MOHAWK CORPORATION NY · 2017. 6. 30. · Pipe-ASME SA312 Type 316L Reactor Shutdown Cooling System...

NIAGARA MOHAWK POWER CORPORATION

300 ERIE BOULEVARD WEST

SYRACUSE, NY 13202

TECHNICAL REPORT TR-5828-1

REACTOR RECIRCULATION PIPINGREPLACEMENT ANALYSIS

FOR

NINE MILE POINT UNIT 1

NUCLEAR POWER STATION

APRIL 22, 1983

8308030346 830422PDR 'ADOCK 05000220',.

PDR f

PWTELEDYNE ENGINEERING SERVICES

130 SECOND AVENUEWALTHAM,MASSACHUSETTS 02254

617-890-3350

Technical ReportTR-5828-1

I

A TELEDYNEENQINEERINQ SERVICES

PREFACE

This is a preliminary report of the Reactor Recirculation PipingReplacement Analysis. As of this date, April 22, 1983, all as-built informa-tion has not been verified. Once all supports have been properly set and

verified, this report will be re-issued as final. All computer output,Appendix I, will be issued with the final report.

A

.tl. ~

4

~ ~ ~ ~~ ~

r ~ ~~ ~ ) I

I II ~ ~' ~ I

I ~ I '~

'

~ ) ~ ~

I I f ~ ~ ~ g ~ ~ II

I I ~ ~ ~ ~

~ I ~ ~ ~~ ~

~ ~

~ ~r

~

I ~ ~ ~ ~ ~ ~ ~ I ~ ~ ~ ~ r I

) ~ I ) ~

I ' ~ ) ~

I ~ ~ ~ ) ) ) ~ ~

i ~

/~ ~

>>-TELEDYNEENQINEERlNQ SERV(CES

COMPUTER RUNS (CONTINUED)

I

13. HX3SA67 4/12/83

14. HX3SA7F 4/12/83

15. HX3SEK7 4/12/83

16. HX3ZFHN 4/18/83

17. HX3SCXV 4/12/83

18. HX3SCZV 4/12/83

19. HX3SCZ3 4/12/83

20. HX3SA7V 4/12/83

21. HX3SBIV 4/12/83

22. HX3SBHR 4/12/83

23. HX3SA6N 4/12/83

24. HX3TH5J 3/16/83

25. HX3TGZ3 3/23/83

26. HX3TJ3 J 3/16/83

27. HX3TF03 3/16/83

28. HX3UA9R 3/17/83

29. HX3TJ6F 3/16/83

30. HX3VH9J 3/18/83

31. HX3VGGZ 3/18/83

32. HX3VGHV 3/18/83

33. HX3TJ7R 3/16/83

34. HX3TDBR 3/2/83

35. HX3SGK7 3/1/83

Technical ReportTR-5S2S-1

~< TELEDYNEENQINEERINQ SERVICES

1.0

2.0

3.0

4.0

INTRODUCTION

SUMMARY OF RESULTS

COMPUTER MODELS

ANALYSIS DATA

TABLE OF CONTENTS

~Pa e

5.0

4.1 Pipe Properties4.2 'perating Conditions,4.3 Material Properties4.4 Valve and Pump Weights

HANGER AND RESTRAINT LOADS

789

10

5.15.25.35.45.5

Constant Spring SupportsVariable Spring SupportsSway StrutsSnubbersRigid Supports

llll111213

6.0

7;0

8.0

9.0

PIPE STRESS ANALYSIS

6.1 Method of Analysis6.2 Weight During Normal Operation6.3 Weight During Outage6.4 Thermal Expansion6.5 Seismic Analysis6.6 Cold Springing of Pipe During Installation6.7 Stress Summary

STRESS RULE INDEX

AS-BUILT RECONCILIATION

REFERENCES

9.1 Drawings9.2 Support Drawings9.3 Valve and Pump Drawings9.4 Letters and Telecopies9.5 Miscellaneous

14

14141616171818

20

23

24

2425293030


-r< TELEDYNEENQINEERINQ SERVICES

10. APPENDICES

TABLE OF CONTENTS CONTINUED

~Pa e

A.B.C.D.E.F.G.H.I.

Miscellaneous CalculationsResponse SpectraSupport SummaryStress SummaryStress Rule Index CalculationsCalculation of Safe End StressTMRPASS CheckCheck Sheet SummaryComputer Stress Results

A-1B-1C-10-1E-1F-1G-1H-1I-1


W TELEDYNEENQlNEERlNQ SERVlCES

1. 0 INTRODUCTION

This document contains the as-built analysis'f the Nine Mile PointNuclear Station, Unit 1, reactor recircul ati on pi ping system replacement.Utilizing TMRPIPE, recirculation loops 12 and 15 were modeled with associatedbranch piping which were not decoupled from the main loop. Loop 12 was chosen

because it has no significant branch piping; loop 15 was chosen because it has

the largest di ameter branch piping associated with it. The reactor recircula-tion piping was analyzed for deadweight, thermal and seismic loadings, as wellas any loadings encountered during construction such as cold spring of thepipe. Teledyne Engineering Services (TES) did weekly field surveys during thereinstallation of the recirculation piping to assure no major problemsoccurred. Weekly reports were written and put on file in Document Control,along with any pictures taken. Following the completion of the reinstalla-tion, TES performed an as-built walkdown of the recirculation system and allthe attached piping.

The criteria used for evaluating pipe stress and support loads is the1977 ASME Boiler and Pressure Vessel Code, Section III, Subsection NC with alladdenda through winter 1979.


-rs-TELEDYNEENQINEERINQ SERVICES

2.0 SUMMARY OF RESULTS

TES analyzed the operating stress conditions for recirculation loops 12

and 15, including the branch piping on loop 15. Operational and outage

deadweight conditions were examined. Both loops.12 and 15 exhibit low levelsof stress.

i)jl I

Five operating thermal cases were examined for loop 15 and two for loop

12. Because loop 15 contains branch piping, and loop 12 does not, more

thermal modes and, consequently, higher stresses are possible for loop 15.

Therefore, as expected, the thermal stresses are higher for loop 15 than forloop 12. Stresses for both loops, however, are within allowable limits.Details of analysis conditions may be found in Section 5.0 and details of the

stress analysis may be found in Section 6.0.

It is noted that many of the recirculation piping supports demonstrate an

upward movement in some thermal cases and a downward movement in others. This

upward movement is largely due to the "valved out" condition which causes a

general upward movement in the recirculation system.'otal travel for allsupports is within the design limits of the supports. Support details may be

found in Section 5.0.

The susceptibility of the new piping system -to intergranular stresscorrosion cracking ( IGSCC) was examined through calculations of the stressrule index. There are three conditions necessary for IGSCC to occur:

1. A carbon content greater than 0.035 percent.

2. A corrosive environment.

3. A stress rule index above 1.2.

l


4

>> TELEDYNE .

ENGINEERINQ SERVICES

Replacement of the original piping with new piping, which has a carbon

content below 0.02 percent, has effectively removed one of the three condi-

, tions. The SRI's are, therefore, presented for review but no further IGSCC

problems are expected to occur. Details of SRI calculations may be found inSection 7.0.

'I

An as-built walkdown of the recirculation piping and all the attachedlines was performed after the replacement of the piping. No significantdifferences were noted between the old as-builts and the new piping. For

details, see Section 8.0.

In summary, the stress levels for the as-built recirculation system

operating conditions meet all the appropriate code allowables.


>s-TELEDYNEENQINEERINQ SERVICES

3.0 COMPUTER MODELS

The following are computer plots for the two loops analyzed. Node

numbers 1-275 correspond to recirculation piping system 32. Node numbers

3800-3899 correspond to the shutdown cooling system 38, and node numbers'900-3999 correspond to the emergency cooling condensate return system 39. See

Ip,

Reference 9.1.18 for the complete isometric of recirculation loop 15. Loop 12

is identical to loop 15 except there is no attached piping. See Figures 3.1and 3.2 for computer plots of loops 12 and 15, respectively.

TECHNICAL REPORTTR-5828-1

'00voazLE Ii<6 ss-TELEDYNE

ENQlNEERINQ SERVlCES

sv5Hitihlt,l)tB

l'raBY l ~ DATE~CHKD. BY~DATE~

}l0

3'P.-e3g)ll 3t 12 Hf/S B

55 bA 93 SC-.}lr

32 4 Kr

92. SII.3 3i&5SS rIA

'

%Q

LCC - NP

S2- l2- H2

llew Il3 ll'4

I ~

I~ p

~fII@ ~ G$ I3

hawutc \)

EII4+1

~vI

~ u~ y

CViu

lj

N

i 32-l2 WC

92 l2.ll 1 D

32- /br II

FIGURE 3.1 RECIRCULATION LOOP 12

TECHNICAL IIIEI'ORT TR-5828-1

33 A3

o9 ~ «I'l

-6-

) "J 4~).C «) ifIOO

A TELEDYNEENGINEERINQ SERVlCES

BY L OATC ~ K~ »P+

CHKO. BY~BATE~~3% Hs QIIP

'l»)07

off't,).)' g2 f"i'F70

3O)-P)I

99.03'l»Y

C.3".-)<)O

38-HS I

3C ~ H5-2

58 ~ T)f) CB 22- 5)'.IC h I f)) iota g)) tp

32 IS-H S

N»3 ~ 02. 92. «)5 Z5 IZbJ, 3B-A2B2-) 5-Heh g)9

S2- I~-Hz

L C:"»TB )Jb

P)f')D'„uPPOPt

~ 0

NG-03C2

)

)3'I)3)5 .HPi- D))

).4rJrn

33)<ungag

AW))0R

32 m5 g7 f)Z-)33.«) ) I))~+2-)r/ g)6

32- m5 ~ 2$

)g, / 92 ~ I5.HIC

g». fY»A.fI I+ » ie

gg-NP3 - rrp

FIGURE 3.2 RECIRCULATION LOOP 15


><-TELEDYNEENGlNEER(NQ SERVlCES

4.0 ANALYSIS DATA

4.1 ~Pi P i (R f 9.4.1, 9.4.3, 9.4.4, 9.4.5, 9.5.10)

Reactor Recirculation Loop System ¹32

Pipe - ASME SA358 Type 316 "Nuclear Grade", SA655 Austeniticsteel piping with 0.02 percent maximum carboy contentand 0.10 percent maximum nitrogen content with mech-

anical properties identical to ASME SA358 Type 316 and

SA655 Austenitic steel.Reactor Cleanup System ¹33

Pipe - ASME SA312 Type 316L up to IV 33-02

ASME SA333 Gr 6 from IV 33-02 to anchor

Reactor Miscellaneous Connections System ¹37

Pipe - ASME SA312 Type 316L

Reactor Shutdown Cooling System ¹38Pipe - Same as System 32 to first IV.

ASTM A358 Type 304 from IV to anchor

Emergency Cooling Condensate Return System ¹39Pipe - Same as System 32 to first IV

ASTM A358 Type 304 from IV to anchor

S stem

32

32

33

37

38

(To First I.V.)38

(After I.V.)39

39

Size in28

2

6

2

14

14

12

10

O.D. in28.0

2.375

6.625

2.375

14.0

14.0

12. 75

10.75

Thickness in1.05

0.343

0.432

0.218

0.937

0.753

0.843

0.574

Weight (lbs)Per Inch

With Water

46.25

0.7,4.198

0.53

16.87

15.1

13.99

9.2


r<-TELEDYNE *

ENQINEERINQ SERVICES

4.2 0 eratin Conditions (Reference 9.5.10)

S stemOperating

Pressure Tem eratureDesign

Pressure Tem erature

32

33

37

38

39

1030 psi1030 psi1030 psi

120 psi1030 psi

550 F

550 F

550 F

350 F

550 F

1200 psi1300 psi1300 psi1200 psi,-1200 psi

569 F

575 F

575 F

~ 575 F

575 F

Load Cases (See Section 6.0 - Complete Description of Load Cases)

Thermal 2

Loop 12 Deadweight 1 Operational deadweight

Thermal 1 Recirculation piping at 550 F

Thermal 2 Reactor at 550 F. All piping at 100 F

with attenuation from nozzleCold springing pipe during installationSeismic

Loop 15 Deadweight 1 Operational deadweight

Deadweight 2 Non-operational deadweightDeadweight 3 Water drained from pump and pump motor

removed

Thermal 1 Recirculation piping at 550 F

Branch piping at 100 F past I.V.Systems 32 and 38 at 350 F

System 39 at 100 F

Thermal 3 Systems 32 and 39 at 550 F

System 38 at 100 F

Thermal 4 Reactor at 550 F

All piping at 100 F with attenuationfrom nozzle

Technical ReportTR-5828-1 -9-

~< TELEDYNEENQlNEERINQ SERVlCES

Thermal 5

Seismic

Reactor at 550 F

System 39 at 550 F

System 32 550 F from reactorto valve NG-02 on suction leg, 100 F

on discharge legSystem 38 at 100 F

4.3 Material Pro erties (Reference 9.5.5)

Moduli of Elasticit

Tem erature Stainless Steel Car bon Steel

70 F

100 F

350 F

550 F

28.3 x 10 psi28.16 x 10 psi26.85 x 10 psi25.75 x 10 psi6

27.9 x 10 psi27.9 x 10 psi6

27.2 x 10 psi

26.0 x 10 psi,6

Coefficient of Thermal Ex ansion

Tem erature Stainless Steel Carbon Steel

100 F

350 F

550 F,

9.163 x 10

9.530 x 10

9.760 x 10

in/in/ F

in/in/ F

in/in/ F

6.13 x 10 in/in/ F

6.71 x 10 in/in/I'.12

x 10 jn/in/ I:

Allowable. Stresses

Material 100 F 350 F 550 F

;'A 358 Type 316

A 358 Type 304

SA 312 Type 316L

SA 333 Gr 6

18.8 ksi18.8 ksi15.7 ksi15.0 ksi

18.25 ksi16.4 ksi

17.5 ksi15.9 ksi13.95 ksi15.0 ksi


r<-TELEDYNEENQ|NEER(NQ SERVlCES

4.4 Valve and Pum Wei hts (Reference 9.3)

Valve Number Dr Wei ht lbs Wei ht w/water lbs

NG 02

NG 03

NG 08

12650

8590

155

13890

9635

155

38-01, 38-13

38-123970

4065

4140

4285

39-01, 39-02

39-03, 39-04

2235

1185

2322

1271

Pump Assembly - Dry 28600

Pump Assembly - Flooded 32000

Motor 13000


r<-TELEDYNE*


5.0 HANGER AND RESTRAINT LOADS

5.1 Constant S r in Su orts

All springs on the recirculation piping are constant supportsprings, except on valve NG08 which has a variable spring s'upport. Theseconstant supports were modeled as forces. The force on these hangers matc)exactly the installed condition. Supports on the suction and dischargerisers wer e replaced with new springs during the outage with new loads of20,000 pounds and 14,125 pounds, respectively. The old springs were set for17,900 pounds and 13,070 pounds as shown on the support drawings; therefore,these drawings do not agree with the analysis.

All support drawings state only a downward travel on the springs,but because of additional thermal cases run, an upward movement, as well, ispresent on all springs. The total movement is still less than the total

, travel rating of the spring. Therefore, the springs should be set to allowfor this upward movement. See Appendix C for details of support loads and

displacements.

5.2 Variable S rin Su orts

All variable springs were input as forces equal to their current hotloads listed on the support drawings for the operation deadweight case. New

cold loads were then calculated using the normal operating displacements.These cold loads were then input as forces for the deadweight during outagecase. See Appendix C for details of support loads and displacements.

5.3 ~S

The sway struts are vibration control devices while in the hotposition. These struts will remain rigid until the load exceeds 1,000 pounds.After the load exceeds 1,000 pounds, the struts deflect with a spring rate of


A TELEDYNEENQINEERiNG SERVtCES

1,000 pounds per inch.. This allows thermal movement while exerting minimalToad on the pipe, but resists vibrational loads. See Section 6.5 for- themethod used for seismic modeling of the sway struts.

These braces should be neutral in the hot position, therefore, theymust be preloaded when, initially installed. The preload will be equa to1,000 times the normal operating thermal movement of the strut's, plus,1<00)pounds. These values are tabulated below.

IISupport Nark No. Loop 12 Disp. Loop 15 Disp. Recommended )reload

Loo 15 in. in. ounds

32-SB-9A

32-SB-9B

32-SB-10A

32-SB-10B

0.37

0.30

0.31

0.44

0.32

0.29

0.31

0.42

1350.

1300.

1300.

1450.

Note'ecommended pr eload is rounded to nearest 50 pounds and finaladjustment should be made with pipe in its hot or operatingposition as per Grinnel Catalog.

L

5.4 Snubbers

All sn'ubbers were modeled as rigid supports for the seismic analy-sis. Two sets of analyses were run. The first was run with the sway strutsrigid, resulting in the sway strut loads exceeding the 1,000 po~~d 'preloydlimit. Consequently, a second analysis was run with a spring rate, of 1,000pounds per inch on the sway struts and in all cases the second analysis

~ q,",f uk'/

governed the design load of the snubbers.

All snubbers were below the manufacturers rated design load withthe exception of 38-HS-1. The'load on this snubber is 11,214 pounds which isabove the allowable of 10,350 pounds. This is a lateral snubber on theshutdown'cooling system close to the tee on the recirculation piping. Because


A TELEDYNE'NQINEERINQ SERVICES

of the location, this snubber is very sensitive to the stiffness of the sway

struts. Therefore, an additional static seismic case was run for the X and Z

directions with the 1,000 pound preload applied in the opposite direction tothe seismic displacement of the strut. In the static seismic Y direction withstruts rigid, the 1,000 pound preload was not exceeded. This caused a

decrease in load of 973 pounds so the total load on snubber 38-HS-1 is 10,241

pounds which is below the manufacturer's allowable. See Appendix C fordetails.

5'5.5 ~di ld 5

There are no rigid supports on the systems analyzed.


W-TELEDYNEENQINEERINQ SERVICES

'i li

6.0 PIPE STRESS ANALYSIS

6.1 Method of Anal sis

The Nine Mile Point Unit 1 Recirculation Piping has been reanalyzed

for stresses and support loadings due to pressure, weight, thermal expansion

and seismic. All recirculation loops are similar in geometry with the exce~-/

tion of the branch piping. The stress levels of the recirculation piping are

therefore bounded by analyzing the geometries of two of the five recirculationloops - one loop with large diameter branch piping and an additional loop withno branch piping.

Loop 15 was chosen because it has the shutdown cooling branch pipingassociated with it. The shutdown cooling piping is the largest diameter

branch piping associated with any of the recirculation loops. In addition," the previous recirculation piping for loop 15 contained a through wall crack.

Loop 12 was chosen because it has no significant branch pipingassociated with it.

It should be noted that the previous stress analysis of record forthe recirculation and branch piping is still valid. The updated analysis inthis report has been completed to analyze as-built design changes,, such as

cold springing of pipe for closure welds. As-built design changes are minimal

and reconciled in Section 8.0 of this report.

The new material allowables are equal or greater than the old mater-

iall

allowables; therefore, the past analysis for the recirculation piping may

be considered conservative. These allowables are shown in Table 6-1.

6.2 Wei ht Durin Normal 0 eration

Deadweight stresses include stresses due to the weight of the pip-ing components, insulation and contents. The spring hangers which are con-

SystemName

RecirculationSystem 832

- MaterialOld System

ASTM 358 TP316.Class 1

TABLE 6.1

PIPING SYSTEMS MATERIAL COMPARISON

Allowable Psi(B31.1 Code)

16000(1967)

MaterialExisting System

'SME SA358 TP316

I AVl K

Allowable Psi77 ASME Code ™

17500

Reactor WaterCleanupSystem 833

ASME SA312 TP316L(Up to IV 33-02)ASME SA333 Gr 6(From IV 33-02to Anchor)

14000(1973)

'15000(1973)

ASME SA312 TP316L(Up to IV 33-02)ASME SA333 Gr 6(From IV 33-02to Anchor)

14000

15000I

VlI

Shutdown CoolingSystem 838

ASTM A358 TP304Class 1

ASTM 376 TP304Class 1 (3" Pipe only)

15900(1973)

ASME SA358 TP316(Up to IV'.s 38-01and 38-13)

ASTM A358 TP304(From IV's to Anchor)

17500

15900

Emergency Cooling ASTM A358 TP304Steam, East and Class 1West LoopsSystem 839

14400(1967)

ASME SA358 TP316(Up to IV's 39-01and. 39-02)

ASTM A358 TP304(From IV's to Anchor)

17500

15900

Note: All allowables correspond to a temperature of approximately 550 F.



stant supports are input as forces equivalent to the rated load of the

springs. The sway struts on the recirculation piping were modeled in tPe hotposition'. Since they were designed to exert no load in the hot position, no

restraint or load was input for the struts in this load case.

6.3 Wei ht Durin Outa e

During plant shutdown, and after the reactor has cooled down, thethermal displacement of the recirculation piping is removed. This causes a

load on the pipe from the sway struts, because they are set to be neutral inthe hot position. This load is equal to 1,000 lbs, plus 1,000 times t:he thermaldisplacement of the struts for the normal operating condition.

Also during plant shutdown, the pump motor may.be removed without chang-

ing the support arrangement.- This is done by first closing the isolationvalves and draining the water from the pump. Then the pump motor is'removed.The sway struts for this case were modeled the same as for the normal shutdown

case. Since the supports are constant force springs, this decrease in thesystem weight causes a net upward force on the pipe which results in a slightupward movement in the pump and an increase in the deadweight stresses. The

maximum increase in deadweight stress is 3,875 psi for the recirculation sys-tem, 1,244 psi for system 38 and 772 psi for system 39.

6.4 Thermal Ex ansion

During normal operation of the plant,'ecirculation loops pre atthe same temperature as the reactor due to high flow rates through t)e loops.That is, with the reactor at 550 F, the loops are also at 550 F., l')e branch

piping which is normally not operating is at 100 F. This represent:s the as-N

designed normal operating condition.

During operation of the shutdown cooling system, the reactor and

the recirculation piping, are at 350 F. The emergency cooling condensatereturn is assumed to be not operating and is at 100 F.


<< TELEDYNEENQINEERlNQ SERVlCES

r

~ During the operation of the emergency cooling condensate return,the reactor and recirculation piping is at 550 F. The shutdown cooling system

is not operating and is at 100 F.

There have been times during operation of the plant when 'a loop (orloops) have been ".valved-out". In this event, the pump is not operating atld

the valves (upstream and downstream) are closed leaving a stagnant leg ofwater below the valves. The stagnant water in the loops cool off to approxi-mately containment ambient, 100 F.

During the operation of the emergency cooling condensate return,the recirculation system could be "valved-out". This would cause only one legof the recirculation piping and the emergency cooling condensate return toheat up to 550 F, while the other leg and the shutdown cooling system. are

still at 100.F.

6.5 Seismic Anal sis

The primary piping in this analysis was analyzed by first using the

ground response spectra. The horizontal ground spectra was obtained by envel-oping the NMPC and Dames and Moore ground response spectra. The verticalspectra was taken as two thirds the horizontal spectra. This spectra is shown

in Appendix B. .The building acceleration at the pipe attachment points wasI

applied to the piping as 'a rigid body acceleration. The building accelerationloads were then superimposed with the loads due to the ground response spec-

tra. The variation of the building acceleration over the elevation range foreach model is relatively constant. Therefore, the building response was

analyzed by taking the maximum acceleration response for the model and using a

static analysis for gravity loading in three directions. The building accel-erations and the accelerations used are shown in Appendix B.

This method is identical to that used in Teledyne Technical ReportE-1562-1 dated October 10, 1972, issued as an addendum to Technical Report E-

1289-6 dated August 26, 1971..


r>-TELEDYNEENQINEERINQ SERVlCES

Since the sway struts on the recirculation piping are non-lineardevices, two sets of seismic runs were made. First, the sway struts weremodeled as rigid supports for the seismic runs. Under this condition, theload on the struts exceeded the 1,000 pound preload. 'After the load exceeds

1,000 pounds, the sway struts act as springs with a stiffness of 1,000 pounds

per inch. A second case was then run with a stiffness of 1,000 pounds per inchfor the struts. The actual response will therefore be bounded by these twocases.

6.6 Cold S rin of Pi e Durin Installation

During the installation of loop 14, in order to make the weld forthe closure elbow on the discharge riser, it was necessary to cold spring thepipe to align the elbow with the riser. This was done with two come-alongs,oriented at 90 to one another, with one come-along radial toward the centerof the reactor. The loads necessary to align the pipe were 2,150 pounds (in theradial direction) and 2,375 pounds. These loads are documented in a controlledwork instruction CWI-1399K-7-14, Rev. B-3, page 61A of 62.

The maximum stress generated from the cold springing of the pipe is4,611 psi. The maximum pipe stress in the recirculation piping is 8158 forEquation 10. Therefore, the maximum pipe stress, including the stress due to

n

cold springing, is 12,769 psi, which is lower than the allowable stress of27,812 psi.

6.7 ~ESThe recirculation piping was analyzed for the operating conditions

discussed in Section 4.2. The evaluation was performed in accordance with thecriteria set forth in the 1977 ASME Boiler and Pressure Vessel Code, SectionIII, Subsection NC including addenda through winter 1979. The maximum stres-ses for each system are listed below. Complete stress results may be found in

'.Appendix D. Detailed computer results may be found in Appendix I. In everycase, the maximum stresses for Equation 9 were governed by the seismic case


~<. TELEDYNEENQINEERINQ SERVICES

with the sway struts modeled as springs instead of rigids. See Section 5.4.for explanation of sway struts. The maximum stress at the safe ends is 4,056psi which is much lower than the allowable of 17,125 psi. See Appendix F forcalculation of safe end stresses.

Recirculation Loo 12 (Pass Run Sequence 8HX3SBIV)

Eq. 8 Max. Stress = 8433 psi

Eq. 9 Max. Stress = 11473 psiEq. 10 Max. Stress = 3611 psi

1.0 Sh

1.2 Si

S

= 17500 9 Node 101

= 21000 9 Node 135

= 27812 9 Node 265

J

Recirculation Loo 15 (Pass Run Sequence PHX3ZFIN)

Eq. 8 Max. Stress = 8228 psiEq. 9 Max. Stress = 11927 psiEq. 10 Max. Stress = 8158 psi

1.0 Sh

1.2 Sh

S

= 17500 9 Node 275

= 21000 9 Node 101

= 27812 9 Node 265

Shutdown Coolin S stem 38 (Pass Run Sequence 8HX3ZFIN)

Eq. 8 Max. Stress = 8890 psiEq. 9 Max. Stress = 12961 psiEq. 10 Max.-Stress = 12868 psi

1.0 Sh= 16400 9 Node 3822

1.2 Sh= 19680 9 Node 3822

S = 27812 9 Node 3802

Emer enc Coolin Condensate Return S stem 39 (Pass Run Sequence 8HX3ZFIN)

Eq. 8 Max. Stress.= 8152 psiEq. 9 Max. Stress = 15344 psiEq. 10 Max. Stress = 15270 psi

1.0 Sh= 17500 9 Node 3902

1.2 Sh= 21000 9 Node 3904

S = 27475 9 Node 3910


-r<-TELEDYNEENQINEERINQ SERVICES

7.0 STRESS RULE INDEX

The stress rule index (SRI) was calculated for both loop 12, loop 15 and

the attached piping. There is a relatively low magnitude of operating stressthroughout the recirculation system which is reflected in the SRI's. The majorvariation in SRI's between loop 12 and loop 15 is a result of the stressindices, most notably the tee indices, which are somewhat large.

*

Therefore,the largest SRI's occur at the tees and because of the material transition, atthe safe ends. The maximum SRI value for either loop is 2.314.

The thermal range used in the SRI program is the maximum range TNRPASS

used in the calculation of equation 10 stresses.

Tables 7.1 and 7.2 contain the summaries of the SRI's for loop 12 and loop

15, respectively. Tables are also included in Appendix E, along with detailedresults. For details of SRI equations and the SRI program, see Reference

9.5.1.

TECHHICAL REPORT TR - 5828 - 1 -21-REVo HOo 0 TELEDYNE ENG INEER ING SERV ICES,.

fffffffffffffffffffffffffffffffffffffffffffffffffffffPROJECTt 5828 20 APRIL 1983

STRESS RULE IHDEX CIIKO MTE ~NZ" +~

as ~Z~ DATE +~~'~~.

HIHE HILE POIHT UHIT 1

fafffffaffffffafffffffffffffffffffffffffffffffffffffffSHEET No OF

PROGRAM NAMECOMMON i CDAHIELS223SRI i EXE r'

TITLERECIRC LOOP 12

CREATION DATE6-DEC-1982 17i53

RUN DATE R TIME13-APR-83 10142l29

NODE100101105115135155156200205

270275

STRESS RULE INDEXSUMMARY'4'4

DESCRIPTIOH SRISAFE END 2o070ELBOW 1+238RUH F'I PE ioi87RUN PIPE io189VALVE io201ELBOW 1.227PUHP io315F'UHP 1o197ELBOW ioi97VALVE 1 i 200ELBOW ii282SAFE END 2 i 091

TABLE 7.1

a

TECHHICAL REPORT TR

REVe HOe 0

Itp tt(I

5828 - 1-22-

aaaaaaaaaaaaaaaaaaaaaaaaaaaasasassassssasaaaaaaaasass

PROJECT» 5828 20 APRIL 1983

STRESS RULE IHDEX

yCIIKO


sassaaaaaaassaaasasasaaaaasaaaaaaasssaaasaasaaaaaaaaaa sHEET Ho,

TELEDYNE ENGINEERING SERVICESDATE YZ~DefE +l~"i"~

OF

PROGRAN NANE,

CONHOH', CDAHIELS223SRI.EXE'3CREATION DATE6-DEC-1982 17'53

TITLERECIRCULATION LOOP 15

RUN DATE20-APR-83

TINE10:13e24

NODE100101105115135155156+55265200205225270275

39023905390539093910391139143916391939233802380638883814381538173821

E INDEXRYE%

'STRESS RULt4 SUNNA

DESCRIPTIONSAFE EHDELBOMTEETEEVALVEELBOWPUNPTEETEEPUHPELBOMVALVEELBOWSAFE ENDTEEVALVEREDUCERVALVEELBOWELBOMELBOWELBOW.ELBOMELBOWTEEELBOWRUNELBOMELBOMRUNRUN

SRI2ei26ie3812e2732e259le2531.271le3752e3122e 314ie2501.343ie270ie4092e154ie6841.348ie5561.418ie807ie8441.7091.586ie6201.5412e2~4ie101ie218ie489le4671 ~ 1891.364

TABLE 7.2


W-TELEDYNEEN|-WEERINQ SERVtCES

8. 0 AS-BUILT RECONCILIATION

As-built dimensions of the recirculation piping and the attached pipingmay be found on Teledyne Drawings E-8414, D-8416, C-8417 and C-8418, (Refer-ences 9.1.19 - 9.1.23). One as-built discrepancy was found which is notaccounted for in the analysis.

The discrepancy, which is on the shutdown cooling system and the emer-

gency cooling condensate return system, consists of replacing the branch

piping from the recirculation loop to the first isolation valve with schedule100 pipe instead of the schedule 80 pipe previously used.

On the emergency cooling condensate return system west bank and thedischarge side of the shutdown cooling system, approximately 2 feet and llfeet of pipe has been replaced, respectively. This change has been accounted

for in the analysis of recirculation loop 15. The maximum increase in stressdue to the pipe schedule change is approximatley five percent of the allowablevalue.

On the emergency cooling condensate return system east bank and thesuction side of the shutdown cooling system, the replaced pipe is only a fewfeet in length, not more than three pipe diameters. Based on the analysis ofrecirculation loop 15, this should result in an insignificant change in thestress in the branch piping. Additionally, the maximum occasional stressobtained from the previous analysis for these systems is 13628 psi. Thismaximum stress is well below the allowable value of 21000 psi leaving plentyof margin for any increase resulting from the change in pipe schedule. No

reanalysis of the recirculation loops which contain these branch piping sys-tems was performed.



9.0 REFERENCES

9.1 ~Drawin s

1. C-26846-C, Sh. 2, Rev. 2

2. C-26847-C, Sh. 2, Rev. 1

3. C-26843-C, Sh. 3, Rev. 3

4. C-26843-C, Sh. 4, Rev. 3

5. C-26852-C, Sh. 2, Rev. 2

6. 706E240, Rev. 5

7. 846D608, Rev. 5

8. C-18248-C, Rev.,3

10. C-18675-C, Rev. 13

11. C-23285-C, Rev. 3

12.

13.

104R877, Rev. 0

C-34145-C, Sh. 1, Rev. 6

14. C-34145-C, Sh. 2, Rev. 3

15. C-34146-C, Sh. 1, Rev. 4

16. C-34146-C, Sh. 2, Rev. 4

9. C-18273-C, Sh. 17, Rev. 3

Recirculation Pump

ment Plan, SectionRecirculation Pump

ment Plan, SectionRecirculation Pump

ment Plan, Section

Recirculation Pump

ment Plan, Section

Snubber Replace-

8 DetailsSnubber Replace-

5 DetailsSnubber Replace-

and DetailsSnubber Replace-

and Details

Reactor Recirculation System 832

Piping IsometricReactor Shutdown Cooling System f38

Piping IsometricEmergency Condenser System f39

Piping IsometricEmergency Cndenser System 839

Piping IsometricReactor Cleanup System $ 33, 33. 1,

33.2 and 33.3

Suspension System for RecirculationLoops

Recirculation Loop Piping Arrange-

ment

Thermal 8 Seismic Control StructuresSystems 33 8 37

Reactor Building Hydraulic Snubbers

for Systems 31 E 33

Reactor Cleanup Piping Section 4-4

Reactor Drain Line System Thermal

5 Seismic Control StructureReactor Pressure Vessel


t

s< TELEDYNEENQINEERINQ SERVlCES

Drawin s Continued

17. C-34147-C, Rev. 2

18. E-8413, Rev. 0

19. E-8414, Rev. 0

20. D-8415, Rev. 0

21. D-8416, Rev. 0

22. C-8417, Rev. 0

23. C-8418, Rev. 0

Recirculation Pump Snubber Replace-

ment Plan, Section and DetailsReactor Recirculation Loop 15 .PS-5,

PD-10 and Attached PipingAs-Built Isometric System 32

As-Built Isometric Systems 33 8 37

As-Built Isometric System 38



9.2 Su ort Drawin s

Mark Number Sketch No./Drawin No.

1. 32-1 1-H1A

2. 32-ll-H1B

3. 32-11-Hlc

4. 32-ll-HlD

5. 32-ll-H26. 32-1 1-H3A

7. 32-ll-H388. 32-11-H4A

9. 32-11-H4B

10. 32-11-H5

ll. 32-ll-H612. 32-SB-1A

13. 32-SB-1B

300-11-HlA, Rev. 2,302-11-H1A, Rev. 2,300-11-H1B, Rev. 2,

302-11-HlB, Rev. 2,300-11-H1C, Rev. 2,

302-11-HlC, Rev. 2,300-11-HlD, Rev. 2,

302-11-HlD, Rev. 2,304-11-H2, Rev. 4,305-11-H3A, Rev. 2,305-11-H3B, Rev. 2,306-11-H4A, Rev. 2,

306-11-H4R, Rev. 2,308-11-H5, Rev. 2

315-11-H6, Rev. 1

309-SB-1A, Rev. 1

309-SB-1B, Rev. 1

301-11-H1A,

303-11-H1A,

301-11-H1B,

303-11-H1B,

301-11-Hlc,303-11-H lc,301-11-H1D,

303-11-H1D,

304-A-11-H2,

307-11-H3A,

307-11-H3B,

307-11-H4A,

307-11-H4B,

Rev. 2

Rev. 3

Rev. 2

Rev. 3

Rev. 2

Rev. 3

Rev. 2

Rev. 3

Rev. 3

Rev. 1

Rev. 1

Rev. 1

Rev. 1


r< TELEDYNEENQINEERINQ SERVICES

Su ort Drawin s Continued

14.

15.

16.

17.

18.

19.

20.

21.

22.

23.

24.

25.

26.~ 27.

28.

29.

30.

31.

32.

33.

34.

35.

36.

37.

38.

39.

40.

41.

32-SB-2A

32-SB-2B

32-HS-1

32-HS-2

32-HS-3

32-HS-4

32-HS-5

32-12-H1A

32-12-H1B

32-12-H1C

32-12-H1D

32-12-H2

32-12-H3A

32-12-H3B

32-12-H4A

32-12-H4B

32-12-H5

32-12-H6

32-SB-3A

32-SB-3B

32-SB-4A

32-SB-4B

32-HS-6

32-HS-7

32-HS-8

32-HS-9

32-HS-10

32-13-HlA =

309-SB-2A, Rev. 1

309-SB-2B, Rev. 1

310-HS-1, Rev. 3, 311-HS-1, Rev. 3

310-HS-2, Rev. 3, 311-HS-2, Rev. 3

312-HS-3, Rev. 1, 313-HS-3, Rev. 1

312-HS-4, Rev. 1, 313-HS-4, Rev. 1

314-HS-5, Rev. 2

300-12-HlA, Rey. 2, 301-12-H1A, Rev. 2

302-12-H1A, Rev. 2, 303-12-H1A, Rev. 3

300-12-H1B, Rev. 2, 301-12-H1B, Rev. 2

302-12-H1B, Rev. 2, 303-12-H1B, Rev. 3

300-12-H1C, Rev. 2, 301-12-H1C, Rev. 2

302-12-H1C, Rev. 2, 303-12-H1C, Rev. 3

300-12-H1D, Rev. 2, 301-12-H1D, Rev. 2

302-12-HlD, Rev. 2, 303-12-H1D, Rev. 3

304-12-H2, Rev. 4, 304-A-12-H2, Rev. 3

305-12-H3A, Rev. 2, 307-12-H3A, Rev. 1

305-12-H3B, Rev. 2, 307-12-H3B, Rev. 1

306-12-H4A, Rev. 2, 307-12-H4A, Rev. 1

306-12-H4B, Rev. 2, 307-12-H4B, Rev. 1

308-12-H5, Rev. 2

315-12-H6, Rev. 1

309-SB-3A, Rev. 1

309-SB-3B, Rev. 1

309-SB-4A, Rev. 1

309-SB-4B, Rev. 1

310-HS-6, Rev. 3, 311-HS-6, Rev. 3

310-HS-7, Rev. 3, 311-HS-7, Rev. 3

312-HS-8, Rev. 1, 313-HS-8, Rev. 1

312-HS-9, Rev. 1, 313-HS-9, Rev. 1

314-HS-10, Rev. 2

300-13-H1A, Rev. 2, 301-13-H1A, Rev. 2

302-13-H1A, Rev. 2, 303-13-H1A, Rev. 3

I

,Technical ReportTR-5828-1 -27-

-r> TELEDYNEENQINEERlNQ SERVtCES


42. 32-13-H1B

43. 32-13-Hlc

44. 32-13-H1D

45. 32-13-H2

46. 32-13-H3A

47. 32-13-H3B

48. 32-13-H4A

49. 32-13-H4B

50. 32-13-H5

51. 32-13-H6

52. 32-SB-5A

53. 32-SB-5B

54. 32-SB-6A

55. 32-SB-6B

56. 32-HS-11

57. 32-HS-12

58. 32-HS-13

59. 32-HS-14

60. 32-HS-15

61. 32-14-H1A

62. 32-14-HlB

63. 32-14-Hlc

64. 32-14-H1D

65. 32-14-H2

66. 32-14-H3A

67. 32-14-H3B

300-13-H1B, Rev. 2, 301-13-HlB, Rev. 2

302-13-H1B, Rev. 2, 303-13-H1B, Rev. 3

300-13-H1C, Rev. 2, 301-13-HlC, Rev. 2

302-13-H1C, Rev. 2, 303-13-H1C, Rev. 3

300-13-H1D, Rev. 2, 301-13-H1D, Rev. 2

302-13-H1D, Rev. 2, 303-13-H1D, Rev. 3 .

304-13-H2, Rev. 4, 304-A-13-H2, Rev. 3

305-13-H3A, Rev. 2, 307-13-H3A, Rev. 1

305-13-H3B, Rev. 2, 307-13-H3B, Rev. 1

306-13-H4A, Rev. 2, 307-13-H4A, Rev. 1

306-13-H4B, Rev. 2, 307-13-H4B, Rev. 1

308-13-H5, Rev. 2

315-13-H6, Rev. 1

309-SB-5A, Rev. 1

309-SB-5B, Rev. 1

309-SB-6A, Rev. 1

309-SB-6B, Rev. 1

310-HS-ll, Rev. 3, 311-HS-ll, Rev. 3

310-HS-12, Rev. 3, 311-HS-12, Rev. 3

312-HS-13, Rev. 1, 313-HS-13, Rev. 1

312-HS-14, Rev. 1, 313-HS-14, Rev. 1

314-HS-15, Rev. 2

300-14-H1A, Rev. 2, 301-14-HlA, Rev. 2

302-14-H1A, Rev. 2, 303-14-H1A, Rev. 3

300-14-H1B, Rev. 2, 301-14-HlB, Rev. 2

302-14-H1B, Rev. 2, 303-14-H1B, Rev. 3

300-14-H1C, Rev. 2, 301-14-H1C, Rev. 2

302-14-H1C, Rev. 2, 303-14-H1C, Rev. 3

300-14-H1D, Rev. 2, 301-14-H1D, Rev. 2

302-14-H1D, Rev. 2, 303-14-HlD, Rev. 3

304-14-H2, Rev. 4, 304-A-14-H2, Rev. 3

305-14-H3A, Rev. 2, 307-14-H3A, Rev. 1

305-14-H3B, Rev. 2, 307-14-H3B, Rev. 1


,

-r>-TELEIXNE* ENQINEERINQ SERVtCES


68.

69.

70.

71.

72.

73.

74.

75.

76.

77.

78.

79.

80.

81.

82.

83.

84.

85.

86.

87.

88.

89.

90.

91.

92.

93.

94.

95.

96.

32-14-H4A

32-14-H4B

32-14-H5

32-14-H6

32-SB-7A

32-SB-7B

32-SB-8A

32-SB-8B

32-HS-16

32-HS-17

32-HS-18

32-HS-19

32-HS-20

32-15-H1A

32-15-HlB

32-15-HlC

32-15-H1D

32-15-H2

32-15-H3A

32-15-H3B

32-15-H4A

32-15-H4B

32-15-H5

32-15-H6

32-SB-9A

32-SB-9B

32-SB-10A

32-SB-10B

32-HS-21

306-14-H4A, Rev. 2, 307-14-H4A, Rev., 1

306-14-H4B, Rev. 2, 307-14-H4B, Rev. 1

308-14-H5, Rev. 2

315-14-H6, Rev. 1

309-SB-7A, Rev. 1

309-SB-7B, Rev. 1

309-SB-BA, Rev. 1

309-SB-BB, Rev. 1

310-HS-16, Rev. 3, 311-HS-16, Rev. 3

310-HS-17, Rev. 3, 311-HS-17, Rev. 3

312-HS-18, Rev. 1, 313-HS-18, Rev. 1

312-HS-19, Rev. 1, 313-HS-19, Rev. 1

314-HS-20, Rev. 2

300-15-H1A, Rev. 2, 201-15-H1A, Rev. 2

302-15-H1A, Rev. 2, 303-15-H1A, Rev. 3

300-15-H1B, Rev. 2, 301-15-H1B, Rev. 2

302-15-HlB, Rev. 2, 303-15-H1B, Rev. 3

300-15-HlC, Rev. 2, 301-15-H1C, Rev. 2

302-15-HlC, Rev. 2, 303-,15-HlC, Rev. 3

300-15-HlD, Rev. 2, 301-15-H1D, Rev. 2

302-15-HlD, Rev. 2, 303-15-H1D, Rev. 3

304-15-H2, Rev. 4, 304-A-15-H2, Rev. 3

305-15-H3A, Rev. 2, 307-15-H3A, Rev. 1

305-15-H3B, Rev. 2, 307-15-H3B, Rev. 1

306-15-H4A, Rev. 2, 307-15-H4A, Rev. 1

306-15-H4B, Rev. 2, 307-15-H4B, Rev. 1

308-15-H5, Rev. 2

315-15-H6, Rev. 1

309-SB-9A, Rev. 1

309-SB-9B, Rev. 1

309-SB-10A, Rev. 1

309-SB-10B, Rev. 1

310-HS-21, Rev. 3, 311-HS-21, Rev. 3

II


<>-TELEDYNEENGINEERING SERVICES


97.

98.

99

100.

101.

102.

103.

32-HS-22

32-HS-23

32-HS-24

32-HS-25

33-HS4

33-H1

38-H1

105.

106.

107.

108.

109.

110.

111.

112.

113.

114.

115.

116.

117.

118.

119.

120.

38-H28

38-HS-1

38-HS-2

38-HS-3

38-A2

39-H9

39-H10

39-H11

39-H16

39-H17

39-H18

39-HS9

39-HS10

39-HS11

39-HS12

39-A2

104. 38-H2

310-HS-22, Rev. 3, 311-HS-22, Rev. 3

312-HS-23, Rev. 1, 313-HS-23, Rev. 1

312-HS-24, Rev. 1, 313-HS-24, Rev. 1

314-HS-25, Rev. 2

3850, Rev 3

3800, Rev. 1, 3801, Rev.', 3802, Rev. 2

2200, Rev. 1

2201A, Rev. 2

2225

2245

2246, Rev. 1

2247, Rev. 1, 2251

C-19711-C, Sh. 1 Rev. 4, Sh. 2 Rev. 3, Sh. 3 Rev. 3

2306, Rev. 4

2307, Rev. 2, 2307A, Rev. 1

2308, Rev. 5

2313, Rev. 4

2314, Rev. 2

2315, Rev. 4

2351-9, Rev. 1, 2352-9, Rev. 2, 2355-9, Rev. 2

2351-10, Rev. 1, 2352-10, Rev. 2, 2355-10, Rev. 2

2353-11, Rev. 1, 2354-11, Rev. 2, 2355-11, Rev. 2

2353-12, Rev. 1, 2354-12, Rev. 2, 2355-12, Rev. 2

C-19710, Sh 1 Rev. 2, Sh 2 Rev. 1

9.3 Yalve and Pum Drawin s

Drawin Number Yalve Number

1.

2.

3.

PA-130064, Rev. 0

PA-129695, Rev. 4

PA-129691, Rev. 0

NG02

NG03

NG08


~<-TELEDYNEENQINEERINQ SERVICES

Valve and Pum Drawin s Continued

4. PB-136241, Rev. 1

5. PB-136242, Rev. 2

6. ACD-31627275, Rev.

7. ACD-31635203, Rev.

8. ACD-31620895, Rev.

9. PA-135191, Rev. 1

10. PB-136358, Rev. 1

ll. PB-136371, Rev. 1

12. PB-137514, Rev. 0

13. C-76395-A, Rev. 0

14. 20511-H, Rev. 5

15. 2F-1037

33-01

33-04

37-07R, 37-08R

37-10R

37-11

38-12

38-01, 38-13

38-02

39-01, 39-02

39-03, 39-04

39-05, 39-06

Recirculation Pump

9.4. Letters Teleco ies and Telecons

Date From To

1. 9/24/822. 11/17/823. 1/10/834. 1/11/835. 4/8/83

Lee A.

Lee A.

Klosowski

Klosowski

Lee A. Klosowski

Lee A. Klosowski

Lee A. Klosowski

Robert D. Hookway

Eric A. SollaEric A. SollaEric A. SollaRaymond M. Pace

9.5 Miscellaneous

1. Stress Rule Index TES Document Number 5838-1

2. 22A2600, Rev. 0, G.E. Design Report Recirculation Piping System

3. Material Comparison Report TES Document Number 5828-2

4. Meeting Minutes from Task Force Meeting ll/23/82 (TES Document

5838-4, Rev. 0, Recirculation Loops 11, 12 and 15 PipingReport, Appendix E)

5. 1977 ASME Boiler and Pressure Vessel Code, Section III, throughWinter 1979 Addenda


<t-TELEDYNEENGINEERINQ SERVICES

Miscellaneous Continued

6. Trip Report 1558

7. Nine Mile Point Internal Correspondence 55-01-013

8. Teledyne Technical Report E-1562-1

9. Teledyne Technical Report E-1289-6

10. Niagar a Mohawk Power Corporation Purchase Order Number 72845

dated 2/28/8311. Trip Report Log TES Document Number 5828-7

Technical ReportTR-5828-1 A-1

-rs-TELEDYNEENQINEERINQ SERVICES

APPENDIX A

MISCELLANEOUS CALCULATIONS

Technical ReportTg-5828-1

. ~LcHKn. eve~ saba~+, p,~pggog. ~pc,C- (5PouJTI+~

5ozz& Pire=-4~0/SHEET NO. OF

~ass

A~~eNo)x AN LNs 't l'i6 Pocl4< R<<><<~~++'~~

5y~~ ~ ~ 32.1

UES<E~ — CA~EoN S~cwu

QPCRATiH6 ~~o: ik~psl

Pgsv~TiON gERCTOI2 '$85SI=L.SoppceveD /9.7 Q'8SL QMQZao~S up~aaC F-a ~ Z</-=V-a~>-/j'~( CowcpcvC'=LgV-) REI=: g i4(@gRoH4~1~ DR4~>Nb e C-/BESS-<

1

~ ~

4- ~

QOzZU=,/VlE'urnF

sue.77'!QyPQ /OO~~ 7.74-7S

Qozz~~ /V'/E

ply@8

$ 0

if ~

D

~0'Y

/I, u

-x~ P'

Q g.= P ~ d" ~7C.

f, = 12-S99K— Nozzle.< rom<

8 p ~go'Ir- = 7iaS xi'X Ib I ~/)q/g N~O~ ~yQ~~&—70 = V8< I- 247.c>l

bP,= (n s'les «)(«'"I» 3 ('7-'~<"'IZ= c . 5 /'S

a x= -n vg4 h.z= c.zKS~y = (~vs.7s -gz~.wsa)C >X~

D- 6<9 I

f


W-lAELIEDII'NEEMG~ ES

DATE l~-~ 2-p EATON. V~~ g~cvvLJ p~

CHKD. BY~~DATE~ij~~Z.P/oz.nc:- 7m'>aiPs~scl

SHEET NO. OF

PROJ. NO. S . 2.

Appenoix A IVih'c'ier Po-iN r Rc 4t2co&7ivnr


SEIIMCESnave~2-9-82.

CHKD. BY~ZQ DAyE /3'gi g2

AweNo/X A

PEACroa. ~g~g (5p~~~~ ~Wprc=.g.mKgg~~~

SHEEr ND, OF

.~ale

Po'It4M REc.'IR.co<Avior&

Szs .=~

CAREoH 5'rae~

PcRATlps CoND: /Q~p ('35'~ Dp

~l>N - QEAcT~~2 g~ss~ g~~~~~D 87 QdsL- ppg

b<>~S ups@) p-~~ p~gg ggq')))~CmC rWV) Rer

3 0 8gg R/c'))p p~ )N(

gOXZ M gj~Pump S>c.? lo

pdoDC lao~~ zpg.yg,'l/$ 0'Y

u

~ ~

~0 p.H<22CL jV./.p"

DP-= 9, d -A7',

— ig.spy~ Not,xc.c p~$P~P 015 c HAR5D

goDc- Z7+247,ot

e >« ~ =671ox)o-",„]„~=38 r-

)( + ~) (6. /Iclx lo H/ ~/ ~)(~~o )~ += o- 282/X g g g~@

4 ) (4 /ld x10" >u/,„/, )(-~ )~ <= o.gyp',~

Technical ReportTII',-5828-1

BY +~ DATE /2. -f~82-

CHKD. BY~L~DATE~~~~ ~ '2P E&ToQ. VGSSCZ 6~~ak FOR.

/vore.u=-7iegm At= @sauce.

SHRKt HO. OF

moo.wo. W ZB

APPEiVDIA A Pie~ g~ Pwr Ream< ~n.Svsrern '32

h k= P,, ~ d -pT'

g = /o. gQgQ

K = g ply xylo ~~)~/ >

47 - 350 F- -7o c- = gcgQ pI

( I+ <~~>IC I< I r) (6 7lo x Id ~l< / r) (g~'t-)4R = Q '234/

z ~= -a-o73/ " az.= o x298~> = (><~» -~sr<<+ )Ci~'~i )(g bio~)o J%~)(g&'> ~)~ ~= <-x~v)

Technica1 Report

~< TELEDYNE ENQINEERINQ SERVlCES

BY DATE3~~CHKO. BY ~OATE3~+~8

SHEET NP. PP

PROD. NP. %828

APiI=ONENg +QgCg g gg I ggg4SWAY STD U7 Pt-+ LO~D

0

/9Z

Y

C, SS-((ooo)= ~ <Ig,~z~

x Qsz)SIN 5 (COb (T,59(OOOO))=T8$ 5Cf4,''

CI >~)CO& 9 (CO> 6:.WS(IOOO))=+ 989,7++

x'is<)cd 25 (co~ O,59(tooa))= taboo.g5@.

CI9~)5I M Z5 (Co> ('59(oooo))= +< Iq, gd w.

I (J ~VATIC X +O'TR ~p(J7~X

ISZ —86,5 f I IS,7Z f8q.75/&g —+66) 4/9 I (9,72 -Q/'7 GQ

-KPCr IZS ISo -'l87,OZ 227,94 5(9. t'5

Ik) ~ATl C Y 8 Cn 4 MgUTS AtZK' k3 7e IJS(04v'-.

qDgCE I<~~ laic 967.o~ -ZZg I -Pgg,85~+-rlC K

i&Z

(SQ

ISZ IO IV -re.lU>(a& g Igq COmP;X y z.

8C. 99 —I I 8,7Z —95'f,7&

-9Oo. q 9 I I 5;7Z —q I'. 55

7OrCS (SS lee —8JS,|' —I 4o'7.( I

~ 'VI I ~ ~ I SF SE ~ ~ 1% P V ~ v

TR-5828-1

r>-TELEDYNE ENQINEERINQ SERVlCES

BY DATE~~CHKD. BY~&DATE~~~ SHEET NO. OF~8'

(I~6Z

looo49~7

Coy)POtJE~ +Cp',~+ OF /cx3o4-~WAy'TRUT PRE L DAD

SSCIOoo) — ~I IS,7Z~

x (Zgz)COB l7(CO& lF 99 CIOC|O))= 190,IQ+

Czez)9ld l7 (do& Co59(l,ooo))=ZZ lO '76~.

~"~AwlC X

x Czos)%IN 97(CCIS C,99gioOO))= F;q79/4a CzqS>

CO& 97 (Coo 6 59(lo.OO))= ~799454,'.cgz I s CQPU\FR='56P g ZgS (s I U ~M5(oAJ

X—+5'Oi/0 I I9,7Z Z IO($8

91,R I - I I 0, 7Z -799, 5

~os~ Zzg Zgo —(5 8.cI —9oz, 8

WA~IC Y. Z rZ

.. ~oRcG S2~r 25o

m>A-riC S- gcnI-I

g$ <g $0~

I+~ )U ~&BIO& $ ZSZ I+ CO<PRE'55m Dy

I9<aol O y Z, 7

S1R'UTS APE trJ WEIU5IouX Y

R@O ID -I I&.7Z- -Z IO 'IG

597,1 t —I I 9,7Z - 1g9 <5Ovc< PZ~r Z<rO D9S l t -227. ~~ -ID&9g9

Technical Report

><-TELEDYNE ENQINEERINQ SERVICES

)BY 'ATE ~~~9CHKD. BY~~DATE~~C

SHEET NO. OFZB

+oF;csq Az 886&

~~TATIC. ~Pl &Id I c- PJ IjH I OOO +QjtJ HAP I +6 RATC1-8'IP.—ggg

Y Pl< —/~ fb PPI@'. -5Z.QQ g-

PE'wULTA,M7 gg/0

~7ATIC ~~5 l~~i 'I IC lrJITH SPP:I 4& PATE 4: ~&IOA.P

%8

PII,-fl /4f W

DI 4, —g~~~g/

aOLTAIJT A/9 /

r

A TELEDYNE ENQINEERINQ SERVICES

BY~ G DATE~0CtlKD. BY~DATE+Z

gag(wog ~ec.«(, I np -(50 Lue

SHEET NO. 'FPBOJ. NO. ZÃ&~,-

Flu& 4,~~- Y~ 3,"

(k2. + +qi, j( '3. k5'<7 ft

Mgt

vv> ~ ~ ~ ~ vv ~ ~ ~ pv > v

TR-5828-1-r>-TELEDYNEENQINEERlNQ SERVlCES

O'C C ~~ OAVE

CHKD. BYE~DATE~~|>gc c.igcu1AYioA Loop - L5 SHEET NO. OF~

PROD. NO..~g

/4- jvcH AL.U6'g

Oi&, = / II.i 0 @ICE'. = P,agr

F lcm''

Loaftd ~t. =

p4cVG 88'- /3

/,8 o. /8

Ug~ve

Ud c.uE

7c rgb (fqguc Vc,7 .'

A TEI EDYNE ENQINEERINQ SERVICES

AAKCHKO. BYS~OATE~ Recit"culorLia& Loc P — L5 SHEET NO.~ OF

PROJ. NO. ~~8

/0 yu p rpw

pldbo tt?5 4

AttvEP Al/ff

F','P = /4',75,g, ] AIi'8= 0E'7%1<'~~(

t,eozlu,)

('o, rm~ g~ )pm+ + )

Bi,Se ~+~t

Vpg,ve ~y-Oi0/C,l ~

'E'h)67H

T

ZZ35 8.QQ IhPe

~>M /5 570TsfL. 4 AT 'Z@5 Y'5 I< ( YE YN4

Y OyAP ~g/~j.

g/c cO +cH-

Pig) r ~ /4'i75 Ie~ 6((k' 0.573 (V

~T+ ( t,aOZ io) -- O.S-OZP &

t Jn~m >AyFT- .- (ja,+ P.)(o,oozy k-)9/l

9S'yfLlJE

'g9' 09

&w7-,'jrZAfdjf'H'S rg

75PEL LV6TI = I/88 l6 + OBW ( >E iu )

5'6" l g P 5 $ Re'gcT. ~me>~ L Dop- igCHKO. BY~OATS J 42 'Sf lO

SHEET NO. OF

7;zcigcuuflio+ guys l5, /gal,'. Ph~~~ch i+ 7ob Zzga

x50 ~id' Ilhvldug+ SSe+S-h" (gESE)

0 +HE'E7 20

tl

+yD Q gt(l

N N~

q.

r/.'h /

h

Porno ~(554cqlog 0 I st@,

/BEE ((F.ZS'jShiuSE')

~Y DATE +'- '.,CHKD. BY~~~ DATE

I4loAC L; P,E QC<OR R6'Gj~C, I OO7,-/gCobkbllVRTL C/)LC(AL/f7/ON/Uagg<~ — / 3 Z~ nest 8 l/3 f

SHEET NO. OF

PROJ.'O.

keF,'@Ajdwa ) mopllwc /50'4 O &E '/4- C. (RE 1/ 2)

CPQr Bysicw4s+ 7obzz.+0

X

o.sr/

.(i~,//d,

'7/5 d)

cS

P PDE

F

gP

]qz) 'Ap "

l.'6

go DG t4o)

QDDF„ l 0 t)I

supp0RT WALL ilTl'3Cf)

t'i)z. sHo 134) ~<>

Tl<hN PtP'E CNo oF

( I)o) .

REF: 5UI'PORT

'3oq-58-gAhHp

MEHI'Oi~~5r, ~y„« t.o~~g

5v1'p6gT''@AT(

p&5

CA~LATig Coar&i~d)PS

s>-TELEDYNE ENGlNEERlNQ SERVlCES

~FACHKO BY3JC Q OATEN/

/>lob<L 'eACT. REc/~ 44'PP- /5Ca~Rereatz C~Lgul g7 ioivqgobH:5 — 2.A. f z5'3

SHEET NO. OF

PROJ. NO.

E<A/I1iom = z,pg-'P

'zF, VIWeA wozIh~vk.4/ Z48+6- C

S~r~r < Ce~~ ~)S.EF Pfi$5IC!jC

m aobEz+o

$ VpPOHT 4TThQWEh/f POINTS

( e2. ANO 2.55) ARE' «/8 LO+E

Ti~~H P) t'E EN ~ oF s ~reoRT > TR~O

REF: 5vPp0RT Ds+5 $ 0$ -$ 6-ioglOB

2,(2$

(Zoo)

/.A'iA/

xg 14V

/~ooE' 5 Z.

h)ogE'pss

( 5'F37~ ZSV.RE 5'5, ~~O( ) '/7

l7'r277

CALCc(687Z'L0 p~o g Dlply)QCg

~«, ( -~ S;W, Z ~a, is%, I+ EZ~)

( '7 C4C,, Zf1 135> jEOYE )

TR-5828-1

(< TELEDYNE ENQINEERINQ SERVICES

BY BATE~+CHKD. BY~DATE~

SHEET NO. OF~Z

AY 57RUT CGLP I GAD ) /CRUCIS AT RODE'9 I &Z @IVY I9$

+E LOAD AFVLIGP 8)'Hg 5WAY'TRUT5 I N 'THE CQ! P

PQ&I~IDhl I & IOGQ~/i4 5 + IOOQW ) 'vol-IGPE g fg WHG CHAU&ElI< I EW &TH Q~ "THE. 9TH UT'5 DUG iQ MHKF,NA,I ~hJ-Vr+C~Iou Aiu~ S= </I-..

~oH ~sR,~L x (HxsggVg): K = t~liv (Ag gT<uvs)

5 (I~>Z) = .SZWC

+ |'I R4) =, 2 f 4

<HEgE+Gg <HG APP-IEe LOAVES A~; I 920 ~ (l5z)IZ'1C 4 (ISW)

>wH qmL~I& %s ),0481 +em I.oNC AAO< eWAU +V5 gl ICAL Q)5TA.Qc.E bW . 5 <eeW

>CI-IER'H-FQW WH

6'GPhPQIJEk)T 0 f- +H E LO4305 I5Sin ySF'(l'<O+ )<eO) = 2'V, 8

V

t- —>(X,B I ~a)yS'I 'MP ~HE 8 ~ ~uE CawiPOUE.~~ A~E)

I ca& I'F .59 (ioz 0) = /0/I.+~ '~)=u.~s ~

Cas C ~ '(IzWo) = /Zg/,0I

-X Caepou<MT

~o5 Zf r'jZQZ) + SIIJS (/9/l ) = /Z76

~RPOUE uT—sin zs'(/z az >+. sos g ('gyp

~vNir~av'. o~ cowpoupu7-zx v'

—/z YC

aqua.'

W-TELEDYNEENQINEERINQ SERVICES

r nBY DATE~CHKD. BY~DATE~F~~@

SHEET NO. 'FPROJ. NO. Z

SNA-/ ~U7 ~Le CO@,D, 5mur~ AW Z5'Z ~D

PRev'loU~ PAGE -rOR 6GUActOV oF A.R=t'KTo -FQkcG,

~Her'~L. z ~on (Hx9RGV5);

3 ~AuC„-.gz) =

> C-5s) =

.9/$ 8

%HE APPLI E D Lo>P~ AQE I &/o (Z~z)i<zo (zes)

(v,srrAUE')

P coNlP'oAJa h.Jl

si~ 6,6 (/s/o + /qzo/= 3/o, 5 w

Mfv I ohms (3> -„p~g)cos /F,93 (IS/0) = / gJO/. & H.co~ c.ss(tycho)= /<10,8 +

X l70

(~c/s) I i

(sS)

-X cc MFOVKM'

I 9 9 7 (/4 // ) —csts / 7 (j$o / ) = —g g JP, 4/"

C+WFavG UT

5/lj t7(/$ o/ /4 co& 87(/+//) = /50 / 2

TJN'uMNA<V'+

Cog~rJEhPr>

v-995' lo f50T

Technical ReportTR-5828-1 B-1

-A TELEDYNEEMQINEERlNQ SERVlCES

APPENDIX B

RESPONSE SPECTRA

a> r

~trna ~ IERIIRIas ss El lsRRass ssssllM aRssstl lf!5I%Ias sac R ss aamn sssss UIBIIs~ cea amas wcL'm~~mssassmsssmasssssmmasssssssasamaaasssssaaaasssssssaumasnaamammmssa

~QSNKRRRRI~RMSIRQQKIN5%850HliHQCXXRIKR)tHHlN~MRRNQSN~~WIHIRIHHHHIBII1HHHIHHRRIRIIE85HHHHWRHIHIIISIHSIHHIKRRHHHRMHSNhHRSllWWNMRIRIRI51IRRRSRIRNRRIIRWNN

~RRWR51INISSRl$ 55RMIRNR~IRW!RRISSWNIRI155IIISRHWR1515IWN515IWMII

NNII W IIWIIISllllMSWSRHS!~~ Rss ~Mwss IsMRMIQsRm~smss $% Rsas assail sRIass snss ssla IRIssssl lassmss %RE~masMHDRss swlssRl~wmsssRRw&pssaaaassssssssaamasssn~amwmssS

~MWaaRRII~~M&sssIISINlsaslss55a~smssRBRIIRCMWRRNHNWKSSHH %$555MRSSllRHNSIIHHHHRI55IHHINHNHWKRSRH

%8 HR551IRHISWIRWS!REN1IIIRRIRS¹IRISIHNRRIII~5 RRNI3$5%%85$ 5IRINIKII15~WHLPP%PLHMSl518lllffM~%%11~N-'%5$~@RRiRI

R IIMHN '1NilR~h~%JWISRHRRINNI185

5 IIIIRI~ il!!l N 1INRIPRSWRIRRNSNIllllllkISlRlh~ N.%@/

~ ~ ii. lllfHu~ 5 la~M Wafi.'$$Ep~RRDRHRswmsRssssIaaaasssUlnsamsMsssa 1 ssRII~~M!ss<MRRF~sms~M~~RsssnssslkaaassssnllsalRlssss~ms&nssdM&~M~RHswic~~wsssmnamsasmssssaaansssslBIIImsssssllRlanslsssssl

rgK~WCISlRH~HSRIHHHHIRISNHHHHHIIHHIHHIIIHNHIHHINHll58H~~~%<a'5WIIINHRHRIRRISIHR RNIHRRRSRHIRR!888RISHINHR

S .iSNII~RIIRIH 1185~555!Elllll585888l5IIIIIIWIIIIIRIHNIIIIIIMHEIN558855lll

I I 5 Rl NIIIMllRII55$l5lllW N

81 5 R1IIS

OCKSPECTRUH

DIRECTION 1

FREQUENCY .... ACCELERATION ..

DIRECTION 3

ACCELERATION

DIRECTION 2

FREQUENCY ACCELERATION

F 100~ 300o500o700o800o900

loooo2e0003oooo4o000F 0006oooo8oooo

lo.ooo20o0005O.OOO

1000000

o054- o058

o070o093oliool20o130o240o320o380o420o420o390

. o3500240ol40olio

o054o058o070

.o093oliool20o130o240o320o380o420o420o390o350o240ol40olio

.. o100o300o500o700o800 ..o900

loooo2oooo3o0004oooo5oooo .

6ooooBoooo

looooo20000050oooo

100o000

... o036o039o047.o062

,. o073o080o086o160o2l3o253o280o280o2600233ol60o093o073

~ ~~ ~

I ~

~rp

I

r

I

~ r Q ~

~ a

gir

~ ~

j

~- ~ ~

fl'

~~ ~ gl'

I ;so['aael '

g 1

l 4

~ ~ ~ P P

0 i ~ '

~ e

5 ~ r,

a

s ~

0

r .

I

(

I

~ C

~ ~

r

0 4

~ ~~ ~

I I

kl

~ y t g f r ~

r

/

rr

I

5

a

~ I ae I ~ ~ ~ ~ '14 44 ~ ~ 11 I \4 ~

I I I 4 }TJP5828-1

. ,;.......,.!." i, f SY

I I C

P7 J;7 7g:";DA

J~t'IAI(~8'~~;,~ ~ t {

. } . I I { >ea { [e{-) j"j-f-))X.~p /5

Q SMVLQES

I '

' I

t

t.ls

C

I

»4 ~ -.I I Q7I

~ ~

~ t.

1

:.,s., 4 }~ ~

I

= ' -.- ~ ~

''6"

. ~ I, ...,. ~ ..., .I....).„j4 e~e

I~ ~

I

s .: ~ I I I

j

I

I

{ I !~ ,'' I

4

{I

.V.....I .

C, '~

~ 4- ~ -;.ee,.i et..t..i. ~./

I

s... e.. 4

I',;~;. ~ .[-4 ~

{

i.I

t ~}

CI I . I

~ 2

~ I ' ~ ' *f

1

I I ( (, ~

I~ ~ '

I I I } I

IIII 4I

I

{I

~ 4C

It

I4..j

I

I t I

I~ 4

I

I~ ~

I aC f 4 "I

~ i~II

~ ~

I

t'

t

I

s

C

L+.4pe

';" t-'aeC I

I

~{'

1 ~

~ I}..~, L

I,.t.-a-e- I

'I

~ ~

?'' ~ " " I''"

~ ee ~ - ~ I I I ~

.. @fly.FO.-ePg-..~lg ...C,uP V{=,, Agl) „

pgEglpjS-'"/ "A+Z QS) 5II,

I I I.4. ~ ~ ~

?--Q..e.. *pgg'}

t

..L:,.":,:,.-:.:..::.: '.,-

1

{-'.' ': I

4~1 w ~ ' w +~6<{},~=:Os..l.8..5' ':41 4

c GQ Ag... ew ~0 t, Ll.7..., {.,I . L,4, '.L

~ I

~ I I I

+".-i."g

C.I I w~ I

I. ~.J

. „...,....:...., .,O(l,....v....,. Q2...,...,.....,...,.:4...0,

'.:-.. ":,:.",;::.'-,.-'.i,equi~'E.'iver'i'wl,.„.82

g 44

I

,.L, i.~ I I

I4

w

~ I

0z

03

0<

PR,(~G~L., PE.VGTr. AT{OH ',- 7;,.;w...:,}.',!..1

FLE4AW{0~- D{= HOZ.EL'' - "r."-O}"-.- p-p;- fO":----. - - e-"--*e- - --"''PF-C{I'COLA { roH .,

t"VH~-.'~gwgL""",:-..P}=K:TQ'0'4i'oN.".:

X-..G6..:., j,.„':, .:....: ...:;...;...";.;., -;,-'-',-:- - ~

-'~CVP>{oa.0F gOZ,~} ~ . {=O<,';.Pi,-,',4",,: ":,l;.;:.;;::,:,"..', },;:,':.';,,-;I;;,",".

~ 1 1 I ~

I I avt II~ I av'll f 4444 PV f te

Tg-5828-1,

5"82+,.S.V.;...C„„.S~ t

':Sae n~m 8//h7.,~CHIL QY~~O> H -'7+"- ' ~ p )~

~ ~ v-.f-.a. L.. - },, ...... „., f„ I .I,.j„)

4

~ » II

I

I t V I

4

.,2....'...:..f

f *'I- a.. 4 ~

)

"'i. " l".f~ ~ ~

~:": ~ --.-"I4

C

4.

I

4

t

~ .4-',

I I

t f t

- ~

I

„I=-I

I

I 4~ f . '=-e

~ ~ ~

I'

255

a

'"" Z35f

I

~ 4

I

I

I

I'

~

I4 ~

! ~

4 ~ ~

I

V ~

I~ ~

44

'

I.L.

V ~4a

~ 'I

I

I „ I I I

;-0

~ 'I

-$'t'-

I'

3 I !

t I f

.',,a J

/CCr L.gP~7goA g

C~3 ~Rahu ~~~ p~~~r= i-u.~«>H 'X-'an.: --;I

.0< C~r~~rlO~l Or- rCACYOl? HOZ.E(:C;"f--.F5'-'Q''.';:: '*-'':::0~ ~~"~"-<~ PS.Hr: l'Ql'q Og ")(--I~i(:".--.-, - ~": . ~

&-EV<~-rfOA gF R,EDCT~CK g(gZ.HALF.;,-ply g

Q5 ELCVATfOg OF Rf-Cl QG(far r(Of~ PVe< (> (~Zf ~af)

Technical ReportTR-5828-1 C-1

A TELEDYNEENQINEERlNQ SERVtCES

APPENDIX C

SUPPORT SUMMARY

~ ~~ ~

~ ~

~ ~ ~ ~ ~, ~ IESREI07W~WWQKH~W&

I~laP>SFa51%8%RRLSRSRK<RF355P'%1SSRHEIRHRr~ka95ti5

1S588RRRI88LEFSI!55mesiewaatreaiwwrjuae8W W RSWWIW88Mr~jFjW~~ee r . NS~~F&a~~l5:.. ESP>'5li

HSB'SSS@$ 858 8

5% .- . RF 45RBP>

~ C, C

pggg~~ 55%, ~

5I - -RI88%- 1I ISR5

LC

L

~ ~ ~ ~ ~ ~ ~ ERREIWW~W&%&~W&

Sla858P~RRSLHQFaMPJ555LLLILwrr~mriaaLLLLl8LPj858555%%%%l%RrSAF~STrf>R LL%%fNzPKN

55 . PW'8/anav>5SSlWiSSfaWagi

~

I

~ ~~ ~

0

~ ~ ~ EEaEBER EReEEESPH~W&SK%~W&

h58555M8%%%%8ILRIRPAFMP25555W %RLLRIRNSRP@M555IS&5&WWW&ILWWFaSPASSS15I1%888IQRILRHl>BR15TiSI858ELIRRlKF'aBFKH1 R.. L % FW SI

=5% .... F~PSal55i- W .. P~EDlSSS-ee . -- a. r~mirir - m

R . 45 5

c

~ ~ ~ ~ ~ IREEHS RRREEI%&~M&WW~W&

N55855SW 'LSLLILmammrsaaa5L LLALLILirrzmkaaa5J1 J JR% JIJSSP@RFdti55

- mW588ELSIEI%LNP>Fa555SLLLLILIRW>FgFNj8L l8 L ~ rm~L FWiil55i

555l5 5N J J F>NPiSlN 8 6 8

~ ~ ~ ~ ~ ~

SW

5Pa5855ENRWRL%8t88RFaPARri555%5l8RLSEILWEr@48555

.

85%1%LLLklESLFAQFdllPI'eeairarwtaia~w~r~aalr.. M Sl RSLIRHSLF'~Fan%>- RW IR r~r'. ar

- 858 M>~ISFia55 P~SRIR D

~a r ~ia~>L ~8 8


<<-TELEDYNEENGINEERING'ERVICES

PREPARED BY: Q.AW DATE -~-cQCHECKED BY: ~ DATE ~a~~F~+

SUPPORT tl0. 32-/Z-H)A 9 tlODE 2,"f

SUPPORT TYPE: COWSTAhT SPRING

As a result of the piping analysis, the design values are:

Load = tzS~o L,X = + c).o'Y = +o-181

K'. Z = + 0.5'I ~

- o-v)R- l7I'

OO"I

From existing support drariing:

Rev.: 2.Drawing tlo.: 3ol - I 2 —8 i 8Load = II,>-5aSpring Size = ~32 <lbao-V

"YQ'otal

Travel = 2,'i<"Actual Travel = )3g," Don<

SUPPORT HO. 52-l2-BlQ 9 l,'ODE 2>SUPPORT TYPE: CONSTANT SPRIhG

~ X = + o-o"'"

Y = + 0-o~~'Z =+ g.7/l

- c.a2o-(79- O.O

From existing support dravY"ing:

Rev.: 7Or airing Ho.: Q o1 - t2-H ) 0Load = //KXnSpring SiZe = s gg i-BS~o-V "3"Total Travel = p 'JzActual Travel =

) ~l~ o~A


Load = J), 55 &


r~-TELEDYNEENGINEERING SERVICES

PREPARED BY:

CHECKED BY:

DATE

DATE

X-83

SUPPORT NO. 3'2->2-H>< 9 NODE 2oSUPPORT TYPE: CONSTANT SPRING

As a result of the piping analysis, the design valves are:

Load = //5g~O L.X = + O.oLY = + o.og

Z =+/.o3

- o.vs 9- /-73- O.Q

From existing support dt awing:

Drawing No.: Qpt-l2 - H iC. Rev.: 2Load = //,5~~Spring Size = ~32 < >6~-<Total Travel = 2'/~ „Actual Travel = 1>/v <~<4

SUPPORT NO. 32-I'2-HJO 9 NODE 26SUPPORT TYPE: CONSTANT SPRING


Load = //,~~a ~ X =+co.oLY = +o.Xo'3—Z =+o'7 )7

From existing support drawing:

Draw'ing No.: 3oi-)5 -H>D Pev.: 2.Load = //,S5oSpring Size = w 3> „<» ~-<Total Travel = Q'lz.

. Actual Travel =) ~/< Dc<~W

Technical ReportTR-SS."S-I

->< TELEDYNEENQlNEERlNQ SERVlCES

r

PREPARED BY: ~ DATE

CHECVED BY: ~/~ DATE

sUPPORT Ho. P2 - / -- H 2. 9 NoDE 22 f

SUPPORT TYPE: CONSTANT SPRING

As a result of the piping analysis, the design valuesC! N

Load = /B~c DX = + o.3IRl'Y =+oo'„LZ = + l.o6

From existing support dravring:

Draviing No. 3c 9 -JX-/-U Rev.: 4Load = /8~Spring Size = ~ ig, F>c 8-4'Total Travel = 2,'I< „Actual Travel =

[ af,~

are:

- o.56b- I-14.- o.o

suppoRT NO. $g -12. - <~ 9 NODE )Q 0


As a result of the piping analysis, the design values

Load = '2o co~ ~X =+o.oY = +o-Zo

~Z = +0 905

From existing support dra;Iing:

Dra;zing No.: „'-".C g-l2- H38 Rev.: 2,Load = /79'~<Spring Size = ~pa F->~g~-H ~>g"Total Travel = 3"Actual Travel =

~/g're:- O-649- 07~/

KC>

Techni cal'. eport,.~»TR-5828-1 .

><-TELEDYNEENQINEERINQ SERVICES

PREPARED BY:

CHECKED

BY'ATE 0 -J Z-c5'3

DATE - 9'- 8$

SUPPORT NO. 3g -fg -3Q 9 NODE /3OSUPPORT TYPE: CONSTANT SPRING


Load = ge ~~ QX =+o 0DY = +o godDZ =+@ yo5


Drawing No.: Zo5- jz -g~ Rev.: 2Load =

Spring Size = ¹3cP F'i6CI-H"g'otalTravel =

3'ctualTravel = ~/8 ~<~+

SUPPORT NO. gZ g Z -r/9'8' NODE

SUPPORT TYPE'ONSTANT SPRING


Load = /'//ZS DX =+ >-+LY =+>.05>LZ =+ o

7g7'rom

existing support drawing:

Drawing No.: 3g6-g2.-~9k Rev.: pLoad = /9oycSpring Size = <35 Fl& 8J-H "8Total Travel = 3"Actual Travel = 3/q Oo~t j

are:

- o-Vr3-0 Qo3-O 6


r< TELEDYNEENQ!NEERINQ SERVlCES

PREPARED BY: — S DATE - - B

CHECKED BY: ," 'ATE - /9

SUPPORT NO. g~ >~ htg3 9 NODE g~O



Load = /g/g~ DX =+ o-OQY = + o.03'7ZZ = +o 747


Drawing No.: 3~ ~g -gg+Q Rev.: gLoad = /3 o7oSpring Size = ~35 F'I 6&I-8Total Travel = 3"Actual Travel = -/q OoMH

are:

- 0-9~3,-a 6d'3- OO

SUPPORT NO. QQ-/g-H5 9 NODE l3 lSUPPORT TYPE: CONSTANT SPRING


Load = g+ou LX =+@-oLY = +o 3Q,„LZ = + ~-27>


Drawing No.: 3'-l2-/5 Rev.: gLoad =

25'pringSize = w j~ p'>~gz yTotal Travel = 7.'/~"Actual Travel =

Technical ReportTR-5S"G- 1

->>-TELEDYNEENQtNEERINQ SERVICES

)PREPARED DY:~~ DATE

CHECKED SY:~)Q DATE - 9 -89

SUPPORT NO. Qg -I5 - HID . 9 tYODE


-o 43/ gQ" O-O


Rev.: 2.Drawing 'No.: 3o/ - g~ -/IlALoad =

'pringSize = ~32. F,sac -V "6"Total Travel = ?'1~Actual Travel = t~/y p~~


Load = ((55o. EN = + o.87/-' = + o. (8,',K"' = + /. K('Q

SUPPORT tl0. 32-/8-Pl/Q 0 tYODE ZZSUPPORT TYPE: COtYSTAt>T SPRING


Load = //,55'g~X = + a.aoY = + 0.07„2 =+(.+7

-a. (4„-/. 7$-9 0


Orawing No.: $~< -gg-~sQ Rev.: 2.Load = II,%So"Spring Size = <32,FYs aa-v "0Total Travel = g'/>Actu l Travel =

oo~~


-r<-TELEDIJ'NEENQINEERINQ SERVICES

PREPARED BY:

CHECKED BY:

IIATE~BZDATE

SUPPORT NO. 32-/5-HJC 9 NODE RO



Load = J/S+D DX = +c).V2<Y =+a

o2'Z

= + /.+oFrom existing support drawing:

Drawing No.: 3O/-g5 -//~C Rev.: 2,Load = Il~+oSpring Size = ~32 F/68< V

"8'otalTravel = 2,'xzActual Travel =

~3g< ~~

SUPPORT NO. 32-/5 Hi~ 9 NODE 26SUPPORT TYPE: CONSTANT SPRING


Load = /g~~~" hX =+a.E5"LY =+a idLZ =+ pe"


Drawing No.: Qol -l5 -HID Rev.:2,Load = il~SD"Spring Size =

B Z p~g ~y ~g"Total Travel = z,yz"Actual Travel =

~ zg„" p~~<


r> TELEDYNEENQINEERINQ SERVICES

PREPARED BY:

CHECKED BY:

DATE /- JS -O3

DATE

SUPPORT NO. 32-/5-HQ 9 NODE221



Load = /gn~" DX =+~ yg6Y = +d.QD<Z =+i.go


Rev.: gDrawing No.: Pop -y~-gg,Load =/~~Spring Size = w ~9 F I c Bog "g"Total Travel =

~'s~'ctualTravel =

,SUPPORT NO. gg-/~-QA 9 NODE /3~SUPPORT TYPE: CONSTANT SPRING

As a result of the piping analysis, the design values are: .

LX = + o.ogPY=+ o gaDZ = +o.87


Drawing No.: g~+ g~ pg~ Rev.: 2.Load = /v gooSpring Size =~ ~pi6g~-H 'g"Total Travel = gActual Travel = 7/g oo~H

Q O


t < TELEDYNEENQINEERINQ SERVICES

PREPARED BY:

CHECKED BY:

DATE -/DATE — - 8

SUPPORT NO. 3+-/g pg 9 NODE 13&

SUPPORT TYPE'ONSTANT SPRING

= o.S9'.

7$0 0


Drawing No.: 3+5- i~ Hp~ Rev.: gLoad = 1p,yeaSpring Size = ~3+ != it,giTotal Travel = g"Actual Travel = ~id @<~4


Load '= Z>u~ QX =+005ZY = +z.3o"LZ = +c.8V"

SUPPORT NO. 3g ig ~yg 9 NODE QS~



Load =. igig~~ LX =+o >2"LY = +o 6Z'=+092'O dl

-061DO


Drawing No.: ~-iS -HqA Rev.: gLoad = 13ovoSpring Size'= ~~ p~~ ~~ + ~>Total Travel =

3'ctualTravel = sf„'>mg


rt TELEDYNEENQINEERlNQ SERV(CES

,PREPARED BY: — 'ATE < -13 -cr 3CHECKED BY: ~ + DATE

SUPPORT NO.. 3Q-/g-/4PQ 9 NODE25D



Load = /gyp'X =+ C-saQY = + 8~3'~<Z =+O e~"

From exi sting support drawing:

Drawing No.: 3'-i5=/4VQ Rev.: 2Load = /3cs7e~Spring Size = ~35 F~+ B~-H '<Total Travel,= 3 "

Actual Travel = ~/~ ~~~

SUPPORT NO. Pg /+ pQ 9 NODE /PQSUPPORT TYPE: CONSTANT SPRING


Load = ~Wed 6X = + o.o"LY =

+o.3g'Z=+o~'rom


Rev.: gDrawing No.: Zo8-15-H5Load =28~Spring Size = ~l'7 F16'-V "S"To.tal Travel =2'l~'Actual Travel =

) ~1>~ P~Q

Technical ReportTR-582S-1

<s TELEDYNEENQINEERINQ SERVICES

PREPARED BY: ~pH DATE

cHEcllED BY:~~ DATE - N-8S

SUPPORT NO. Qg - rn~ -O 7 8 NODE J 7 <SUPPORT TYPE: SNUBBER


Load = g„X =+ 0-o/Y =+o )76-'Z = + o.685

-o 5)2- O.GS |'.

0;o"Change in length of snubber:

Normal operating;— o. 6oMaximum = 0.6o


Drawing No. C- 3Q/$5 -C»> o<0RevisionSnubber Type = ~~<~<'~ ~ '~~~'+'c-Snubber Size = FSA -35Cold Piston Setting = N-h-Hot Piston Setting = g 8-

Rated Desi gn Load = Sa, Go

SUPPORT NO. PQ-c-~'> - -~ 9 NODE

SUPPORT TYPE: SNUBBER


Load = 46sg' X =+V.al Y =+a)76.~-Z = + o 659

Change in length of snubber:Normal operating = -~ 7Maximum = O.S 7


Drawing No. C-ZV~~~ + ~H't=~Revision 6Snubber Type = »~'~'~ ~'= ~'~~Snubber Size = P~~R-SKCold Piston Setting = HhHot Piston Setting = HR

Rated Design Load = 5o,mao

Technical ReportTR-5S2S-1

~> TELEDYNEENQlNEERlNG SERVlCES

PREPARED BY:

.CHECKED BY:

OATEN-c~&DATE 5 ~r+9

SUPPORT NO. Q2- ~ -~ 1 9 NODE >5



Load = $8 I Qy LX =+ o-afY =+o f85l Z =+o.SVQ

- o-7ZS/ v90 0

Change in length of snubber:Normal operating = co. V3 "

Maximum =

From existing support, drawing:

Drawing No. C-3d i'd@-C z~ io~zRevisionSnubber Type = P~e, r- ~ ~~ e~~.~.cSnubber Size = P<h 35Cold Piston Setting = H allot Piston Setting = v,h.

Rated Design Load = 5~ ~&~'I

SUPPORT NO. '3P- mZ,-lo' NODE 13



Load = 4j/c~g .>X = + ~-</Y =+o.o7Il' = + o.7~7

Change in length of snubber:Normal operating = o.(7Yaximum = O,'7p


Drawing No. C,-39) g(-C +> o=Z

Revision 4Snubber Type = I'+«~'<Snubber Size = I'~ R -3,Cold Piston Setting = veHot Piston Setting = H 8

Rated Design Load = ~ D cc><

- a.r2 ~- o.a

Technical, ReportTR-5S28-1

><-TELEDYNEENQlNEERlNQ SERVtCES

PREPARED BY: ~ DATE

CHECKED BY: DATE +5 89

SUPPORT NO. Q2, —M - -J I 9 NODE



Load = /35'~~ X=+ o-ol'Y =+a ~Z)~7- =+o g(g

Change in length of snubber:Normal operating = /-

7t'aximum= /.7g"From existing support drawing:

Drawing No. c.- Z,MII6-C S~Z o~RRevisionSnubber Type = F'hcir=ic Sci~ »<T<Snubber Size = PER 3QCold Piston Setting = HhHot Piston Setting = Hp

Rated Design Load = ~~c ohio

SUPPORT NO. Q2, I.n5 -/2, 9 NODE


As a result of the piping analysis,

Load = /ggg I'X =

LY =

—Z =

the design values are:

+ o.o+O ted& „+o 47>

Change in length of snubber:Normal operating = j.7g

'aximum=( 7g"


Rated Design Load = 5ooaO

Drawing No. C.-SEI IV<-< Sg g or-2Revision pSnubber Type = P r cia <,Snubber Size = PSR 35

. Cold Piston Setting = va'ot Piston Setting = Hb

Technical ReportTR-.5828-1

t <-TELEDYNEENQINEERlNQ SERVlCES

PREPARED BY. ~ S

CHECKED BY:

DATE 0 / -8

DATE

SUPPORT NO. 3 2 - vng Q2.


-0 7'/-73O.O

Change in .length of snubber:Normal operating = D <73Maximum = a.pe


Drawing No. C,-39 I 9g-C. 5 H ~om gRevisionSnubber Type = P<ci~ic 4i~~~ r=<cSnubber Size = PS,A-35Cold Piston Setting = H+Hot Piston Setting = t'~~

Rated Design Load = O oo</

As. a result of the piping analysis, the, design values are:

Load = 2cgc)g*

DX =+o-oQY = + o.03'

=+/ o3

,SUPPORT NO. 32-m5 -'25 9 NODE l7>SUPPORT TYPE: SNUBBER


Load = ZX = + a.o"LY = + o-I &'"

LZ = + o.79"

Change in length of snubber:~ Normal operating = D.Sg

Maximum = c.'77


Drawing No.C -39IVS=C 5~ I o~3RevisionSnubber Type = Pnc.Yr-ic Scic=~a-, r=,~Snubber Size = PSA-3SCold Piston Setting =ra

~ Hot Piston Setting = wP

Rated Design Load „= ~co,~

, Technical ReportTR-5828-1

-r<-TELEDYNEENQINEERINQ SERVICES

PREPARED BY: — S

CHECKED BY:

DATE~DATE

SUPPORT NO. 3 2 - rn S —W5 9 NODE 1 70



Load = + ggc) DX = + Ogo"DY = +4014"LZ

=+&.79'hange

in length of snubber:Normal operating = Q 5/Maximum = g gg"


Drawing No. c.- 3 9>9K-C S>~ i or- QRevision gSnubber Type = PAc ~c Scil=.&T<p= cSnubber Size = pZA -3+Cold Piston Setting = HAHot Piston Setting = 86

Rated Design Load = 5W o~SUPPORT NO. Q Q-~$ -2 I 9 NODE /Q

.SUPPORT TYPE: SNUBBER

As a result of the piping analysis, the design

Load = QQ'7+7 zx =+ ~87LY=.+a

tQ'Z=+

/ $ 8Change in length of snubber:

Normal operating = 0.3CMaximum = f ~c/


Drawing No. C -39~'F6-C S~ to~<Revision 4/Snubber Type = P~~«'~«<~~~~'~Snubber Size = PS& 35Cold Piston Setting = HAHot Piston Setting = Hh

Rated Design Load 5o, COCA

values are:

- o.6/,- l QO" 0-D


-w TELEDYNEENQINEERINQ SERVICES

PREPAREO BY: !='7l 5 0ATE~C'- 3 B3

CHECKED BY: ' DATE

SUPPORT NO. 32- ~S- Q(5 9 NODE lgSUPPORT TYPE: SNUBBER


Load = 4/@ $7',X = + a.9oQY =+ aa6QZ =+ / 0'/

Change in length of snubber:Normal operating = cp./SMaximum =


Drawing No. ~ - 3 cpj V4-< 5w l o~ 2RevisionSnubber Type = P~ <~~~~

Snubber Size = PS&-3~Cold Piston. Setting = tUA-Hot Piston Setting = wA

Rated Design Load = +W oOc3

values are:

- 0-61-/ rKO.O

SUPPORT NO. Qg-P3~ 2 l 9 NODE IQ



Load = /]3~ nX =+O go<Y =+o ]oZ=+)~]

-o 7.2- /-7'P

OO

Change in length of snubber:Normal operating = /-77Maximum =


Drawing No.C-30/46-C <HA o~2,RevisionSnubber lype = &&Civic Sci~~r>vieSnubber Size = PSA-3SCold Piston Setting = aleHot Piston Setting = PA

Rated Design Load = KAco~~


-s>-TELEDYNEENQINEERINQ SERVICES

PREPARED BY: WZ 0ATE~8CHECKED BY: ' @ DATE -

/0'UPPORT

NO. 3g-~S -~< 9 NODE l~/



Load = / 4 /P~ LX =+o.e8'Y

=+o./g"Z =+/.P~

Change in length of snubber:Normal operating = 1 /7Maximum =

~ 7+"


Drawing No. C -3Q/Q5-c. ggg, p„gRevisionSnubber Type = PA<i~'ic- Sci~=~vir-i~Snubber Size = |PWCA -~Cold Piston Setting = RAHot Piston Setting = N 6

Rated Design Load = QO,oOO

values are:

SUPPORT NO. ~ -H5- jr 9 NODE 3,Q a3SUPPORT TYPE: SNUBBER

- o.3g"- O.O

0 0Change in length of snubber:

Normal operating = O. /oMaximum = o.VQ"


Drawing No. 22~/~~Revision eo~uwc~eu-Snubber Type = f=i62o[ 5 S~n<c=Snubber Size = 2 h. cy'zCold Piston Setting = 2 veHot Piston Setting = 3"

Rated Design Load


Load = /C Qg/ EX = +~-<PY = +o-J 7AZ = + 0.7$

I


- -r<-TELEDYNEENQlNEERING SERVtCES

PREPARED

BY'HECKED

BY:

DATE

DATE — / P- 5

SUPPORT NO. Q2- W5-2/ 9 NODE



Load = /p+~g ZX = + c.qgQY =+ o og'

Z = + (. <1"

- D.73

O.

0'hangein length 'of snubber:Normal operating = D. 9'gMaximum = / gy."


Drawing No. c, - 3Q /i/ (g-QRevision ~/Snubber Type = i~cir'«S«i<7iwtc.Snubber Size = PSk-'3gCold Piston Setting = H6Hot Piston Setting = HR

Rated Design Load = 5O,O~

SUPPORT NO. $ Hg g 9 NODE~op



Load = 4462" LX =+o.a'Y

= +O./QLZ = +o.5'3

Change in length of snubber:Normal operating = o.o5Maximum = 0

22'rom


Drawing No. 220 <Revision /Snubber Type = Pl< "„~ ~ ~~ ~Snubber Size = A '/~ cY<Cold Piston Setting = Q~/t6Hot Piston Setting = g 3/q

Rated Design Load =

are:

- 0;79'0.22„- o o9


s> TELEDYNEENGINEERlNQ SERVlCES

PREPARED BY: ~ DATE 0-/~-CHECKED BY: - 7~8'ATE 4 /+ 85

SUPPORT NO. 3$ -HQ -J 0 9 NODE 3 ~ ~ l



Load = g gag LX = + o.~eY=+0

DZ =+o 32

Change in length of snubber:,.Normal operating = l-2 /Maximum = / g g "


Drawing No. 235 I -~Revision ISnubber Type = Fig %~D / ST EDicE=

, Snubber Size = ~ "< ~~~Cold Piston Setting = 2, "l~~Hot Piston Setting = g ~/ie

Rated Design Load = /6 35

are:

SUPPORT NO. 3, f-PQ -Q 9 NODE Q Q 2,/SUPPORT TYPE: SNUBBER


Load = 2'7R~ pX =+0.opQY =+no'Z

= +c.Z<

Change in length of snubber:Normal operating „= &->8~Maximum = O. Vc9


Drawing No. 2 3S/- 'lRevision /Snubber Type = F'1& Roc 8 'Svaovi~Snubber Size = 2 '~z. cv E.

Cold Piston Setting = 2, ")i6Hot Piston Setting = g ~/iq

Rated Design Load .= /D, MO

are:

- o.g8- i.BI- 0-O~

1


rs-TELEDYNEENGINEERINQ SERVICES

PREPARED BY:

CHECKED BY:

DATE~DATE

SUPPORT NO. 32 -JQ-g g 9 NODE Q g~SUPPORT TYPE: VARIABLE SPRING


Hot Load =8o'old

Load = 42

Normal Operating

2 X =+o.q 1

4 Y = +o.olaz =+j.i~"

2 Y =-/.Z)"

from existing support drawing:

Drawi'ng No.: Q/5-g~ pbHL =c9aCL =CASpring Type = Fi & Q -g ~Spring Size = "9"> ~ ~

Rev.: I

SUPPORT NO. 3Q-/Q-Hg 9 NODE gL/~SUPPORT TYPE: VARIABLE SPRING


Hot Load = 8OCold Load = g2

Normal Operating

DX =+0 OZY =+O oats<z =+ o g~g

L Y = -/.2o'

c).s 8'I- /-Zd-O.O

from existing support drawing:

Drawing No.: 3/5-/2-H6HL = c9o"CL=42Spl"ing Type = t=ie B-24&Spring Size = "g",w ~

Rev.: l


-W-TELEDYNEENQINEERINQ SERVICES

PREPARED BY:

CHECKED BY:

DATE

DATE ~ ~~ 88

SUPPORT NO. Q8-/J28 9 NODE QQ)QSUPPORT TYPE: VARIABLE SPRING


Hot Load = c9/oOCold Load =83]O

Normal Operating

DX =+c3-DQ Y = +o./5DZ =+o.23

DY =


Drawing No.: 222+HL'= Btoo ~CL = 772KSpring Type = F >6 gZSpring Size = "F", ~/6

SUPPORT NO. 39-8/I 9 NODE 3o1~3

SUPPORT TYPE'ARIABLE SPRING


Hot Load = 2,gmCold Load = 2, c/<g

Normal Operating

QX =+O.O4 Y = +o.38"<Z = + o.SO

DY = O.gg


Drawing No.: g3 ag .

HL = 2.2.Co"„CL '= g+g /Spring Type = Fi& 8%Spring Size = "0"y ~~3

Rev.: <


r< TELEDYNEENQINEERINQ SERVICES

PREPARED BY:

CHECKED BY:

DATE -J5-DATE

SUPPORT NO. 3Q - H Q 8 NODE

52'UPPORT

TYPE: VARIABLE SPRING


Hot Load = g/Ag DX = +O.OBCold Load = )7gg DY =+O",

DZ =+a 2>Normal Operating DY = -y ~~i


are:

-o 9S„- ].82-oo9

Drawing No.: 2306HL = 4>~HCL = /73OSpring Type = t=jb 0~Spring Size = "5" l2.

Rev.: 9

SUPPORT NO. 3 I -HlO 9 NODE 3 l l2SUPPORT TYPE: VARIABLE SPRING


Hot Load = 3)oo DX =+c~Cold Load = 3I$5 QY = + c.S3"

'Z

=+0.3)'ormalOperating 2 Y = a.~3"


are:

Drawing No.: 2QoQHL = 9looCL = 3c/ooSpring Type = Fib 82Spring Size = "F" ~ J3,

Rev.: 2


r~ TELEDYNEENGlNEERlNQ SERVlCES

«««r «««ee «««ee «««r r«««««r r«r ««oe oooo ««««««««««eo r «ee «««««««r ««r 4 rr rr««««oe oe 0 r ««oe rr

DRAWINGS) NINE NILE POINT UNIT 1

VHR PASS WITH SWAY STRUTS e 1000>/»

DATEs THR04/12/83 PIPING ANALYSIS SUPPORT SUMMARY PROGRAM

HEV Gforce«rrrr«rr««r««rr«r«ee«r«r«ee«rr««r«rrrrr«r«r«rrrrir«r«rrrr«r

SUBJECTe REACTOR RECIRCULATION LOOP 12

PROJECT!'

5828 I~e ef «r rrrr«r rr«r «r

I

Ieee «co««reed ««««r»««roe««eerrr«rr««~rr«ee«ee«r«r«rrrr«reerrrrr««««r«rrr««reer«r««r««I

N 0 Z Z L E / A N C H 0 R R E A C T I 0 N S

POINT CONDITIONFORCE (LBS)

FY FKMOMENT (IN«LBS)

MX MY MZ

100 WEIGHTTHERMAL,(4)THERMAL (")OBE SEISHICHAX SEISMICOBE ED EDHAX Eel DY

10270

«8805178517853925392

r ee rr ee rr1083111461

«34006710

«26507688768873647364

««rr«««18362

«21102

100160

«8605111511156075607

r««««««10978

«11478

83690107910

«139130374592374592493648493648

«rr«««r1059841«923681

«3105370

«12810202288202288276800276800

r««r«r»484149

«492209

13232050100

«190890213918213918259262259262

««rrrr«655601531751

I

275 WEIGHTTHERMAL (+)THERMAL (")OBE SEISHICMAX SEISMICOBE E,EDMAX E ~ E ~ DX

(+)(ee)

10880

«2703963396332643264

«««rr«r8117

«7487

7102650

«67105212521244164416

ee«rrr«r12989

«15629

«100860

-16O423442343),003100

««««eer«8095

«7595

674800

«85690244606244606268164268164

ee«r«««r580251

«530981

«902051730«8160

1985741985742194002194OO

460684435154

27940725430

«268S10234348234348229252229252

«rrrr««1216970ee704470

Techni cal Report

TR-5828-1

->>-TELEDYNEENGINEERINQ SERVICES

re«e«we«e«swee««»»see«»«ere«reer«see«err»e«esses«e«roe««er»ere«see«ore«««ooooI DATKt TNR PROJECT!I 04/12/83 PIPING ANALYS1S SUPPORT SUMMARY PROGRAH 5828 II REV G I««see«res«««wer«ws«sw«w«s««wesweeesses«««s««e««sees«««w«wee«sr«e«e«se«««sere«

SUBJECT) REACTOR RECIRCULATION LOOP 12 II II DRAWINGS'INE MILE POINT UNIT 1 II THR PASS WITH SWAY STRUTS RIGID IIsw»ww««ss««e«se««««w«re«w««««««w«««r««««rse«w«r«s«e«««e«»sere«ees«ee«««»e«»I

N 0 Z Z L E / A N C H 0 R R F A C T I 0 N S

POINT CONDITION FXFARCE (LBS)

F'Y FZHOHENT (IN»LBS)

NX HY HZ

100 WEIGHTTHERMAL (+)THERMAL (s)OBE SEISMICMAX SEISMICOBE EoE ~

HAX ED EeDY

(+)(«)

«10270

«88019651965

984984

seserw«3209

«3839

«34006710

«26505651565129362936

«sere««11898

»14638

100160

«8601794179414351435

r«wee««3490

»3990

83690107910139130

94011940117312073120

«see«s«358731

«222571

«3105370

«1281086137861378164081640

«ses'ree172837

«180897

13232050100

o190890125586125586

8638886388

e«e«eer394395

»270545

275 WEIGHTTHERMAL {+)THERMAL (e)QBE SEISMICMAX SEISMICOBE E ~ E ~

MAX E,E,OY

(+)(«)

10880270

1645,1645

599599

»sere«e3135

«2505

7102650

«67104220422038253825

re«e««e11406

-14046

«100860

«160~ 1609

1609820820

sse«se«3189

«2689

674800

85690187516187516199380199380

eeeees«454376

«405106

«9020'1730

«816077088770887619376193

w«seer«195992

«170462

27940725430

«26881079959799595387253872

o«es«se887202

«374702

Technical Report

TR-5828-1

EENQlNEERINQ SHIV'tCES

'W 'W Aw &% &W W W H 'w 'w w &% &W & % &&& 0+ &~ &e &&&A % 0 & 0 ~ W W W 'w w W 0 W 'W & w Ol W Io A W A w w &W &% % % % & &w w & W W w W w W W W &

I DATE:I 04/18/83 PlPlNI&% W % W &N W W H % &% W N % % W % W &&&W

I SUBJECT+ REACTORII DRAWINGS:I

7('i f<

G ANAI YSXS SUPPER'!'U (:.A/;Y P!tt't PA';tC(' (i

WWWW&WWW&4PWWSW&WW'IOWW&&IA &&&\It&&WAN&

t C1RCl!LAT1UN LDt)> l 5

ivINE Hlt. E PUlt-'T d~(l'f= 1

'KHR PASS ~1Th S!~AX S'i wi("(6 (~( i ooott/"

PVOJ!.C k".

5@ 2tt 1)

))

'

&% W W % A W W % W W &W W ~ N &Wl OO W &W & 'A &&w &&W & & &W 0 W W && W W &% W w & W w w W W w w w wI0ZZ

LE�/

AH(.'HOB A C i I t.'( 6

POINT CDNDITXONV(!RCE (LBS)

FY t'

(rt((„(: ~'1'l((-L(.S>(~ X ,li /

100 HEIGHTTHERMAL (t)THERMAL ( )DBE SEISMIC'AX SEISMICOBE E,ED

'NAX ED EeDY

(+)(-)

"1b00

"32306458e45858e55865

W Sl PP 0' % W

12323-15703

201V8600

184008'/9o879b66296629

%&A&&%&

2201635836

1b0730300

o600o600'1 0027002

& H &W &~ IP

)44b3"13753

32((9015((8440-1&bt 0v

41) 0) 64) 1<") 64343!(34343y3

WW&A

23bt', /30-10((b) i u

14«502(! r3'/0

03i(i 04b34 i. t(4b53v21853V218

W&WW

il35t)8ob'! 1i'.66

0662(JG

-Hlb4802ow'i/ 1

2ew'/ol313 17i313)72

~ w oe w w & W

ee45b3- ls2t 193

275 Wh IGHTTHERNAL (t)THERMAL ( )OBE SEISMICHAX SEISNICOBE ED ED

NAX EeE~DY

700

3b206583658347254725

%&WW&laW

11379-)47b9

3270?22ev-5680

5123512340654065

w w % pp W &Ol

34'1 1911b99

19010360

1302)302'14371437

W&OIIOAWW

13290"2740

-1( e7100

»6029602324)62324)o21(04b2)0045

Syeya wesw

44(i(t b 211b2132

580901497010

0o) 23()2'1/3U2c'/348g9)348

W%%&mO

2)597bG-o0 /t. bo

-() 185935207((

-19lbb60s236293236292b'95!32b953.3

~ ~ &&w&&8'133b2

-2bt~05(. i

3822 HEIGHTTHERMAL (t)

'HERMAL ( )OBE SEISMlCMAX SEISHICDBE E ~ E ~

NAX E ~ E ~ DY

(+) .(-)

-1102890

02'100

"210015101510

WWWWWAw

6390-3720

6680((

3030salb131513741374

lO W W & 'W &%

9370-2o90

-320

),064G3(124342413041304

weewwto&%

4729-lb689

34)33v0

-bl66)V8!3bb,

. 8),3Fbl/909v

. )29090'WWWA WA

bb1b0b-38bo3>

3'/6/00

b22600)5/b43l 5'/843)('Vti27

'(/~(V627&~&&M8'/b J (1),

«943((V)

l523V9 l'/39

\'49

/c.'4m.'/2

504 tV. b04(tv

'W & ~ W % & W

)82382-'1b4 (.i'

Technical Report

TR-5828-1<> TELEDYNE

NQ

'w eee w w w w w w w w w w w w / sp w Q 're w w w w w w w w w w w w w w w w w w w w w w w w w w w w w w w w w w w w w w ee w w w w w w w w w w w w w «w w «««I DATEoI 04/18/83I

TERPIPING ANALYSIS SUPPOH'I SUMI'CHARY PROGRAfi

HFV G

PROJf.:,C'C:. I582ff I

Iw w w w w w w w w w w w w w w w w w Q w w w w w w w ee w w w w w w w w w w w w w w w w w w w w w w «w w w w w ««w w w w «w w w w w w «w w w w «w w w

I SUBJECT!I'DRAMINGS:

I

REACTOR RECIRCULATION LQQP 15

f<INE MILE POI:<T V i41 I 1

TMR PAS» WITH S'~AY STRuJ ~ ('voow/"w w w w w w w w w w w w w w w w w w ~ w w w w w w w w w w w w w w w w w w w w w w w w ee w ee w w w w w w w ««w w w w «w w ee w «w «««««w w w w 1I

N 0 K K L E / A N C H 0 R R E A C T J O if S

POINT CONDITIONFORCE (LHS)

FX FZf',O.:Ef T (Xf'-L»S)

i~ X f"Y M'j'.

3992 WEIGHTTHERMAL (t)THERMAL (w)OBE SEISMICMAX SEISMICOBE E ~ E ~

MAX E E ~ DY

(t)( )

1903190

0864864

14361436

56812301

12500

«35901001100121232123

wwwwwww

4374-5464

100

«430603603944944

wwwwwww

1548"1988

-23i967440

041395413956267662676

wwwwwww

169192106392

31048130

0gbb322~5327669078690

ww«w««w155663

-107223

56270199770

02384223v4259729>9729

««w«w«w33961/-83572

Techni cal Report

TR-5828-1

% % &W % W &&% % N pl % &%W &Q % % W W % % % u &W % % &% % + H % % % % w &W W & 10 % % &&w % W W % W &&% W % w &W % W w 0 w OP W W &w W &&

PROJECT:5828


TMR PASS WITH SWAY STRUTS RIGID%%&WWWN%&HWHN%%%&H+W%&W%%%WNH&%%NH%W'WHAWWHWWH&%&MA&tNA'WWHHOIWHIW&&&&HWPOA&&&%WWI

DATE: THR I04/18/83 PIPING ANALYSIS SUPPORT S(tNMA tt Y 8 ROGR AMi I

REV G IW W H % W W W % + + % Q + W % % % % % W $$ + W Q W W m + 0' m w + % % W % % H u W &&&w % &% % W &W % % W A % && % & H % W w % H w w w A Ol W & w %

SUBJECT: REACTOR RECIRCULATION LOOP 15'

IDRAWINGS! I

I

N 0 Z Z L E / A N C H 0 R R E C 7 I 0 N S

POINT CONDITION

100 WEIGHTTHERMAL (+)THERMAL (~)OBE SEISMICMAX, SEISMICOBE E,EDMAX E ~ E ~ DY

(+)(-)

FX

1500

"32303126312619241924

%%%%'%%%

50508430

150730300

2868286821132113

% Sl W % W N %

5861"5131

FORCE (LBS)FY

20108600

184006941694146704670

ewraaea18201

-32021

328901508440

1956001087011087019131591315

}741347"362727

14450249370

02179872179871,82026182026

WAWH&&%

663834"400014

666200

-815480l55807j bb80'I,13b31b135315

W&&%WHH

357742-1039982

Hor~VNT (Itt-LBS)HX t:Y i~i Z

275 WEIGHTTHERMAL (+)THERMAL ( )OBE SEISMICMAX SEISMICORE E ~ E ~

MAX E,E.DY

(+)( )

700

~352032603260

930930

WW%%%%'a

4260~7640

327022260

56804560456042534253

awaNAA~3434311223

19010360

01670167015391539

W ~ I% % 'P W +I

137b93209

1067100

602960190884190884193718193718

HWWW%W%

384603-1094273

580901497010

0146514146514

5852758527

HWWW&%%

1760142~20b042

-61859352070

1915b601237 3712373/

84414844 /4

W % W % W Ot &

498421218b63l

3822 WEIGHTTHERMAL (+)THERMAL ( )OBE SEISMICMAX SEISMICOBE E ~ E,MAX E ~ E ~ DY

(+)(")

1102890

02070207011091109

QWHHWA&

59603290

66800

~303013171317

847847

% Ill/ % % % + %

88452165

&3200

106403588358810241024

%AWW&WW

4612"1b572

3413300

-51e6908198281982Hb16385163

AWAWWOIW

508475342505

376700

-e22600l50322lb032214'I 91114'I 911

WWWW&%%

33b903883163

1523091739

02370323703373723/372

~ W W Ol W OI %

1680456J075

Techni cal Report

TR«5828«1

7

»eeeeeaeaeeaeeaaeeeyeeeeeeeewaaeeeaeeaaeawaeww«v«awe«wee»a»awe«»wawa«w«ave«a«, I DATE: rMR PROJECT: I

04/18/83 PIPING ANALYSIS SUPPORT 8'UMMAicY PROGRAM 5828 II REV G Ia w a v w a a a a e a w e e 'w e e a a e a w w e a e e a w a a e a e e w a w w a «w w w w w w w w w» w a w w a e w e» w w v w w w «w w «w «w w w a w

I SUBJECT) REACTOR RECIRCULATION LOOP 15 II II DRAWINGS'INE MILK POIN'1'NIT 1 II TMR PASS NITH SIAY STRUTS RIGIO IIw w w w a » wee a e e a e a» w e e e »a w w e w a w w a a» a a a a» a a a e w a «a a e ««a a a w w a w a w «w «w «a w w w w «w w «w v w 1

N 0 Z Z L E / A N C H 0 R R E A C T I 0 N S

POINT CONDITION FXFORCE (LBS)

FY FZ'aOME(~ T ( Ih LBS)

MX " »Y MZ

3992 HEIGHTTHERMAL (+)THERMAL (e)OBE SEISMICMAX SEISMIC

'BE EoE ~

MAX E,E,DX

(+)(e)

1903190

0786786832832

»eawaaa49981618

12500

»3590944944

10831083

a e a e a e 'e

32774367

"100

-430583583562562

aaaawww11461586

231967440

035435354353362633626

awe»a«a134181

71381

31048) 30

031220312203548035480

«wav«ww115141-66701

56270199770

026496264902934729347

»ww«vww311878"55836

Technical ReportTR-5828-1 D-1

. <> TELEDYNEENQINEERlNQ SERVlCES

APPENDIX 0

STRESS SUMMARY

Technical Report

TR-5828-1<s TELIEDYNE

ENGINEERlNQ SERVCCES

9'10008/"XsrrisereeeewereeeeeieoerrsrerosreresrsrerreoroesrrerwrrossereessseorsorsrseI

I DATE> THR PROJECT! II 04/12/83 PIPING ANALYSIS SUPPORT SUMMARY PROGRAM 5828 II REV G IsrrsrsrrerrerrsrrrerereeerrsoreessrireereessrrerrseeerresrrsereeeeereesreesssI SUBJECT) REACTOR RECIRCULATION LOOP 12 II II DRAWINGS: II

T R E S S S U M M

NC r 3652

MODE

100101103105110115120125130135140145150155a56

,205210215225

.250254255260265270275

EQ ~ (8)PSI

8261,8433»8134

'078,

8077,8076,8074»8073,8073

'073„

e078,80690810008043,4409»8063080750

'0440

8052;8037,8034

'022,

8020».8030

'i88

~

8123

'»OSH

PSX

17500,17500017500o17500

'7500,

17500,17500,17500»17500o17500

'7500,

17500»17500,17500»17500,17500,

'7500o17500

'17500o

17500,. 17500,

17500'7500»

17500'7500

'7500

'Q»(9)PSX

10096,11471 ~

9559'789,

9057

'38'0265»

10953,11398»11473

'09620

9478,9059»

10744,5602»9478,8747

'640»

9282,9370o9308

'662,

850908758

'554o

9472,

1»2SHPSI

21000 ~

21000021000021000

'1000,

21000,21000

'1000

'1000,

21000,21000,21000021000021000

'1000,

21000,21000

'1000,

21000021000021000,21000

'1000»

21000'1000,

210000

ALL POINTS COMPLY WITH THE RULES OF NCr3652 ~

Techtlical ReportTR-5828-1.

-ss TELEDYNEENGINEERINQ SERVICES

eeepeoppepeooppeoepeeeeoeepeoopeoppooeopooeegoopoppooopopoepoopooopooopopooooI DATEs TMR I,I 04/12/83 PIPING ANALYSIS SUPPORT SUMMARY PROGRAM'I REV 6 I«eaaaooyaa»epe»«»epee»ae«ae«eep«oooo«epee««ysppeaoeo««epee»eoeeoeewooepeeaooeoX SUBJECTS REACTOR RECIRCULATION LOOP 12 II II DRAWINGS! NINE MlLE POINT UNXT 1 II THR PASS WITH SWAY STRUTS 9 10000/" IIa«a««aeeeaa»«a»pep»see»»»a«pa«epee»o«ee««ee««»ee«»eee««»ape»epee»epee«epee«I

S T R E S S S U M M A R YNC e 3652

EQo(10)PSI

SAPSI

EQ» (11)PSI

SH+SAPSI

THERMALCONDITIONS

100101103105120115120125130135140145150155156205210'15

225250254255260265270275

ALL POINTS

577 o

1274,735o435,487o539,

83o829a975o

1010,'176o

1351»337io2360o1026,1323,1802o849,

'89o

1238»1292o1528,1582

'61),

355201669,

COMPLY

'27812'7812,

27812,27812,27812,27812,27812 o

27812,27812o27S12,27812,27812,27812,27S12,27812,27812,27812,27812,27812,27812»27812,27812,27812

'7812,

27812,27812,

WITH THE RULES OF NC«3652 a

1

1

1

1

1

1

1

1

1

1

1

1

1

1

1

1

1

1

1

1

1

oe

22

e 22

e«

2

22

e

2e

22

o22

«22

Technical Report

TR-5828-1W. TELEDYNE


aeseeaeeseeeeeseasoeesesasessseeessessseseesesesesseeoeoess'seseeeeeeeeesseeeeDATE! TNR PROJECT! I

04/12/83 PIPING'NALYSIS SUPPORT SUHHARY PROGRAM 5828 II REV G IssrsresasesasssssaeawsesoeeserseesssessseeessoessseseseesesseeesseeeeseeeeeeeI SUBJECT! REACTOR RECIRCULATION LOOP 12 II II DRAWINGS! NINE MILK POINT UNIT 1 I

.X THR PASS WITH'WAY STRUTS RIGID IIeaaeeesr»eesereassesssssosseaeessesseesesesseeeesesesesoeeaeessseseeeserseeI

S T R E S S S U H

NC s 3652

NODE

100101103105110115120125130135140145150155156205210215225250254255260265270275

EQ ~ (8)PSI

8261o8433,8134

'0,78,

8077,8076,8074o80730S073,8073,8078o8069,S100,8043o4409

'063

'075

'044,

8052'037

'034

'022

'8020,

8030o8188o8123,

ioOSHPSI

17500 ~

17500 ~

17500o17500

'7500,

17500017500,17500,17500,17500,17500o17500

'7500,

17500'7500,

17500'7500

'7500,

17500 ~

17500'7500,

17500'7500,

17500,17500>17500,

EQ ~ (9)PSI

8792,9312o8635

'428

'447,

8451o8379,8425

'6970

8526oS505o8476o8484,8647,4679oS698 ~

8650,8460o8492 ~

8603o8482o8266o8266

'443o

8666o8853o

io2SHPSI

21000'1000

'10000

21000'1000,

21000 ~

,21000o21000o21000,21000

'1000,

21000,21000o21000o21000,21000

'1000

'1000,

21000'1000

'1000,

2i000o21000021000o,21-000o21000,

ALL POINTS COMPLY WITH THE RULES OF NC 3652,

I

Technical Report

TR-5828-1r< TELEDYNE


e oooo r e o re oooo»oooo coo e or«ared re oar or dr «ed e oe ee e r d or re orre o ooe eer eeodeere ceo«DATEi TMR PROJECT! I

04/12/83 PIPING ANALYSIS SUPPORT SUMMARY PROGRAM 5828 II REV G IOre»aero»err«a»»re»O«r«a»rreedae«ear«rara«O»re«rrr«errrrererr«adore»dr ~ re»OreI SUBJECT! REACTOR RECIRCULATION LOOP 12 II IX DRAWINGS'INE MILE POINT UNIT 1 II TMR PASS WITH SWAY STRUTS RIGID IIepee»ra»eeorrra»err»»oar«oooo»aero»re»oooo»rrrrorrrrraoeroroeeeeeoeoeaoere»I

S T R E S S S U M M A R Y

NC « 3652

NODE

1001011031051101151201251301351401451S0155156205210215225250254255260265270

EQ',(10)PSI

577 ~

1274'35

'35,

487'39

'83e

829'75

'010

'176

'351,

3371'360

'026

'323

'802

~'49

~

989,1238,1292

'528

'582

'611,

3552,1669

',A

PSI

27812'7812,

27812,27812,27812

'7812

e

27812'7812

~

27812,27812e27812

'7812

'7812'7812o

27812 '27812,27812

'7812,

27812,27812,27812

'7812'7812

'7812,

27812,27812,

EQ,(11)PSI

SH+SA'PSX

THERMALCONDITIONS

1 o 21 r 21 r 21 21 r 2

e1 e 21 e 21 e 21 o 21 o 21 r 21 e 21 o 2

1 r 21 r 21 o 21- o. 21 o 21 r 21 e 21 o 21 o 21 d 21 o 2

ALL POXNTS COMPLY WITH THE RULES OF NC«3652'

Technical Report

TR«5828-1

a« 'a «a a w a a e» w a w a a a a« a w a a« w w w a« w a a w w a a a« a a a «a» wee a a «w «a w w w w ee w a« w «' a w a a a a «w «a «««w «

I DATE: TERI 04'/18/83 PIPING ANALYSIS SUPPORT SU'<t'lARY PROGPAt>

REY G

PROJECT:5828

~!a a I»a a W a a a a W wa aaaw aa w w «« a« «a «a w a a a« a a« «a a «a« a «w w «w a a w «a a« w «!»a a w w w «a!» «a!e a a ««w w a w «Js a «

NINE NILE POINT UNIT 1

TMR PASS WITH SWAY STRUTS

I SUBJECT! REACTOR RECIRCULATION LOOP 15II DRAWINGS!I 9 10000/"

I

II

Iwwweeeeawawwaaawe»waaaaaaaawwaaaaaawaawwawawwwwww«««aaww««a«ac»«wee«wee««wee«aaawaf

S T R E S S S U H 'A

NC 3652A R Y

NODE

100101103105110110115120125130135140145150155156205210215

'225250254255260260265 .270275260

3802

EGA�

(8)PSI

8126,8209,8171 ~

8090,8044

'032

'058

'054,

8054,8057,8058,8090,8074»8095»8051

'412

'074»

8074'044,

8049'031

'0280

8024,8014,8054

'1640

8189'228,

8087'456

',0SH

PSI

17500,17500

'7500

~

17500,17500

'7500

'7500

'7500,

17500,17500,17500

'7500

'7SOO

~

17500,17500,17500

'7500

'7500

'7500,

17500,17500

'7500,

1750017500

'7500,

17500'75oO,

17500'7500

'7500,

EGA�

(9)PSI

10371,11927

'746

'288

'896.

8833'844

'0578,

11136,11472

'1523

'0997.

9523'302

'08v4,

Saei,9191

'707»

8596'115,

9120 '9060»8719 ~

8398'492,

9186»9665.9813

'411

'0387»

1 ~ 2S>'SI

21000'1000

'1000~

21( u0 ~

210(i'1000

'1000

'1000

'1(!GV ~

21GOV ~

21000'1000,

21CGO ~

21000'1000

'1000.

21000,21000

'1000

~

21000'1t00,

210( 0,21G00 ~

21000'1000.~

21000.21000

'1000

'1000

'1000.

'echni cal Report

TR-5828«l<> TELEGYNE

ENGÃEERRQ SERVCES

a a a a e a e e a e ace e a a e e e e e e a e a a e a e a a «a a a a a a a a «a «a «e a a a a a a a a «a a a «a «a e a« a ««a a «a a ««a aI'ATE! TKR P RO J F-C'1': 1I 04/18/83 PIPING ANALYSIS SUPPORT St>ÃblARY PROGPA>4 5828 I'I REV Ge a a a a a e a Ipl e a a a a Ma a a a a a a a a «a a a e a a «a a a a a a ««e «a «««««««a a a a «««a «a «a ««««a v «««««« '«««I SUBJECT( REACTOR RECIRCULATION t OQP 15 rII .DRAWINGS: NINE @II.E. POlNT UNlT 1 II THR PASS WITH SHAY STRUTS (+ 10004/" IIa ace a a e e a a a e a a a e a e e a e e e «a a «e a« a a« a a a a «a a «««««a a «a a «a «««a« a «««a a «a a ««««««v «a I

S, T R E S S SNc 3652

A R

'ODE

38033804380638073808381138133888381438153816381738183819382038213822

1103902390339043905390939103911391239133914391539163917

EO ~ (8)PSI

4987»5314»5508

'646

'653

6448'049

'103

'379

'925,

6132»6722,6812.,6403,6021.7926

'890,

8027,8152

'664

'158»

6350'829

'196

'468»

6715'871,.

6075,6123

'351,

6269

'»OSH

PSZ

17500'7500

~

17500'7500

'7500

~

16400'6400

'6400,

16400,16400

'6400,

16400'6400»

16400,16400

'6400

'6400

'7500,

17500'7500

'7500

'7500,

15900'5900

'5900

'5900

'5900

'5900

'5900

'5900,

15900,

EQ ~ (9)PS1

7353'123

'325

'201

'004

'933,

7227'626

'094.

725f ~

7304'038

'899

'332.

7890'1361,

12961»8861,

13950'806»

15344,15112,10201

'0107

'433

8304'219

'713.

7821.8288»7374,

1 ~ 2SHPSl

21000 ~

21000'1000

'100'1GAO

~

19680.19&80 ~

1968V ~

19680 ~

19epo ~

19680,19680

'9680.

19680,19660.19680 '1968u ~

21000'1000

~

21600'1000

~

21000 ~

.>9080.19080

'9080

'9080

'9080.

19080 ~

19080.19080

'9080.


a a a a a a a a a a a a a a a a a a a Q a a a a a a a a a a a a a a a a 'a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a ss a a a a a a a

PRO<)KCT:5828

a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a ee w a a a a a ss a a a a a a a a a a a a a ss ss a a a «a a a 1

I DATE: ~ r~R II 04/18/83 PIPING ANALYSIS SUPPQHT SUh)MARY PHOO<<AYI'EVGaaaaalalaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaassyaas aaaaaaaaaaaaassisssaaa«»I SUBJECTS REACTOR RECIRCULATION LOOP 15 lII DRAWINGS: NINE MILE POlNT VNll 1

I rMB PAss w1TH sv AY s l'i u fs 9 loons/"

S T R E S S S 0 'I X A R Y

NC 3652

NODE

39183919392039213922

, 3923392439253926392739283992

EQ ~ (8)PSI

6195'239~

6119'015

'092

'803~

6193,6400,6110

'930,

6542,2802

'',OSH

PS?

15900'5900,

15900'5900

'5900

'5900

'5900

'5900

'5900

'5900,

15900

'Qo(9)PSl

8404,9218

'332

'332

'436.

10085,8793.8201 ~

6980.79s8,9715 ~

3913,,

1.?SHFSl

19080,19080

'9vso

19080'908u,

1908'9080

'9080

'908o,

19080.1908u.19080

'LL

POINTS COMPLY WITH THE RULES OV NC 3652 '

Technical Report

TR-5828-1

w TELEV(NEENQMEERMQ SERVK ES

a a a a a a a a a a a a a a a a a a a a a a a a a a % a a a a a a a a a a a a a a ee a a ee a a a a a a a a a a a a a a a a a a a a a a a a 'a a a a a a a a

I*III

SUBJECT!

DRAWINGS:

" I DATE.!I 04/18/83Ia a 'a a ee a a a a a a

PIPINGTHR

ANALYSIS SVPPQR'f.'UYit1A+Y PROGRAiel

REV G

a a a a a a a a ee a a a a a a a a a a a a ee a a a a 'a a a a a ee a a a a a a a a a a a a a a a

REACTOR RECIRCULATION LOOP 15

NINE RILE POINT UklT 1

'I'HR PASS WITH S".AY STRJTS ea 1OOOf:/

PROJEC f e

5828

a a a a a a a a a a a a a a ee a a a a ee a ee a a a a ee a a a a a a a a ee ee a a ee a ee a a ee a a a a a ee a a a a a a ee a ee a a a ee a a a a a a a a a a a PI

S T R E S S S U 0! t! A A Y

NC " 3652

NODE

100101103105azo110115120125130135140145150155156205210215225250254255260260265270275260

3802

EQ,.(10)PSI

2990,6602

'688,'980,

1999'878,

2798'857„

2915'974

'988

'054

'124,

7053'718

'613,

588l»7953

'615

'670

'767

'789,

3881'639

'489,

8158'530»

3840,2988»

12868»

SAPSI

27812,27812 ~

27812'7812

'7812

'7812

'7812,

27812'7812»

27812»27812»27812

'7812,

27812»27812,27812

'7812

'781'2

~

27812»27812

'7812

~

27812'7812,

27812'7812,

27812,27812»27812,27812,27812»

e

t'.Q ~ ()1)Psl

SHtSAf'S I

Tdf,"ICb>AfCO.iDI7IOVS

224

4

A a

4 a4'

a

a~e

44 a

a

4 54 a 5

aa

(] a

0 ~

Techni cal Repor.t

TR-5828-1

w W 'w w w w w W w w w w w w W w W W w e e w e 'e w w e w e w w e e w e e w e w w e &e e e e e e e w e e e e e w w w e e e e e w e e e e w e e w w e w e e

I DATE! . TNR

I 04/18/83 PIPING ANALYSIS SUPPORT Sl«~AHY P

I REV Geewwwwwwwwwwwwwwwwweewwwewewwwwewewwweweeeeeeeeeeewe

I SUBJECT!, REAC TOR RECI RCUI ATIUN LOOP 15II DRAWINGS: NINE NILE POINT UNIT 1

I THR PASS MZTH Si>AY STRUTS

ROGRAHPRO JEC1 o

5828

}0000/"

e e e e w e w e e e \I e e w e e 'w e w e w e e w w

w ww wwww www w e ww w }

S T R E S S S 0 N J% A R Y

NC 3652

NODEEQ ~ (}0)

PSXSA

PSIh,i.(l})

PSISHIKSA

PSITt~r".t<HAL

CO~D1TI04S

38033804380638073808381138}33888381438}53816381738183819382038213822

1103902390339043905390939103911391239133914391539163917

'11906,8765

'587

'225

'898

'0183%

5956,5313,

11323,12369.5356,2926,1572e2804,'904%

6938'573%

607,3501,3284,6287%6190,6777

'5270.

15235'537

'3774

'3159

'}920

'874%

3442e

27812'7812

'7812

'7812

'7812,

27600,27600

'7600,

27600,27600%27600

'7600,

27600'7600

'7600.

27600,27600,27812%27812,27812,27812,27812

'7475e

27475,2747Se27475

'7475

'7475

'7475

'7475

'7475'

00

w

w

w

Technical Report

TR-5828-1

EEM~EERKQ

a se a a a a a a Q a a a a a se % a a ss a a a a 'p a a a a a a a a a a a a a a a a a a a a a a a a «s a a a a a a a a a a a es a a a es a a a a a a es a a a a a

PROJECT:5828

PATE: TNRI 04/18/83 PIPING ANALYSIS SUPPffR'f'Uf'NARY PROGRAMI REV G

a a a sea a a es a a es a a a a a a a a a a a es se a se a a a a a a a a es es es a a a a e' es a a a a a a a a a a a se a a e a a a a es a a a a a a w a a a se

I SUBJECT! REACTOR RECTRCULATIObl LOOP 15II DRAWINGS: NINE blI LE POX f~"T UNIT 1

I PASS W>Tf'f SWAY S.jRUTS ,4 )000~/n

)I,1'

a se a a

I

1

«aaaaaaesaaaaaaaaaaaaaaaaeaaaesaaaaaaeaesesaaaaseaaaaaaaesesaseaaaaaesesaweaaaa»esseaasegI

S T R E S S S U tl Ni A R Y

NC a 365?

NODE

391839193920392139223923392439253926392739283992

EQ» (10)PSI

9662»10197~

'331,

5262'813,

9749'883t

4485 ~,4196

'3900

4517,1385

'APSI

27475,27475

'7475,

27475'7475

'7475

'7475,

27475,

27475'7475'7475,

27475

'(~, (11)PS)

SH+SAPSl

THERHALCGi'J Ci 1'T IOfs S

Q a 3

0 30 3

0 - 3

P a 3

0 3P a 3Q ~ 3

p5

0 5p a

AlL POXNTS COMPLY WITH THE RULES OF NC 3652 '

Technical Report

TR-5828-1

a a r a a a a 'a a a a a a a a a a a a a a a a a a a r a a a a a a a a a a a a a a ee a r a se a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a

NINE MI4E POINT Vl<IT 1

THR PASS HIT)( SNtAY STl(0'1'S HIGID

I DATE: THR PROJECTI 04/18/83 PIPING ANALYSIS SUPP(.)l(T SUMMARY PRO('RAV = 5828I REV Ga r a a a a a r a a a a a a a a ee a g a a ee ee es se a a a a a a a es a ee a a a a a a a a a a a a a r a a a a a a a ee a a a a a a a a a a ee a ee ee

I SUBJECT'EACTOR RECIRCULATION LOOP 15II DRA'r/INGS!I

III

IIII

Ia a a a ee a a es a a a a a ee a a a a ee a a a a a a a a a a a a a a a a a a es a a a a a ee a ee a ee se a ee a a a a a se a a a a a ee ee a a a a» a a a r a a I

T H E S S S 0 M

NC 3652l! A R Y

NODE

100101103105110110115120125130135140145150155156205210215225250254255260260265270275260

3802

EQ,(8)PSI

8126 '8209,8171,8090,8044,8032

'058,

8054'054,

8057'058,

8090,8074,8095

'051,

4412'074,

8074»8o44,8049,8031

'028

'024m

8014'054,

8164,8189

'?28,

8087'456,

1 ~ OSHPS?

17500'7500'

17500'7500,

17500'7500,

17500 ~

17500 ~

17500'7500,

17500'7500,

17500,17500

'7500

~

17500'7500

'7500

'7500

'7500,

17500'7500

'7500

'500o

17500'7500,

17500'7500,

17500'7500

'Q

~ (9)PSL

9017 ~

9685m9144.8863

'512,

8432'739,

8473,8441,dH99,8712

'510,

8491'626

'717,

s707„8582.8609

'434

'463

'685,

8519'441,

8278'225

'597,

8665,9034,836n.SeSS ~

1 ~ 2S)iPSI

2100() ~

21000'100()~

21000'1000

'1000,

2100() ~

21000'100''(l

e

2.1000 ~

21000'1000

'1000

'1V()() ~

21000'1000

'10OD

~

21000,2100(),21oooe21() oo.21000,21000 ~

2100oe21000

'1000

'1(.'OO

~

21000'1000

~

21000.

'echnical Report

TR-5828-1

a a a %e a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a»e a a a a a a a a a a a a a 'a

PROJECT:5828


THR PASS HITM SWAY STRUTSa a a a a a a'a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a»e a a a a a a a a e» e» a a a e» a a a a a a e» e»»e a a ee a a a a a a a a a a»e II

I DATE; THR II 04/18/83 PIPING ANALYSIS SUPP<>R'0 SUNI'ARY PHDGRAt". II REV G Ia a a a a a a a a a a a a a a a 'a a a a a a a a a 'a a a a a a a a a a a a 'a a a a a a a a a a a a a a a a a a a a a a a a a a a 'a a a»e e» a e» e» a a a a a

I SUBJECT! 'EACTOR RECIRCULATION LOOP 15 II 1

I DRAWINGS'I RI( ID

T R E S S S U M N

NC - 3652A R Y

NODE

38033804380638073808381138133888381438153816381738183819382038213822

1103902390339043905390939103911391239133914391539163917

EQ ~ (8)PSI

4987'314

'508

'646

'653%

6448'049%

6103'379,

5925'132,

6722,6812%6403

'02i

~

7926,8890

'027%

„

8152,4664,6158,6350

'829»

6196'468

'715

'871,

6075,61.23,6351,6269,

1,0SHPSI

17500'7500

~

17500'7500,

17500'6400

'6400

'6400,

16400'6400,

16400,16400,16400

'6400,

16400'6400%

16400'7500,

17500,17500„17500,17500

''5900.

15900'5900

'5900,

15900'5900

'5900

'5900,

15900

'Q

~ (9)PSI

6574'371

'758.

7619'662

'706

'151,

6603,6937

'084,

7141,7S06,7674

'114

'503

'0725

'2236

'561,

11838%7920%

11980,11916

'5o5,

8157'105

'608

'630

'818

'89?

~

7393'959.

1 ~ 2SHPSI

21000,21000

'1u00

~

21GGO ~

21000'9680

'9680

'968u

~

19680'9680

'9680

'9680

'9680

'9680

'9680

'9680

'9680%

21000,21000 ~

21000 ~

21000 ~

21000,19080

'9080.

19080'9080,

19080'908v

~

19080,19080

'9080,

\

Technical Report

TR-5828-1

a a a a a a a a a a \ a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a w a a a a a a a a a a a a a a

,I DATE:I 04/18/83I

Tl~HPIPING ANALYSIS SUPPORT SUhlNAHY

PBn(".RAh'KV

G

PHOJECT: l5828 I

Ia a a a a a a a a a a a a a a a a aalu 'a a a a a a a a a a a a a a a a a a a a a a a a Is a a a a a a a a a a a a a a a a a a a a as a a a a a a a a a a

I SUBJECT! REACTOR RECIRCULATION LOOP 15 II 1'DRAWINGS'INE h>ILE POINT UNIT 1 II THR PASS HITH SNAY STRUTS RIGID I

a a ass a a a aa a a a aa a aa a ap a aa a a a a a a a ass a aa aaa ss a a a a a a a a a as ass a a a aaaei a es a esa aa a a a a a a a a a a II

S T H E S S S U h< H A H Y

NC " 3652

NODE

39183919392039213922392339243925

- 3926392739283992

EGA�

(8)PSI

6195'239~

6119'015,

6092'803,

6193'400

'110,

5930'542,

28 0'2~

1 ~ OSHPSI

15900e15900

'5900

'5900,

15900,15900,15900

'5900

'5900

'5900

'5900,

,15900

'Q~ (9)

PSI

7267 ~

7577,7) 30 ~

I094 ~

7658'973

'611

'563,

6673')21

'555

'522,

1,2SHPSZ

19080'9080

'9080

'9080

'9GBG

~

19080'9080

'9080

'9o8v.

19080'908o,

19080'LL

POINTS COMPLY WITH THE RULES OF NC 3652 '

Technical Report

TR-5828-1

~r> TELIEDYNEERPIMEERMQ

W % % %%% ~S W % '% % H W % &% % % fP Q H %H % W % W % % % A W &% % % &W H &H &&&W W H A Sl W el IO %

I DATE'&H &&&W W H A Sl W el IO % A % % H w W % w IO % % W &Ol H W W w & W W fO % % &

I 04/18/83 P

TkR

IIPING ANALYSES SUPPURT SU otiARY PROC

T RPROJECT'RAM

5828 I1

REV G%% w w w % &fo & w w % '0 w %% A 'p oI % % w & w w w w op &m &H % w &% w m w &N&W%W%H%&%%

I% ~ W H % W &&W &W W W W W fa &w &H % w &% W w W &N

I SUBJECT! REACTOR RECIRCULATW W W W fa &w &H % w &% W w W &N &w H W && W W &H W W A H H &

IION LOOP lb l

I DRAWINGS!II

ININE NILE POINT UNIT l

l~TNR PASS WITH SitlAY STRUTS RIGID

%%WNNPW%%%%%%%%%%%%+lo&%W&oIWWW~A&&W&W W % % W W A A lO W

l~8 &W &&& W W W W W W &W &&mme m esse se w yew w w ea w w m w ee m w w I

S T R E S S S U H ~) A R X

MC 3652

NODE

1001011031.0511011011S120125130135140145150155156205210215225250254255260260

'265270275260

3802

EQo (10)PSI

2990,6602,6688,2980

'999

'878,

2798'857,

2915'974o

2988'054,

3124;7053,3718

'613

'881o

7953,3615

'670,

3767'789

'881o

2639,2489,8158

'530

'840,

2988o12868. ~

SAPSI

27812,27812,27812,27812

'7812,

27812o27812

'7812,

27812,27812

'7812

'7812

'7812,

27812'7812

'7812o

27812o27812

'7812,

27812,27812,27812o27812,27812,2~81227812,27812,27812

'7812

'7812o

EQo (11)Pb I.

Sh+SAPS1

Vault.a.~

ALCONDITIONS

2 524 - 54 54 - 54 S

4 54 a 5

4 - 54 ~ 54 5

4 ~ 54

55

4 54 a 54 544 b4 - 54 w 54 5

54 ~ 540 20 2

'echnical Report

TR-5828-1E

ENQSlEEFHNQ

a 'w w a a w w a a w a a w W a a W W w a a a a ee a w a a w w a a a w w w a a w a w a a w a a w w a w w w w w a a a a a w a w a w a a a w w w w a 'w w a a w

I DATE! TMR, I 04/18/83 PIPING ANAI YSI S SUPPORT SVlilklARY PHOGRA<

I REV Gawwaaaawawawwawaawawaaawaawawwaaawaaawaaawwwawwwwwaaaawawa

PROJECT!5828

SUBJECTS

DRAltjlINGS!

REACTOR RECIRCULATION LOOP 15


TMR PASS 'iilITH SHAY SVRU1S HIGXOIw a a w w a a a w w w a w w a a a w a w a w w w ee a ee a a w a a a w w a a w a a a a ee ee w a ee a w w ee ee w ee ee w w w w ee ee ee w a ee a ee a w w ee a ee a ee 1

S T R E S S S V M K A ie Y

NC 3652

NODEEQ0(10)

PSISA

PSIEQ0 (11)

PSISH+SA

PSI7HEHlilAL

COWOlT10isS

38033804

-380638073808381138133888'81438153816381738183819382038213822

11039023903390439053909

'910

3911391239133914391539163917

11906,876506587

'225,

3898'0183,

5956'313,

11323012369,

5356'926

'572

'804,

4904,6938

'573

6070350103284,628706190

'7770

15270,152350

7537013774013159,119200

8874 ~'442

'7812

'7812,

27812'7812

'7812

'76000

27600027600

'7600,

27600,27600

'7600

'7600,

27600'7600

'7600

'7600,

27812,27812

'78120

27812,27812

'7475,

27475<27475„2s475027475,27475

'74750

27475'7475'

w

Q

p000 aQ ee

p w

0„00] w

0pp w

Q

ppQ a

00Q

Q a

Q ee

0p w

0-00 a

-Q a

222

222222222'

1

2223333

333333333


a a a a a a a a a a a a a a a a a a a g a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a

I DATE> TMR PROiJECT: 1I 04/18/83 PIPING ANAt,YSIS SUPPORT SUAHARY PROGRAH .5828 II REY G'a a a + a a a a a a a a 'a a a a a a a a a a a a a a a a a a a w a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a a aI SUBJECTS . REACTOR RECIRCULATION LOOP 15 II II DRAWINGS ~ NINE MILE POiNT UNIT 1 1I TNR PASS WITH SWAY STRJTb RlGID '

~raaaaaaaaaaaapaapaa'aaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaI

S T R E S S S U tl $1 A H Y

N C 3 6 5 2

NODE

391839193920392139223923392439253926392739283992

EQ , ( 1 0 )PS I

9662'0197

'331

'262

'813

'749

'883»

4485'196

~

4390m4517

'385,

SAPSI

27475'7475„

27475'7475'7475,

27475,27475,27475~27475,27475

'7475

'7475~

hQ, (11)PSl

SH+SAPSl

THKHYALCGND1TLUNS

0 30 30 - 3

0 - 30 30 30 30, 30 50 50 " 'b0 5

ALL POINTS COMPLY WITH THE RULES OF NC 3652 '

Technical ReportTR-5828-1 E-1

-w-TELEDYNEENQtNEER(NQ SERVICES

APPENDIX E

STRESS RULE INDEX CALCULATIONS

TECHNICAL REPORT TR - 5828REVi NOo 0 TKI %DYNE IENGXHEIERXMl3 GIERVXCKG

88NN88888888NN88NNNN88NN8888NNNN8888NN8888PROJECTS 5828 20 APRIL HNSTRESS RULE IISEXNINE IIILE POINT INIT I

~888888NNNN8888NN8888888NNNN8888

BY EZ5 MTE ~z'z3cee

PROGRAM NAMECOMMON i C DANIELS223SR I i EXE ) 3

TITLERECIRC LOOP 12

CREATION DATE6-DEC" 1982 17853

RUN DATE 8 TIME13-APR-83 10i42329

NODE100101105115135155156200'05225270275

STRE SS RUl E INDEX'4l SUMMARY'4l

DESCRIPTION SRISAFE END 2o070ELBOM 1+238RUN PIPE 1 i187RUN PIPE 1 i189VALUE io201ELBOM io227PUHP 1+315PUMP iii97ELBOM io197VALUE ii200ELBOM 1.282SAFE END 2+091

BY XLR'" DATE HLZ+~NSSSNNSSSSNNNNSSNNNN888NSNSSNSSSSNNSSSPROJECTt 5828 20 APRIL 1983

STRESS RULE IHDEX

HIP% HILE POIN INIT 1

NSSSNSNNNNNNNSSNNN8888888888888888NSN8

CRS DATE

SHEET HO, OF

TECHNICAl REPORT TR - 5828 - 1

REVO HOO', TELEDYNE ENGXNEERXNG SERVXCEG)8

PROGRAM NAMECOMMON 1 C DANIELS223SR I i EXE 8 3

TITLERECIRC LOOP 12

CREATION DATE6-DEC-1982 17153

RUN DATE R TINE13-APR-83 10i43o26

NODE NUMBER 100 DESCRIPTION SAFE. END

SY ( Y IElD STRESS)B2 (PRIMARY STRESS INDEX)P (OPERATING PRESSURE)Ci (SECONDARY, STRESS INDEX)Ki (LOCAL STRESS INDEX) iiiiiooooC2 (SECONDARY STRESS INDEX) iooooK2 (LOCAL STRESS INDEX) iioiiiioiC3 (SECONDARY STRESS INDEX) ioioiK3 (LOCAL STRESS INDEX)EA (MODULUS OF ELASTICITY> i i o. o o

EB ( MODULUS 5F ELASTICITY)Z (SECTION MODULUS>TEMP ON A SIDE OF NODETEMP ON B BIDE OF NODEALFA OF HATERIAL A ~ ooooooototoooALFA OF MATERIAL B oooiiiiioooooiPIPE OUTSIDE DIAMETER i+ i i o o i i i i iPIPE MALL THICKNESS o o i o o o i i o i o o o

MXDEADWEIGHT o o o o ~ o t 83693 e

THERMAL 1 oi.ooooo 107908oTHERHAL 2 o o i. o o i i

-139128'AXIMUM

THERMAL RANGEDEADMEIGHT RESUlTANT

CALCULATED VALUEPH = (P)(Do)/2TPB = (B2)(DMH*X)/ZRESIDUAL STRESS.OF=

THE STRESS RULE INDEX IS

tt ~ o 19350o00OS O 1 i00oooo 1055o00OOOO 1 o10O O O O 1 i20

~ ~ O ii00O 1 o80

O O O io00O O 1,70oooo 25800000

'+i i 26100000'o ~ o 577 o5210

oooo 550o00ooi ~ 550 F 00oooo OO9760E 05

0.7120E-05OOOO 28O0000OOOO io0500

MOMENTSHY-312

'371i

-12814'45594'56567o

S OF STRESS14067'71

i27000+67266o

2O070

MZ

132320'0098'190895+

TECHHICAL REPORT TR - 5828 " l.REVE HOA 0 TELEDYNE ENGXNEER XNG SERVXCES

8888888888888888888888888888888888888888888888888888

PROJECT A 5828 20 APRIL 19MSTRESS ROLE ISEXHIHE HILE POIHT OHIT 1

88888SSSSSS8888888888888888888888888888888888888888888

DT —DATE

CHKO

EDEET DD DF =--

PROGRAM NAHECOMMON l C DANIELS223SR I EXE '

TITLERECIRC LOOP 12


RUN DATE R TIME13-APR-83 10143D28

NODE NUMBER 101 DESCRIPTION ELBOM

SY (YIElD STRESS) A A D D A A D A i D D

B2 < PRIMARY STRESS INDEX)P (OPERATING PRESSURE)Ci (SECONDARY STRESS INDEX>Ki (LOCAL STRESS INDEX) .DDAAC2 (SECONDARY STRESS INDEX>K2 (LOCAL STRESS INDEX) AAADAC3 (SECONDARY STRESS INDEX) A

K3 <LOCAL STRESS INDEX> A..AAEA ( NODULUS OF ELASTICITY)EB (NODULUS OF ELASTICITY)Z "< SECTION MODULUS >

TEHP ON A SIDE OF NODE D D D D D D

TEMP ON B BIDE OF NODEALFA OF MATERIAL A ADDDAAAAiAALFA OF HATERIAL B AADDAAADDDPIPE OUTSIDE DIAMETER A D A A A D o

PIPE MALL THICKNESS D D D D D D A A A

HXDEADWEIGHT AADAA.A -83686DTHERMAL 1 AAADAAAA -107903DTHERMAL 2 DAAADADD 139114D

'AXIHUH THERMAL RANGEDEADWEIGHT RESULTANT

CALCUlATED VPN = (P)(Do>/2TPB = (B2><DMHAX)/ZRESIDUAL STRESSQF=

THE STRESS'RULE INDEX IS

AADADD AD 19350DOODAADDA ~ 3D60A ~ DAAAD ~ 1055 F 00

~ DAD 1D20~ AD ~ D ~ AA 1 DOO

A A D D D A 4D80D A ~ A D A A D',00A A D D A A A ~ 1AOO

DADDY ~ iAOOADDAAA.D

25800000'AAAADDD25800000'~ AADDDD 577 '210

DDADDD AD 550 F 00ADDDDAD ~ 550AOOA ~ DADDD ~ OD9760E 05

AD ~ ADDD OD9760E 05DDDDD 28D0000DDAD ~ DDD iD0500

MOHENTSMY

312A

-5270'2809D

345551D156553'LUES

OF STRESS14067 D

976'7000A5685'Z

-132308i-50088D19087ii

TECHHICAL REPORT TR - 5828 ,- 1

REVB HOo 0 TELEDYNE ENGINEERING SERVICES8$ 88888888888888$ 888888888888$ 88888$ 888888888888888888

PROJECT B 5828 20 APRIL 1983

STRESS RULE IHDEX

HIHE NILE POIHT UHIT 1

8$888888888888$ 888$ 888888888888888888888$ 8$88888888888

BY~

DATE ~+'~'

BABB~ |ITE uizgzg

SHEET HOB OF

PROGRAM NAMECOMMON o CDANIELS223SRI o EXE r'3

. TITLERECIRC LOOP 12

CREATION DATE6-DEC-1982 17 t 53

RUN DATE R TIME13-APR-83 ioo43o29

NODE NUMBER 105 DESCRIPTION RUN PIPE

SY (YIELD STRESS) o o o o o o o o

B2 (PRIMARY STRESS INDEX>P (OPERATING PRESSURE) ooCi,(SECONDARY STRESS INDEXKi (LOCAL STRESS INDEX>C2 (SECONDARY STRESS INDEXK2 (LOCAL STRESS INDEX) ooC3 (SECONDARY STRESS INDEXK3 (LOCAL STRESS INDEX)EA (MODULUS OF ELASTICITY)EB (MODULUS OF ELASTICITY)Z (SECTION MODULUS)TEMP ON A SIDE OF NODE o o o

TEMP ON B SIDE OF NODEAl FA. OF MATERIAL A o o oo o o o

ALFA OF HATERIAL B o o o o o o o

PIPE OUTSIDE DIAMETER'IPE MALL THICKNESS o o o o o o

ooooo 19350oooooooo iooooooo'055oooooooo '1oio~ ~ ~ oo io20ooooo 1 oooo oooo io80ooo loooooooo io70ooooo 25800000oooooo 25800000oooooo 577o5210oooo'50oooooooo 550oooo ~ ~ oo Oo9760E 05ooooo Oo9760E 05

ooo 28ooooooooo 1.O5OO

MOMENTSMY3767o7004o

-40365.260473o

46762.ES OF STRESS

14067o81o

.27000o5313o

o o o o o o

o o o o o o

o o o ~ o

) oooooooo'

ooooo ~ oooo) ~ ~ oo~ ~ oo

o ~ ooo~ o ~ oo

~ ooooo

oooo'ooooo

ooooooo ~ ooooo ~ oo ~ o

oooooo

ALU

MXDEADMEIGHT o o ~ ~ o o o 11111 o

lTHERHAL 1 oooooo ~ o 62597oTHERMAL 2 o.oooooo 62683o

"HAXIMUH'HERMALRANGEDEADMEIGHT RESULTANT

CALCULATEDPM = <P>(Do)/2TPB = (B2><DMMAX)/ZRESIDUAL STRESSOF=

HZ45266o76244o

-147155o

THE STRESS RULE INDEX IS ioi87

TECH4ICAL REPORT TR - 5828 - IREVo 40) 0 TELEDYNE ENGXNEERXNG SERVXCES

8888888888888888888888888888888888888888NN8888888888

PROJECT> 5828 20 APRIL 1983

STRESS RULE 14DEX

HIHE llILE POIHT UHIT 1

8888888888888888888888888888NNSSSSSNNSSSSSSSSSSSSNN

sc ~5M(D DATE ~ ~ ~~

SHEET 40'FPROGRAM NAMECOMMON l C DANIELS223SR I, EXE '3

TITLERECI RC LOOP 12

CREATION DATE6-DEC-1982 17!53

RUN DATE 8 TINE13-APR-83 10343o30

NODE NUMBER 115 DESCRIPTION RUN PIPE

SY (YIELD STRESS)» i i i i i i i i o i i o o o i i i 19350+00.. B2 (PRIMARY STRESS INDEX) 1+00

P (OPERATING PRESSURE) ..ioiioiiiooo 1055i00Ci '(SECONDARY STRESS INDEX) oooiooo+i iii0K1 (LOCAL STRESS INDEX) iiiioooiooo+o 1 i20C2 (SECONDARY STRESS INDEX) i>00K2..(LOCAl STRESS INDEX) ~ ooooooooo ~ oi ii80C3 (SECONDARY STRESS INDEX) ioooiioeo 1 F00K3 (LOCAL STRESS INDEX) oiii.oioooio+ 1 i 70

~ EA (HODULUS OF ELASTICITY) o o + o o o ~ ~ o ~ 25800000+.,EB (MODULUS OF ELASTICITY) ioooo.oioo 25800000'o. Z (SECTION MODUI US) oiieooooooo+iiii 577>5210.TEMP ON A SIDE OF NODE oiioii+iioooii ... 550i00TEMP ON B SIDE OF NODE iiioioiioioioe 550i00ALFA OF MATERIAL A iiiiiiiiioi.iiiioiiOi9760E-05

''ALFA OF MATERIAL B .oiiiooiii+iiiiooo Oi9760E-05PIPE OUTSIDE DIAMETER 28o0000PIPE MALL THICKNESS o o o o + ~ o o t o o o t t t t t ii0500

MOMENTSMX HY

DEADWEIGHT o o ~ ~ ~ o o 7094'767'THERMAL 1, ooii.oui -69474'004 iTHERMAL 2 eooiioii 98674'40365mMAXIMUM THERMAL RANGE

322852'EADWEIGHTRESULTANT45474'ALCULATEDUALUES OF STRESS

PH = (P)(Do)/2T14067'B

= (B2)(DWMAX)/Z79'ESIDUAL'TRESS

27000'F=

5508'Z44759'7430'184077'HE

STRESS'ULE INDEX IS 1+189

TECHHICAL REPORT TR - 5828 " IREVo )IOo 0

II|lo %IIN8888888888888888NSSNSSSN8NSSSNSSSSNNNSN

PROJECTo 5828'0 APRIL 19MSTRESS RULE II)EXHIIK HILE POIN lNIT 1

SSN88888NN888NNNSNSNN888N8888888NSNSNS

ST ~h. OATE pe~S'$

9ATE 2 3

TELEDYNE ENGXNEERXNG BERV'XCEG

PROGRAM NAMECOHHONooCDANIELS223SRIoEXE)3

.,TITLERECIRC LOOP 12


RUN DATE 8 TIME13-APR-83 10o43o31

NODE NUMBER 135 DESCRIPTION VALVE

SY (YIELD STRESS) oooooooooooB2 <PRIMARY STRESS INDEX) oooP,, (OPERATING PRESSURE) oooooCl (SECONDARY STRESS INDEX)Ki (LOCAL STRESS INDEX>C2 (SECONDARY STRESS INDEX)K2 (LOCAL STRESS INDEX) oooooC3 (SECONDARY STRESS INDEX)K3 (LOCAL STRESS INDEX)EA (MODULUS OF ELASTICITY>EB ( HODULUS OF ELAST ICITY )Z (SECTION MODULUS) ~ ~ o ~ ~ o o o

TEHP ON A SIDE OF NODE o o o o o ~

TEMP. ON B SIDE OF NODE o o o o o o

ALFA OF MATERIAL AALFA OF MATERIAL B ooooooooooPIPE OUTSIDE DIAMETER o o o o o o o

PIPE MALL THICKNESS o o o o o o o o o

MXDEADWEIGHT o o o o o o o -10740 o

THERHAL 1 ~ o ~ o o o ~ o 100012 o

THERHAL 2 oooooooo 258507oHAXIHUM THERMAL RANGEDEADWEIGHT RESULTANT

CALCULATED V'PH = <P)(Do>/2TPB = (B2)(DWHAX>/ZRESIDUA STRESSQF=

oooo 19350o00o o o o io00oooo 1055 F 00

ooo ioi'0,o o o o io20~ ~ ~ io00oooo io80

~ ~ ~ io00ooo io70

oooo 25800000ooooo 25800000ooooo 577o5210oooo'50o00oooo 550o00oooo Oo9760E-05oooo Oo9760E-05~ os ~ 28o0000

ooo io0500MOMENTS

HY3767o7004o

-40365o605100o

44005oS OF STRESS

14067o76o

27000o6387o

o o o o

o o o o

o o

~ ~ ~ o

~ o o o

oooo~ o ~ o

o o ~ o

~ o ~ o

o o o o

~ o ~ o

~ o o ~

o o o o

oooooooooooo o

~ ~ o

ALUE

HZ42508o

137iiio-348035o,

THE STRESS RULE INDEX IS io201

TECHNICAL REPORT TR - 5828 - 1

REUA HOA 0 TELEDYNE ENGXNEERlNG SERVICES

PROGRAM NAMECOMMON ', CDANIELS223SRI, EXE $ 3

RECIRC LOOP 12

NN8$$$$NN$$$$$$8$$$$$$$$8$$$$$$$$$8$$$$$$888888

PROJECTS 5828 20 APRIL 19N'TRESSRULE INDEX

HIHE NILE POINT UHIT 1

$8$$$tN$8$$$$$$$$$$$$$$8$$$$NN$$$$88$8$8$$8$8$ |N

CREATION DATE6-DEC-1982 17o53

RUH DATE 5 TIME13-APR-83 10o43o32

BY @K'= DATE ~B'++

NODE NUMBER 155 DESCRIPTION ELBOM.

SY (YIELD STRESS)R2 (PRIMARY STRESS INDEX) oooooooP (OPERATING PRESSURE)Ci (SECONDARY STRESS INDEX) ooooot(1 (I OCAL STRESS INDEX)C2 (SECONDARY STRESS INDEX) oooooK2 (LOCAL STRESS INDEX> oooooooooC3 (SECONDARY STRESS INDEX)K3 (LOCAL STRESS INDEX)EA (MODULUS OF ELASTICITY)EB (MODULUS OF ELASTICITY) t o o o o o

Z ( SECTION MODULUS )TEMP OH A SIDE, OF HODE ootoooooo ~

" 'TEMP ON B SIDE OF NODEALFA OF MATERIAL A

ALFA OF MATERIAL R ooooooooooooooPIPE OUTSIDE DIAHETERPIPE MALL THICKNESS o o o o o o o o o o o o o

HXDEADMEIGHT . -15229THERMAL 1 ooooooot -32156oTHERMAL 2 oooooooo 196028oHAXIMUM THERMAL RANGEDEADMEIGHT RESULTANT

CALCULATED VALUEPM = (P)(Do)/2TPB = (R2)(DWMAX>/ZRESIDUAL STRESSOF=


oooo 19350o00

hatt

~ 3o60oooo 1055t00tttt io20

t io00tttt 4o80,t

hatt

1 o00~ t io00~ t 1 o00

25800000ooooo 25800000ootto 577o5210oooo 550o00oooo 550o00otto Oo9760E 05oooo Oo9760E 05at 28o0000tttt io0500

MOHENTSMY1484o

14855o-60277o640237o

15412oS OF STRESS

14067o96o

27000o'8135 o

io227

MZ-1847o

153563o-439894o

TECHHICAL REPORT TR "'828 - iREUo HOo 0 TE:WEDVXE E.'ee XwEER X Ve eE:Rv Z CE:e

8888888888888888888888888888888888888888888888888888

PRMECT'5828 20 APRIL 1983

STRESS RULE IHKXHIKE NILE POIHT uHIT i

BY @8M~= DATE +'~ 'QMI~ DIITE' +SHEET HOo OF

PROGRAM,NAMECOMMON ' DANIELS223SR I EXE ] 3

TITLERE CIRC LOOP 12

CREATION DATE6-DEC-1982 17t53

e'UN

DATE 8 TIME13-APR-83 10143833

NODE. NUMBER 156 DESCRIPTION PUMP

~ o o ~

o o o o

o o o

o

o o o

o o o

o ~ ~

o o o o

o o

o o o o

o o o ~

~ o o o

o o o o

o o o

o o

o o o o

o o o o

~ o o

NXDEADWEIGHT ooooooo -15057oTHERMAL 1 oooooooo -29746oTHERMAL 2 o ~ o o o ~ o o 189918 o

MAXIMUM THERMAL RANGEDEADWEIGHT RESULTANT

CALCULATED VPM = (P)(Da)/2TPB = (B2)(DWNAX)/ZRESIDUAL STRESSOF=

ALUE


SY (YIELD STRESS) oooooooooooB2 (PRIMARY STRESS INDEX)P (OPERATING PRESSURE)Ci (SECONDARY STRESS INDEX)Kl (LOCAL STRESS INDEX) oooooC2 (SECONDARY STRESS INDEX)K2 (LOCAL STRESS INDEX)C3 (SECONDARY STRESS INDEX)K3 (LOCAL STRESS INDEX) oooooEA (MODULUS OF ELASTICITY)EB (NODULUS OF ELASTICITY)Z ( SECT ION NODULUS)TEMP ON A SIDE OF NODE ooooooTEMP ON B SIDE OF NODE ooooooALFA OF MATERIAL * ooooooooooALFA OF MATERIAL B ooooooooooPIPE OUTSIDE DIAMETER o o o o o o o

P IPE WALL THICKNESS o o o ~ o o o o ~

oooo 19350o00oooo 4o90oooo 1055o00~ oo io50

~ o F 00~ oo ho60

o ~ o ~ io00ooo io00

lo0025800000o

oooo 25800000ooooo 577o5210oooo 550o00.os ~ 550o00oooo Oo9760E 05oooo Oo9760E-05

ooo 28o0000o o io0500

MOMENTSH,Y

1433o15030o

-60720o633698o

15247o8 OF STRESS

14067o129o

27000o14275o

io315

MZ-1926o

15246io-437100o

TECHHIM REPORT 'R " 5828 - iTELEDYNE ENDXHEERING BERVlCEG

888888888888888888888888888888888888888888888888888888

PRMEGTo 5828 20 APRIL NQSTRESS RULE Il6EXNllE llILE POIllT INIT 1

888888888888888888888888888888888888888888888888888888

BY+++ DATE ++

ceo

SHEET No OF

PROGRAM NAMECOMMON', CDANIELB223SRI, EXE'3

TITLERECIRC LOOP 12


RUN DATE 8 TIME13-APR-83 10)43o34

NODE NUMBER 200 DESCRIPTION PUMP

SY (YIELD STRESS) oo+oiiiiioiiiiii+.i 19350i00B2 (PRIMARY STRESS INDEX) ioiiio+oooi 1 F00P (OPERATING PRESSURE) iiiioi.iioiii 1055i00Ci (SECONDARY STRESS INDEX) iiooiiioo 1+10Ki (LOCAL STRESS INDEX> 1+20C2 (SECONDARY STRESS INDEX) ...oo,,oo io00K2 (LOCAL STRESS INDEX) oioiiiiiiiioo ii80C3 (SECONDARY STRESS INDEX) oiooiiooi io00K3 (LOCAL STRESS INDEX) ii70EA (MODULUS OF ELASTICITY) o o o o i o i i o i

25800000'B

(MODULUS OF ELASTICITY) o i i o o i+ o o+ 25800000+Z (SECTION MODULUS) i i o o o o o i o i o i o i+ o 577i5210TEMP ON A SIDE OF NODE o i o o o++ i i o o i i i 550o00TEMP ON B SIDE OF NODE o o o o i o iiio o iii 550o00ALFA OF MATERIAL A i i o i i i i o + o + i . o o i o o 0 o 9760E-05ALFA OF MATERIAL B i i o i o o i o i o o o i o o i i i Oi9760E-05PIPE OUTSIDE DIAMETER o o ~ o o o o o o o + o o o + 28o0000PIPE WALL THICKNESS iooooooiooooooioo io0500

HOHENTBHX HY

DEADWEIGHT i+ o. o i o -20485'72 tTHERMAL 1 i i o i i i o i 130230'7719mTHERHAL 2 tatooott 238344+

"97343'AXIMUM

THERMAL RANGE545126'EADWEIGHTRESULTANT 20553+

CALCULATED V*I UES OF STRESSPM' (P)(Do)/2T 14067iPB = (B2)(DWMAX)/Z

36'ESIDUALSTRESS27000'F=

6200'Z

-1478+96713'284961+

THE STRESS RULE INDEX IS 1+197

TECHHICAL REPORT TR - 5828 " IREVi HOo 0 TELEDYNE ENGXNEERXNB SERVICES

&&&88&8&8&N&N&N&NSNNNNS&N&8NNS&&8&NS&PROJECTl 5828 20 ..APRIL 19MSTRESS RULE IlIEXHIHE HILE POIHT UHIT I

8&&&8&SSS&&S&&NNSSNNN&NSNNSNSNNN&S&NSS

BY ZEP MTE +'~

SHEET No OF

PROGRAH NAMECOMMON 8 8DANIELS223SRI i EXE f 3

TITLERECIRC LOOP 12

CREATION DATE6-DEC-1982 17 $ 53

RUN DATE 8 TIME13-APR-83 10843836


SY (YIELD STRESS)B2 (PRIMARY STRESS INDEX)P (OPERATING PRESSURE>Ci (SECONDARY STRESS INDEXKi (LOCAL STRESS INDEX)C2 <SECONDARY STRESS INDEXK2 (LOCAL STRESS INDEX)C3 <SECONDARY STRESS INDEXK3 (LOCAL STRESS INDEX) oiEA (MODULUS OF ELASTICITY)EB (MODULUS OF ELASTICITY)Z <SECTION HODUI US)TEMF'N A SIDE OF NODE o o iTEMP ON B SIDE OF NODEALFA OF MATERIAL A oiooiioALFA OF MATERIAL B o ii o o i o

PIPE OUTSIDE DIAHETERPIPE WALl THICKNESS i i o i o o

o ~ oeoooo 19350+003 i 60

o ~ o ~ eoto 1055@00tttttt ii20io004i80

~ ttt ~ ii001o00

~ tttt ~ 1+00i+iiiii+25800000'ioooioo

25800000'ootoooo

577@5210~ ooooooo 550@00totttooo 550@00~ otootoe Oo9760E 05oootoooo 0 ''760E 05

~ le 28o0000io0500

MOMENTSHY

-3568'1843'68369'58854'2835'LUES

OF STRESS

14067'42'7000m

5796m

HXDEADMEIGHT o i o i o i i -18592+THERHAL 1 oioooooo f197721THERMAL 2 oooioiio -21183ioMAXIMUM THERMAL RANGEDEADMEIGHT RESULTANT

CALCULATED VPH = (P>(Do>/2TPB = (B2)(DMHAX)/ZRESIDUAL STRESSQF=

HZ12769i17977+

-85356'HE

STRESS RULE INDEX IS 1 i 19'7

TECHNICAL REPORT TR - 5828 " IREUSE HOi 0

8 8TELEDYNE ENGXNEERXNG SERVXCES

NNSSNSSSSSSN88NSNSNNNSSNSSNSNNNNSPROJECT! 5828 20 APRIL. NHSTRESS RULE IHDEX

'HIlK NILE POIN INIT 1

SNSSNSNSNSSSSSNSSNSSSNSSNSSNSSSSNSS

"I~%a', CI(D DATE

PROGRAM NAMECOMMON: CDANIELS223SRI, EXE i 3

TITLERE CIRC LOOP 12


RUH DATE 8 TINE13-APR-83 ioi43t37

NODE NUMBER 225 DESCRIPTIOH VALVE

SY (YIELD STRESS> ~ oeo ~ ooooto ~ o ~ ooB2 (PRIMARY STRESS INDEX) ioiiiioiP (OPERATING PRESSURE) oooioiiooiCi (SECONDARY STRESS INDEX)Ki (LOCAL STRESS INDEX) .iioioooooC2 (SECONDARY STRESS INDEX)K2 (LOCAL STRESS INDEX) +oioooooooC3 (SECONDARY STRESS INDEX) oeooii

. K3 (LOCAL STRESS INDEX) oooooooiooEA (MODULUS OF ELASTICITY) o o+ i o i iEB (MODULUS OF ELASTICITY) i o o o o i o

Z (SECTIOH MODULUS) o o o i i o o o i o o o iTEMP ON 'A SIDE OF NODE iiiiiiiooiiTEMP ON B SIDE OF NODE ii o o i o i++ iiALFA OF, MATERIAL A oioiooooooooooo*LFA OF MATERIAL B o i ~ o e t o ~ i ~ ~ ~ ~ o o

PIPE OUTSIDE DIAMETERPIPE WALL THICKNESS

HXDEADWEIGHT eiiiiii

-29970'HERMAL

1 oioiiiio122407'HERMAL'ooiiiiio -26898ii

MAXIMUM THERMAL RANGEDEADWEIGHT RESULTANT

CALCUlATED VALUESPH = (P)(Do)/2TPB = (B2)(DWNAX>/ZRESIDUAL STRESSOF=

oio 19350+00igloo

1055ioo1 iioii201+001.SO1+001 i 70

25800000ioui 25800000+oio 577o5210oio 550ioo

550oooOi9760E-05Oi9760E-05

28ooooo1.05OO

MOMENTSNY

-7759m

13029'24916+

592638>31028'F

STRESS

14067'4'7000'348+

NZ

2077'130268m

313123'HE

STRESS RULE INDEX IS 1+200

TECHHICAL REPORT TR - 5828 - 1

REVi HOo 0 TELEDYNE ENGXNEER XNG BERVXCES

&S&NNSSSSSNN &S&NN&N8NNSSSSNSNSSSN&NNNNPROJECT I 5828 20 „. APRIL 19N .

STRESS RULE IHK(HIHE HILE POIHT UHIT 1

NSS&SSSNN&NNSSNNNSSS&88&NSSSSSNSNSSNNSN

BY ~D MTE +~

'. PROGRAM NAMECOHHONiCDANIELS223SRIiEXE$ 3

TITI ERECI RC LOOP 12


RUN DATE K TIME13-APR-83 10843+38

NODE NUMBER 270 DESCRIPTION ELBOW

SY (YIELD STRESS) i o i i o i i o o i o

B2 (PRIMARY STRESS INDEX) i o o

P (OPERATING PRESSURE) ,,oatCi (SECONDARY STRESS INDEX)Ki (LOCAL STRESS INDEX) ooo ~ o

C2 (SECONDARY STRESS INDEX)K2 (LOCAL STRESS INDEX) .oooiC3 (SECONDARY STRESS INDEX)K3 (LOCAL STRESS INDEX) scionsEA ( MODULUS OF ELASTICITY)EB (MODULUS OF ELASTICITY)Z (SECTION MODULUS)TEMP ON A SIDE OF NODETEMP ON B SIDE OF NODE o o i+ i o

ALFA OF MATERIAL A o o i o o i i+ o o

ALFA OF MATERIAL B o o o o o o o o o o

PIPE OUTSIDE DIAMETERPIPE MALL THICKNESS ~ o o o ~ o++ i

MXDEADWEIGHT o o s i o o i 62036mTHERHAL 1 ttotot+o

84479'HERMAL2 oieiioii-305495'AX

IHUH THERHAL RANGEDEADMEIGHT RESULTANT

CALCULATED VPH = (P)(Do)/2TPB = (B2)(DWHAX)/ZRESIDUAL STRESSOF=


~ ~ ~ io ~ ~ o 19350i003+60

oooooooo 1055t00~ itt ~ 1 i20

~ ~ ~ io004i801+00ii00io00

oteooooo 258000001oi++i+io 25800000'.oo++oooo 57715210++oooooo 550o00~ toooooo 550 F 00o'ooooo ~ o Oo9760E 05tooooooo Oo9760E 05

28o0000io0500

MOMENTSHY

-8376+

2664'2574'63543'7914'LUES

OF STRESS14067+

423+

27000'0822+

io282

HZ26338m

-237290>"643753'

TECHNICAL REPORT TR " 5828 - 1

REVE NOD 0 TKI KD'YNK KNHXNKIERXNH &KRVXDKR8888888888888888888888888NN8888NN88888888888888IN

PROJECT! 5828 20, APRIL,1983

STRESS RULE INDEX


888NN888888888NN8888888888NNNNNN888888888NN

BY ~ + DATE

SHEET NOB OF

PROGRAH NAMECOMMON ) CDAHIEl S223SRI o EXE ~ 3

TITLERECIRC LOOP 12

CREATION DATE6-DEC"1982 17o53

RUN DATE R TINE13-APR-83 10)43839

NODE NUMBER 275 DESCRIPTIOH SAFE END

SY < YIElD STRESS) o o o o o o o o o o

B2 (PRIMARY STRESS INDEX) ooP (OPERATING PRESSURE)Ci (SECONDARY STRESS INDEX)Ki (LOCAL STRESS INDEX) ooooC2 (SECONDARY STRESS INDEX)K2 (LOCAL STRESS INDEX) ooooC3 (SECONDARY STRESS INDEX)K3 (LOCAL STRESS INDEX>EA (MODULUS OF ELASTICITY> o

EB < MODULUS OF ELASTICITY>

Z (SECTION MODULUS> oooooooTEMP ON A SIDE OF NODE o o o o o

TEHP ON B SIDE OF NODE o o o o o

ALFA OF MATERIAL AALFA OF HATERIAL B o ~ o o ~ o o o o

PIPE OUTSIDE DIAHETER o o o o o o

PIPE MALL THICKNESS o o o o o o o o

HXDEADWEIGHT o o o o o o ~ 67480 o

THERHAl 1 oooooooo -3800oTHERHAL 2 oooooooo 85687oMAXIMUM THERMAL RANGEDEADWEIGHT RESULTANT

CALCULATEDPH = (P)(Do)/2TPB = (B2)(DWMAX)/ZRESIDUAI STRESSQF=


o

o o o

~ o

o o

o

o ~ o

o o

~ o

o o o

~ o

oooooooooo o o

o o o

o o o

o o

VAL

oooooo 19350o00~ ~ oooo io00oooooo 1055o00~ ooooo io10

Boffo io20ooooo 1 o00.

oo oooo io80ooooo io00

oooooo io70oooooo 25800000ooooo'6100000ooooooo 577o5210oooooo 550 F 00,oooooo 550o00oooooo Oo9760E 05o ~ oo ~ o 0 '120E 05ooooo 28o0000o o o o io0500

MOMENTSHY

-9020o-8163o51733o

999403o73590o

UES OF STRESS14067o

127o27000o69304o

2o091

HZ27938o

-268809o725431o

I

TECHNICAL REPORT, TR

REVo NOo 05828 " 1

TELEDYME ENRIMEERINH RERVICEGNNSNN88888888888888888NNSSNNSSS|N888888888

PROJECTI 5828 20 APRIL 19M

STRESS RULE INDEX

HIHE NILE POINT UNIT 1

88888888888888888NN888888888NNSSSSNN888888888888888

SY ~Q MTE AMCea SATE <~ '>

SIKET m OF

PROGRAM NAMECOMMON 1 CDANIELS223SRI o EXE i 3

CREATION DATE6 "DEC-1982 17 853

TITLERECIRCUL,ATION LOOP 15

RUN DATE20-APR-83

TIME10813524

NODE100101105115135155156255265200205225270275

3902390539053909

~ 3910391139143916391939233802380638883814381538173821

STRESS RUL44 SUMMA

DESCRIPTIONSAFE ENDELBOWTEETEEVALVEELBOWPUMPTEETEEPUMPELBOMVALVEELBOMSAFE ENDTEEVALVEREDUCERVALVEELBOMEl BOMELBOWELBOWELBOMELBOMTEEELBOMRUNELBOWELBOWRUNRUN

E INDEXRY44

SRIiii26is381212732o259ii253ii2711+3752i3122+3141 i 250io3431 i270ii4092i1541 i 6841 i 3481 i556i i 4181 i 8071 i 8441 i 7091 i5861 i 620io5412+2241+101io218li489ii467ii189io364

TECIIICAL REPORT TR " 5828 " 1

REV» I)o 0 „TE'I EDYQIE; IENRXHEERXH& BIE:RVXCIER

888NN8888888888NN8888888888888888888888888NNSS

PROJECTo 5828 „20 APRIL NGSTRESS RULE ISED(NIHE HILE POIN INIT 1

SSSSSSSS8NNSSSNNNNSS@NNNSSNNSSSSS

Bf ~~+ 9hTE

+'HEET

No OF

PROGRAM NAMECOMMON o CDANIELS223 SR I o EXE f 3



RUH DATE IL TIME20-APR-83 ioo13o53

NODE NUMBER 100 DESCRIPT ION SAFE END

SY (YIELD STRESS) oooooooooooooooB2 (PRIMARY STRESS INDEX) oooooooP (OPERATING PRESSURE) oooooooooCi (SECONDARY STRESS INDEX) oooooKi (LOCAL STRESS INDEX),C2 (SECONDARY STRESS INDEX)K2 (LOCAL STRESS INDEX)C3 (SECONDARY STRESS INDEX) oooooK3 (LOCAL STRESS INDEX)EA (MODULUS OF ELASTICITY) o o o o o o

EB (NODULUS OF EI ASTICITY)Z (SECTION NODULUS) ooooooooooooTEHP ON A SIDE OF NODETEMP OH B SIDE OF NODE ooooooooooALFA OF MATERIAL A ooooooooooooooALFA OF MATERIAL B ooooooooooooooPIPE OUTSIDE DIAHETERPIPE MALL THICKNESS ~ o o o o o ~ o o o o o o

MXDEADMEIGHT ooooooo 32892oTHERMAL 1 oooooo ~ o 1508435oTHERMAL 2 oooooooo -189884oMAXIMUM THERMAL RANGEDEADMEIGHT RESULTANT

CALCULATED VALUEPM = (P)(Do)/2TPB = (B2)(DMMAX)/ZRESIDUAL STRESSQF=

oooo 19350oaoo ioao

io55,oaoooo ioiaooo io20~ ~ oo iooaoooo io80~ ~ ~ o ioaaooo io70oooo 25800000o

26100000oohio 577o5210oooo 550oaooooo 550ooaoooo Oo9760E 05oooo Oo7120E 05

ooo 28oaooaoooo i.o5oa

MOMENTSHY

14454o196178o249372o

1790972o75687o

S OF STRESS14067o

131o27000o71771o

HZ66616o

-815482o-249386o

THE STRESS RULE INDEX IS 2o126

TECHHICAL'REPORT TR - 5828 - .iREV» MO» 0 TELEDYNE ENGXNEERXNG SERVXCES

asssaaasaaassesssssaa'asaaassaasaaasasssssasfaaaassass

PROJECT» 5828 , ~ 20 APRIL 1983

STRESS RULE IHBEX

HIRE MILE POIHT UHIT i, '.assaasaeeaaasaaaaasssasasaaaeaaaaaeaaaaeaaasaeasassess

BY E~ 4 IRATE&~'~

SHEET HO» OF

PROGRAH NAMECOMMON i LDANIELS223SR I » EXE t 3 '


CREATION DATE6-'DEC-1982 17»53

RUN DATE 8 TIME20-APR-83 10»13)53

NODE NUMRER 101 DESCRIPTION ELROW

SY ( YIELD STRESS)»» ~ »»»»»»» ~ ~ »»»»»'»» 19350 ~ 0082 (PRIMARY STRESS INDEX) »».»».»»»»» 3»60P (OPERATING PRESSURE> »»»»»»»»»»»»» 1055»00Ci (SECONDARY STRESS INDEX) »»»»»»»»» '»20'K1 (LOCAL STRESS INDEX) ...»»,»,»,»», i»00C2 (SECONDARY STRESS INDEX) »»»»»»»»» 4»80K2 (LOCAL STRESS INDEX) i»00C3 (SECONDARY STRESS INDEX'-rrrr~rr--- --1»00-K3 (LOCAL STRESS INDEX) »».»»»»»»»»»» i»00EA (MODULUS OF ELASTICITY) .. 25800000EB (MODULUS OF ELASTICITY> ...,...,,, 25800000,Z (SECTION MODULUS) »»»»».»»»»»»»»»» 577»5210TEMP ON A SIDE OF NODE »»»».»»»»'»»»». 550»00TEMP ON R BIDE OF NODE »»».»»»»»»»»»» 550»00ALFA OF MATERIAL A »..»».»»»»»»»»»»»» 0.9760E-05ALFA OF MATERIAL R ....,...,... ,..., 0,9760E-05PIPE OUTSIDE DIAMETER ., 28. 0000PIPE WALL THICKNESS»»»»»»»»»»,»»»»»»» 1 »0500

MOMENTSHX HY

DEADWEIGHT .»»»».» -32888» -14454»THERMAL 1 .»»»»»»» -1508397» -196185»THERHAL 2 »»»»»» ~ » 189877» -249373.MAXIHUM THERMAL RANGE 1790954»DEADWEIGHT RESULTANT 75679»

CALCULATED VALUES OF STRESSPH = (P)(Do)/2T 14067PB = (B2)(DWHAX)/Z 472»RESIDUAL STRESS 27000»QF= 17699»

MZ-66609»815548»249373»

THE STRESS RULE INDEX IS 1»381

r

TECHNICAL REPORT TR - 5828 " 1

REUD NOA 0 TELEDYNE ENGXHEERXNB SERVXCES

888$ 88888888888888888888888888888888888888888888888888

PROJECTD 5828"

20 APRIL 1983

STRESS RULE INDEX

HIHE NILE POIHT UNIT 1

88$ 8888888888888888888888888888$ 8888888888888888888888

DT ~ DATE ——CID DATE

SHEET NOD OF

PROGRAM NAMECOMMON o CDANIELS223SRI o EXE) 3



RUN DATE 5 TIME20-APR-83 10o13o54

SY (YIELD STRESS) oooooooooooooooB2 (PRIMARY STRESS INDEX) oooooooP (OPERATING PRESSURE) oooooooooCi <SECONDARY STRESS INDEX) oooooKi (lOCAL STRESS INDEX) oooooooooC2 (SECONDARY STRESS INDEX) oooooK2 (LOCAL STRESS INDEX) oooooooooC3 <SECONDARY STRESS INDEX) oooooK3 (LOCAL STRESS INDEX) oooooooooEA (MODULUS OF ELASTICITY) o o o o o o

EB (MODULUS OF ELASTICITY) o o o o o o

Z (SECTION MODULUS) ooooooooooooTEHP ON A SIDE OF NODETEMP ON B SIDE OF NODE ooooooooooAL'FA OF MATERIAL A ooooooooooooooALFA OF MATERIAL B ooooooooooooooPIPE OUTSIDE DIAHETER o o o o o o o o o o o

PIPE WALL THICKNESS o o o o o o o o o o o o o

oooo 19350o00oooo 2o80oooo 1055o00oooo 1 o50

4o00~ os 3o70oooo io00oooo io00

o io00oooo 25800000o

25800000ooooo 577 '210oooo 550o00oooo 550o00oooo Oo9760E 05oooo 0 '760E 05oooo 28o0000

o io0500MOMENTS

HY-11982o

-267627o-23097io1784902o

53665oS OF STRESS

14067o260o

27000o81769o

MXDEADWEIGHT 26187THERMAL 1 ooo.oooo -1097078oTHERMAL 2 ooooooo. 28489oMAXIMUM THERMAL RANGEDEADWEIGHT RESULTANT

CALCULATED VALUEPH = (P)(Dra)/2TPB = (B2)(DWMAX)/ZRESIDUAL STRESSOF=

NODE NUMBER 105 DESCRIPTION TEE

MZ45284o

1251791o-132994o


II

TECHHICAL REPORT TR " 5828 - 1

REVo HOi 0 TELEDYNE ENGXNEERXNG SERVXCES

8888888888888888888888888888888|N88888888NN88888

PROJECTS 5828 20 APRIL 1983,

STRESS RULE IHOEX


88888888888888888888888888NN8888NN8888888

py B PP

PROGRAM NAMECOMMON! C 9 AN IELS22 j SR I o EXE I 3

~ TITLERECIRCULATION - LOOP 15


RUN DATE 5 TIME20-APR-83 10)13855

NODE NUMBER 115 DESCRIPTION TEE .

SY (YIELD STRESS) i i o i i i i i i o o o i i o iB2 (PRIMARY STRESS INDEX)P (OPERATING PRESSURE) i i o i o i o i i o

Ci (SECONDARY STRESS INDEX)Ki (LOCAL STRESS INDEX) oooiiooiiiC2 (SECONDARY STRESS INDEX)K2 (LOCAL STRESS INDEX) iiiiiiioooC3 (SECONDARY STRESS INDEX) ooioooK3 (LOCAL STRESS INDEX)EA (MODULUS OF ELASTICITY)EB (MODULUS OF ELASTICITY)Z (SECTION MODULUS) oooiioooo+oooTEHP ON A SlDE OF NODE oooooooooteTEMP ON R BIDE OF NODE ioiiiooo+oiALFA OF MATERIAL A iooiiooiiiioiiiALFA OF MATERIAL B oooiiooooooooooPIPE OUTSIDE DIAMETERPlPE WALL THICKNESS o o o t t t t ~ i ~ o o o e

19350i002i80

1055o00ii504e003o70ii00io00io00

eoi25800000'ui

25800000o'oo

577i5210550o00

owe 550i00Oi9760E-05Oi9760E-05

28i0000io0500

HOHENTSMY-811+

-67805'125349m

1676017+35024'F

STRESS

14067'70'7000'1071'X

DEADWEIGHT ~ o o ~ + + i 22955 o

THERHAL 1 ooooioii-905728'HERMAL

2 oooo+ooi149853'AXIMUM

THERMAL RANGEDEADWEIGHT RESULTANT

CAL.CULATED VALUESPH = (P)(Do)/2TPR = (B2)(DWMAX)/ZRESIDUAL STRESSQF=

A

HZ26440 i

1034704'26586io

THE STRESS RULE INDEX IS 2i259

TECIICAL REPORT TR - 5828 " 1

REVD NOD 0 TELEDYNE ENIBINEERIHG SERUI CEB

88888888888888888888888888888 88888

PROJECT 1 5828 20 APRIL 1%9STRESS RULE II)EXNHE NILE POII'IT I

8888888888888888&8888888888888888888888888

DT ~+ DATE

SHEET No OF

PROGRAM NAMECOHHONi CDAHIELS223SRI o EXE t 3


CREATION DATE6-DEC-1982 17!53

RUN DATE 8, TIME20-APR-83 10 o 13 o 56

NODE NUMBER 135 DESCRIPTIOH VALVE

BY, (YIELD STRESS) otooottootoB2 (PRIMARY STRESS INDEX) o o o

P, (OPERATING PRESSURE)Ci (SECONDARY STRESS INDEX) o

Ki (LOCAL STRESS INDEX) toot ~

C2 (SECONDARY STRESS INDEX) o

K2 (LOCAL STRESS INDEX) tttttC3 (SECONDARY STRESS INDEX)K3 (LOCAL STRESS INDEX)Ek (MODULUS OF ELASTICITY)EB (MODULUS OF ELASTICITY)Z (SECTION MODULUS> otooooooTEMP ON A SIDE OF NODE ototttTEHP ON B SIDE OF NODEALFA OF HATERIAL A ooooooottt*LFA OF MATERIAL B oooooooootPIPE OUTSIDE DIAMETERPIPE WALL THICKNESS o o o o o o o o o

HXDEADWEIGHT ~ ~ o t o t ~ 2456 o

THERHAL 1 oooototo -830550oTHERMAL 2 tottttoo 277838tMAXIMUM THERMAL RANGEDEADWEIGHT RESULTANT

CALCULATED VPH = (P)(Do)/2T'ra = (B2)(DwHAX>rz

. RESIDUAL STRESSGF~


oottotto 19350o00t ~ tt ~ it00oooooo ~ t 1055o00tttotttt ioiOttttttt io20tttttttt it00otttttt io80ttottt ~ io00stot'o70

ttoootto 25800000otooooooo 25800000too ~ ootoo 577t5210ooooo ~ to 550o00o ~ oto ~ ot 550o00oottooto Oo9760E 05hottentot Ot9760E 05tttttttt 28o0000tt ~ tttt ~ it0500

MOMENTSHY-8iio

-67805o-125349o1789716t

34547oALUES OF STRESS

14067o60t

27000t10079o

1t253

MZ34450o

1004508o-399503o

TECHNICAL REPIT TR " 5828 "'REVo HOo 0 TELEDYNE ENGXNEERXNG SERVXCES

SNNNNNNNNSSNNSSSNSNSNSSSNSSSSSSNNSNPROJECT t 5828 20 APRIL 198K

STRESS RULE INDEX

HIRE NLE POIHT INIT iSSSSSNSSSSSSNSSNSNNSSSSSSNSSSNNNNSNSSNS

BY W

SHEET N OF—

PROGRAM NAMECOMMON o LDANIELS223SRI o EXE ) 3



RUH DATE E TINE20 APR 83 10ii3i57

NODE NUHBER 155 DESCRIPTION ELBOW

SY (YIELD STRESS)B2. <PRIMARY STRESS INDEX>P (OPERATIHG PRESSURE) oooooCi (SECONDARY STRESS INDEX) o

Ki (LOCAL STRESS INDEX> o.oooC2 <SECONDARY STRESS INDEX> ,K2 (LOCAL STRESS INDEX)

. C3 (SECONDARY STRESS INDEX)K3 (LOCAL STRESS INDEX)EA (MODULUS OF ELASTICITY>EB (MODULUS OF ELASTICITY) o o

Z (SECTION NODULUS) ooooooooTEHP OH A SIDE OF NODE ooooooTEMP OH B SIDE OF NODE ooooooALFA OF MATERIAL AALF* OF MATERIAL B ooooooooooPIPE OUTSIDE DIAMETERPIPE WALL THICKNESS o o o o o o o o o

MXDEADWEIGHT o o o o o o o -17810oTHERMAL 1 oooooooo 144234oTHERHAL 2 oooooo.o 151863oMAXIMUM THERMAL RANGEDEADWEIGHT RESULTANT

CALCULATED VPH = (P)(Do)/2TPB = (B2)(DWHAX)/ZRESIDUAL STRESSQF=

oooooo ~ o 19350o00~ o ~ oooo 3o60

oooooooo 1055o00~ oooooo io20oooooooo io00oooo'o 4o80oooo oooo io00

~ ooooooo io00ooooooo ~ 1 o00oooooooo 25800000ooooooooo 25800000ooooooooo 577 '210oooo oooo 550o00oooooooo 550 F 00~ ooooooo Oo9760E 05o ~ ~ ooo ~ ~ 0 '760E 05oooooooo 28o0000oooo's io0500

MOMENTSHY

-1604o-66883o

-141807o1008482o

1834ioALUEB OF STRESS

14067o114o

27000o11195o

MZ4079o

564234o-441432o

THE STRESS RULE INDEX Is io271

TECNIICAL REPORT TR " 5828 " 1

REUo No 0 TE:LEDY'NE: E:H83 XHE:E:R X NG DERV X C:E:R

SNNSSNSSSNNNSNNSNSNNNNNSNNSPROJECT! 5828 20 APRIL i%9STRESS RULE INEXHIHE PILE POIHT NIT i

8888NNSNNSSNSNSNNSSNSSSNSNNSNSNNSS

BY MM BATE &KM

PROGRAM NAMECOMMON o CDANIELS223SRI o EXE r 3



RUN DATE 8 TINE20-.APR-83 10oo13o58


ooooo 19350o00oooo 4o90~ oooo 1055o00oooo io50ohio io00

o 6o60ooooo 1,00,o o o ~ io00oooo io00ooooo 25800000o

25800000ooooo'77 '210oooo 550o00ohio'o 550 F 00ooooo Oo9760E 05ohio Oo9760E 05boffo 28o0000ooooo io0500

MOMENTSMY

-1621o-66862o

-142174o996775o

18178oES OF STRESS

14067o154o

27000o18425o

o o

o o o

o ~ o

o o

~ o ~

o o ~

oooo o o

o o o

o o ~

o o ~

o ~ o

o o o

o

o o

o o

o

MXDEADMEIGHT o ~ ooooo 17656oTHERHAL 1 oooo'o 163695

'HERHAL2 oooo oooo 145281oMAXIMUM THERMAL RANGEDEADMEIGHT RESULTANT

CAI CULATED VALUPM = (P>(Do),/2TPB = (B2)<DWNAX)/ZRESIDUAL STRESSQF=

SY (YIELD STRESS)B2 (PRIMARY STRESS INDEX)P <OPERATING PRESSURE>Ci <SECONDARY STRESS INDEX)Ki (LOCAL STRESS INDEX> oooooG2 (SECONDARY STRESS INDEX)K2 (LOCAL STRESS INDEX>C3 (SECONDARY STRESS INDEX) o

K3 (LOCAL STRESS INDEX) oooooEA ( MODULUS OF ELASTICITY)EB (MODULUS OF ELASTICITY) o o

Z (SECTION NODULUS) ooooooooTEMP ON k SIDE OF NODETEMP ON B SIDE OF NODE o o o o o o

ALFA OF MATERIAL A .oo.o.ooo.ALFA OF MATERIAL B ooooooooooPIPE OUTSIDE DIAMETERPIPE MALL THICKNESS o o o o o o o o o

HZ4008o

555333o-438422o

THE STRESS RULE INDFX IS io375

TECHHICAL REPORT TR - 5828 " 1

REVD HOD 0 TE:L,E:DY'NE: IENR X NEE:R X ND RERV XDER

$$8$88$ 88$ 8$88888$ $$$$8$8$$$8888$ $$$$8$$$$$88$ $$8$$8

PRMECTI 5828 20 APRIL 1983

STRESS RULE INEXHIHE HILE POIHT UHIT 1

$$$$$$$$$$$$8$8$$8$8$$$$88$ 8$$$$8$$$$$$$$$$8$888888

BY ~P='DATE

am~ DATE<M/Y»

PROGRAM NAMECOMMON oo CDANIELS223BRI o EXE)3



RUN DATE ID TIME20-APR-83 10$ 13o58


SY (YIELD STRESS) ooooooooooo82 (PRIMARY STRESS INDEX)P (OPERATING PRESSURE) ~ o o ~ o

Ci (SECONDARY STRESS INDEX)Kl (LOCAL STRESS INDEX) oooooC2 (SECONDARY STRESS INDEX)K2 (LOCAL STRESS INDEX) oooooC3 (SECONDARY STRESS INDEX) o

K3 <LOCAL STRESS INDEX)EA < MODULUS OF ELASTICITY)EB (MODULUS OF ELASTICITY)Z (SECTION HODULUS) o o o o o o o o

TEMP ON A SIDE OF NODE,...,.TEHP ON B SIDE OF NODEALFA OF MATERIAL A ooooooooooALFA OF HATER IAL 8PIPE OUTSIDE DIAHETER ~ ~ o o o ~ ~

PIPE WALL THICKNESS o ~ o o o ~ o o o

HXDEADITIEIGHT o o o o o o o 1927 o

THERMAL 1 oooooooo 1022249oTHERHAL 2 ooo ~ ~ ~ oo 454716oMAXIMUM THERMAL RANGEDEADWEIGHT RESULTANT

CALCULATED UPH = (P)(Do)/2TPB = (B2)(DMHAX)/ZRESIDUAL STRESSOF=

oooooooo 19350o00oooo oooo 2o80oooooooo 1055o00

ooooooo io50~ oooooo 4o00

oooooooo 3o70oooooo ~ 1.00

oooo io00~ o ~ ooooo 1 o00

25800000oooooooo,o 25800000ooooooooo 577o5210~ ~ oooo ~ ~ 550o00~ oooooo ~ 550o00oooooo ~ o Oo9760E 05o ~ oooooo Oo9760E 05,

ooooooo 28o0000ooooooo io0500

MOMENTSMY

-11883o-37818 o

-114103o2324655o

14640oALUES OF STRESS

14067o71.

27000o85227o

HZ-8331o

-131 1201'o482336o


TECIICAL REPORT TR - 5828 - 1

REVo ttOo 0 TELEDYNE ENGINEERING SERVICES

SSSNSN888888$ 8NSSSSSNSSNSSSSNNNNNNWSSSN8 PROJECT) 5828 20 APRIL 1%9

STRESS RULE II>EXHIRE NILE POIN lNIT 1

NSSNSSSSSNNNSNSNSSNNNSNSSSSSSNNSS

ST mMCID DATE ~

SKET N, = OF

PROGRAM NAME

,COMMON)CDAHIELS223SRI o EXE t3

TITLERECIRCULATION LOOP'5


RUH DATE L TINE20-APR-83 10t13t59


SY (YIELD STRESS) oooooooooooB2 (PRIMARY STRESS INDEX) oooP (OPERATING PRESSURE) oooooCi (SECONDARY STRESS INDEX) o

Ki (LOCAL STRESS INDEX) oooooC2 (SECONDARY STRESS INDEX)K2 (LOCAL STRESS INDEX)C3 (SECONDARY STRESS INDEX)K3 <LOCAL STRESS INDEX>EA <MODULUS OF ELASTICITY) o o

EB <NODULUS OF ELASTICITY)Z (SECTION MODULUS> ...,...,TEMP ON A SIDE OF NODE ooooooTEMP ON B SIDE OF HODEALFA OF MATERIAL A o o o o o o o o o tALFA OF'ATERIAL B tooooooootPIPE OUTSIDE DIANETERPIPE MALL THICKHESS o o o o o o o t t

MXDEADMEIGHT o t o o o ~ o 4494 ~

THERMAL 1 o ~ o t t ~ o t 1203193 ~

THERMAL 2 -275379MAXIMUM THERMAL RANGEDEADMEIGHT RESULTANT

CALCULATED VPM = (P)<Do)/2TPB = (B2>(DMMAX>/ZRESIDUAL STRESSQF«-

tote too 19350o00tt ~ ttttt 2t80too ~ ~ ooo 1055o00ttt ~ ttt 1o50

tott ~ ttt 4o00~ t ~ tttt ~ 3o70tt ttt io00

tt ~ ttt ~ t io00tttttt ~ t io00oooooooo 25800000ooooooooo 25800000ooo ~ otooo 577 '210

tooted

oto 550o00ooo ~ o ~ o ~ 550t00otooott ~ Oo'9760E 05oo ~ oto ~ o Oo9760E 05tttttttt 28o0000ttttttt io0500

'.MOMENTSMY

49492o899622o760222o

2213052o'59403o

ALUES OF STRESS14067o

288o27000o84512o

MZ-32543o

-1373348o26738it


88888888888888888NN8888888888888888888888888

PROJECT) 5828 20 APRIL 1983

STRESS RULE II)EXHIRE NILE POIN MT 1

C@O OATE<~'~

TECIICAL REPORT TR - 5828 - 1

REVB HOD 0 TELEDYNE,EblBXNEERXNG SERVXCES8

,BY DATE

PROGRAM NAMECOMMON I C DANIELS223SRI o EXE D 3


CREATION DATE6-DEC-1982 17 $ 53

RUN DATE 8 TIME20-APR-83 10+14o00


SY (YIELD STRESS> o.oooooooooooooooB2 (PRIMARY STRESS INDEX)P (OPERATING PRESSURE)Ci <SECONDARY STRESS INDEX) ooooooKi (LOCAL STRESS INDEX) ooooooooooC2 (SECONDARY STRESS INDEX) ooooooK2 <LOCAL STRESS INDEX) ooooooooooC3 (SECONDARY STRESS INDEX)K3 (LOCAL STRESS INDEX>EA (MODULUS OF ELASTICITY)EB (MODULUS OF ELASTICITY> o o o o o o o

Z (SECTION NODULUS> oooooooooooooTEMP ON A SIDE OF NODE oooooooooooTEMP 'ON B SIDE OF NODE oooooooooooALFA OF MATERIAL A oooooooooooooooALFA OF HATERIAL B oo ~ oooo ~ ~ o ~ ooooPIPE OUTSIDE DIAHETFR o o o o o o o o o o o o

PIPE MALL THICKNESS oooooooooooooo

HXDEADMEIGHT o o o o o o o -22102 o

THERMAL 1 oooooooo 1365308oTHERMAL 2 o ~ o ~ ~ ooo 303765oHAXIHUH THERMAL RANGEDEADMEIGHT RESULTANT

CALCULATED VALUESPH = (P)(Do)/2TPB = (B2)(DMHAX)/ZRESIDUAl STRESSOF=


ooo 19350o00o io00

1055o00~ ~ io10ooo 1 o20o o o io00o ~ io80~ os io00os io70

25800000oooo 25800000o

577o5210550o00

ooo 550o00OD9760E-05

ooo Oo9760E-05ooo 28o0000~ oo io0500

HOHENTSHY

-1327 o

-69727o-172215 o

1748652o22224o

OF STRESS14067 o

38o27000o

995io

io250

HZ1909o

224835o-286512o


REUo IIOo 0 TELEDYNE ENGXNEERING SERVICESNNNSSNSSSSSSSN8888NSSNSNSNNSNSN8NNSNN

20 APRIL 19IGPROJECT! 5828

STRESS RULE IISEXIIIIIE NLE POIHT mIIT I

88888SSSNSSNNSSSNNSNSN88NSNNSSNNSSNN

BY ~ BATE

X'HI<a

SHEET No OF

PROGRAH NAMECOMMON+ C DANIELS223SRI o EXE i 3


CREATION DATE6"DEC-1982 17o53

RUH DATE R TIME20-APR-83 10 o 14 o 02


SY (YIELD STRESS) ooooooooooooooooooo 19350o00B2 (PRIHARY STRESS INDEX) oo ~ o ~ o ~ oo ~ o 3o60P (OPERATING PRESSURE) ooooooooooooo 1055o00Ci (SECONDARY STRESS INDEX) ooooooooo io20Ki (LOCAL STRESS INDEX) ooooooooooooo io00C2 (SECONDARY STRESS INDEX> ooooooooo 4o80K2 (LOCAL STRESS INDEX) ooooooooooooo io00C3 <SECONDARY STRESS INDEX) lo00K3 (LOCAL STRESS INDEX> ooooooooooooo io00EA (NODULUS OF ELASTICITY> oooooooooo 25800000oEB <NODULUS OF ELASTICITY) oooooooooo 25800000oZ (SECTION NODULUS) o o o o o o o o o o o o o o o o 577o5210TEHP ON A SIDE OF NODE oooooioooooooo 550o00TEMP ON B SIDE OF NODE ~ o o o o ~ o o o o ~ o o o 550o00ALFA OF MATERIAL A oooooooooooooooooo Oo9760E-05ALFA OF MATERIAL B ooooooooo,ooooooooo Oo9760E-05PIPE OUTSIDE DIAMETER o o o o o o o o o o o o o,o o 28o 0000PIPE MALL THICKNESS ooooooooooooooooo ,io0500

MOMENTSHX MY

DEADMEIGHT o o o o o o o -20131 o -5550oTHERMAL 1 oooooooo 1280857o -56962oTHERMAI 2 oooooooo -275204o -148968oMAXIMUM THERMAL RANGE 1595316oDEADMEIGHT RESULTANT 26765o

CALCULATED UALUES OF STRESSPN = (P)<Do)/2T 14067oPB = (B2)(DMMAX>/Z 167oRESIDUAL STRESS 27000oOF= 16073o

HZ16742o

-410962o-71488o


TECSIICAL REPORT TR " 5828 - iREVo ROo 0

8TELEDYNE ENGXNEERING SERVICES

88888888888888888888888888888888888888888888888888SS

PROJECTS 5828 20 RPRIL f983STRESS RULE IHDEX

HIHE HILE POIN INIT i88888888888888888888888888888888888888888888888888888

BY

CHKD

SHEET No OF

PROGRAM NAHECONMONS CDANIELS223SRI i EXE i 3



RUN DATE R TIME20-APR-83 fOii4$03

NODE NUMBER 225 DESCRIPTION VALVE

SY <YIELD STRESS) o o o o o i o o o i o i i o i o o

B2 (PRIMARY STRESS INDEX) i i o . o i i i o

P (OPERATING PRESSURE) o o o'o o i o o o e iCi.(SECONDARY STRESS" INDEX>Ki (LOCAL STRESS INDEX) oeoiiiiooioC2 (SECONDARY STRESS INDEX) ooiooeoK2 (LOCAL STRESS INDEX) iiooooiiiooC3 (SECONDARY STRESS INDEX)K3 (LOCAL STRESS INDEX) iioeeioooioEA < NODULUS OF ELASTICITY> i" i o o i i o

EB (NODULUS OF ELASTICITY)Z (SECTION NODULUS) o i i i i i o i o i o o o +

TEMP ON A SIDE OF NODE ooiiooooooooTEMP ON B SIDE OF NODE iiiiiioioi+oALFA= OF MATERIAL * oooooi+oiioiooiiALFA OF MATERIAL B i i o i i i i i o o i i i+ o iPIPE OUTSIDE DIAMETER o o i i i o o o o o o o o

PIPE MALL THICKNESS 'o o xiii o i o i o o iii

oo i9350e00fo00

oi 1055o00i i 10i i 201 F00 ~

io801 F00fo70

25800000'i

25800000'i

577o5210550o00550i00

Oo9760E-05Oo9760E-05

28e00001 i0500

HOMENTSNY

-f1883'37818'114103o

2198065m29319'F

STRESS4067+

51 i7000'352'X

DEADWEIGHT o i i i i i o-26793'HERMAL

1 xiiio i o i 1108172mTHERHAL 2 ooootto ~ 309964'.HAXIMUH THERMAL RANGEDEADMEIGHT RESULTANT

CALCULATED VALUESPN = (P>(Do>/2T 1PB = (B2)(DMMAX>/ZRESIDUAL STRESS 2OF= 1

HZ

716'1345908i

331757m

THE STRESS RULE INDEX IS fo270

BY 8Z DATE

CHKD DATE+

8NN8N888N888888N88NN8NN8N8NN88NN8NPROJECT) 5828 20 APRIL NUSTRESS RULE INDEX

HIRE NILE POIN NIT 1

NN8N88N8NNNNN8N88N8NNN888888888


TELEDYNE ENGXNEERXNG SERVXCESQjI

PROGRAM NAMECOMMON+ CDANIELS223SRI t EXE ~ 3



RUN DATE 8 TIME20-APR-83 10)14104


SY (YIELD STRESS) ooooooootoB2 (PRIMARY STRESS INDEX)P, (OPERATING PRESSURE)C1 (SECONDARY STRESS INDEX)Ki (LOCAL STRESS INDEX)C2 (SECONDARY STRESS INDEX)K2 (LOCAL STRESS INDEX) ooooC3 (SECONDARY STRESS INDEX)K3 (LOCAL STRESS INDEX)EA ( MODULUS OF ELASTICITY>EB. (MODULUS OF ELASTICITY)Z <SECTION NODULUS)TEMP ON A SIDE OF NODE o o o o o

TEMP ON B SIDE OF NODEALFA OF MATERIAL A oooooooooALFA OF MATERIAL B oooooooooPIPE OUTSIDE DIAMETER ooooooPIPE MALL THICKNESS o o t o o t o o

MXDEADMEIGHT ooooooo -22935oTHERMAL 1 .o.o.oo. 207082tTHERHAL 2 ~ o o ~ o ~ o o 368912 o

MAXIHUM THERMAL RANGEDEADMEIGHT RESULTANT

CALCULATEDPH = (P)(Do)/2TPB = (B2)<DMHAX),/ZRESIDUAL STRESSQF=


ttoooooto 19350o00~ ttttttt 3o60

o ~ otooo ~ o 1055o00ttttttt ~ t io20ttt ~ ttttt io00ttttttttt 4o80~ ~ t ~ ~ t t t t io00t ~ tt ~ tttt io00t ~ ottoo ~ ~ io00oooot oooo 25800000oooooooooo 25800000ott ~ oo ~ ~ tt 577o5210~ ~ oottooo 550o00ttttt

hatt

550o00oo ~ ttooto Oo9760E 05o ~ ot ~ oooo 0 '760E 05tt ~ tt ~ ttt 28o0000tttt ~ tttt io0500

MOMENTSHY

53699o927154o80402io

2042626o68489o

VALUES OF STRESS14067o

427o27000o19790o

io409

HZ-35794 o

-1659925o295935o

TECHHICAL REPORT TR " 5828 " 1

REVo HOi 0

8TEI E:DY'NE', ENI3XNEE',RXNI3 RERVXDE:R

888888888888888888888888888888888888888888888888888888

PROJECTS 5828 20 APRIL 1%9STRESS RULE IHDEX

, HIHE NIlE POIHT UHIT 1

8888888888888888888888888888888888888888888888

wE l<~~~~

SHEET HOo OF

PROGRAM NAMECOMMON:CDANIELS223SRI EXE$ 3


CREATION DATE6-DEC-1982 17)53

RUN DATE 8 TIHE20-APR-83 10114805

NODE NUMBER 275 DESCRIPTION SAFE END

~ ~

~ ~

~ ~

MXDEADWEIGHT iooiooo -10670boTHERMAL 1 i.iioi+i -602958mTHERMAL 2 oiiioiio -23305boMAXIMUM THERMAL RANGEDEADWEIGHT RESULTANT

CALCULATED VPM = (P)<Do)/2TPB = (B2)(DWHAX)/ZRESIDUAL STRESSOF=

ALU


SY (YIELD STRESS) oioiioiiiio. B2 (PRIMARY STRESS INDEX) coo

P (OPERATING PRESSURE) icosiCi (SECONDARY STRESS INDEX)Ki (LOCAL STRESS INDEX) oiscesC2 <SECONDARY STRESS INDEX) o

K2 (I OCAL STRESS INDEX) oooo+C3 (.SECONDARY STRESS INDEX)K3 (LOCAL STRESS INDEX) iooooEA (MODULUS OF ELASTICITY)EB <MODULUS OF ELASTICITY) o iZ (SECTION MODULUS)TEMP ON A SIDE OF NODE o o i o o o

TEMP ON B SIDE OF NODE i i i o o o

ALFA OF MATERIAL A o o o o o o i i o iALFA OF HATERIAL B o t e o o o o o ~ o

PIPE OUTSIDE DIAMETERPIPE WAI L THICKNESS

ootot 19350+00lo00

i ~ oot 1055@00iiiO

~ ~ io20io00io80

~ ~ i F00lit ~ io70toto@ 25800000+ooooo 26100000oooooe 577+5210tt ~ oo 550+00oot ~ o 550100otto+ Oo9760E-05o o o t o 0t7120E 05

28o0000io0500

MOMENTSHY

58092m

955913'49770+

2300048'36335+

ES OF STRESS

14067'36'7000'3358'<154

HZ

-61858'19155bio

352065'


TELEDYNE ENGINEERING SERVICES88&NN &88&8 88888888888888888888888&88888&&888888

PROJECT) 5828 20 APRIL 19N .STRESS RULE IHDEX

HIHE HILE POIHT INIT 1

888888888888888888888888888888888888888888888888888

DT ~ DATE P

OID~ DATE ~i~DDEET FI OF

PROGRAH HAHECOMMON 1 C DANIELS223SR I t EXE i 3

,TITLERECIRCULATION LOOP 15

'REATION DATE6-DEC-1982 17153

RUN DATE R TIME20-APR-83 10114107


BY (YIElD STRESS) o t o o t o o o o o

B2 <PRIMARY STRESS INDEX)P (OPERATING PRESSURE) ooooCi (SECONDARY STRESS INDEX)Ki (LOCAL STRESS INDEX)C2 (SECONDARY STRESS INDEX)K2 (LOCAL STRESS INDEX) ooooC3 (SECONDARY STRESS INDEX)K3 (LOCAL STRESS INDEX> ooooEA ( MODULUS OF ELASTICITY) o

EB (NODULUS OF ELASTICITY)Z (SECTION HODULUS) oooooooTEMP ON A BIDE OF NODE o o o o o

TEMP OH B SIDE OF NODE t ~ o t o

.ALFA OF HATERIAL A o o o o o o ~ o ~

ALFA OF MATERIAL B ootooooooPIPE OUTSIDE DIAMETERPIPE MALL THICKNESS o o o t o o o o

t t t ~

t ~ t tt t t

t

ttttt t t

tt t t ~

t t tt ~

t tt t t~ t t tt o t tt t t tt ~ t ~

t t t t

MX-2729o

-220144oOo

DEADWEIGHTTHERMAL 1 ooo ~ ottoTHERHAl 2 ooo ~ oootMAXIMUM THERNAl RANGEDEADWEIGHT RESULTANT

CALCULATED VALUPH = <P)(Do)/2TPB = (B2)(DWNAX)/ZRESIDUAL STRESSQF=

otot ~ 19350t00tt

hatt

2o80o ~ oo ~ 1055o00tttt ~ io50tt ~ ot 4o00ttttt 3o70tttt 1,00tttt io00ttttt io00

25800000oooooo 25800000ot ~ ttt 88oi246ootto 550o00oo ~ ot 550o00ooooo Oo9760E-05

Oo9760E-05o ~ ooo " 12o7500tttt ~ Oo8430

MOMENTSMY

-10987o-182232o

Oo328664o

14236tES OF STRESS

7978o452o

34844o53690o

NZ8632t

162322oOo

THE STRESS RULE INDEX IS 1 o'684


RPPB HOo 0 TELEDYNE ENG INEER ING SERO ICES88888888888888888888888888888888888888888888888888

PROJECTt 5828 20 APRIL 19NSTRESS RULE IHILEX

BBYE ~ ~

0'go 69 *


888888888888888888888888888888888888888888888888 SHEET HOB OF

PROGRAM NAMECOMMON o CDANIELS223SRI o EXE $ 3


CREATION DATE6-DEC-1982 17 o 53

RUN DATE 8 TIME20-APR-83 10 oo 14 'o08

NODE NUMBER 39O5 DESCRIPTION VALUE

BY (YIELD STRESS) oooooooooooooooB2 (PRIMARY STRESS INDEX) oooooooP (OPERATING PRESSURE)Ci (SECONDARY STRESS INDEX)Ki (LOCAL STRESS INDEX)C2 (SECONDARY STRESS INDEX)K2 (LOCAL STRESS INDEX) oooooooooC3 (SECONDARY STRESS INDEX)K3 (LOCAL STRESS INDEX)EA <MODULUS OF ELASTICITY)EB ( MODULUS OF ELASTICITY)Z <SECTION NODULUS) ooooooooooooTEMP ON A SIDE OF NODE o o o o o o o o o o

TEMP ON B SIDE OF NODE ooooooooooALFA OF HATERIAL A ooooooooooooooALFA OF HATERIAL B 'o o o o o o o o o o o o o o

PIPE OUTSIDE DIAHETER o o o o o o o o o o o

PIPE WALL THICKNESS ~ o o o o o o o o o o ~ o

HX-2729

'220144o

.Oo

DEADWEIGHT o o o ~ o o o

THERMAL 1

THERHAL 2 ooooooooMAXIMUM THERMAL RANGEDEADWEIGHT RESUl TANT

CALCULATED VALUEPM = (P)(Do)/2TPB = <B2)(DWMAX)/ZRESIDUAL STRESSQF~

oooo 19350ooooooo iooooooo 1055ooo

ohio ioiooooo io20

o ~ ~ ioooohio 'io80

o o a,OOoooo io70oooo 25800000ooooo 25800000ooooo 40o9228oooo 550ooo

550 F 00Oo9760E-05

oooo Oo9760E 05~ oo ~ ioo7500ooo Oo5220

MOMENTSMY

-1069io-173999o

Oo288963o

3416ioS OF STRESS

10863o835o

36594o16186o

MZ-32330o

68995oOo

THE STRESS RULE INDEX IB io348

TECHMICAL REPORT TR " 5828 - 1

REV$ MQ$ 0

))p$)f

TILEDYNK

8888888888888888|NNNSNN888888888

PROJECT t 5828 20 APRIL 1983

STRESS RULE IHDEX

MIRE MILE POIHT OMIT 1

SSSNNSSSNNSSSSSNNNNSSSSSSSSSSSSSSSS8 8SNNSSSS SHEET H0$ OF

KNGiX HKKRX NH RKRU X C:IE&

$$$$$$$$$$$$$$$$$ 8$ P~~ DATE +'7~

PROGRAM NAMECOMMON i C DANIELS223SR I o EXE t 3


CREATION DATE6-DEC-1982 17$ 53

RUN DATE E TIME20-APR-83 10 t 14 i 09

NODE NUHBER 3905 DESCRIPTION REDUCER

SY < YIELD STRESS> o i $ i i o i i o $ $ $ i i i i $ i i 19350 F00B2 (PRIMARY STRESS INDEX) $ $ . $ i o o $ i o o 1$ 00P (OPERATING PRESSURE),,...,,, », o, 1055,00Cl (SECONDARY STRESS INDEX> $ $ +$ oooio lo50Kl (LOCAL STRESS INDEX) ii+iiioi++ooo 2>00C2 <SECONDARY STRESS INDEX) oio$ o+oio io30K2 (LOCAL STRESS INDEX) 1>00C3 (SECONDARY STRESS INDEX> $ i+oiooo+ 1 F00K3 <LOCAL STRESS INDEX) io00EA (MODULUS OF ELASTICITY) ~ 25800000EB <MODULUS OF ELASTICITY) i i o i++++ o o 25800000'

(SECTION HODUL,US) +i$ oooooiiiooooo 40o9228TEMP ON A SIDE OF NODE + i i o o+ i i o o i o o o 550i00TEMP ON B SIDE OF NODE ...,...,...,,, 550,00ALFA OF HATERIAL A iiiioi+iiiioooiooo Oo9760E-05ALFA OF MATERIAL B ii$ iioioooooiioioi Oi9760E-05PIPE OUTSIDE DIAMETER i i i i+ o o o s o i o o o e 10o7500PIPE WALL THICKNESS + $ + o i i o i i o i o+ i i o+ Oi5220

MOMENTSHX HY

DEADWEIGHT ...,... »2729, -1069iiTHERHAL '1 o o ~ ~ $ ~ e o 220144 ~

-173999'HERHAI

2 $ oooooto Oi OiMAXIMUH THERHAL RANGE

288963'EADWEIGHTRESULTANT 34161CALCULATED VALUES OF STRESS

PH ~ (P)(Do)/2T 10863>PB = (B2)(DWHAX)/Z 835$RESIDUAL STRESS 36594"QF~ 30906$

HZ-32330+

68995$0+

THE STRESS RULE INDEX IS 1+556

TECOICAL REPORT TR - 5828 - 1

REVe NOi 0 veweDVWe exeXWeearxa aeauXCae

)sN888NNN8NNSNNNS WS4

PROJECTS 5828 20 APRIL 1983

STRESS RULE ISDHIRE HILE POIN UNIT 1

NWSNCWSSSNNNSN88$ NNNSNCSNCSSNSNANNA

ST ~ZP 8ATE<4~ ~

STREET Ne OF

PROGRAH NAME'OMMONSC DANIELS223SRI i EXE $ 3

TITLERECl RCULATION LOOP 15


RUN DATE L TIHE20-APR-83 iOoi4fif

NODE NUNBER 3909 DESCRIPTION VALVE

HZ

-55578'167920i

Oo

SY (,YIELD STRESS) o o i i o i i i i o. i i i i i++ i i8800+00B2 (PRIMARY'STRESS INDEX> ooiiioiooio fo00P (OPERATING PRESSURE) iiiiiioiiiiii 1055+00Ci '(SECONDARY STRESS INDEX) ooooiiioi iiiOKi (LOCAL STRESS INDEX) isis.oioiiooi f i20C2 (SECONDARY STRESS INDEX> oooooooio io00K2 (L.OCAL STRESS INDEX) iiioooo+iioii io80C3 (SECONDARY STRESS INDEX) ooiooooio i+00K3 (LOCAL STRESS INDEX> 1+70EA <MODULUS OF ELASTICITY) 25800000EB <NODULUS OF ELASTICITY> ...,...,,, 25800000,Z (SECTlON NODULUS) iiiooieooooioooo 40+9228TEMP ON A SIDE OF NODE ioooiioiooiooo 550o00TEHP ON B SIDE OF NODE o+ o t i o e ~ t o o o o o 550s00ALFA OF MATERIAL A ~ ~ ~ o ~ o ~ oo ~ t ~ ttttoo Ot9760E 05ALFA OF MATERIAL B epo+io+ooeioooiioo Oi9760E-05PIPE OUTSIDE DIAMETER + i o o o o o o o o o o o+ e 10o7500PIPE MALL THICKNESS i o i i o i o i o o i i o i i o i Oi5220

'OMENTS

HX NYDEADWEIGHT ~ o o t o o o 2729 ~

-9940'HERMAL

1 ooioiooo -220144'153100oTHERH*L 2 tttt ~ oo+ Oi OoMAXIMUM THERHAL RANGE

316386'EADMEIGHTRESULTANT56526'ALCULATEDVALUES OF STRESS

pM = (p)(Do)/2T 10863iPB = <B2><DWNAX>rZ 138iiRESIDUAL STRESS 36594 iQF =. 17393+

THE STRESS RULE INDEX IS fi418


REVo HOo 0 TELEDYNE ENGINEERING SERVICES88888888888888NNSSSSNN8888888888888888888888

PROJECT t 5828 20 APRIL 1%9

STRESS RULE IHK(HIHE HILE POIHT UHIT 1

88888888888NNSSSNNSSSSSSSSSSS8NNSSSSSSSNNSSSS

PROGRAM NAMECOMMON o CDAHIELS223SRI o EXE ~3

TITlERECIRCULATION LOOP 15


RUH DATE 8 TINE20-APR-83 10)14 o 13

NODE NUMBER '910 DESCRIPTION ELBOW

SY (YIELD STRESS> ooooooooooo.o.o.ooo 18800o00B2 (PRIHARY STRESS 1NDEX) ooooooooooo 3o30P (OPERATING PRESSURE> oo.ooooooo.o. 1055o00Ci (SECONDARY STRESS INDEX> ooooooooo io30Ki (LOCAL STRESS INDEX) ooooooooooooo 1 o00.C2 (SECONDARY STRESS INDEX) ooooooooo 4o40K2 (LOCAL STRESS INDEX) ooooooooooooo io00C3 (SECONDARY STRESS INDEX) ooooooooo io00K3 (LOCAL STRESS INDEX) ooooooooooooo io00E* (MODULUS OF ELASTICITY) oooooooooo 25800000oEB (HODULUS OF ELASTICITY) o o o o o o o o o o 25800000 o

Z (SECTION NODULUS) oooooooooooooooo 40o9228~ TEMP ON A SIDE OF NODE oooooooooooooo 550o00

TEMP OH B SIDE OF NODE oooooooooooooo 550o00ALFA OF MATERIAL A oooooooooooooooooo Oo9760E-05ALFA OF MATERIAL B oooooooooooooooooo Oo9760E-05PIPE OUTSIDE DIAMETER o o o o o o. o o. o o o o o 10o7500PIPE MALL THICKNESS ooooooooooooooooo Oo5220

MOMENTSHX NY

DEADWEIGHT o o ~ o o o ~ 2729 o -9602oTHERHAL 1 ooo ~ oooo 220144o -14368ioTHERMAI 2 oooooooo Oo OoHAX1MUH THERMAL RANGE 38022$ o

DEADWEIGHT RESULTANT 19168oCALCULATED VALUES OF STRESS

PM = (P)(Do)/2T 10863oPB = (B2)(DMMAX)/Z 1546oRESIDUAL STRESS 36594oOF= 44140o

NZ-16363o

-274703Oo


TECHHlCAL REPORT TR - 5828 " 1

REVB HOo 0 TELEDYNE ENGXNEERING SERVICESSNSSSSNSNSSSNSNSNNNSSSNNSNSSNSNSSNNNS

PROJECT» 5828 20 APRIL 1983

STRESS RULE ISEXHIHE HILE POIHT UHIT 1

NN888888888888NSSSSNNSSSSNNSNSNSSNNSNNSS

BY ~= BATE+

CeS WE +~'

BOEET BO OF

PROGRAM NAMECOMMON ) C DANIELS223SR I o EXE j 3



RUH DATE R TIME20-APR-83 10 o 14 o 15

NODE NUMBER 3911 DEBCRIPTIOH ELBOM

SY ( YIEl D STRESS >

B2 (PRIHARY STRESS INDEX) otP (OPERATING PRESSURE)C1 (SECONDARY STRESS INDEX)Ki (LOCAL STRESS INDEX> tootC2 (SECONDARY STRESS INDEX>K2 (LOCAL STRESS IHDEX) oo ~ o

C3 (SECONDARY STRESS INDEX>K3 (LOCAL STRESS INDEX) ottoEA (HODULUS OF ELASTICITY)ER ( MODULUS OF ELASTICITY)Z (SECTION MODULUS) oootottTEMP 'ON A SIDE OF NODE ...,.TEMP ON R SIDE OF NODE ...,,ALFA OF HATERIAL A ~ o t o o o t t o

ALFA OF MATERIAL R ootttottoPIPE OUTSIDE DIAMETERPIPE MALL THICKNESS

t t t t~ ~ ~ t

t t t t tt t t t tt t t ~ tt t t t t

t t t tt t t ~ tt t tt t ~

t t t tt t t tt t ~ tt t t t t~ t t t t~ t t t ~

t tt t t ~ t

HX-26625t

-166300tOt


DEADWEIGHT o o o o ~ o o

THERMAL 1 oo ~ ooottTHERHAL 2 ttot hattMAXIMUM THERMAL RANGEDEADWEIGHT RESULTANT

CALCULATED UALUEPM = (P>(DO)/2TPB = (B2)(DMMAX)/ZRESIDUAL STRESSQF=

18800o00ttt 3o30oooo 1055t00tttt 1o30tttt it00t ~ ~ t 4o40os ~ 't00~ ~ t io00ttt it00

25800000t25800000o

tt ~ 40o9228

ditto

550o00otto 550o00too ~ Oo9760E 05oooo Oo9760E 05ttt 10t7500tttt Ot5220

MOMENTSHY

-6599t-91108 t

Oo379342o

28224oS OF STRESS

10863 t2276t

36594t44046t

io844

HZ6645o

-328548tOt

BY ~~ DATE KCBEB~ DATE <~YE' B

888888888888888888888888888888888888888888888888

PROJECTl 5828 20 APRIL 19NSTRESS RULE I@EX

NilK NILE POINT lIIT 1

INNNgdtl

TECHHICAL REPORT TR " 5828 " 1

TELEDYNE ENGINEERING SERVICESDftf

PROGRAM NAMECOMMON'CDAHIELS223SRI EXE33

RECIRCUl ATIOH LOOP 15

CREATION DATE6-DEC-1982 17 t 53

RUH DATE 8 TIME20-APR"83 10114ii7


SY (YIELD STRESS) ttttttttttB2 (PRIMARY STRESS INDEX)P (OPERATING PRESSURE)Ci (SECONDARY STRESS INDEX)Ki (LOCAL STRESS INDEX)C2 (SECONDARY STRESS INDEX)K2 (LOCAL STRESS INDEX)C3 (SECONDARY STRESS INDEX)K3 (LOCAL STRESS INDEX) ttttEA (MODULUS OF ELASTICITY) tEB (MODULUS OF ELASTICITY) tZ (SECTION MODULUS) t ~ t t t t tTEMP ON A SIDE OF NODE t t t t tTEMP ON B BIDE OF NODEALFA OF MATERIAL A tttttttttALFA OF MATERIAL B tttttttttPIPE OUTSIDE DIAMETER t t t t t tPIPE MALL THICKNESS t t t t t t t t

MX9562t

96902tOt

DEADMEIGHT ~ t t t t t tTHERMAL 1 oooo ~ tttTHERMAL 2 t ~ ~ ~ ~ tttMAXIMUM THERMAL RANGEDEADMEIGHT RESULTANT

CALCULATEDPM = (P)(Da)/2TPB = (B2)(DWMAX)/ZRESIDUAL STRESSOF=

~ t t t t t ~ t t 18800 t00t ~ ~ t t t ~ t t 3 t30tttt ~ t ~ tt 1055t00~ ~ t t t t t t t it30tttttttt ~ it00

t ~ t 4t40~ ttt ~ ttt ~ it00ttttttttt it00tttt ~ tttt it00t ~ ttttttt 25800000tttttttttt 25800000ttttttttt 40t9228~ t ~ tttttt 550t00t ~ ttttttt 550t00t ~ ttttttt OB9760E 05ttt ~ ttt ~ t Ot9760E 05ttt ~ tt ~ tt 10t7500tt ~ tttttt OB5220

MOMENTSMY6994t

138446tOt

327663t15170t

UALUES OF STRESS10863t

1223t36594t38489t

MZ9476t

-280724tOt

THE STRESS RULE INDEX IS it709

TECIICAL REPORT TR " 5828 - 1

REVo HO« 0 TELEDYNE ENHXNEERXND RERVXDER

«)tSNNSSSSNN88$ $8$88888888888$ 888888888888888888888888

PROJECT« 5828 20 APRIL 1'7N

STRESS RULE IHK(HIHE NILE POINT NIT I888888888$ 88888888888888$ 8888$ NN88$8888888

BY '«TEapp gz" 6CIO OATE + ~

SHEET HOo OF

PROGRAH NAMECOMMON o CDAHIELS223SRI o EXE r 3



RUN DATE 8 TIHE20-APR-83 10ii4119

NODE NUMBER 3916 DESCRIPTIOH ELBOM

BY (YIELD „STRESS) ooooooooooooooooooo 18800o00B2 (PRIMARY STRESS INDEX) ooooooooooo , 3o30P (OPERATING PRESSURE) ooooooooooooo 1055o00Ci (SECONDARY STRESS INDEX) ooooooooo 1'o 30Ki (LOCAL STRESS INDEX> ooooooooooooo io00C2 (SECONDARY STRESS INDEX> ooooooooo 4o40K2 (LOCAL STRESS INDEX) ooooooooooooo io00C3 (SECONDARY STRESS INDEX) ooooooooo io00K3 (LOCAL STRESS INDEX) ooooooooooooo io00EA (MODULUS OF ELASTICITY) o o o o o o o o o o 25800000 o

EB (MODULUS OF ELASTICITY> oooooooooo 25800000oZ (SECTIOH MODULUS) oooooooooooooooo 40o9228TEMP ON A SIDE OF NODE oooooooooooooo 550o00TEMP ON B SIDE OF NODE oooooooooooooo 550o00ALFA OF HATERIAL A oooooooooooooooooo 0.9760E-05ALFA OF MATERIAL B oo..oooooooooooooo Oo9760E-05PIPE OUTSIDE DIAMETER o o o o o o o. o o o o o o o 10o7500PIPE MALL THICKHESS o o o o o o o ~ o o o o o o o ~ o Oo5220

MOMENTSHX HY

DEADMEIGHT 9869 6823oTHERMAL 1 ooooo.oo 105451o 133697oTHERMAL 2 oooo oooo Oo OoMAXIHUH THERHAL RANGE 220949oDEADMEIGHT RESULTANT 24319o

CALCULATED VALUES OF STRESSPH = (P)(DQ)/2T 10863oPB = (B2)(DMHAX>/Z 196ioRESIDUAl STRESS 36594oQF= 27015o

HZ21153o

-140797oOo


TEmHICAL REPORT TR " 5828 - 1

REVo HOo 0 TELEDYNE ENGINEERING SERVICES

$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$

PROJECT t,5828 20 APRIL 19MSTRESS RULE IHDEX


$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$

av ~~+CHQ INTE

Zo e3

QKET N OF

PROGRAM NAHECOMMON i L DANIELS223SRI o EXE13



RUN DATE 8 TIME20-APR-83 10+ 14122

NODE NUMBER 3915'ESCRIPTION ELBOW

HX19231 o

51606oOo

DEADWEIGHTTHERMAL 1 ooooooo ~

THERHAL 2 oooo ooooHAXIHUH THERHAL RANGEDEADWEIGHT RESULTANT

CALCULATEDPM = (P)<Do)/2TPB = (B2)(DWHAX)/ZRESIDUAL STRESSOF.=


SY <YIELD STRESS) ooooooooooB2 (PRIMARY STRESS INDEX) ooP <OPERATING PRESSURE) o o o.Ci (SECONDARY STRESS INDEX)Ki (LOCAL STRESS INDEX)C2 <SECONDARY STRESS INDEX)K2 (LOCAL STRESS INDEX) ooooC3 <SECONDARY STRESS INDEX)K3 (LOCAL STRESS INDEX)EA (HODULUS OF ELASTICITY)EB (MODULUS OF ELASTICITY)Z (SECTION MODULUS) oooooooTEMP ON A SIDE OF NODE oooooTEMP ON B SIDE OF NODE oooooALFA OF HATERIAL A o ~ o ~ o o o o o

ALFA OF MATERIAL B oooooooooPIPE OUTSIDE DIAMETER o o o o o o

PIPE WALL THICKNESS o o o o o o o o

oooooooo'o 18800o00oooooooo ~ 3o30ooooooooo 1055 F 00

o ~ o ~ ooo io30oooooooo io00ooo ~ oooo ~ 4o40~ oooooo ~ ~ io00~ oooooooo io00,o ~ ooooooo io00

25800000oooooooooo 25800000oooooooooo 40o9228~ oooooo ~ ~ 550o00ooooooooo 550o00ooooo oooo Oo9760E 05oooo oooo'o9760E 05

oooo ~ o ~ o 10o7500ooo ~ o ~ ooo Oo5220

MOMENTSHY2775 o

52009oOo

253892o206iio

UALUES OF STRESS10863o

1662o36594o30557o

io620

MZ6875o

243091o'o

TECHttICAL REPORT TR - 5828 - iREVt Nt 0 TELEDYNE ENGXNEERXNG GERVXCEB

PROJECTS 5828 20 . APRIL i%9STRESS RULE ISEXHI% HILE POIHT NIT i

888888888&SNN&SNNS&88&888888888&NNSSNN&88888888

BT ~ MTE

(3e -WE+~ 6~

PROGRAM NAMECOMMON t CDANIELS223SRI t EXE r 3



RUN DATE R TIME20-APR-83 10tti4$ 25


MX-4492t

-35491tOt

DEADWEIGHT tttttttTHERMAL 1 tt ~ tttttTHERMAL 2 t ~ ttttttHAXIHUH THERMAL RANGEDEADWEIGHT RESULTANT

CAlCUlATEDPM = (P)(Do)/2TPB = (B2)(DMMAX)/ZRESIDUAL STRESSOF=

THE STRESS'-RUl E INDEX IS

SY (YIELD STRESS) tttttt.tttB2 (PRIMARY STRESS INDEX>P 'OPERATING PRESSURE) t t t tCi (SECONDARY STRESS INDEX)Ki <LOCAL STRESS INDEX)C2 (SECONDARY STRESS INDEX)K2 (LOCAL STRESS INDEX)C3 (SECOND'ARY STRESS INDEX)K3 <LOCAL STRESS INDEX) ,tttEA ( MODULUS OF ELASTICITY>EB (MODULUS OF ELASTICITY) tZ (SECTION NODULUS) tttttttTEMP ON A SIDE OF NODETEMP ON B SIDE OF NODEALFA OF MATERIAL A tttttttttALF* OF MATERIAL B ttttttttt

. PIPE OUTSIDE DIAHETER t t t t t tPIPE MALL THICKNESS t t t t t t ~ t

ttttttttt 18800t00~ ttttttt 3t30t ~ ttt ~ ttt 1055t00ttttt

hatt

it30ttttttt ~ t it00ttt ~ ttttt 4t40tttt

hatt

~ it00~ ~ tttttt 1t00

~ ~ tt ~ tt it00ttttttttt 25800000tttttttttt 25800000ttt ~ tttttt 40t9228t ~ tt ~ tt ~ t 550t00tt ~ ttttt ~ 550t00tttttttt ~ Ot9760E 05

Ot9760E-05tttttt ~ 10t7500tttt ~ ~ ttt Ot5220MOMENTS

MY-1862t

-24978tOt

242746t6133t

VALUES OF STRESS10863t

495t36594t29359t

1 t 541

MZ3737 ~

238835tOt

BY E~~ DATEC ~~~JJ

~,„yz ssSNNSNNSNSSSNNNNSNSNNNNNSNSNSSSSSNPROJECT! 5828 - 20 APRIL 1983

STRESS RULE IHDEX

HIRE NILE POIHT 131T ISHEET HOo OF

TECHNICAL REPORT TR " 5828

TELEDYNE ENGINEERIHG SERVICES"II

PROGRAM NAMECOMMON i CDANIELS22|SRI o EXE ) 3

.TITLERECIRCULATION LOOP 15


RUN DATE 8 TIME20-APR-83 10oi4$ 28


SY (YIELD STRESS> ooooooooooB2 (PRIHARY STRESS INDEX>P (OPERATING PRESSURE) ooooCi (SECONDARY STRESS INDEX)Ki (LOCAL STRESS INDEX) ooooC2 (SECONDARY STRESS INDEX)K2 (LOCAL STRESS INDEX)C3 (SECONDARY STRESS INDEX>K3 (LOCAL STRESS INDEX) ooooEA ( NODULUS OF ELASTICITY)EB (MODULUS OF ELASTICITY)Z (SECTION NODULUS) oooooooTEMP ON A SIDE OF NODE o o o o o

TEMP ON B SIDE OF NODEALFA OF MATERIAL A oooooooooALFA OF HAT'ERIAL B oooooooooPIPE OUTSIDE DIAHETER o o o o o o

PIPE MALL THICKNESS o o o o o o o o

MXDEADMEIGHT .oooooo -3587oTHERHAL 1 o ~ ooooo ~ -575966

'THERHAL2 oooooooo OoMAXIMUM THERMAL RANGEDEADMEIGHT RESULTANT

CALCULATEDPH = (P)(Do)/2TPB = (B2)(DMHAX)/ZRESIDUAL STRESSOF=


o ~ ~ oo ~ oo ~ 19350o00oooooo ~ oo 2o80ooo ~ ooooo 1055o00

oooooooo io50ooooooo 4o00

ooooooo 3o70~ o ~ o ~ ~ ooo io00ooooooooo 1o00oo ~ oo ~ ~ o ~ , F 00ooooooooo 25800000oooo'oooooo 25800000oooooooooo 117 '068ooo ~ ~ oooo 550 F 00ooooooooo 550o00ooooooooo 0 '760E 05ooooooooo Oo9760E 05

~ ~ oo ~ ~ oo 14o0000ooooooooo Oo9370

MOMENTSNY

-5599io-1473479o

Oo1615886o

57252oVALUES OF STRESS

7882o1361 o

33750o90158o

HZ-11399o328955o

Oo

TECHNICAL REPORT TR " 5828 " 1

REVo NOi 0 TELEDYNE ENGXNEERXNG SERVXCES88888888888N888NSNSNNSSSSN88NSNNSNNN

PROJECT! 5828 20 APRIL f9lQSTRESS RULE ISEXNINE NILE POINT lIIT 1

NSSSN8888NSSSSNNNNNSSNNN88NSNSNNNNSS

BY M~~) MTE+~~+

SHEET NO> OF

PROGRAM NAMECOMMON o CDANIELS223SRI i EXE f 3



RUN DATE 8 TIME20-APR-83 10$ 14+31


SY (YIELD STRESS) o'ooiioiooooeooooioo 19350+00B2 (PRIHARY STRESS INDEX) iiioooii+ii 1+13P (OPERATING PRESSURE> oiooiioioiioo 1055i00Ci (SECONDARY STRESS INDEX) .eiiiiooo iiOSKi (LOCAL STRESS INDEX> ,,o.,o,.o,o,o ii00C2 (SECONDARY STRESS INDEX) tooootooo 1 F50K2 (LOCAL STRESS INDEX) oooooooooooio it00C3 (SECONDARY STRESS INDEX) 1 F00K3 (LOCAL STRESS INDEX) ooooooooiooso 1 F00EA (MODULUS OF ELASTICITY) o i o i i o o o o o 25800000 iEB (MODULUS OF ELASTICITY) ...,...,,, 25800000,Z (SECTION MODULUS) ...,...i,io+,+ii 117o8068TEMP ON A SIDE OF NO'DE oooioooooooooo 550o00TEMP ON B SIDE OF NODE ooiioooiiioioi 550+00ALFA OF MATERIAL 'A oioiiiooiiioiooooi Oi9760E-05ALFA OF HATERIAL B ...,...,...,...,,, 0,9760E-05PIPE OUTSIDE DIAMETER 14 0000PIPE MAl L THICKNESS 0+9370

MOMENTSMX MY

DEADWEIGHT ~ e o e o o t 26234 t-35627'HERMAL

1 i ~ i i i i i i 505139 t-645298'HERHAL

2 ooooo ~ oo 0+ OoHAXIHUH THERMAL RANGE 827123+DEADWEIGHT RESULTANT 128829+

CALCULATED VALUES OF STRESSPH = (P)(Do)/2T

7882'B

= (B2)(DWMAX)/Z1236'ESIDUALSTRESS 33750m

QF=

10926'Z

-120993'12059+

Oi



REVo HOo 0 TELEDYNE ENGXNEERXNG SERVXCES

88888888888888888888888888888888888888888888888888

PROJECT! 5828 20 APRIL 1%9

STRESS RULE IHDEX

HIHE HILE POIHT UHIT I8888888888888888888888888888888888888888888888888

BY ~~4 BATE L~'~Mg

PROGRAH HANECOMMON+ C DANIELS223SRI o EXE ) 3


CREATION DATE6-DEC"1982 17o53

RUN DATE L TIHE20-APR-83 10 f 14 i34

NODE NUMBER 3888 DESCRIPTION RUN

SY (YIELD STRESS) ooooo.ooooooooooooo 18800o00B2 <PRIHARY STRESS INDEX) ooo ~ o ~ ~ oooo io00P (OPERATING PRESSURE) ooooooooooooo 1055o00Cl '(SECONDARY STRESS INDEX) io10Ki (LOCAL STRESS INDEX> oooo'ooooooooo io20C2 (SECONDARY STRESS INDEX) ooooooooo io00K2 (LOCAL STRESS INDEX) io80C3 (SECONDARY STRESS INDEX) ooooooooo 1,00K3 <LOCAL STRESS INDEX) ooooooooooooo io70EA (NODULUS OF ELASTICITY) oooooooooo 25800000oEB (NODULUS OF ELASTICITY) 25800000Z (SECTION MODULUS> oooooooooooooooo 98o5421TEMP ON A SIDE OF NODE oooooooooooooo 550o00TEMP OH B SIDE OF NODE oooooooooooooo 550o00ALFA OF HATERIAL A oooooooooooooooooo Oo9760E-05ALFA OF MATERIAL B oooooooooooooooooo Oo9760E-05PIPE OUTSIDE DIAHETER o o o o o o o o o o o o o o o 14o0000PIPE MALL THICKNESS Oo7530

MOMENTSNX HY

DEADMEIGHT o ~ o ~ ~ o o 47913 o -1605oTHERNAL 1 oooo.ooo 34747o 54439ioTHERMAL 2 oooooooo Oo OoMAXIMUM THERMAL RANGE 551432oDEADMEIGHT RESULTANT 54544o

CALCULATED,UALUES 'OF STRESSPM = <P)<D0>/2T 9807oPB (B2>(DMHAX)/Z 554oRESIDUAL STRESS 33750oQF= 132iio

HZ26016o

-80673oOo


TECSlICAL REPORT TR " 5828 " 1

RFV. HOo 0 TELEDYNE ENGXNEERING SERVXCES888888888

20 APRIL 1983PROJECT t 5828

STRESS RUlE IenHIHE llILE POItlT lNIT 1

88888888888888888888888888888888888888888888888888

B'f MTE +

Clmg IjA~ 8

PROGRAM NAMECOMMON o CDANIELS223SRI o EXE) 3

TITLERECIRCUl ATION LOOP 15

CREATION DATE6-DEC-1982 17 8 53

RUN DATE tt, TIME20-APR-83 10 t 14 8 36

I


iiiioo.moo 18800+00~ ~ ~ tt ~ 2i90

oo+o ~ oooto 1055@00ii201 F003o80ii00

~ I t t ~ i>00tttttttt ~ 1>00ooooooeioo

25800000'oooioiioo25800000mttttttttt ~ 98i5421~ t t t I t t ~ 550i00

550>00oooooo ~ ooo 0+9760E 05~ i ~ ooooo ~ o Ot9760E 05

}4F0000ttttttttt ~ Oi7530HOHENTS

,HY

-1605'4439ii

Oo661272m

62390mVALUES OF STRESS

9807m1836+

33750+27462+

HX5820ii

375210'iDEADMEIGHTTHERHAL 1 oo ~ ooot ~

THERHAL 2 oootooooHAXIMUM THERMAL RANGEDEADMEIGHT RESULTANT

CALCULATEDPM = (P>(Da)/2TPB = (B2)(DMMAX)/ZRESIDUAL STRESSQF=

SY (YIELD STRESS)B2 (PRIMARY STRESS INDEX>P 'OPERATING PRESSURE)Ci (SECONDARY STRESS INDEX)Ki <LOCAL STRESS INDEX) ionC2 (SECONDARY. STRESS INDEX)K2 <LOCAL STRESS INDEX>,C3 (SECONDARY STRESS INDEX)K3 (LOCAL STRESS INDEX> mooEA.(MODULUS OF ELASTICITY)EB <MODULUS OF ELASTICITV)Z (SECTION MODULUS) ooooooTEMP ON A SIDE OF NODETEHP ON B SIDE OF NODE ~ o ~ o

ALFA OF MATERIAL AALFA OF MATERIAL B . o ii e ii e

PIPE OUTSIDE DIAMETERPIPE MALL THICKNESS o o o o o o o

HZ22419+11675'i

THE STRESS RULE INDEX IS ii489


REVo HOo 0

PP span$88888888888888NNSSSSSSNN888888888888888888

PROJECTS 5828 20 APRIL 19IQ

STRESS RULE IHBDHIKE HILE POIHT UHIT 1

888888888888888NNSSSSSSNNSSSS|NNNSSNNNNSSNNSSS

BY ~W

CHK9

'ATE t.~~'~

SHEET Ni OF

TEl EDYNE ENDXNEERXND GERVXDER

PROGRAM NAMECOMMON'DANIELS223SRI EXE i 3



RUN DATE IL TIME20-APR-83 10814838


BY (YIELD STRESS) iioiioioooiiiiioooe 18800+00B2 (PRIHARY STRESS INDEX) ioioiiii+oo 2+90P (OPERATING PRESSURE) oiooooiioooi. 1055o00Ci (SECONDARY STRESS INDEX) i.i..iooi 1,20Ki (I OCAL STRESS INDEX) ooooiooooioei 1<00C2 (SECONDARY STRESS INDEX) 3+80K2 (LOCAI STRESS INDEX> ioiooo+iooooo 1+00C3 (SECONDARY STRESS INDEX) 1 F00K3 <LOCAL STRESS INDEX> i+oooiiiiooio ii00EA < MODULUS OF ELASTICITY) + i i i o o i i + o 25800000 o

EB. (MODULUS OF ELASTICITY> o o i o o o e i o e 25800000mZ (SECTION MODULUS) >s o oui.o iooio e o i 98i5421TEMP ON A SIDE OF NODE 550 00TEMP ON B SIDE OF NODE i iiiii+i o ii o o+ 550i00ALFA OF MATERIAL A +o+oooooooooieooio Oo9760E-05ALFA OF MATERIAL B ioioiooiiioiiiiiio Oi9760E-05PIPE OUTSIDE DIAMETER o o o i e o i i o i o o o o i 14i0000PIPE WALL THICKNESS i . i i o i i i o i i i o i+ ++ Oo7530

MOMENTSMX HY

DEADWEIGHT o i o i o o i 17208o 637mTHERMAL 1 oooooooo 534930m

479904'HERMAL

2 otoetoo ~ Oo OiMAXIHUH THERMAL RANGE

722387'EADWEIGHTRESULTANT 27074mCALCULATED UALUES OF STRESS

PH = (P)(Do)/2T 9807'B= (B2)(DWMAX)/Z 797'ESIDUALSTRESS 33750m

OF=

29818'Z

20892'3382'o

THE STRESS RULE INDEX IS ii467

'TECHHICAL REPORT TR

REVo HOi 0

SSSSSSSSSSSSSSSSSSSSSSSNNSSSSSSSSSSSSSSSSSS

PROJECT! 5828 — 20 APRIL 19MSTRESS RULE IHK(HIHE NILE POIHT UHIT 1

SSSSSSSSSSSSSSSSSSSSSSSSSSSNNSSSSSSSSSSSSSSSSS SHEET HOo'F

-= 5828 -1'ELEDYNE ENGINEERXNG SERVICES

BY

PROGRAH NAMECOMMON 1 L DANIELS223SR I o EXE I 3



RUN DATE 8 TINE20-APR-83 10 1 14140

NODE NUMBER 3817 DESCRIPTION RUN

CPM = (P)(Do)/2TPB = (B2)(DWHAX)/Z

. RESIDUAL STRESSOF=

SY (YIELD STRESS) o o o o i i o i o o o o o o o o o o i 18800i00B2 (PRIMARY STRESS INDEX> i o o o i i o i o e i . ii00P, (OPERATING PRESSURE) e i o i o o i i o + o i o 1055 o 00Ci (SECONDARY STRESS INDEX) o o o i i i o i o

' ii0Ki (LOCAL STRESS INDEX> i i i o i i o o o i o i o io20C2 <SECONDARY STRESS INDEX> io00K2 (LOCAL STRESS INDEX) oiooiooooiiio 1+80C3 (SECONDARY STRESS INDEX) 1 F00K3 (LOCAL STRESS INDEX) oiooiooooioio 1 i70EA <MODULUS OF ELASTICITY) + i o i o o o+ o+

25800000'B

(MODULUS OF ELASTICITY') o o i > o o i o i o 25800000'(SECTION HODULUS) i i i i o i o i o o ii e+ i i 98i5421

TEMP ON A SIDE OF NODE io>oooi>oooooo 550o00TEMP ON B SIDE OF NODE + i i o i i i i o i o o o o 550o00ALFA OF MATERIAL A iiiiiooooi+ooooooo Oo9760E-05ALFA OF MATERIAL B ioiii.ioooiii+oiio Oi9760E-05PIPE OUTSIDE DIAMETER o o o i o o i o i o o o+ o o 14o0000PIPE. MALL THICKNESS o + o i o o i i o o o + o w ~ o + Oi 7530

MOMENTSHX HY

DEADMEIGHT . -115959 11208>THERMAL 1 oooiioi.

234742'75912'HERMAL

2 tttoo+oo Oo OiH'AXIHUH THERMAL RANGE

303695'EADMEIGHT»RESULTANT

118791'LCULATED.VALUES OF STRESS

9807'205'3750'686'Z

23218m78624+

Oo

THE STRESS RULE INDEX IS ie189

SWSSSSSNNSSNNSNNNNSNSSNNNSNSN8NPROJECT oo 5828 20 APRIL i983STRESS RULE INEXHIHE HILE POIHT UHIT 1

SSSNSNSSNNSNSSSNSSSN8888888888888NSSNNS888

MTEI

SHEET HOo OF

TECHHICAL REPORT TR " 5828 " iTELEDYNE ENGXNEERXNG SERVXCES

SY

PROGRAM NAMECOMMON o C DANIELS223SRI o EXE ~ 3



RUH DATE lh TINE20-APR-83 10ii4i42

NODE HUMBER 3821 DESCRIPTION RUN

SY (YIELD STRESS) ooooooooooooooB2 (PRIMARY STRESS INDEX>P (OPERATING PRESSURE) ooooooooCl=(SECONDARY STRESS INDEX)Ki (LOCAL STRESS INDEX) ooooooooC2 (SECONDARY STRESS INDEX) ooooK2 (LOCAL STRESS INDEX> ooooooooC3 (SECONDARY STRESS INDEX)K3 (LOCAL STRESS INDEX) ooooooooEA (HODULUS OF ELASTICITY) o o o o o

EB (MODULUS OF ELASTICITY) o o o o o

Z (SECTION NODULUS) oooooooooooTEMP ON A SIDE OF NODE oooooooooTEMP OH B SIDE OF NODE oooooooooALFA OF MATERIAL A ooooooooooooo*LFA OF MATERIAL B o ~ oooooooooooPIPE OUTSIDE DIAMETER o o o o o o o o o o

PIPE MALL THICKNESS

HX240409o

-470066oOo

DEADMEIGHT o o o o o o o

THERHAL 1 ooooooooTHERHAL 2 ooooooooMAXIMUM THERMAL RANGEDEADMEIGHT RESULTANT

CAL.CULATED VAl UPH = (P)(D0)/2TPB = (B2)(DMHAX>/ZRESIDUAL STRESSOF=

ooooo 18800o00o o io00

oooo'055o00ooooo 1oiO

ooo io20oooo'o00~ oo ~ o io80

oooo 1o00oooo io70o'oooo 25800000oooooo 25800000oooooo 98o5421oooo'50o00oooo 550o00oooo Oo9760E 05~ oooo Oo9760E 05ooooo 14o0000oooo Oo7530

MOMENTSMY

36026o-537814o

Oo720051o243687o

ES OF STRESS9807o2473o

33750o1629io

NZ16997o90929o

Oo


II

I

~~ (.I

N

'I

Technical ReportTR-5828-1 F-1

-rs-TELEDYNEENQtNEER(NQ SERV(CES

APPENDIX F

CALCULATION OF SAFE END STRESS

suvuis Eaux uA @vs vTg-5828-1

-<>-TELEDYNE ENt-WEEWNG, SERVICES

BY

CHKD. B

OATE~+T++

OATE~ PIPIT Pf /L C Poach' >~/ 7 f-SHEET NO. OF

f'O K 7'/IF CANC uaF41 los 0 f-''rrIPS ~4b Srkr:"ME5

P4'R r-E5 Ah/ 5 AO HKh/7 S ~8 g8 8'X7 FWC7E'lO F CoQ"PI PZ'D Ke 2'S hhlb HbhLEA/TQ LoC4L ~K&BWK PIPE'c-

7 lo p5 'F 7 Hg Fox.c,oairt/6 coo P'5 cow pung R'u%5:

paAb me/gg 7'

NE'RW4 C

7 He KNtrf <

1 IIExwgc. 5

/Irxr~a+RHx3xev pHx g JY Ep,'5

//X$ C'a'X V

~~7'I< 5~/5&IC X "P/R HX35/ 5 2

Y- br'X3SQ6+Z- >IX. H'rrSSW pP

PYPJh&IC. 5MS+I C X - bl~

f- PIR

P - lOIR,

5&/S A/4 F-'uWS Urer Co/T/V ~IFru~O S~a y>7Rt/T5 WOi)CIEb ~IT'h' S Pk/rt/g Con/Sr-A&7- OI-"

FF dg 8/

TR-s828-i 8 TELEDYNE ENQINEERINQ SERVICES

BY

CHKD. BYDavc~<~4'/4E

P7/L8'>rnite un!j 7SHEET HO. ~ OF

F

COO F'SSAFE E/VS'F Po ACES (EgS) A%ST IHOP1E~S (Fat -l PS)

/t/APE'po

RAIQ L 75/5Co/ b I T'/OAI

QXIA 6Folic&

f-hÃIS'/Is'4a

Z-IqI SS'EW R'oes c'w4L

Hu+8 u7y-Axepg ort E'W7

P-A)C/5'o&~~

OFAb"~F/4HT

jlfFRPfA L.2

7 HER'hfA/S

SV.AWING SF/5X-bIR4. S.g-beg,

z,oop.

/~ pa, - 3~9F.

~a 9t)-s.s VZ. '/< > ~

- z/ y, (os&/-

—S-/5 +.

ygy g8.

'BS<2)ZOS goC,

~g W/.

zzz>. -PsSoS'.

> g >sg. ~os PPR

-/ f'/5 f. 7+//5.—2'/'g /pe. —5//op/-

S. 5',p-C IR

bfPI, SE'/$5-bIg

f f$ > +3'+F

++8'5 +9l $ .

—s /go.

s-/z+.

~eg /z./.

'Zg '/go,

z/os3d. 2/722.

~nzznO. >1y)ua.P. 5'.

y- bigh.S,'8-biR

ToTRLS'/

C V-. 7+2'L. g zing.

5"> /2.

$g P/0,

g4 'p~.zPP F~ F193~.

+Bc fdic- goyyoo.

I~O/OO(, kd 0 003

9K WH'E'AXI&gA7 HFR~AL WAhlg E //PS 'VEER'SED FPR 7/PlD

SHOWA ~I OP/.

TR-5828-1r>-TELEDYNE ENQlNEERlNQ SERVlCES

BY F~CHKD. B

DATE~~~~DATE~ ~/itfF p7/L 8'olk/7 cfhll7

SHEET NO.. OF~8'

L.OO | /S

spry spry pomcs5 (ass) AND hfoRE~s (l~-~ Es)

NeDE'7~

hhlQLVS/S Ax M <Comb t rIou FOnCE

7- hX /$'//8/8

7-apl $''Hews

q-o z~ow 4 g.

pfa+8 4'7y-rlX/'5pg ore EP7

P-AX/5~ O&a~

>EAb-ma-( ~HT ~2 l3. /23 ~ ~y,gy ~ IiZ . -I/4'59K

ST'4T IC SP/5X"b i'g

S. 5./- Lsd,

$.5;p-'blF

'DfN. SK'l$5-b]gD. S.y- b)Rb.S.~-bit

-W'/5C. -S O'Vi.

-isis, 9479,-Zopf. —Qy0$ ,

z32.

iz 6O. 3a ~9.

is @5'.

P8'0 i

/gal.

I Z8<. -I~y«C. 922 ~fr

(ig ig g p/) pry/'//o) g'I/<~ .

I g O)~O. -3/3'ops', -2/g<PF

g~ -//] gj. +gg37: ) gogh?-

gag FD. gaff/. —s Sli.

3'ggS. Ig C /du. QRWfgO 2/+DO>.

)'// 35PFo. n4~D <zP/~

7 54'2 ~ ~ 2233do. Jypl oo ~

ToTRLZ g5 Py /'gyo X2.45'lylygZiy. PWZ8'l3, I25,$ )g

9K Vh'6'4XIAtJA 7 HERNIAL 'RA)VQ E II/$ l3EEA'SED .FPR'II/5

TR-5828-1

>>-TELEDYNE ENQINEERINQ SERVICES

BY ZWbCHKD. BY

DATE~~~ ~~'~SATE~< ~/~E'jq g po/+7 uwxTZ

SHEET NO. OP

PROJ. NO

5~EZSSES 8 i SAFd ad& nloP8$ dF C ooF i5

4 OM IdP

~X « ~ S7-Ra>

A/I/t, L PDgcE' 5 8/5 +Cgo55 SEC T'/4'4A t ARE'A Vr E3 -IT- ZS-.y

s~ w./A gg f 'F4 p p sf

QpE'R~l sT R~Q

sA+A'R F o REN (I. ATJJ FokcE) +/Ax'5 F P'-RcE)

~ ~+'.7./

58'I 5

pg 6" rsjC8I 3gg, 'P

zaa.A g sr'~ C~ @~a.P Qy mwsro~~c. ~o~m~

Z-3 Q= sa<hk ~~~1 = F'I PE

~inDlvS'-O

e~zO~~ ~ ~~~~~8 a C,h R WWS~i OF bv BC Tl$~isa 4 =P>

P'oLQ g hf de ZAN"ol- /Af4'JZT74

miTn > = bL

TF b32

Tg-5828-1

-r>-TELEDYNEENQINEERINQ SERVICES

BY

CHKD. BY

DATE~E'~~3DATE+~ /V(MB ~ I L. H P'uIIV7 uA//7 2-

SHEET NO. OF

~SZS'o

Too rOO ComV=

~~~~we (i+)(<E'WX7 — I'5'Ifp, Z)

FEnJ bin/ g S7-WdSS

i/o6 oo/ ~ I' oos Z'

as'794/

SEC7-I 4 'o f) v L 05 =

My i Z 8 7 5' l

TR-5828- tr>-TELEDYNE ENQINEERINQ SERVICES

BY

CHKD. BY

SATE~i~~DATE+ A/IN+ ~1 L E pogrv7 UNIT X

SHEET HO. OF,~FRF

Kobe'y~ ca~.SHEQXI sT~~ c'Au+6'0 p, / ro@5iop'4 c. ~o~E~

7 OTCSgo~A a ~oH8g/7 = i/98 2/7

(iqy rZiy)(F")/@ iud.5

IZf7 p'wt

Ee~ bs~a s7-RcH

5G'~b(,~6 Mo&~~ = 7 g Q PI3 + /Egg pl'g

i+/+'/ p'

"/, = '~'~~~' ~<i'S Ps i

rarA c. 5'< sS E'5

h'o pE'pp hg I4+WHmAg

BFnib in/~

rorhI

Ws. 6"

4//o.~S dO,p Ps<

do PE 2 'P5

sarah

R

gZVX iiiiq

~a7 4 i-

V5',0/po,

» 9'7

ops, o ps>

SAFE Eub pcs o mg @LE g5 i 7 Iz5 f'5/. Nore: ST'KagS cs iidya Spy> C~uszR.y87lv<<P'

PP8'O wino c r p~4w gb 70 0 sec r/o~-

Technical ReportTR-5828-1 G-1

r> TELEDYNEENQlNEERINQ SERV(CES

APPENDIX G

TMRPASS CHECK

TR-5828-1

-W-TELEDYNEENQINEERINQ SERV!CES

.BY DATE+ I~ ~+CHKD. BY 0 DATE~M

~Zua A'I~POI~ uWIr S

Pdss z~sn-SHEET NO. OF

PROJ. NO. &8ZB

PAS ~ RC/ItI C+bCK

Technical Report

-«-TELEDYNE ENQINEERlNG SERV C

BY O*YE~CHKO BYZ2BOAYE~QJJCg

FA>+ CHIC I Hp'SSFXq

SHEEY NO. OR

PROJ. NO, 2

/Zoo /Zoo /. 0 /09,782

/~O /~a /0, 75', 5'7y I, 0

ea, a ~ass- iiS i'a> Sqo~70 C/,oG)

~OX)E w>8J Q ''@CO )JI) ~57~~ 8< C.7mB) gog,78Z

AoDE B9'ZS /ZDD(ro, 7~)q C.sr~)

$885 vll'TH QvJAy'~>U~ /OOQ~/iU,

NC O~/Zoo< f g~ ga 99oZ7

SHOP

loÃSd z l(z@olz

/SIC do 5gyeqg

8qo58 c gyp

8~o ~ CSSOZZWro>yean~

~+~~ ~ cs~s<s ~ zzi~~~a105, 782

E4 /0 JJ > ~D PJJ Z g Pq 8

A8ZE 88/6 gggaqJ'Q. gg+

O'0J)g gcygg 20/9q'5+C, &9&

0

Technical Report

<<-TELEDYNE ENQIMEERINQ SERVICES

BY DATE~CHKO. BY~OATE~ZAJM

FASTS cREcg HX9NWZN

SHEET NO. OF

PROJ. NO. BZ8

Eccl I5Vooe ) )5l7EAPV/Fl&HT'ONE'NT5 I N-I 8&)

Nx Nv Mzxz 9'6o c5'/b z6g+o

V ply. g p)W.

949(, o 8Z579oX PIC.

Nx ~gac o

HV' 4 I I <O ~88O Z7gZO

HN zqzszo /o97oo &octo

STAG JC. &El&PIC, HONE~& (IN-4&5)

ggDZ7

g~x = szv~/Ylry= /<@aqua

Hgg= zoo/og

PweAHIC- &El&HIC HOMEH15 IN-C-5~)

Hx

5yHp

X ~In. Y PIR. 2 PI Z,

2/77ZO 7d 4/c Sg9yqo

/qeC ZO 9ISVO IC oyyO

zc q /9o 8889'o 28gydoCDNG I RED SFISM) C. 5OHKHV&< Hxx ZH~ ZNre/6/ 457 +5hz99'+$ 87/Yls = (~w )'+%w.)

(~M-)'&

= /ZZZ/0

. Hey = zzz &pc

8Rs = yootog

/oh''Sb z

~A~TELEDYNEENQINEERINQ SERVICES

BY oar E '~~5CHKO SY<c&~ATE~ZEF'dG

c/t rc< /-/XW52'M

SHEET HO ~ OF

PROJ. NO.

LocF'5NoDa //5 caMT1 N UE'0

msRHP i HomE.N<s (ie- us)gx

THERMAL 1 -9$+7D -Pg/$ 0 /'7g 70

THEW4L 2 ( +1090 —/95o9< -/279 /d

THERMA,L9 / 7Q8o -64qld —/574 7o

MERHAL4 /y9'856) -/ZP9~~ -Z@58(,o

THmelAL 6 -qo.579o —.&boa /094

7'4v(|Ylv

M fzANc-E'. ~G/'.MALg - ~t=R'PAL 5YlY. NY gQ HC'= Hg

)o9958'o y 79so /goo pc o/(p 750/ z

Techni cal Report

-><-TELEDYNE ENG,INEERiNG SERViCES

DATE

CHKD. BY~~9DATE~~+C%PAss cHeck Hpsypg g

SHEET NO. OF

PROJ. NO.

t cop /5Noes 98I@PERDU/El &HT HONE NT5 I 4-L8&)

Hx Mvyze/o +8~ zZIZo

9TAH IG &5I5HIC HOHS'C & (IN-L&5)

Nx

Hy

H.

X VIR. V CiP;.28'/ C OOg PIP.

ZOIC'DZB'o

pg 9g g ZQQ

Zgzd,c ZOO lg 7O

Hex = ZS<z7

Hay = ZOyFJJg

~kZ =

Z<5Cul'V'NAHIC.

&Gl&HIC HOtu1EHq5 IN- L55)X 'PIP. 7 PIR'. 2 PIR'.

H< 87q6O /I f4o Z7g lo

Hy 476'PO et'F9O I PZOO

Hp. y 774 o 7o8o RgzoCORGI RED Sg ITIC gOHKHT&< 8~x ZHw X Nre

QQQ22 7205'/ 7585/

Yl~ =. (~w~)'+(se«)'Sm-)

Hex = go9'9'5

Hay = 8/QZ6

f1 F:s = 4 qzgo

/Zg bo

Technical, ReportTR-5828-1


BY DATE~f85CHKO. BY&~PRTE~fd~

cHEc< Hxggpz N

SHEET NO. OF

PROJ, NO, Z

/.aoF'5'GDE

ge /5 ~ ~QT~ N Qg~

~<~~AL MoHE'NT5 (lN- ~g)

M>~«~L ~ aoy~yg g~7ggg

. TH~+( g Q / g Qg()

THH2~L Q g~y/qo goya o ~q

209 $/0 ~/970 gg Z70

5 +4)'77/ 0 ) 78 Q/

WkfEgHRL. ZYlx

1»>8~ 3f o/So ggqgo

Technical Report

<>-TELEDYNE ENQINEERINQ SERVICES

BY DATE~IOHKD BY~DATE~XDNS

pAss cHEck HXDBF24'HEETHO. OF

FROA HO.

gaoF'5Nor E Bq~~VSWVWS lS I-l~ HO~<NTS l ~-»~)

Hx Hy MK/ohio +&9/~

W- Yl~

Sb@O7

STATIC. &FISHJC. HOgE~S (IN- 4&5)

Nx

Hy

H8

X PIC.

600

//OO

V VlZ,

9oSo 7c8095o Zo/So

gc 50 pago / g /0

Hex = 77%

Ylzy = zopf 7

Hrz = I lope

PYNAHIC. &6'1SHIC- NOMEN'N-L8~)

X ~IZ. Y Pla. 2 PlR'.

Hx pg 58& 7Z 8D 29)9G'y

Zo7 I0 8 Zoo Z ~97o

Hp 24&&0 to 5)o, CORGI RED SS IllC- KOH8 HT&< Hzx ZHzy ZNreqqqc4 ~/~95 Ipqrsgy = (~a~)'+(W Y)+(SWE.)

Nzx = @ZZgO

Hay = >OSCa8

ll~s= PZqyZ

Techni cal ReportTR-5828-1 -W-TELEDYNEENQINEERINQ SERVICES

BY DATE</~~8~CHKD. BY~~DATE~Z~>

cH Q~QI= Q)egg F2AjSHEET NO. OF

PROJ. NO. 2

~oF'VODE ~ 45 cGNTI N VG'P

~6'RHAL MoME'NT5 (IN - W~)

5xI90~ —9/o / 0 7~o

TH~4L 2 Qgqc> gg 7c qgc 50

HE'R'MAL9 —f g~ I ~ —/g~~/8/dc Z 97m 8 Pyro

THGRYlA,L 6 J Q.7+@ -QQ~ / Bcpl~

YlAx)NuM fzANc-E'- ~ Gg'g4,LHx Ny

f zol 0 ) goo z~oy5 MA( RSW~

2c9&9'5

TR-5828-1


BY DATE~AUCHKD. BYA&»DATE '~0~

FA,ss cHGCW HX9~+ggSHEET NO. OF

PROJ. NO.

p'A,S> +le 5QAg &TRUT& Rl&P>

Loot 15

/ Z6 /Z~ ISA Z888zo jnz Izcu9VZo Iform IZm /O,75

l,o5~ 790

97<

I

l,o /og,7HZ

I.D qC,C89 Z997o

29/79'7 /74K099'r98o

9oap7

<rieV zqSW

bQ 8 Uo&E /Z5 IZED F82 ~ SZZZ44C/ aQ

aOCJZSGZCT taCe(l ) ~CCZ7 > zy CZ69) /D9,78~

IUD>E &920 /ZGO (JOi7S'9&70y c.~~~)

AsPE /25 g~ 7' z2Pc ~s/7~7)

7/So

NODE 582o 9+79 + = 7>oD/o &178 2

z59/0 T" 47/'Pl )gC, 68s

Eg 10 ~DE /ZS f 74609'9~FR

EroDE ~8Zo 085'7O = +9'0+/69,7HZ

Techn1cal )report

-r>-TELEDYNE ENGIWEERWG, SERV!CES

BY P OATE+~y8~./I I)

CHKD. BY DATE~i+Fhss cHEci; HA9PVH 4

BMEET MO. OF„„„,~FJS

LCeF'~Noc E IZ@

PEADW'F1&HT HONENT5 l 4-l-85)

Nx Hv725 o . 8/o 9/9'ao

&VATIC.. &El+A)C. HOHZ~5 (IN-L85)

922z4

X PI%.

Nx /4+7c

HY 'Z4ZOC~&07D

Y CIR. g VIr.7Z 80 7// 0

/ZQ )g&ZO

// goo bgqO

Hex = 7»I~Ylx'y = 6 5'z4 I

Hrz = C 7877

PYNAMIC &6'l&MIC- HOME'NT5 tN - LS~)

Hx

5yHz

X ~IS. Y Pin. 2 PIR.

989&o 25/Zo +989o4C Il0 gza9c 96 57o

44Z7o zq 6 go > I c SoCO&GI RED SEISMIC. 5OHKHT&< Hex ZH~ ZNre

/soIz7 /0988) /2&799

yl> = C~~ >'C~w>'y~.,>.

H@( = 57//7

QRy = 7'pggO

~a~= 6R'/~

ZP/7S 7

I ecnn> ca i ~eporr.T,R-5828-1

-r> TELEDYNE ENQINEERINQ SERVICES

. BY DATE

CHKD. BY~>~ATE~2~0F~ss cHEcg H/9P'F HAI

1

SHEET NO. 'FPROJ. NO. Z

LooF'S'oDE

Z5 . cakT)NUES

THGRHA,L MoME'NTs (IN - ~5)

5x HyfHERHAL 1 -7Z+gg -gggbg'007oTt«MAL2. IOqSZo -lSSOgo -/So29+

THERMA,L9 -gyygg -gag to -53++0

~~wm~d.z~eryo -iZSSSO -BVSZ7o

vBmNAL s -88y98a -Cpgoo /c/C ohio

ylAXixlvM FZAN6-E". +Hpg~L4 - THEKYAI 5YIX 8f QTE HC. = Hg

88( gO g7ygO (>QQS&O

iecrinIca( HePortTR-5828-1

r>-TELEDYNE ENQINEERINQ SERVICES,

BY ORT~W'CHKD. BYM~~ATE~~~~

Palsy CHECK I~x9F7gxjSHEET NO. OF

PROJ. NO. +8~8

pooP /5Ncc 6 88M17EADV/5'1 &HW MONE'NT5 I 4-l-8>)

Nx Nv Nez7ZSo po /qo zo7M

STW IC. &El+HlC MONE~& (IN- L&5)

%- Ylr,g(pQZ 7

Nx

Hy

H.

X PlR.

7720Y Clp:.

/I ggo /o/ 7o

8,8/o c 7oo $7zo

29oqo 0/Zo

Hfx = zo128

g Ky = cj fbi 08

MgZ = Z94 7+

Y PIP. 2'IR./<~do zC9ZoI 7OlO /545G

X ~iz./8'7( /9o

Hx

Hp /54/o 8 I BO 72'VO

coHSl RED SF(SM lc Hog s'NT&< 8~x ZH~ 2 Nre9 977T /Z9'4 78 50 gpss

yl~ = (~~~)+(~e«)+SHj")

PY,NAHlC- &Gl&MlC- HO&EN$5 lN- l 5~)

8~x = Madqgrey = goo7o

8RS = 9705'9'

I LCIIIII Cl I ICePOrtTR-5828-1

-«-TELEDYNE ENQINEER|NQ SERVlCES

BY DATE~i~ +9CHKD. BY~DATE~V~C

FWS5 CHEcK HA9~/-IgEHEET NO. OF

PROJ, NO 5 ZS

LOoF'5NOVa 98ZO CaNTI N V GO

*

-rhGRH AI HONE NTS (IN - AS)

gx Nv HefHER~L 1. —Q~BD -gcf7$ gg 870++

TH<WAL2 ->/O'O'BO -989'89< B88/O

vHzR~L 9 -7/g/g -gq7$ 5o g g/40

TH%I ~l-Q —/'7999K -/ TO/ O'O QQ g@O

7HEF'YlAL 5 D&700 —/7+g&O Q /50

~ I slue ~c-a'. CHEi2% AL. Z.

Ylx NV gs~i~9eo >8~8~ RAMG6

+08 f70

f

r er;rrrr)r:a r KeportTR-5828-1


BY DATE:~/j9>CHKD BY~DATE~A~O

I W:-s <Hect= HxrZ+HMSHEET NO. OFPROJ. NO. '9 +8

loof'/5goo E gq/OPEAOWS t &Ha @gee NTS I e-I S~)

Nx Nvgz ZPG /9'8o 58 7c

STAY'IC. &El&HIE, HOME~& (IN-L&5)

X CIR. Y VIZ.

/ops g>9a (z&o

- Hx@+370

H~x = 9qio

HY . 5(p9O

H~ z55ogg 7o

agob gygp

PYRAMID Sgl&MIC HOIVlEgq5 IN- LSS)

X +IR. V PIR'. 2 PIR.Hx gg 2G ++&0 /QZ/oHv'ps'8~o i &zoo

+8/0 // Z5o g987OCORGI RED Sg ISTIC. QOH~HT&< 8~x ZHw 2'N~e

/fg 4 9 g zyppa 9bzg'7

gy = (ZHE)'+(KMgE3+(SHEE)'F:x

= Idq~~

Hay = /sr 7Oq

Hgz= zb77/

<7/'7 /

Technscai KepuiiTR-5828-1

-r< TELEDYNE ENQINEERINQ SERVICES

BY DATE

CHKD. BY~DATE~gOOQpAss cH'e-ce Hx92%AN

SHEET NO. OF

PROJ. NO, ~ EF

icxoP 15

HORDE' fZO coNa1 N UED

~GRHAI MoME'M5 ClN- A'>)

5xfHEF:HAL 1. -9'7+D

Hetaye -97+go

THEeq~L 2 -RR I'0 -4&7o -qS'96a

THERMAL9 -Q@57o -/855O -Sg/oqC

Met ~L q —pq+0 /@+0 —ag79oMmNALS —$ 4490 -2/Slo —/8z/9o

~~HvH ~c-,e'. ~ERHAL 9Hx % gs

Q(c 670 &8~~ &90 f> ~488'f7


->>-TELEDYNE ENQINEERINQ SERVICES

BY DATE~+9CHKD. BY~QDATE~20 EB

pp~>s cH~<g l]X5&SH P

SHEET NO. OF

FROJ. NO. >6

PA5> HATH ow'AY SVP:VW R't~lP, «<P I<AcaE/o5 IZao igloo g6 l o5 ] o 9~/ f6764

He <cz~989q zcoWH

(qua/+ 7/5/58

l05 /zoic 28) ~ 4d7bb

a.~ ~8> + /S~~eq CiD~) 999

MoD< l05

25094 9

Technical ReportTR-587.8-l

><-TELEDYNE ENQINEERINQ SERVICES

B Y " OATS~8+CHKO. BY~OATE~2+M

p4ss ch'Gcg I-I)(9&8HR

SHEET NO OF

PROJ. NO. BZ

LooP IZNQPG'09:PEADW'51&HT'ONE'NT5 I N-t 8&)

Nx Mv////0,9770 +Bz To

SZA<iC. SSie<~C. Zogems ~is-ms)X cia. Y rim g ~ir./&So zqz 9o 874 l>/9''0 78o z74/o

~/C qo <~><> Zg 7o

Hrx = dSSZ0

Ylg.'y = c9'Pbo

~ P.P = 4C VW8

PleAHic. &6'lsgic. HoMEHf5 IN- L6~)

Hx

Hy

Hp

X ~in. '/ pic. 2 Ptz.QSZ 5o 9b IWO Ze'WOO

qoqqo /99'6o 97730

92 /9'o zGVgo gee ooMAGIRED 5F'lSM JC NOH@ NT&< 8~x ZH~ .2'Nrelg@9gl /ZS99'8 //SS'+9

fly = (~W~)+(aaF).(XSK.)'

= 6/8Z/

Hay, = 5'l9'PG

Has = 6888+

zoggy

TR-5828-1

-><-TELEDYNE ENQINEERINQ SERVICES

DATE~+~~BY

CHKO. SYAgR.OATS~~I'A55 cHGct HX&e'HF

SHEET NO. OF

PROJ. NO. Z 8

NODS'O g coN 7'I NV&p

iHGR>'tAL t 'lOMENTb ( I N- 48&)

Vlx N~ H~

mmwAw ~ -5z( ce> am '7bgpo

msRr-w,~ z 5ZC go ~Ed,0 -/47/SC

HAxiHurl pAN&E: ~EggqZ Z —ypZ~+lYlX Yls Yla YlC= Hg

/Z <z8a dado ZZS@9'O zdo4 S

I 8COfl1 Cd I fCLPUl'ITR-5828-1


BY DATE+~ 8SCHKD. BY~~ATE~2~O

pAss cH Ect. H x9eg HR

SHEET NO. OF

PROJ. NO. - Z8

C coFace e $98PEADWEI&I-IT'OMENT'5 I N-L.S>)

Hx Hv He9'89o 7 pC o ~d zo

S1-AT'I G &El&HI C, HOg&'~& (IN- L&5)

Nx

Hy

X PIR. V PIR. g PIP./9''o 2/9Ga //sago

cygne

ZZD +ZZ8>

z4 5'Kqo /Dao

9~x = Zr"9'~/

gg.y= qzz9'/

Hgs =

Z/6'v'NAZI@.

SEISMIC HO&EHV5 IN- LS~)

X ~IF:. Y PIP. 2 PIR.

Hx @99"zo /9/So Wzsa'0

Hy Z89'ZO 9'Z/O 4Z7SOI

~2, /8/70 S5'70 / 7/3oCoal &I @ED SF'ISTIC 5OHS'HT&< Hex ZHw ZNre

gyro &of59.

gy =(ZMe)'+(W,T)+5MEE)'gx

—— ro. Qgy = ~Z+ZP

8qp = ZS~S'O

l<sB/

TR-5828-1

r<-TELEDYNE ENQINEERINQ SERVICES

gF/ +

~oP (z

BY DATE~~ +~-

CHKD EY~SDATE~ZO~ghats cH-Ge.< Hxsae Hp;

SHEET HO. OFZ

lvoDG' 5g c.oNT't HQgP

wamcNm (i'- t-8~)

I5'$920 t &090 -/8/590T7-DERMAL 2 —$4jf974'yQ -g$q ZO fg 7 f+O

HAxlHuK gANc-E': THERMAL2- CHEÃHALX

'eve. ~~~a.goc280 +77Eo 68++7o cpg~g~~g



BY DATE~CHKD. BY~DATE~~E

FAGS cHGcw HX&5BZV

SHEET NO. OF

PROJ. NO. 8

pAM Wl-rH +wAy MR~ AT Icoc+li~, Lccr

ACUTE'og

(Zoo t ZooJ2QO JgOO

8 /o5 )0ga l.o& z.w8 gqq loNB

yzego~9O89

wouw /os /ace gag 4CYd47'570Z)g p/,os/

/ZDGCPS 7 p~~ @(/D558 v"2d9D89)

Dg

Dg go A9~ /oS4

2d d989"7

Technical ReportTR-5828-1 , -<tI TELEDYNE ENGINEERING SERVICES

~ HF

BY DATE

CHKO. BY~OATE~2<83pq~s CHE~K HxBSexV

SHEET HO OF

PROJ. NO.

LooF' 2goo 6 105

PEACW51&H~ HONENT5 IN-L8~)

Hx Ny Me1I t I o &77o g6z 7o

S7W IC. &GI&HID Hog&~& (lN- 4&5)

X r rz. Y VIm.

Nx zqqyo zBzlo 9+Z6 o

Hv >so>qo po /(isoyoy/o ybayo @95m

Hc,- Ylx

Hex = /o/~oz

8 ay' //'9//8+

HgP =

PPZZEF'YNAHIC.

Mt&eic Ho&8975 IN- LS~)

X ~tR. Y PIR'. 2 PIR,

S/oeo g58qO ///9oMv /sly 7o /8~8o IsrZgo

<8/'qo 8+o 95//ocoH&I W~ Ss.ismic. Nows st< Hxx ZH~ XHre

zzbay/ meal ld~/PF

yl~ =(<w~)+(~x.~)+C~~-)'F:x

=/z<78y'<v

= /'//38THF's= 9/g7o

I

TR-5828-1


BY/

DATE~3~ SHEET NO. OF

CHKD. BY~~ATE~~~

pooP l2.

ASS CHECW HX998XVPROJ. NO.

)MODE'05 CONY'INO8'P

FeÃAI vos<<Nm (ix- ~so')

Vlx Nv H~

TechnicaI Repot t-<>-TELEDYNE ENQlNEERlNQ SERVlCES

BY DATE~~9CMKD. BY~DATE~+EE87

pA+s cHsc< H-x95ss v

F

BMEET MO. OF

FROA MO. EZ8'ooF'Z

Voc E

V~ACWS to H~ HOm<N<S (I e-L.S~)

Hx Ny Mz$ 8 2O 77/AFO 9 / 8O

STAR IC. &El&PIC HOME~& (IN-LSS)

X PIC. Y PIR g Plied.

Nx ~869o DP+go ~rye a~Y DgSpo 2%o 8$+Zo

B /zo gZ9'o /<goo

(o5'68

8rv = 9'+/f8H~~= ipse

1/'Y'NAHI C. &5'I &HIC HOM5 g T5 IN - L59)X 'Plg. 7 Plg. 2- Plg,

Hx y/yea X+7SO Z7yO

gy 7+9/0 />989 /O/0 KO

ggapy ggqO +//doCORGI H~ SS.ISTIC. NOH<HVS< 8~x ZH~

%Nrem

/29'79o 222z5/ w4bso

fly = (~e~)+(~e.Y)+(~~..)

H« = arsrrHxv = /sD+N9'

ze =Zsyzp

rTR-5828-1 '>

TELEDYNE ENGINEERINQ SERVICES

BY DATE~~ICHKO. BYMOATE~4+AX

PAss cHEck Hx'99 XV

SHEET NO. OF

PROJ. NO.

INoDG'/5'oNT'lNUKD

miE~NAt t zc +E..Nm (iv-Ws)VI< N~ H~

<i 'writ 1 /699/0 /9090 -/q'T7o

. THERMAL2 -/++770 -g+ pZQ pg+7gc7

MAX(muK pAN<E: 748RML X - 7h'EP~L Z

YiX Ylx HZ YlC=6+gogo &iso Fazed o


N

H-1

-r>-TELEDYNEENGINEERING SERVICES

APPENDIX H

CHECK SHEET SUMMARY



The following check sheets are included for documentation of checking

procedure. All computer runs pertaining to this report have been accounted

for by the specified analysts and checkers. Comments made in this appendix do

not affect the analysis results presented.

Ly tte N. Be jamin, ngineer

L o E. arr n, Engineer

Cc r M PCv-

Eric A. So a, Prospect Engineer


CHECKING PROCEDURE FOR PIPING ANALYSIS

(To be kept with Analysis Documents)

MODEL NO. l-00DRAWING ISOMETRIC NO. 5-OTHER REFERENCE

DRAWINGS NOS.

4J Ih > c isrn<c (sreoYs ebs>o i9

PROJECT NO. '&ANALYST $ A ROM

A. THERMAL AND DEADWEIGHT PORTION

Check for title card information.Should contain the following:problem no. or 'system descr iption,load case (deadweight, thermal I,etc.), analyst's .initials, date,run no., project no.

Checked S Date Comment 0

QX

2.

3.

5.

Geometry (Check coordinates atterminal ends and critical inter-mediate points such as branchconnections,'changes of directionor pipe size, valves, restraints,etc.). Use of computer plot isadvi s'able.

Check coordinate system (Doesanalytical model agree withspecified plant or piping co-ordinate system.)

Check, pipe ~roperties (O.D., Thk.,Wt., E 9 70 F, ~ 9 pipe tempera-ture, .etc.). Use material andsection property tables and pipeelement input data sections ofTMRSAP.

Check for pipe element connec-tivity.

9-8-89g-Za~

2/2/79

TechnicalTR-5828-1

Report

CHECKING PROCEDURE FOR PIPING ANALYSIS (Cont'd)

Checked. B Date Coment 8

6.

7.

8.

Check to ensure valves andother components which representa concentration of mass areproperly modeled; i.e., checkthat mass C.G. and orientationare correct. (Use nodal loadand mass tables.) If valvebody is modeled as an equiva-lent pipe element with dis-tributed weight, be sure thata concentrated weight is notalso specified and vise versa.Valve bonnet and/or yoke shouldbe modeled as a stiff elementunless information to the con-trary is specifically provided.

Check that all pipe fittingsare modeled properly.

Check that correct elbow orbend radius is used. Usepipe element input data sec-tion.

9 Check that temperature distri-bution {hT's at nodes) repre-sents the specified operatingmode. Use,nodal coordinatetable. Check that all im-portant thermal modes havebeen considered.

10. Check thermal displacementsand directions at nozzles.Be sure direction and signagree with coor diante system.Use boundary element tableof TNRSAP.

Check anchors and restraintsfor proper location and con-straint direction. Use nodalcoordinate table and boundaryelement table.Caution: Avoid putting re-straints at either end ofan wed-ef w elbow element.

2/2/79



S

Checked B Date Comment f12. For, deadweight, check to ensure

that deadweight card with -1.0in y-direction is used. (Checkelement load case multipliertable for -1.0 beside y-directiongravity.)

13. For thermal expansion runs, checkto see if thermal card is usedand a 1.0 is printed besidethermal distortion in the elementload case multiplier table.Note: If pipe is thin-walledwith high internal pressure,there can be a significantchange in elbow flexibility.This should be considered byinputting internal pressurein the model.

~,

Check stresses* against the fol-lowing allowables:Deadweight (normal operation):5.,000 psiThermal expansion range:20,000 psi*Be sure to include the properintensification factor ifthe program hasn't accountedfor one.

The above allowables representonly guides, not the maximums,but when exceeded one shoulddiscuss with the project Manager.

14.

15. Check equipment nozzle loads tosee if they meet. specified al-lowables. If no allowables areavailable, use the followingequivalent stress criteria forthermal expansion.Butt welded nozzle: not toexceed 12,000 psiFlanged nozzle: not to exceed6,000 psi

- 0-

2/2/79

'h


smutsCHECKING PROCEDURE FOR PIPING ANALYSIS (Cont'd)

Lower allowables can be used asexperience and judgement dic-tates; e.g., a pipe stress limitof 10K of yield stress is com-monly used for nozzle criteria.

16. Check for excessive thermal ex-pansion loads in both nozzlesand restraints that may becaused by lockup from opposingrestraints.

Ch k~8K ot c tl

3-/0-

Space is provided below for additionalcheck items that Project Manager wantsto specify.

2/2/79

rIt

Technical ReportTR-5828-l


B. SEISMIC INERTIA PORTION

(See Note 1 BelowChecked B 'Date Coment 0

2.

Check for title card information.Should contain the following:problem no. or system description,load case (deadweight, thermal 1,etc.), analyst's initials, date,run no., project no.

Geometry (Check coordinates atterminal ends and critical inter-mediate points such as branchconnections, changes of directionor pipe size, valves, restraints,etc.). Use of computer plot isadvisable.

3.

4.

6.

Note 1:


e

Check pipe ~roperties (O.D., Thk.,Wt., E 9 70 F, ~ 9 pipe tempera-.ture, etc.). Use material andsection property tables and pipeelement input data sections ofTMRSAP.

Check for pipe element connec-tivity.Check to ensure valves andother components which representa concentration of mass areproperly modeled; i.e., checkthat mass C.G. and orientationare correct. (Use nodal loadand mass tables.) If valvebody is modeled as an equiva-lent pipe element with dis-tributed weight, be sure thata concentrated weight is notalso specified and vise versa.Valve bonnet and/or yoke shouldbe modeled as a 'stiff elementunless information to the con-trary 'is specifically provided.

Items 2 to 7 not required if performed in Thermal and Deadweight Portion.9 /0 /7'

I

I

Technical ReportTR-5828-.,1


Checked 8 Date Comment 8

7.

8.

9.


Check that correct spectra used;envelope must be used when amultisupport system exists (i.e.,different floors of buildings or

- different equipment, etc.) Checkpoints to ensure good curve fit.Check to ensure correct dampingcurves are used and that peakshave been broadened by at least+10%.

Shock direction correct.Check to see that X, Y, Z shocksrun "separately with the correctdirection specified on the di-rection card. in each case.

10. Check that enough nodes are usedto predict the correct responseof the system.

Check to ensure that the analy-sis is performed to at least33 hertz.

6-g5

12.

13.

Check to see if all restraintsincluding snubbers are modeledin properly. (Use nodal pointcoordinate table and boundaryelement. table. )

Check to see if both earthquakes(1/2 SSE and SSE) are run. Anoption to this would be where amultiplier is specified for theSSE earthquake.

Check seismic stress. As a ruleof thumb, if it exceeds 5000 psifor any one-direction for the1/2 SSE earthquake, bring it tothe attention of the Analyst orProject Manager.

g-0- $

2/2/79

L



15. Check support (particularlysnubbers) loads. If low ( lessthan 1008) bt ing it to the at-

" tention of the Analyst or theProject Manager.

16. Check seismic displacement forexcessive values. As a rule ofthumb, if it exceeds 1.0 in. forany direction, bring it to the

. attention of the Analyst orProject Manager.

17. Check valve accelerationsagainst specified allowables.

Checked 8

'

Date Covalent f

g-/0-g5

2/2/79

Technical ReportT R-5828-1


C. STATIC S SM PAP ON

See Note e ow

Check for title card information.Should contain the following:problem no. or system description,

. load case (deadweight, thermal 1,etc.), analyst' initi'als, date,run no., project no.

Checked B Date Comment 0

2.

3.

Geometry (Check coordinates atterminal ends and critical inter-mediate points .such as branchconnections, changes of directionor pipe size, valves, restraints,etc.) Use of computer plot isadvisable.


Check pipe Broperties (0.0., Thk.,Mt., E 8 70 F, ~ 8 pipe tempera-ture, etc.). Use material andsection property tables and pipeelement input data sections ofTNRSAP..

6.

7.

'.

9

Check for pipe element connec-tivity.Check that all pipe fittingsare modeled properly.

Check to ensure all restt aintsincluding snubbers are modeledin correctly. (Use nodalpoint coordinate table andboundary element table.)

Have X, Y, Z shocks beenrun separately2

Has a deadweight card beeninput with the correctmultiplier.

8- o-as

Note 1: Items 2 to 6 not required. if performed in Thermal and Deadweight Portion.

2/2/79

Technical ReportTR-5828-1 'VV"

CHECKING PROCEDURE- FOR PIPING ANALYSIS (Cont'd)

10. Have all restraints (anchors,nozzles, rigids and snubbers)been displaced by the correctmagnitude + direction? (Checkinput in the boundary elementtable. )

11. Is'he phasing of anchor/support movements correct2Discuss phasing considerationswith Project Manager.

12. Check 'end effect stresses. 7fexceed 5000 psi per directionwith intensification factor,bring to attention of Analystand Project Manager.

Checked 8 Date

9 /0- gg

9 /0-8+

Comment f

2/2/79

r,


CHECKING PROCEOURE FOR PIPING ANALYSIS (Cont'd)

G. COMMENTS

rrz.e- ave/AK oH> PEDJEe7 .

acr LIGP

i~6 a f=lolO6 2.E

Technical ReportTR-5828-'1


(To be kept with Analysis Documents)

MODEL NO. ' ~~ 2

DRAWING ISOMETRIC NO.

OTHER REFERENCE

DRAWINGS NOS.

PROJECT NO.

ANALYST Qe= Are)~

Checked B

A. THERMAL AND DEADWEIGHT PORTION g~u/> /gI. Check for title card information.

Should contain the following:problem no. or system description,load case (deadweight, thermal 1,etc.), analyst's,initials, date,run no., project no.

2. Geometry (Check coordinates atterminal ends and critical inter-mediate points such as branchconnections, changes of directionor pipe size,'alves, restraints,etc.). Use of computer plot isadvi s ab 1 e.

3. Check coordinate system (Doesanalytical model agree withspecified plant or piping co-ordinate system.)

4. Check pipe ~roperties (O.D.; Thk.,Wt., E 9 70 F, ~ 9 pipe tempera-ture, etc.). Use material andsection property tables and pipeelement input data sections ofTMRSAP.

5. Check for pipe element connec-t ivity,

Date Comment 0

Az

0-/ 7-P

)„v'/2/79

Technical ReportTR-S828-l


Checked B Date Cement 0

6.

7.

8.

Check to ensure valves andother components which representa concentration of mass areproperly modeled; i.e., checkthat mass C.G. and orientationare correct. (Use nodal loadand mass tables.) If valvebody is modeled as an equiva-lent pipe element with dis-tributed weight, be sure thata concentrated weight is notalso specified and vise versa.Valve bonnet and/or yoke shouldbe modeled as a stiff elementunless information to the con-trary is specifically provided.



3-I t-8~

r- l7-g ~

9. Check that temper ature distri-bution (hT's at nodes) repre-sents the specified operatingmode. Use nodal coordinatetable. Check that all im-portant thermal modes havebeen considered.

10. Check thermal displacementsand directions at nozzles.Be sure direction and signagree with coordiante system.Use boundary element tableof. TMRSAP.

g= /

Check anchors and restraintsfor proper location and con-straint direction. Use nodalcoordinate table and boundaryelement table.Caution: Avoid putting re-straints at either end ofan end of an elbow element.

2/2/I79




12. For deadweight, check to ensurethat deadweight card with -1.0in y-direction is used. (Checkelement load case multipliertable for -1.0 beside y-directiongravity.)

13. For thermal expansion runs, checkto see if thermal card is usedand a 1.0 is printed besidethermal distortion in the elementload case multiplier -table.

Note: If pipe is thin-walledwith high internal pressure,there can be a significantchange in elbow flexibility.This should be considered byinputting internal pressurein the model.

14.

15.

Check stresses* against the fol-lowing allowables:Deadweight (normal operation):5,000 psiThermal expansion range:20,000 psi*Be sure to include the properintensification factor ifthe program hasn't accountedfor one.

The above allowables representonly guides', not the maximums,but when exceeded one shoulddiscuss with the project Manager.

Check equipment nozzle loads tosee if they meet specified al-lowables. If no allowables areavailable, use the followingequivale'nt stress criteria forthermal expansion.

Butt welded nozzle: not toexceed 12,000 psiFlanged nozzle: not to exceed6,000 psi

2/2/79

Technical ReportTR-,5828-1

CHECKING PROCEDURE FOR PIPING ANALYSIS {Cont'd)

Lower allowables can be used asexperience and judgement dic-tates; e.g., a pipe stress limitof 105 of yield stress is com-monly used for nozzle criteria.



Space is provided below for additionalcheck items that Project Manager wantsto specify.

2/2/79

Techni calTR-5828-1

Report



{See Note 1 Below)Checked B Date Ceanent f

2.

Check for title card information.Should contain the following:problem no. or system description,load case (deadweight, thermal l,etc.), analyst's initials, date,run .no., project no.

Geometry (Check coordinates atterminal ends and critical inter-mediate points such as branchconnections, changes of directionor pipe size, valves, restraints,etc.). Use of computer plot isadvi sable.

8-IB-B> 9g.

3.

4.


4

Check pipe ~roperties {0.0., Thk.,Wt., E 9 70 F, ~ 9 pipe tempera-.ture, etc.). Use material andsection property tables and pipeelement input data sections ofTMRSAP.

Q~P $ Pl~C I

q g.gp ~~W~ I

5. Check for pipe element connec-tivity. H<TPl

6.

Note 1:

Check to ensure valves andother components which represent 9-4-M <umbela concentration of mass areproperly modeled; i.e., checkthat mass C.G. and orientationare correct. (Use nodal loadand mass tables.) If valvebody is modeled as an equiva-lent pipe element with dis-tributed weight, be sure thata concentrated weight is notalso specified and vise versa.Valve bonnet and/or yoke shouldbe modeled as a stiff elementunless information to the con-trary is specifically provided.

Items 2 to 7 not required if performed in Thermal and Deadweight Portion.2/2/79




7.

8.

Check that all pipe fittingsare modeled proper ly.

Check .that correct spectra used;envelope must be used when amultisupport system exists (i.e.,different floors of buildings ordiffer ent equipment, etc. ) Checkpoints to ensure good curve fit.Check to ensure correct dampingcurves are used and that peakshave been broadened by at least+10K.

P .a

mrs /

g-(5-6~ P -6

9. Shock direction correct.Check to see that X, Y, Z shocksrun separately with the correctdirection specified on the di-rection card-in each case.

10.

12.

13.

Check that enough nodes are usedto predict the correct response , g 0of the system.

Check'to ensure that the analy-sis is performed to at least33 .hertz.

Check to see if all restraintsincluding snubbers are modeledin properly. (Use nodal pointcoordinate table and boundaryelement table.)


-4-e~

~~.-/8 -6)

3-z8 > p-ID

14.. Check seismic stress. As a ruleof thumb, if it exceeds 5000 psifor any one-direction for the1/2 SSE earthquake, bring it tothe attention of the Analyst orproject Manager.

2/2/79t


I


SERVlCES

15. Check support (particularlysnubbers) loads. If low (lessthan 1008) bring it to the at-

'ention of the Analyst or theProject Manager.

16. Check seismic displacement forexcessive values. As a rule of

. thumb, if it exceeds 1.0 in. forany direction, bring it to the

- attention of the Analyst orProject Manager.


Checked 8

R.c>

Date Cogent 8

2/2/79

TechnicalTR-5828-1

Report

CH»CI'ING PROCLDURE FOR PIPING ANALYSIS (Cont'd)

C. STATIC SE SM Pnn nMSee Note I Below

Ch eked B Date Comnent 0

2.

3.

4,

Check for title card information.Should contain the following:problem no. or system description,load case (deadweight, thermal 1,etc.), analyst's initials, date,run no., proJect no.

Geometry (Check coordinates atterminal ends and critical inter-mediate points such as branchconnections, changes of directionor pipe size, valves, restraints,etc.) Use of computer plot isadvisable.


Check pipe Hroperties (O.D., Thk.,Mt., E 9 70 F, ~ 9 pipe tempera-ture, etc.). Use material andsection property tables and pipeelement input data sections of

'YiRSAP.

3- ze-6>

p pc(

5. Check for pipe element" connec-tivity. P o ~Q-Q $ pose /

6.

7.


Check to ensure all restraintsincluding snubbers are modeledin correctly. (Use nodalpoint coord nate table andboundary element table.)

3- zp-85

Po7g /

8.

9.

Have X, Y, Z shocks beenrun separately2

Has a deadweight card beeninput with the correctmultiplier.

>-Z8-83 t.

9-b-85

!tems 2 to 6 not required if performed in Thermal an" Deadweight For:io~

Technical ReportTR"5828-1

seIVICEB


Checked 8 Date Comment f10. Have all restraints (anchors,

nozzles, rigids and snubbers)been displaced by the correctmagnitude + direction? (Checkinput in the boundary elementtable. )

ll. Is'he phasin'g of anchor/support movements correct?Discuss phasing considerationswith Project Manager.

12. Check 'end effect stresses. Ifexceed 5000 psi per directionwith intensification factor,bring to attention of Analystand Project Manager.

PA-

2/2/79

TechnicalTR-5828-1

Report

SERNCES

CHECKING PROCEDURE FOR PIPING ANALYSIS (Cont'd}

E. TMRPASS PORTION Checked B Date Comment 0

2.

3.

5.

6.

7.

Check title and drawing infor-mation. Is informationcentered in title block? ..Isproject number corrects

Check that all necessary loadcases have been input.

Check'o see that correctmultiplier for DBE is used.See Project Manager forcorrect multiplier.

Check that the combined seis-mic option is appropriate tothe project. See ProjectManager for correct combina-tion of directional responses.

Does coordinate system reportedagree with hanger and restraintlocations drawing7

Has correct pressure 'stressoption, dynamic load option,been usedl Check with ProjectManage for correct equation.

Check member data for correct OD,thickness, and radius. Check thatcorrect pipe properties are usedin analysis of branch connec-tions.

@'gg V

8. Check that all.important datapoints are analyzed (as a mini-mum, elbows, restraint locations,tees, reducers, S.M. fittings,and any other possible highstress points). The order ofinput has to be in the sameorder as punch output.

1

I2/2/79

TechnicalTR-5828-1

Repor tE..

NGSERNCESCHECKING PROCEDURE FOR PIPING ANALYSIS (Cont'd)

Checked B Date Convent 0

9.

10.

Check that correct pipe class,design and peak pressure, andallowable stresses are correctfor each data point.

Check that the correct designa-tion of runs and branches areused. For each branch connec-tion the data point should beanalyzed 3 times. Once asbranch and twice as runs.

12.

13.

Check that the punch outputused is from final checkedTMRSAP runs. Has the punchedoutput been input in thecorrect order (i.e., D.M.,thermal, seismic, end effects,and dynamic)2

Check thru each punch outputlisting for any warning mes-sages.

Check each data point forcorrect intensification fac-tor and stress indices, ifapplicable. Use stress in-tensification factors andstress indices table.

15

16.

Scan stress summary. Dostresses look reasonable?

As a minimum check last pipedata point stress calcula-tions for Equations 8, 9,9 OBE, and 10 of NC-3652 andEquation 9 of NB-3652.

Have all restraints beenanalyzed for the correct di-rection and type?

Oo design, loads and thermaland seismic movements lookreasonable's a minimum,check last restraint pointfor correct plus and minusdesign load and movement.

2/2/79



Checked 8

17. Have all anchor locationsbeen analyzed for 'design loadsand moments'heck last anchorpoint design loads.

SERVICES

Date Comment f

3 49~

2/2/79



G. COMMENTS

Ssi ', 0 Q 5%> 4 ~ de@ c.u f'~

c+5E A/Lc./

CC

/ rl/

Technical ReportTR-5828-1 ENGN~ERNQ SE%'CM


{To be kept with Analysis Documents)

MODEL NO. ' DM

DRAMING !SONETRIC NO, l= —c9

OTHER REFERENCE .

DRAWINGS NOS.

sY<~l 8l,oaa /i~) pps$

PROJECT NO. gANALYST . C~

A. THERMAL AND DEADMEIGHT PORTION

Checked B Date Cogent 0

1. Check for title card information.Should contain the following:problem no. or system description,load case (deadweight, thermal I,etc.), analyst's initials, date,run no., project no.

2. Geometry (Check coordinates atterminal ends and critical inter-mediate points such as branchconnections, changes of directionor pipe size, valves, restraints,etc.). Use of computer plot isadvisable.

3. Check coordinate system (Doesanalytical model agree withspecified plant or piping co-ordinate system.)

4. Check pipe ~roperties (0.0., Thk.,Mt., E 8 70 F, ~ 9 pipe tempera-ture, etc.). Use material. andsection property tables and pipeelement input data sections ofTlQSAP.

5. Check for pipe element connec-tivity.

WifB g-7+ -z Q o 3

A M

2/2/79

Techni calTR-5828-1

Report

NQ SERVICESCHECKING PROCEDURE FOR PIPING ANALYSIS (Cont'd)

Checked B Date Coment f6.

7.

8.

9.

10.

Check to ensure valves andother components which representa concentration of mass areproperly modeled; i.e., checkthat mass C.G. and orientationare correct. (Use nodal loadand mass tables.) If valvebody is modeled as an equiva-lent pipe element with dis-tributed weight, be sure that

,a concentrated weight is notalso specified and vise versa.Yalve bonnet and/or yoke shouldbe modeled as a stiff elementunless information to the con-trary is specifically provided.



Check that temperature distri-bution (bT's at nodes) repre-sents the specified operatingmode. Use nodal coordinatetable. Check that all im-portant thermal modes havebeen considered.

Check thermal displacementsand directions't nozzles.

, Be sure direction and signagree with coordiante system.Use boundar y element tableof. THRSAP.

Check anchors and restraintsfor proper location and con-straint direction. Use nodalcoordinate .table and boundaryelement table.Caution: Avoid putting re-straints at either end ofan end of an elbow element.

) -(gg~

W(c3 g ~/g

~ze-8~ p- li8-Xo&3 c:>9

2/2/79

TechnicalTR-5828-1

Report


Checked B Date Cogent f12. For deadweight, check to ensure

that deadweight card with -1.0in y-direction is used. (Checkelement load case multipliertable for -1.0 beside y-directiongravity.)

13. For thermal expansion runs, checkto see if thermal card is usedand a 1.0 is,printed besidethermal distortion in the elementload case multiplier table.Note: If pipe is thin-walledwith high internal pressure,there can be a significantchange in elbow flexibility.This should be considered byinputting internal pressurein the model.

14.

15.

Check stresses* against the fol-lowing allowables:Deadweight (normal operation):5,000 psiThermal expansion range:20,000 psi*Be sure to include the properintensification factor ifthe program hasn't accountedfor one.

The above allowables representonly guides', not 'the maximums,but when exceeded one shoulddiscuss with the project Manager.

Check equipment nozzle loads tosee if they meet specified al-lowables. If no allowables areavailable, use the followingequivalent stress criteria forthermal expansion.Butt welded nozzle: not toexceed 12,000 psiFlanged nozzle: not to exceed6,000 psi

I


~TEA~JPV NcENQNP~INQ SERIES

CHECKING PROCEDURE FOR PIPING ANALYSIS {Cont'd)

Lower allowables can be used asexperience and judgement dic-tates; e.g., a pipe stress'imitof 10 of yield stress is com-monly used for nozzle criteria.


Checked B Date Comment f

Space is provided'below for additionalcheck items that Project Manager wantsto specify.

2/'2/'79

TechnicalTR-'5828-1

Report .%TELE'<RNCMCHECKING PROCEDURE FOR PIPING ANALYSIS (Cont'd)


(See Note 1 Below)Checked B Date Conment f

2.

Check for title card information.Should contain the following:problem no. or system description,load case (deadweight, thermal 1,etc.), analyst's initials, date,run no., project no.

Geometry (Check coordinates atterminal ends and critical inter-mediate points such as branchconnections, changes of directionor pipe size, valves, restraints,etc.). Use of computer plot isadvi sable.

. 3-z8-8> -/

nravP I

3.

4.

5.

6.

Note t:


Check pipe Icroperties (O.D., Thk.,Mt., E 9 70 F, ~ 9 pipe tempera-ture, etc.). Use material andsection property tables and pipeelement input data sections ofTMRSAP.

Check for pipe element connec-t 1 vity

Check to ensure valves andother components which representa concentration of mass areproperly modeled; i.e., checkthat mass C.G. and orientationare correct. (Use nodal loadand mass tables.) If valvebody, is modeled as an equiva-

'entpipe element with dis-tributed weight, be sure thata concentrated weight is notalso specified and vise versa.Valve bonnet and/or yoke shouldbe modeled as a stiff elementunless information to the con-trary is specifically provided.

Items 2 to 7 not required if perform

P,D q-g-gy pans I

p 0 g-g -gp Iwvp I

rau7'C /

poTB I

ed in Thermal an." Oeadweigh. Portion.2/2/79

TechnicalTR-5828-1

Report

S

,. CHECKING PROCEDURE FOR PIPING ANALYSIS {Cont'd)

Checked 8 Date Coment f7.

8.

9.


Check that correct spectra used;envelope must be used when amultisupport system exists {i.e.,different floors of buildings ordifferent equipment, etc.) Checkpoints to ensure good curve fit.Check to ensure correct dampingcurves are used and that peakshave been broadened by at least+10%.

Shock direction correct.Check to see that X, Y, Z shocksrun separately with the correctdirection specified on the di-rection card in each case.

oPC i

10.

12.

13.

14.

Check that enough nodes are usedto predict the correct responseof the system.

Check to ensure that the analy-sis is performed to at least33 hertz.

Check to see if all restraintsincluding snubbers are modeledin properly. (Use nodal pointcoordinate table and boundaryelement. table. )


Check seismic stress. As a ruleof thumb, if it exceeds 5000 psifor any one-direction for the1/2 SSE earthquake, bring it tothe attention of the Analyst orProject Manager.

3 Zg g) ll

2/2/79


CHECVING PROCEDURE FOR PIPING ANALYSIS (Cont'd)

MSERVICES

15. Check support (particularlysnubbers) loads. If low (lessthan 100') bring it to the at-

'ention of the Analyst or theProject Manager.

16. Check seismic displacement forexcessive values. As a rule ofthumb, if it exceeds 1.0 in. forany direction, bring it to theattention of the Analyst orProject Manager.


Checked 8 Date Covalent 8

yugo ~ps V

y-ZG-

Te chni ca 1

TR-5828-1Report 'VC"TERM'NE

NQ SBVAC~M

CHiCl'ING PROC""DURE FOR PIPING ANALYSIS (Cont'd)

C. STATIC SE ~M Pnu nMSee Note 1 Be ow

Ch eked 8 Date Comnent 0

. 1. Check for title card information.Should contain the following:problem no. or system description,load case. (deadweight, thermal 1,etc.), analyst's initials, date,run no., project no.

2.

3.

Geometry (Check coordinates atterminal ends and critical inter-mediate points such as branchconnections, changes of directionor pipe size, valves, restraints,etc.) Use of computer plot isadvisable.

Check coordinate system (Doesanalytical model agree withspecifjed plant or piping co-ordinate system.)

Check pipe IIroperties (0.0., Thk.,Mt., E 9 70 F, " 9 pipe tempera-ture, etc.). Use material andsection property tables and pip'eelement input data sections ofTYiRSAP.

p & Q Q-g~ ~o1C I

o~1

5. Check for pipe element connec-tivity. pr~re l

6.

7.

9

Check that al 1 pipe fittingsare modeled properly.

Check to ensure all restraintsincluding snubbers are modeledin correctly. (Use nodalpoint coordinate table andbo'undary element table.)

8ave X, Y, Z shocks beenrun separately2

8as a deadweight card beeninput'with the correctmultiplier.

~ora/

!:e.".s 'o 6 not required if performed in The".mal an" Deadweight Por-.io~.

v,i v > p„

't

II

'I

l

l,


OV TELEDYNEEk " 'G S&VCES

CHECKING PROCEOURE FOR PIPING ANALYSIS (Cont'd)

10. Have all restraints (anchors,nozzles, rigids and snubbers)been displaced by the correctmagnitude + direction? (Checkinput in the boundary'lementtable. )

Checked 8 Oate

g-g~~

Comment f

11. Is'he phasing of anchor/support movements corr ect?Oi scuss phasing considerationswith Project Manager.

12. Check 'end effect stresses. Ifexceed 5000 psi per directionwith intensification factor,bring to attention of Analyst'and Project Manager.

0 9-Zg-g~

2/2/?9



E. TMRPASS PORTION Checked B Date Convent f

2.

3.

5.

6.

7.

Check title and drawing infor-mation. Is informationcentered in title blockf Isproject number corrects

Check that all necessary loadcases have been input.

Check to see that correctmultiplier for DBE is used.'See Project Manager forcorrect multiplier.

Check that the combined seis-mic option is appropriate tothe project. See ProjectManager for correct combina-tion of directional responses.

Does coordinate system reportedagree with hanger and restraintlocations drawin97

Has correct pressure stressoption, dynamic load option,been use47 Check with ProjectManager for correct equation.

Check member data for correct OD,thickness, and radius. Check thatcorrect pipe properties ar e usedin analysis of branch connec-

tions'~

iso 9-ga-

-M-8

~ ZQ-85

8. Check that all important datapoints are analyzed (as a mini-mum, elbows, restraint locations,tees, reducers, S.M. fittings,and any other possible highstress points). The order ofinput has to be in the sameorder as punch output,

'3-Zs-g 5

2/2/79

PN IsineNaN=-WNQsERNcES

Date Comment f


CHECKING PROCEDURE FOR PIPING ANALYSIS (Cont'd)~Ch kdB

9. Check that correct pipe class,design and peak pressure, andallowable stresses are correctfor each data point.

Check that the correct designa-tion,of runs and branches areused. For each branch connec-tion the data point should beanalyzed 3 times. Once asbranch and twice as runs.

gu g z,s-g)

v'5-Z

)-8 >

12.

13.

14.

15

'6.

Check that the punch outputused is from final checkedTMRSAP runs. Has the punchedoutput been input in thecorrect order (i.e., D.M.,thermal, seismic, end effects,and dynamic)2

Check thru each punch outputlisting for any warning mes-sages.

Check each data point forcorrect intensification fac-tor and stress indices, ifapplicable. Use stress in-tensification factors andstress indices table.

Scan stress summary. Dostresses look reasonable?

As a minimum check last pipedata point stress calcula-tions for Equations 8, 9,9 DBE, and 10 of NC-3652 andEquation 9 of NB-3652.

Have all restraints beenanalyzed for the correct di-rection and type?

Do design loads and thermaland seismic movements lookreasonable2 As a minimum,check last restraint pointfor correct plus and minusdesign load and movement.

2/2/79

k



p% t ~~l i~

17. Have all anchor locationsbeen analyzed for design loadsand moments7 Check last anchorpoint design loads.

Checked B Date Co@vent f

2/2/79

l

tI'

I

Techni cal ReportTR-5828-1


"'i>Q S&VCW

G. COMMENTS

iS /IT /'A

c I < 8 Fo (pw'i(D57g coo

w c c. 8 c EC uo


~> TELEDYNEENQINEERINQ SERVICES

APPENDIX I

COMPUTER STRESS RESULTS

BOOK 2

'0".

ip

? ~ ~

I

Date post:	21-Nov-2020
Category:	Documents
Upload:	others
View:	0 times
Download:	0 times