~Ol)~ ----- f~

Su(Vlt~ ~p

LINE 3B S LJlPL( 0 1 F~~

Suppl~ Lt)E + VLPC 2 f (St 12tvIVJ La J__ 2S1 p tINt b~ UiJJIiAJ 32 lt

Sq I[AP_ f S ]

bull

r---------------~~~~~----------~~~------~~~~----~__----------~------A FER MIL A B SECTION PROJECT SERIAlCATEGORV PAGE

V ENGINEERING NOTE RDDcent CiNO UT1ampJrlE~ 382 3 I c FI NAME

Russ R 0C I r0S-

DATE REVISION DATE

1-2+-CfS

SUBJECT

FrzoN- ~- Bligt SiEC~ICAuJ ) N 2 f1oQI ~A1e rA~ JOshy

5 j)s As A vvOIl-S- e A SE ~ IN II - cALCV( A 1t -rH r

IV PP I J u (i) -6 ~00

0 - 1 ---P 12 -- 13 ~ 1-( - ~S) 10 - I I ~ l- Ilt 5 ( I~S4tP)

CAl C lor alS 111 8( o OfoJ E Oc -ri-4 Co ~PP((0 j~()M -1 e L Z t-l~A-Oet Tb riotpound SO-~dO TH=- 62-E-rv(L

~LOw P~-r1-4 Ie I D Gr~ T I - A I- IN -r ILC (510 1Irct) To PIP $1pound

p)J) cJ err H S A-t 1-6 OJEoe AP w-- ali C AJ 6E l)s~o AT ~ 0 J ~ Lcl c AIUE~ AJO IJ ~a ~amp rJ 0 11) bull -

r NIl-I u-rfZ- r pound C 1gt4A1tT II FIA~ IF 1 11+1CD~t-I SH 4Q

~ I Ei eo P de 6 Bmiddot S J

(AAJ1o -rr~ 11 PA-lfAJIt 410 ~

~NI~I 5 ~S ~

11 Ity ~ ~ ~ IS lit

L- e 10 J

l- I eo -0shy II

L E laquoshy I t

10 F-I J

5 ~

2 Lt F-i

430 0 J

FERMI LAB SECTION PROJECT SERIALmiddotCATEGORY

ENGINEERING NOTE IltD IOcent Cil Yo (jr11-l1lffS

SUBJECT

6P Figt~ SQI-EIJ Olt) L~2 r~~ N I fltfi (Igteuro DATE IFlEVISJON DATE

1-24-95

511f f~

~POOI I 3 3 f~I~SGllt ~o

jd 3 bt II

A

2 _Z B pSt foflt q 3 sJN

middotr(ampfS~f -tbSsdt1o

middot-shy

A-~ ~ CO~OJ eoS T) at MIrfpound PbIL wtIIIJ~ PtL6~SV~ 30 p~

-r ~ ca I~ fQn S p i _ I S IS(R)

_ (276 psi)C3oSi- = S4 flt Fo(C- Q3 s-f_ 6Pl)o 41

) Itgt - (1 S pS) ( I I ~ 0 )

30 fS

lt 5 e j gt F~e

811 fo I 00 flr~ Ofl- p ~

LPOD I -= bull 277 Igt ce I 0 f~

e 0 fLtiLIitJ( FO iL P II~~ j

APoo l II 200 r si1middot110 30 fft

1-gt ~ A jI-IJcbpr-w- o=~5 f~J1)~II2-3 ~ D It v5J I 0 S J1j JfO O ~

30 ~gtit

V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt

cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME

Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I

I Z J- I 5

SUBJECT

1HS

SotIE-LDS 8 1J1~1t-crP-r5 coOL TZgt Tto-f PO bull Jshy

-1 A -

-r ~ 4 V~~ (L e 7vAJ T p1tJ Z=- 5

I 5 ~ J 5 1 S W _- - bull -r i3 Co

to p 0 I ~ A PPtto )I 2f I lVA- 1sSAIS- tJJ Z- l- liA- -rlJ s~ -I H1pound f (fA- 1~ ) ~5 I ~fV fleP 0 ta

) 0middot 1 ltD ~~c Q ) -111 g

1000cc ~ 11iL L I I~ )1 5 ~ 1~ )L I L )or 710 ~( ~S

l4~ B~fV CLMI Q~ ( I

I S S~M~ ---~ 18)

~~~ d 1middotmiddotI~

=

V A

SECTION PAGEFERMI LAB

F4ENGINEERING NOTE NAMESUBJECT

OATE I~ REVISION DATE 1-2-75

PPIJU

~ ~ 50 t 5

FQ~ Je-J i (tf- 1tJ Pt PI( (i= f1I~ f II -z)

6~ ~lfI-l (35(11) z 3 f-~1r

10 I I ~ ~ Itt ~2 S lS J 3oa

30 (S -J~

-

o 2 y)shy

)( -Fett- -liamp~

A ~() 5-r6-1(tJ ~

~_ 1-1( q S jZampt ( So ~middot 10 11--A~ rc -(ii ~tC~ ~Ipound lOOIO~S I( CPltr-cII_-rlQIs ~

(

It V

FERMILAB

ENGINEERING NOTE SECTION

I2D ID~ PROJECT CItlaquogt l)1LT cS

SEIIALmiddotCA TEGORY

3823(1) PAGE

GI

SUSJEcr

So~eNOICgt TIA ~+e-Ilt -I t--J a NAME

1rpo S-rAte 0gtJO 7 o~ ~ OA TE

1-lb-95 IREVIS10 OA TE

~ W 1-shy

II oilI r5j o() Qtq ~ -ru8t Ii I -jMIfJ ) QP= 03 F-L

-= 40 9~]I I 50$ 2fIIt(V-Ob ~4J gt

~IS CotJIlAOJJ 5ufPl~ PIE r

IV It LE IT IlL 1 00 ]I O~5 w~

r=-Q~ t1~EgtSo A-ra (~ ccUI --JAr4amp~

S It I~O) IX 12 Z middotSot ~S 1-t-JTc6P1 ~ l-t I bull 4b 9~

PRESSURE DROP CURVES

The following curves may be helpful in determinshying the proper line size for your transfer requireshyment These charts represent loss of pressure due to fluid flow through a pipe Total pressure drop also includes additional loss of pressure (head) due to any increase in elevation

Please notice that a smaller diameter rigid pipe line can accommodate the same flow capacity as a larger diameter flex line This is signficant when considering heat-leak (liquid loss) and system purchase cost

LIQUID NITROGEN Pressure Drop Due to Fluid Flow Rigid Piping --- Flexible Piping ----shy

~ 10004middot ~ ~ $ 6 If 2 3 s 6 119 --r shy 2 3 1I 2 I 3 5 6 7ft

bull oS

2

r- shy -- shy rshy -shy

I

100

I

i

- shy

I

I I i

i f

~Vl~10 j

Lshy

I

i

2 ~

I

~

-

i I I

II i I

i I illI

I I II I

10shy I ~

V

- I ~ ii

V jp ~

~

~ Iojoo

-~ 10-- oloshy

$$Hfi

Y shy~ V I

III ~fO Jo I TIl

11~ V Ibull itoftl fO rD I ~ J ~ t~

Il ~fO

~ ft Qshy ~ ~fO~ b ~ tf1 ~ -tt L

io- k~ l dIi~~ t

V I r ~~~r ~fO ~ V

~ ~~ri V Q~ ~

V Wi gtr ~~ ~1~ ~r itoIl ~

~-lt shy I ll~ t----~ J

-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V

jp Ili-shy ~~rmiddot

J ~ 100- 10 ~V rt 1 lorshy

2 3 S 91 2 3 A S 6791 2 3 S 67 2 791 2 3 A 67

J 5

2

I r 6 5 3

2

Jbulls bull

2

000001 00001 0001 01 10

PRUSUAE LOSS DUETO FWIDFLOW PSIIFOOT

48

Each piping section undergoes helium mass spectrometer testing (1 X1 o-e CClsec sensitivity) followed by a seven day vacuum retention test to ensure the vacuum integrity prior to shipment

A SECTION PROJECT SERIAL CATEGORY PAGEFERMILAB

V ENGINEERING NOTE SUBJECT NAME

Rusgt R IJ c I-J S -ILPc DATE REVISION DATEI

f- 2= - q5

COIoJS~eR ~-r~tgt V -P e e-e 1 lt) So T A -r S bull

IlJ 50 IE 0 II) DE I CaJ rec~c jL-r QiOrA1- - 270 vJ ) IJ 41 (7101

L ~ bull Po C II- fL cJ GsT I M r- __ S A 2E 70J Ppound__ ~Q~

4fltD ffI2-H-APS Itr-J ~OO I TOv~ 4u uJ Faa -r~ t-JSrfjIL UNE S

f -J MPEfJ QfA-1 I = SO

Q ~i 2 -0 w

Yf - ) -l 8 ~q ~sH b- 4S 35 ~ - 1-129 ~

t (f bull 2MIi 1-= bsf ( ~A-r -avo) O1L~ N~ I

C ALCcJ-Aj~ FOtt- rh-=- 43595 -=5 - ) p PIamp00 -

bull 00435 IS

I cto J _ ~ -F(3

I 03 5 ~ I 0 S -5 ) Z

S)(71135) 11cf-rt3)(JOID ~s)-= 6P =3amp2 (

00 - ( 30 5 ~ ) ~

SECTION SERIALmiddotCATEGORY PAGEFERMILABo ENGINEERING NOTE SUBJECT NAME ~ rlt u ~ gt - _~ I j-

DATE jREVIS10N DATE i Cl - I - ~-l-

L~e U-TUES ~

Peurof ~1c~-r

tV J 34~2 gt_~o)~) 47 vJp-- ~J-

1 00-00 w fy)S-S 3 ~ eJshy ~ 0 =5 yenHtlt ~ 3+ ~ iS

SA1ELt- 1i Ii euro p oe5 -1 (

--J~ ~ ~

~ ~IZe S -zeuro

~

~

14 w f156 vV

14 5ze 14 w

---------------------------------------------------shy

use

I 9 WATT

I -I ITT 5 )

( I )

(i 0)

(15)

I gt yJ

3 vJ 3hW 4 vJ

I 1

U -TuBE gt 4~ 11 ) 34 SZS

3 B w) L 3~ s~

IS u--ruf~ =gt 53 W gt

3 II -2

ishy 34 i 5-ZC43 wi I tJ c L V ~ 8 A1O t-lE Etl Dj

A V

SUBJECT

L~e

FEAMILA8 SECTiON

ENGINEERING NOTE i()Dcent

[ lJ SE

PROJECT

ct~o J~-I~5

~)(At 1lt NAME

j -(--

SERIAlmiddotCATEGORY

~ ~~ -- ~-~

PAGE

-1_

DATE REVISION DATE ic - 17- -14

AS-SVME 118 -I OD X 0028 JA-IL -rU8INamp 5 lt1lt

AsSilM~ 12( DF LeN(rrH l3ef=orc 761J( Ie 5vt-IK -J LJ SKI~ z

Q L

bull OO~ W 1UiC l~ (v-t06-E

l I 5 ~ - S

A SECTION PAGEFERMILAB

13V ENGINEERING NOTE NAMESUBJECT

thJ5 tlt li ~ ~ 5 lt

S I U-TUe~ - 28 VI

10 I U -TIIB=- ~ 32 vV I S I u-TJ6E --7 3b W

H tA( UcA-~

0p-r-rgtrt)

3~middotoo

o oct 0101 CT11 10111 o 70

Pepound A vS -as D SIVmiddot 3lf- -+ CHIMVf( i-Jb--r l(JpO CALC

d

3 0 D - 3 11o bb W ----- O hb W ( 8 Bb)= f) 7 e VJ 30bO

FoP- SP 5 J Eft- cv

14 NAMESUBJECT

ltwltlt R~ -H~l LoADS ~Or 5D-EJgtigt 1- V L Pc

DATE IREVISION DATE -rrt A ) S ~ Ii(L t- -l e s I bull I e - 1

SECTION PROJECT SERIAlmiddotCA TEGOFlY PAGEFERMILAB ~e(u gt1 ~-rco ENGINEERING NOTE ltClJ-JJIIC J VUe 363 II

I ~ cJo 5 W 7

o SECTION PROJECT SERIAlCATEGORY PAGEFEFlMILAB RJJ )- 5

I2C()5 JIENGINEERING NOTE Vd)c e 5- ollj

NAMESUBJECT

Ru Co I NS -ST~AO S-rAf ( H EAT I-oAO S OA TE REVISION OA TEI--ri) S( c-oJ 0 I 0 ~ o-J So ~GI2- LIN e

10 - 2 () - 91

1 4- 3 Af

L- - g1 1

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NAME

RwSS DATE REVISION DATE IO-2I-qy

Sgt~ I) Steo1lf

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lt

K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe

valid accurate model validity

flow turbulen flow type f 01620391 friction factor Must enter a guess

000005 epsilon ft pipe roughness

62 D in Pipe inside diameter 5 L ft Length of pipe

A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot

ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase

deltaP 00556327 psig Total pressure drop for the pipe

phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter

25 m L-M constant Look up in Table 719

2 n L-M constanti Look up in Table 719

316 CG L-M constanti Look up in Table 719

184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719

lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water

sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water

BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity

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