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 ~
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es -r- I - bull C U R IL -bullbullrr Es j M e os AlE 70 vJ PEft- 0 ~~
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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
) 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
-------------~ ~~~--~~~~--
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-
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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
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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
~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
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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
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DATE jREVIS10N DATE i Cl - I - ~-l-
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ENGINEERING NOTE i()Dcent
[ lJ SE
PROJECT
ct~o J~-I~5
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j -(--
SERIAlmiddotCATEGORY
~ ~~ -- ~-~
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
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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
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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
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SEE
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SUBJECT
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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
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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
) ) )
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
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)
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(I 00 f-L~ K (0 Ii) 3 5 Sf
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-
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c_ bull OQ435 s -
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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
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ENGINEERING NOTE SECTION PROJECT
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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
J o N
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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
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 -
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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
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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
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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)
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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
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II
b~ CCSlev aroL7 Tal-f ) TLo - 19 S
fr6crgt ~- aQC-- tftCND 1)11 A
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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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dcDf
II
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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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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-
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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
) ) )
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
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
-------------~ ~~~--~~~~--
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
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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~ ~
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
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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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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)
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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
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
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IDATE REVISION DATE
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r -) (ttF~t4 (
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~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
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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
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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
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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__
~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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(1-lt= 30r 4-r c) elb-gt$)
Pz c Jr 1 fl()
lt
K3output Unit Comment Lockhart Martinelli correlation for two phase pressure drop through an adiabatic horizontal pipe
valid accurate model validity
flow turbulen flow type f 01620391 friction factor Must enter a guess
000005 epsilon ft pipe roughness
62 D in Pipe inside diameter 5 L ft Length of pipe
A 00019478 m2 cross sectional area 8 nrlot gs Total mass flow rate 1067 rhoL kgm 3 Liquid density 3401 rhog kgm3 density of the gas 2864 muL JlPa-s Liquid viscosity 1594 muG JlPa-s Gas viscosity 00003 sigmaL Nm Surface tension of liquid 05 x quality = mdotGmdot
ReL 214500 Reynolds for liquid nrlotL 0076 kgs Mass flow rate for liquid ReG 20290 Reynolds for gas nrlotG 0004 kgs Mass flow rate for gas dpdLL 73408407 Palm 6P~ for the liquid dpdLTP 25168498 Palm 6P~ for the two phase
deltaP 00556327 psig Total pressure drop for the pipe
phiL 1 8516366 Lockhart-Martinelli parameter X 82850398 Lockhart-Martinelli parameter
25 m L-M constant Look up in Table 719
2 n L-M constanti Look up in Table 719
316 CG L-M constanti Look up in Table 719
184 CL L-M constant Look up in Table719 20 C L-M constanti Look up in Table 719
lambda 1 7407229 Baker diagram dimensionless parameter 12 rhoair kgm3 density of air 998 rhoH20 kgm3 density of water
sigh 153404 Baker diagram dimensionless parameter 073 sigmaH2 Nm Surface tension of water 1000 muH20 JlPa-s viscosity of water
BakerXa 50700 X - axis value for Baker plot BakerYa 870 lbmhr-ft Y-axis value for Baker plot c 1 M 1 RsubL 54006278 Volume fraction of liquid phase RsubG 45993722 Volume fraction of gas phase GasVel 1312847 mls Gas velocity LiqVel 6771178 mls Liquid velocity
) )
SOlENOID PIPE SECTIONS~6Le i
LINE ~ pe$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 -
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
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)(~ 387
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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
(
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H
I
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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
~ )
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~ M )
f ltgt0 ~O~ I 0 bull ~
If g -rI ~ t shy ~T
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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)
------
------
--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
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
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ENGINEERING NOTE SECTION PROJECT SERIAl-CATEGORY
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L2 SUBJECT
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IREVISION DATE DATE
5-30 -atS
IIFo(t 1i1 ~)( CQoj 0 bull 11 )t-I ~ ~) Afo-JO A Scu [0
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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 ______
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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
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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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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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--
--
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I
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UR
E 7
~-----------------~
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bull
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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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Russ uc lSt150(pound IJO I D CooLDowN f FLOw RATES e+ c DATE REVISION DATEI
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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
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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
~
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ENGINEERING NOTE 50 LEr-gta D
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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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It it 73 I - S it J(~I
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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
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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SUBJECT NAME
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It-w FERMILAB
ENGINEERING NOTE SECTION PROJECT SERIAl-CATEGORY
3S23 I IS PAGE
rl4
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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
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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
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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
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SUBJECT
FERMILA8 SECTION
ENGINEERING NOTE
FIGURES
PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES
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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
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i bull I rI -j r
I
I (~
I I
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1 -
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bullII i
~ I
I
l
-bull
bull
bull iii
bull iii
-I
+m
-_
-
--
--
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I
FIG
UR
E 7
~-----------------~
-----t----
I
bull
ex t
l
--l
J ~ --
I
r-shy
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shy~-~ 0shy-
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I bull II
I Ii
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4 ~
I
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v uJ Cl J ~
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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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ENGINEERING NOTE SUSJECT
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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
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IaJ = 4 31Z ~d- hov-r = 4S3z l~
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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
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6P 0( ~~ampJ S-
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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
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SECTION SERIALmiddotCATllGORY PAGE
61 SUBJECT shy
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SECTION
lWjocent 38l~ HS FERMILAB
ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE
SUBJECT
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~ 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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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
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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3B23115 SERIALmiddotCATEGORY
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5-30 -atS
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-
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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
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) )
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 ______
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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 ]
r J1
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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
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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
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
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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
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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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ENGINEERING NOTE 50 LEr-gta D
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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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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
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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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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38 Z- 3 bull Il $ PAGE
L2 SUBJECT
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IREVISION DATE DATE
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
---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
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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
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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
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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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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
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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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i bull I rI -j r
I
I (~
I I
I I I~
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1 -
Ibull
bullII i
~ I
I
l
-bull
bull
bull iii
bull iii
-I
+m
-_
-
--
--
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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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NAME
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FERMILAB
ENGINEERING NOTE seCTION
PROJeCT SERIAl-CATEGORY
LH poundfFtel 38 23 II 5 PAGE
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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
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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
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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
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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
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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$)
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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
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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SUBJECT NAME
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3S23 I IS PAGE
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RDIDcent PROJECT
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3S23IlS PAGE
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NAME
DATE IREVISION DATE
5Z-hQ5 1
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1 Sbil shy 1107
30 1-1107
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38 Z- 3 bull Il $ PAGE
L2 SUBJECT
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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
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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J8 CO bull 0049 N2 tu~bullbull
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l Sch lOS H return SS
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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
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
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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)
------
------
--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1
0~--
i i
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i bull I rI -j r
I
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I I
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1 -
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bullII i
~ I
I
l
-bull
bull
bull iii
bull iii
-I
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-
--
--
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I
FIG
UR
E 7
~-----------------~
-----t----
I
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
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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
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App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc
PROJECT SERIALmiddotCATEGOIIY PAGE
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LH poundfFtel 38 23 II 5 PAGE
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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
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
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30 fS
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811 fo I 00 flr~ Ofl- p ~
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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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V A
SECTION PAGEFERMI LAB
F4ENGINEERING NOTE NAMESUBJECT
OATE I~ REVISION DATE 1-2-75
PPIJU
~ ~ 50 t 5
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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
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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
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Lshy
I
i
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i I illI
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10shy I ~
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11~ V Ibull itoftl fO rD I ~ J ~ t~
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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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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
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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 ~
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ct~o J~-I~5
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PAGE
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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
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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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115 W r 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
i 0 -z) lt4
- L
---13) -1 ~PE 5r~ )
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It1V1i-middotoBvl= 13w
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VA-JE (s III 0 )0 W shy( I AI -r c f1Jb IN
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b 4 - v 1 iJg~S
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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
-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 ~~
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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
) 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
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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
-------------~ ~~~--~~~~--
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J8 CO bull 0049 N2 tu~bullbull
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l Sch lOS H return SS
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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
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
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SUBJECT
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ENGINEERING NOTE
FIGURES
PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES
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FERMI LAB
ENGINEERING NOTE SECTION PROJECT
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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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0~--
i i
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i bull I rI -j r
I
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I I
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l
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bull
bull iii
bull iii
-I
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-
--
--
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I
FIG
UR
E 7
~-----------------~
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I
bull
ex t
l
--l
J ~ --
I
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shy~-~ 0shy-
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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
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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-
~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
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cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME
Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I
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OATE I~ REVISION DATE 1-2-75
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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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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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13V ENGINEERING NOTE NAMESUBJECT
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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__
~eI~ p PI ~
7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy
JS
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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
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
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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
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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 -
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-d- = ZYIl
Xl--= ~-~-Fo 158~119h 032 yj - kF ~f 1t--1I96
Afo()
S TIlO
Vft TtJ~ =- 6Po() 2 f5i
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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
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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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FERMllAB
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
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J o N
(
N N
H
I
J
1 shy
c e-l ~w ~ UI
CIgt
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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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~ M )
f ltgt0 ~O~ I 0 bull ~
If g -rI ~ t shy ~T
0
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0 0
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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
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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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NAME
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---
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FERMILAB
ENGINEERING NOTE seCTION
PROJeCT SERIAl-CATEGORY
LH poundfFtel 38 23 II 5 PAGE
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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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1~ JN(Jo 001 3 Reo P
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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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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 -
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F4ENGINEERING NOTE NAMESUBJECT
OATE I~ REVISION DATE 1-2-75
PPIJU
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FERMILAB
ENGINEERING NOTE SECTION
I2D ID~ PROJECT CItlaquogt l)1LT cS
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3823(1) PAGE
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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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io- k~ l dIi~~ t
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jp Ili-shy ~~rmiddot
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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
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DATE jREVIS10N DATE i Cl - I - ~-l-
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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
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NAMESUBJECT - LopD$ R -J 5- -=- - shyDATE JREVIS10N DATE
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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__
~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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(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
H-3 J I
-
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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
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5TA-re(j)
t Ik- pewAn ~~-r L10
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p 9 ( 5 i9 5 A $TAI
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-d- = ZYIl
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Afo()
S TIlO
Vft TtJ~ =- 6Po() 2 f5i
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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
39 Yf ) = 5
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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 ~
~_ 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
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IV It LE IT IlL 1 00 ]I O~5 w~
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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
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I
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Y shy~ V I
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11~ V Ibull itoftl fO rD I ~ J ~ t~
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~ 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
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DATE jREVIS10N DATE i Cl - I - ~-l-
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FEAMILA8 SECTiON
ENGINEERING NOTE i()Dcent
[ lJ SE
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ct~o J~-I~5
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SERIAlmiddotCATEGORY
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PAGE
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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
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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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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
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f 2 I) w -+ ITV A IZb vJ
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It1V1i-middotoBvl= 13w
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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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jY - ooogt -tL d~
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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
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
-
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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
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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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FIGURES
PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES
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ENGINEERING NOTE SECTION PROJECT
-1-(0 lJT111TIES
SERIAL-CATEGORY
3823 II S
SUBJECT
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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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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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LH poundfFtel 38 23 II 5 PAGE
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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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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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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
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SECTION
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ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE
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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)
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
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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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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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SUBJECT
FEAMILAB SECTION
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__
~eI~ p PI ~
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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
-
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
39 Yf ) = 5
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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
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SUBJECT
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FIGURES
PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES
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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
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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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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
-_
-
--
--
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I
FIG
UR
E 7
~-----------------~
-----t----
I
bull
ex t
l
--l
J ~ --
I
r-shy
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shy~-~ 0shy-
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I bull II
I Ii
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4 ~
I
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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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App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc
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II-qmiddot11
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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
NO E eurotJ - 3SQ M- -t-Ow (lp1G-S ~fZC ioVH(v 5- (I IiS
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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
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6P 0( ~~ampJ S-
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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
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SECTION SERIALmiddotCATllGORY PAGE
61 SUBJECT shy
e-X~Allip rwJ ~TE 71tpoundL
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ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE
SUBJECT
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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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-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
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13V ENGINEERING NOTE NAMESUBJECT
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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 ~
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JS
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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
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
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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~
~ ~
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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i i
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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
-_
-
--
--
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I
FIG
UR
E 7
~-----------------~
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I
bull
ex t
l
--l
J ~ --
I
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shy~-~ 0shy-
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I bull II
I Ii
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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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LH poundfFtel 38 23 II 5 PAGE
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SOLEr-JOID CoOLDOIIIAJ t - LOIN RpoundS euro-+c OATE [REVISION OATE
I 1 - I 0 - Ttj
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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
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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
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3823 f( Dishy
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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
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- 2 lttr
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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
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
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
~
~
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
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
10 ~ 1 I UAUEOOV
11 ~7 I I I Flow Fath Flaw
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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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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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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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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
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
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FIGURE 4
SUBJECT
FERMILA8 SECTION
ENGINEERING NOTE
FIGURES
PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES
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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
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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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i bull I rI -j r
I
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I I
I I I~
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1 -
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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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NAME
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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
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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
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1-24-95
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V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt
cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME
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I Z J- I 5
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1HS
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ENGINEERING NOTE SECTION
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SEIIALmiddotCA TEGORY
3823(1) PAGE
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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
I
100
I
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I
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io- k~ l dIi~~ t
V I r ~~~r ~fO ~ V
~ ~~ri V Q~ ~
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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
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13V ENGINEERING NOTE NAMESUBJECT
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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__
~eI~ p PI ~
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(1-lt= 30r 4-r c) elb-gt$)
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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
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
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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
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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
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SUBJECT
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FIGURES
PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES
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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
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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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0~--
i i
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I
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I I
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~ I
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l
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bull
bull iii
bull iii
-I
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-
--
--
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I
FIG
UR
E 7
~-----------------~
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I
bull
ex t
l
--l
J ~ --
I
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shy~-~ 0shy-
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I bull II
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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 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
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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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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
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ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE
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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
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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
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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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
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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
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ENGINEERING NOTE SECTION PROJECT
-1-(0 lJT111TIES
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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)
------
------
--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1
0~--
i i
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bull
bull iii
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UR
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
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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ENGINEERING NOTE SUSJECT
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PROJECT SERIALmiddotCATEGOIIY PAGE
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II-qmiddot11
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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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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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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
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SECTION SERIALmiddotCATllGORY PAGE
61 SUBJECT shy
e-X~Allip rwJ ~TE 71tpoundL
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SECTION
lWjocent 38l~ HS FERMILAB
ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE
SUBJECT
E JIIftIIIEI) 0 KATeuro 7 mev(
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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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PAGEA V
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
c ~J(E9 17-1-1 R t Co ~SI(1
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2BgtW
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SUBJECT
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VLt
NAME -shy
lt5J2---E ~PK_(9 DATE j ~EVSION OA TE
-ltl-17 ~ -2b-~S RN2shy
CE4ampO IZN 72 bull ~ J~ I t
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h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~
(055 -173i ~
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SECTIONft FERMILA8
V ENGINEERING NOTE SUBJECT
PIlOJECT SERIALmiddotCATEGOIlY PAGE
3823 1( 5 NAME
5C-u-v ~Cu4
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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
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1513Z~2 Z-S
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~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
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
)
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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
~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
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
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SUBJECT
FERMILA8 SECTION
ENGINEERING NOTE
FIGURES
PROJECT SERIAL-CATEGORY PAGE GR-I0 J--TIES
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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
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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~
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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
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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
PROJECT SERIALmiddotCATEGOIIY PAGE
U~ AeFflltIlJ 3823 115 ~ 2 NAME
USs Ruc I 0] S(I DATE IREVISION DATE
II-qmiddot11
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NAME
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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~ ~ ~
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~
~
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
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
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SUBJECT
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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)
------
------
--If---------------=-=r-~-F-~-~-~-~-~-~-~-~-~~~~~ 1
0~--
i i
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i bull I rI -j r
I
I (~
I I
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1 -
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bullII i
~ I
I
l
-bull
bull
bull iii
bull iii
-I
+m
-_
-
--
--
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I
FIG
UR
E 7
~-----------------~
-----t----
I
bull
ex t
l
--l
J ~ --
I
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shy~-~ 0shy-
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I bull II
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4 ~
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v uJ Cl J ~
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IbullbullI Imiddotaf
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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 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
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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
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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
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SECTION SERIALmiddotCATllGORY PAGE
61 SUBJECT shy
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OATE JAEVISION DATE
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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
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NAME
RwSS DATE REVISION DATE IO-2I-qy
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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
)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
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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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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)
------
------
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0~--
i i
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i bull I rI -j r
I
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I I
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~ I
I
l
-bull
bull
bull iii
bull iii
-I
+m
-_
-
--
--
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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
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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
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
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-
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~
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14 w f156 vV
14 5ze 14 w
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3 II -2
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
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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~
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
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
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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
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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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--
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I
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UR
E 7
~-----------------~
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bull
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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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LH poundfFtel 38 23 II 5 PAGE
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I 1 - I 0 - Ttj
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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)
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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
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3823 f( Dishy
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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
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NAME
RwSS DATE REVISION DATE IO-2I-qy
Sgt~ I) Steo1lf
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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
I Ibull I
9 o 2 III J o en
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FIGURE 4
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 iii
bull iii
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-
--
--
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I
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UR
E 7
~-----------------~
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I
bull
ex t
l
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I
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v uJ Cl J ~
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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
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
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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
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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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A
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J
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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
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6P 0( ~~ampJ S-
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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
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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
E JIIftIIIEI) 0 KATeuro 7 mev(
~I~ ID ~Agt fItU6 (II e) 6 OATE IREVISION DATE
-7middot S
011 df (
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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
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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
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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
SUBJECT
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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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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
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1-24-95
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V SECTiON PROJECT SERiAL-CATEGORY PAGEFERMllABIt
cP111 -111-11 3823 17RDDcent F3ENGINEERING NOTE NAME
Rwsgt 12J-I~I-1 DATE ltI REVISION DATE I
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1HS
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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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I
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-- l t~ -~ ~~ ILW vomiddott V I- l l~1111 lt-1-~~~ V
jp Ili-shy ~~rmiddot
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J 5
2
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2
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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
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DATE jREVIS10N DATE i Cl - I - ~-l-
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A SECTION PAGEFERMILAB
13V ENGINEERING NOTE NAMESUBJECT
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FEAMILAB SECTION
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__
~eI~ p PI ~
7~~~pound V4Zof fcrf N(~~ ~S~ fpJ ----------~--~------~~~ --------------shy6 V-= I~middot5 Ld0-e1shy
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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
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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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
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i bull I rI -j r
I
I (~
I I
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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=
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v uJ Cl J ~
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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
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
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
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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
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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)
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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
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II
b~ CCSlev aroL7 Tal-f ) TLo - 19 S
fr6crgt ~- aQC-- tftCND 1)11 A
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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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dcDf
II
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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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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-
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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
------
------
--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
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-
--
--
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I
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UR
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
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
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PROJECT SERIALmiddotCATEGOIIY PAGE
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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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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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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
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SECTION SERIALmiddotCATllGORY PAGE
61 SUBJECT shy
e-X~Allip rwJ ~TE 71tpoundL
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SECTION
lWjocent 38l~ HS FERMILAB
ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE
SUBJECT
E JIIftIIIEI) 0 KATeuro 7 mev(
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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
-
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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
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VLt
NAME -shy
lt5J2---E ~PK_(9 DATE j ~EVSION OA TE
-ltl-17 ~ -2b-~S RN2shy
CE4ampO IZN 72 bull ~ J~ I t
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h -= 1~~ ~ h(vfL OS5 v~ 133 amp3OqlntlhJ 2)f V v7s ~
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SECTIONft FERMILA8
V ENGINEERING NOTE SUBJECT
PIlOJECT SERIALmiddotCATEGOIlY PAGE
3823 1( 5 NAME
5C-u-v ~Cu4
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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
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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
~-----------------~
-----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
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LH poundfFtel 38 23 II 5 PAGE
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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
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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
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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
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SECTION SERIALmiddotCATllGORY PAGE
61 SUBJECT shy
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o seCTIONFERMILAB
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Russ Ru c1t-l~K1PIPE So- 5 ~ cap~soJ DATE REVISION DATE I-rQ CD ~
3-1gQS
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OATE JAEVISION DATE
3-15-1S
33 dco r- prJO p c-c Dltigt D (A cIltIIZlt
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ENGINEERING NOTE SECTION PROJECT
3823 f( Dishy
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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
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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
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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
--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
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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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J
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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
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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)
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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)
CDf So W-- 0 10 PIPe S Z- I (J bull I T I ~
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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
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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
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PROJECT SERIAlmiddotCATEGORY PAGE C1210 i)-rtLlrt(S
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NAME
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Sgt~ I) Steo1lf
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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
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
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App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc
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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
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
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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
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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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(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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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
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 ~
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~ 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
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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
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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App~JO I X A- SO(EJVo1o C-OOlOOW t FQ vJ -e ~ E-rc
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U~ AeFflltIlJ 3823 115 ~ 2 NAME
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II-qmiddot11
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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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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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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
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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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SECTION
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ENGINEERING NOTE o SERIALmiddotCATEOORY PAGE
SUBJECT
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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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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
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1Ur-gt y ~ -+ I rM~(-r~ V bull A _ Q II~
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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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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
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
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NAME
CATE IREVISION CATE
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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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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)
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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
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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(
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011 df (
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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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PAGEA V
FERMI LAB
ENGINEERING NOTE SECTION PROJECT
3823 f( Dishy
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DATE PEYISION JA TE fi t11- 22-11 -2 - 15 tJ4shy
c ~J(E9 17-1-1 R t Co ~SI(1
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_ ~~~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
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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__
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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
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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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
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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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AP WIjt ~ 3~ T Zootlt IIV I 300 Ilt 00 [S16f 11
J
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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-
~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
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( Oz~ rCfIJM- w~ 1Jf) oro j Cb 1-1)
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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
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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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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IREVISION DATEDATE
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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)
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
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fr6crgt ~- aQC-- tftCND 1)11 A
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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
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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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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
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(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)
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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
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100 k ( I-c ISU kI I
k~ 535 I ~~ Out 793 v3 2 3fgt shy
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(K~ - S~SII) J _ 23~q
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(0011 ) lt o ~rs)
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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
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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