Forwards "WPPSS 2 Purge & Vent Valves Seismic ...

7)REGULATORY 1M)ARMATION DISTRIBUTION SY Q i (RIDS)

W)

ACCESSION NBR: 8307120309 DOC. DATE: 83/06/22 NOTARIZED: NO DOCKET

FACIL:50-397 WPPSS Nuclear Proiect. Unit 2P Washington Public Powe 05000397AUTH.NAME AUTHOR AFFILIATION,

BOUCHEY.G.D. Washinaton Public Power Supply SvstemRECIP.NAME„RECIPIENT AFFILIATION

SCHWENCERPA Licensino Branch 2 (

SUBJECT: Forward ds "WPPSS 2 Purae L Vent Valves Seismic 8 Hydr odvnamicAna'Ivsiss" per SER Outstanding Issue 26

DISTRIBUTION CODE: BOOIS COPIES RECEIVED:LTR i ENCL 5 SIZE:TITLE: Licensina Submittal: PSAR/FSAR Amdts L Related Correspondence

NOTES: ~( 0'@ 5/G4I" ISac %Q~RECIPIENT

ID CODE/NAMENRR/DL/ADLNRR LB2 LA

INTERNAL: ELD/HDS2IE/DEPER/EPB 36IE/DEQA/QAB 21NRR/DF/CEB 11NRR/DE/EQB 13NRR/DE/MEB 18NRR/DE/SAB 20NRR/DHFS/HFEBOONRR/DHFS/PSRBNRR/DSI/AE8 26NRR/DSI/CPB 10NRR/DS I/ICSB 16NRR/DS I/PSB 19NRR/DSI/RSB 23RGN5

EXTERNAL: ACRS 01DMB/DSS (AMDTS)LPDR 03NSIC 05

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TOTAL NUMBER OF COPIES REQUIRED: LTTR 53 ENCL 06

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Washington Public Power Supply SystemP.O. Box968 3000 George Washington Way Richland, Washington 99352 (509) 372-5000

June 22, 1983G02-83-550

Director of Nuclear Reactor RegulationAttention: Mr. A. Schwencer, ChiefLicensing Branch No. 2Division of LicensingU. S. Nuclear Regulatory CommissionWashington, D.C. 20555

Dear Mr. Schwencer:

Subject: NUCLEAR PROJECT 2QUALIFICATION OF WNP-2 CONTAINMENTVENT AND PURGE VALVES

References: 1) Letter, A. Schwencer (NRC) to R. L. Ferguson, (SupplySystem), "Request for Additional Information""; datedSeptember 16, 1982, Docket No. 50-397

2) NUREG-0892, WNP-2 SER, Outstanding Issue No. 26,"Operability of Purge Valves"

3) Letter, G. D. Bouchey (Supply System). to A. Schwencer(NRC), G02-83-170, "Nuclear Project No. 2, gualifica-tion of WNP-2 Containment Vent and Purge Valves",dated February 24, 1983

Reference 3) provided partial response to the Purge and Vent valveoperability concerns cited in Reference 1) and 2). This letter transmitsstress analysis work to address the remaining open issues.

The enclosed reports provide the qualification stress analyses for thesubject valves and their operators. Each has a positive margin of safetywhen the stress caused by a safe shutdown earthquake is combined withsafety relief valve operation along with chugging or annulus pressuriza-tion. Acceptance criteria are from Section III of the ASME Boiler andPressure Vessel Code or the AISC Steel Construction Manual, whichever isapplicable.

These margins of safety were found only with the modifications describedin the attached reports. These modifications will be performed prior tooperation of WNP-2.

8307i20309 830622PDR ADOCX OSOOOS97E,;,, ', PDR

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IL@STAN>~ ~

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lr

Mr. A. SchwencerPage 2

June 22, 1983

With the modifications in place, these valves will remain functionalthrough forty years of postulated hydrodynamic events, five operatingbasis earthquakes, and one,.safe shutdown earthquake.

phdG. D. Bouchey, nagerNuclear Safety and Regulatory Programs

RWH/sms

Attachments

cc: Mr. R. Auluck - NRCMr. W. S. Chin - BPAMr. A. Toth - NRC Site

I.I

~ ~

Washington Public Power Supply Sys'.emP.O. Box 968 3000 George Washington Way Richland, Washington 99352 (609) 373-6000

The attached reports are the structural analysis of the purge and ventvalves and operators installed at NNP-2. The loads used in th. anal'"-'iare the valve operating loads combined with the dynamic '~oads whichwould result from seismic and hydrodynamic events as determined by thepiping analyses for the plant.

There are three reports attached. They separately address:

1) The 24-inch butterfly valves manufactured by BIF (identified asQID 361106),

2) The 30-inch butterfly valves manufactured by B:F (identified asQID 361104), and

3) The air operators manufactured by Miller Fluid Pcwer and suppl'.edby BIF as a part of the'alve assembly (identified as QID 018C01').

These reports have been prepared by Cygna Energy Services for ti e St ppliSystem's Equipment Qualification Group and are in heir compl-te formin the Equipment Qualification files. However, in the '.ntei"est ofconserving space in the transmittal to the U.S. NRC, pages wh'.ch areduplicated in the reports have been removed from all but one of thereports. Also, documents which have previously beett submitted to ".h=

. U.S. NRC are not attached as stated in the report.'

WASHINGTON PUBLIC POPOVER SUPPLY SYSTEM

SUPPI.IElh TII,A)IShllTTALFORhl(AREA WITHIN HEAVYBORDER To BE COMPLETED BY SUPPLIER)

B

To THK ATTENTloNoF: Dennis Arms tron3 p p 0 G gOGNIZAQTg A HA PCEg /gU Y

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PAGE OF ~1

NEW P RKNUBhjlTTAL

1200 Jadwin Suite R h nd W

THK FOI LOWING PUBLICATIONS/DRAWINGSARE SUBMITTED FORt

@APPROVAL Q REVIEW Q INFORMATION DISTRIBUTION

NO. OF PRINTS DF EACH HD.DFREFRDDUBIBEES DF ~EH5UBMITTED BY: Fawaz Khanachet

Assistant Pro ec~ana

i'EQUESTED DATEOF RKTURNI

P.O. NOc

WORK ORDER NOI

SPEC. NOz

SUBVKNOOR: 0NT./P.O. NO.: SPEC. SECT. NOi

ITEMNO.

PUBLICATIONORDRAWING NO.

REV.NO. PUBLICATIONOR DRAWING TITLEri dna e ua , R t. or

ID 3 0

MANUFACTURERWPPSS

ACTION

T- RB C na T-644RB

COMMENTS: IUSE ADDITIONALSHEETB IF REQUIRED) TO BE REVIEWED BY

ECEIVCD BY: IPURCHASING ONLY) TRANSMITTED BY: (PURCHASING ONI Y)

NAMP ROVED BY:

OAITLK AT

ACTION LKGENOaA ~ APPROVED FOR PUBLICATION

AN ~ APPROVED AS NOTED FOR FABRICATIONWP 770 R I

~ INFORMATIONONLYNA ~ NOT APPROVED

IIIIIIIIIIIIIIIIIIIIIIIIIIIIII

FinalQualityicationReport

I

PROJeCT'.. . Equipment Seismic/Hydrodynamic RequalificationJOB gNO„:",„82P 4 4

———CAXm-NO' OT.p1.F

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CLIENT- Washington Public Power Supply System

!>+ QTD"NO=;, ''361'10fI~g

'I llr TITLE,'. '. Equipment Seismic and Hydrodynamic Requalification of...24" Cylinder Operated Butterfly Valves for:

CSP-V-3,4,5,6, and 9

CEP-V-3A, and 4A

II ~

I (.-II

PREPARED BY:

fn qREVIE!KD BY: E(..~!D ~ . n . lr,

APPROVED BY:

DATE

Lo des nandez 6 9 83DATE

DATE

yd~w/ s+~ gee'«~

g ld. JiQ+i84AI

REVISION: 3

~/i%~

REVISION STATUS REPORT

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DATE

PRE'D BY

REV'D BY

APPROVEDBY DESCRY'PTiOH

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REVISION 3

WASHINGTON PUBLIC POWER SUPPLY SYSTEM

REQ UALIFICATIONCERTIFICATE

WNP- 2 gzDI 361106

coMPDNKNTNot CSP V 3g CSP V 4 g CSP V 5g CSP V 6g CSP V 9g CEP V 3A 6 CEP V 4

24" Cylinder Operated Butterfly Valves

MANUPACTURKRtBIF A-206765

MODKI NOI

EQUIPMENT CLASSIPICATIONs Qg ACTIVE Q PASSIVE

SK15MIC QUALIPICATIONREPORT REPKRKNCKI

C ana Re ort Ot.01/F OID 361106"24" C linder-Ooerated Butterfl Valve"

Reauired action: 1) Remove A-307 Ear Bolts and replace with A-325.

2} Reinforce va'lve ear grou with 4" shear platesto aualifv air operators for reauired fatiauecvcles.

THK ABOVESKISMIC ANO

THK CURRENT NRC SKI5MICAND

QUALIPICATIONREPORTS HAVE BEEN RKKVALUATKDIN ACCORDANCKWITH

CRITERIA'

~ IKEK5TANOAROS 244 (1575)

2 USNRC RKOULATORYCUIOKS 1.$ 2, 'I,144

2» 5TANOARO REVIEW PLANS 2&Pe 2»14eEN

~WSKkggW

THKABOVE COMPONENT HAS BEEN P'OUNO ACCEPTABLE POR PKRPORMINQ IT5 INTKNOKOSAI ETY RKLATKDPUNCTION

WHEN SULIECTKD TO THE PLANT SPKCIPIC VIBRATORY

r'1 ~

LOAO5.

rRKPARED BV Plp>v 0 r»,',/c /3'' Fr»', =< >/i.a~

RKVIEWKDBY+.'~rd~ i"'< rr~z «» I

APPROVED BY

9$ $»12574

OATK~

2.0 SQRT FORM(S) AND REFERENCES .

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WASHINGTOt4 PUBI IC POWER SUPPLY SYSTEM

Qualification Summary of EquipmentQIDN 361106

Ref. No.LANT NAME'P-2 TYPE

I ~ NSSS, GE BEE rn GE

coMPGNENT NAME, 24" C 1.0 er. Butterfly ValvecoMPoNENT NO.CSP-V- 4 9CEP-V-3A ET 4A

I ~ SCOPE: NSSS Q BOP

MOOEL NU4BER. A-206765

~. VENOOR: B~F

OUANTI TY:

4 ~ IF THE COMPONENT IS A CABINET OR PANEL, NAME ANO MOOEL NO. OF THE OEVICES INCLUOEO:

N/A

PHYs IOAL oEscRIPTIoNI > APPEARANcE Butter f1 Valve with 8" C 1 0 erato

o. oIMENSIoNS: 24" nominal diameters

c WE I GHT: 847N - Valve Ass; 6764 — 0 erator & bracket

6 LOCATION: BU I LO I NG:

ELFVATION Maximum elevation: 495 'CSP-V-3A & 4A)

T, Fl ELO MOUNTING OONOITIOHS: Q BOLT (NO SIZE )

Q MELO (LENGTH

sYsTEM IN wHIcH LccATEo. Containment Suppl Pur e S stems

FUNcTI oNAL oEscR I PT I oN Primary Containment iso 1ation, orevent ionof the release of radioactive material to the environment.

c. I S THE EOUIFMENT REOUIREO FOR: HOT STANOBY COLO SHUTOCMN

P] BOTH

9 PERTINENT REFERENCE OESIGN SPECIFICATION: WPP

NEITHER

ec. 2808-

I I I. IS EOUIRIENT AVAILABLEFOR INSPECTION IN THE PLANT: YES NO

PAGE I OF 5

REVISION,Q 2.2

Qualification Summary of Equipment (Continued)QID-":. 361106

C(NBI NATION OF TEST & ANALYSIS

l

IV l EQUIPMENT QUALIFICATION METHOD:I

TEST QX ANALYSIS

QUALIF(cATIQN REpcRT ~ 24" c 1inder-ooerated Butter f1 va lve*

(NQ ~ TITLE 6 DATE) OT 0 1 . F Revision 3, June, 1 98 3

CCMPANY TIIAT PREPARED REPCRT: e

cQMPANY THAT REYIEwFQ REPORT: washin ton Public Power su olv svstems*Plus original valve analysis

V, III BRAT ION I NPUT:~ I a

~l. LOADS CONSIOEREO: a. SEISMIC ONLYI'a

Q HYCRQOYNAMIC ONLY

c. Q CCMBINATON OF (a) ANO (b)CM ) Cf'~l'2

MET)K)O OF C(MBINING RRS: Q ABSOLUTE S(H Q SRSS OTHER (SPECIFY)

I

REQUIRED RESPONSE SPECTRA (ATTACH THE GRAPHS):I

<4 ~ DAMPING CORRESPONDING. TO RSS: CBE Q SSE

Ref. No.

I ~I

I 15

3,4

I 5 REQUIRED ACCELERAT ION IN EACH DIRECTION: Q ZPA Q OTHER (SPECIFY) )i/~h 15

QBE sos - Attached F/B . V ~

Attachedl J, ~ t6. WERE FATIGUE EFFECTS CR OTHER VIBRATION LOADS CONS IDEREOT

Q YES NO '

TF YES; DESCRIBE'OADS CQNSIOEREO ANO HOW THEY. WERE TREATED IN OVERALL QUALIFICATION FRO(BAM:I

d

w tures a vzed we e not

art of the ressure boundar

'- NOTE:, IF MORE THAN ONE REPORT, COMPLETE I TEMS IV TI4(OUGH Yl I FOR EACH REPORT

PAGE 2 CF S

2.3

Qualification Summary of Equipment (Continued)QlDg 361106

ROI. No.Vl~ IF QUALIFICATION BY TEST THEN COMPLETE»:

1. SINGLE FREQUENCY Q MULTI-FREQUENCY Q RANOO4iaaf ~ ~ 5

2+ Q SINGLE AXIS MULTI-AXI S SINE BEAT

~ ' ill"

3 NO, OF QUALIF ICATION TESTS: OBE SSE OTHER (SPECIFY)i ~ ~

4. FREQUENCY RANGc:

5, NATlRAL FREQUENCIES IN EACH DIRECTION (SIDE/SIDE, FRONT/BACK, VERTICAL):

S/S ~ F/B

6 METHOD OF DETERMI NING NAT(RAL FREQUENC I ES:

LAB TEST IN SITU TEST ANALYSIS

7. TRS .ENVELOPING RRS USING MULTI-FREQUENCY TEST: Q YES (ATTACH TRS 4 RRS GRAPHS) Q NO

v~ ~ =~

8, INPUT g-LEVEL TEST: CBE S/S ~

SSE S/S i9, LABORATORY MOUNTI NG:

F/8 a

F/8 s"»+i I i1F (

BOLT (NO. a ----0 FUNCT I 0 OPE L TY ER EO: ES NO Q

) C3

NOT APPLICABLE

I I ~ TEST REULTS INCLUDING MODIFICATIONS MADE:

12. OTHER TEST PERFORMED (SUCH AS AGING OR FRAGILITY TEST, INCLUDING RESULTS):

NOTE IF QUAL IF ICATION BY A CCMB I NTATI ON OF TEST ANO ANALYSI 5 i ALSO COI4 LETE I TEM VI"I ~

PAGE 3 OF 5

rQNAWAVWWI»»»»»»»»P A AA REVlS10N '3i 2.4

E, ~

~F»»»»»~ ~ ~S w» 'w

'Qualification Summary of Equipment (Continued)QID~ 361106

Vl I. IF QUAL IF ICATION BY ANALYSI S, THEN CO4PLETE:

Ref. No

I ~ METHOO OF ANALYSIS:

STATIC ANALYSIS

Q 0YNAMIC ANALYSIS

2 NATLRAL FREQUENCIES

s/s - 10.81 Hz

MOOEL TYPE:

Q5O . Qa)4.Q COMPUTER COOES:

iC EQUI VALENT STATIC ANALYSI S

T INES I STCRY Q RESPONSE SPECTRIH

IN EACH OIRECTION (SIOE/SIOE, FRONT/BACK, VERTICAL):

26.1 Hz v ) 100

Q IO Q FINITE ELEMENT Q BEAM Q CLOSEO FCRM SOLUTION

PREQUEL Y RANGE ANO NO OF MODES CONSIOEREO

OTHERABSOOLTE SIR [)(j SRSS Q (SFECIFY)

GOVERN I NG LOAO

OR RESPONSE

CCIBI RATICRPLPB-BR&&1

STRESS

ALLO6ABLE

26880 (PS )

6600a (PS )

TOTAL

STRESS

19538

SE I SMI C

STIIESS

15743LCCATI OR

CPP-T)-3&4A, IOENTIFICATION

,o,Valvel EarsEar 'Bolts CSP-V-3&4 pipe-normal 15777 18382

3301958884

86400 (PPI) I

+/66000 (PPZ)i

Drive Rod CSP-V-4 rod-normal 8543

pipe-normal.57543'hr- Bolts CSP-V-6

HANO CAI.CULATIONS

5, METHOO OF CCHBINING DYNAMIC RESPONSES:R' ~

6, OAI»IIIO: CBE SSE~ F

7» SUPPORT CONS IOERATIONS IN THE MOOEL:

8 CR I T ICAL STRlJCTtRAL ELEMENTS 6

BE MAX» CRITICAL

I, OEFLECTION

<0. 01"LCCATI ON

Valve disk radialdeflection

MAxIMMY ALLQIABLE

OEFLECTION TO ASSURE

FUNCTIONAL OPERABI L I TY

approx 1/8" radialclearance

VT»IFA»»»»»AA»~'»» R AA WW

*Final.response accelerations rom pining analysisBre=uBed.

I

~A»»AA»l'&w»A»AYYFFA»»A»L»»YAAF„AHA»»»A»AA

~ F PT (S 4

PAGE 4 OF 5

Revision 2 2.5

Qualification Summary of Equipment (Continued)gQID 361106

Vill. REFERENCES

' * \

D-207110-P., D-207110-G,(Valve Data Sheets)

A-206767,18", 24" & 30" Butterfly Valve - General

C-26096,"Certified Dimension for Model A-83-B Cylinder"

> ~

'l~ ~

2. 4'PPSS Unit 2 Drawin s:

CSP-807-81 '8CSP-809-1.2

CEP-625-3.4

CEP-625-1.2

D.220-0310

Containment Purge Air Supply» ~ >" pr

Suppression Pool Vacuum Breaker

From Reactor Nozzle X-67 to SGT-Fu-lA,~ (>>

From Reactor Nozzle X-67 to SGT-Fu-lA,>>> >g

Support and Erection Isometric-IR64(Johnson Controls)

~ >

1B'B,

l

3. BIF Report TR-27234 and TR-27235, "Dynamic Torque Calculation ofButterfly Valve; Sizes 24 and 30 inch", dated November 1P, 1982.

4. Report //TR-74-7 by McPherson Assoc., Inc., "Design 6 SeismicAnalysis 24" Cylinder operated Butterfly Valve." (Rev. 1) 1/5/76.

5. WPPSS letter to Cygna Energy Services, GE-02-RVH-018',-12/47/82.

REFERENCES CONTINUED ON PAGE 2.6

Completed By

Rovlowod By

gP l>

~t<a'A~>t ~p~.,~>.../~ ~. +b'g'/>>$

g$~ j($p '. ~~ g glcj'/fgPago 5 of 5

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CalculationSheet

. /PcoIect Prepared By: "II .I Date

Washin ton Public Power Su l S stem L.C.~ Fernandez 5/27/83I

Subtect Checked By.Equipment Seismic/Hydrodynamic Requal.

Date+ .-~/=~

CSP & CEP 82044 OT.01.F

QID 361106Rev. No.

2Sheet No.

2.6

SECTION 4.4. REFERENCES (CONTINUED):

~ ~~i 4 - .. ~j-/z: rQ.pr.c~~~~J c/g// c

6. Cygna Energy Services Communications Report, R. Ricappito,BIF Valve, and J. Rakowski, CES, "BIF'alve Dimensions",2/11/83.

7. Cygna Energy Services, Project Manual Design Criteria,DC-1, Rev. 1, November, 1982.

8. Cygna Energy Services, Equipment Qualification WalkdownVerification Forms, Revision 1, dated 1/5/83.

9. WPPSS, %3P-2, Safety Related Mechanical Equipment ListSummary Sheets, dated 2/10/83.

10. "AISC Manual of Steel Construction", American Instituteof Steel Construction, 8th Edition, 1980.

ll. Preliminary Transfer of Final Burns & Roe Piping Loadsfor CSP-V-1,2,3,4,5,6 and CEP-V-3A&4A, received 4/13/83.

12. Cygna Energy Services, "Equipment Seismic and HydrodynamicRequalification of 30" Cylinder Operated Butterfly Valvesfor CSP-V-1, & 2, and CEP-V-lA, & 2A," File No. OS.01.F,QID No. 361104, Revision l, June, 1983.

13. Cygna Energy Services, "Equipment Seismic and HydrodynamicRequalification for 8", 10" and 12" Bore Air CylinderOperators," File No. 1P.01.F, QID No. 018001, Revision 0,May, 1983.

14. USNRC, "Standard Review Plan, NUREG-0800"

15. Cygna Energy Services, "Equipment Seismic and HydrodynamicRequalification of 24" Cylinder Operated Butterfly Valvesfor CSP-V-3,4,5,6, & 9 and CEP-V-3A & 4A," File No. OT.01.F,QID No. 361106, Revision 3, June, 1983.

ccoe co

CalculationSheet

Pcotect I~ . ~ < / . w P)cpa)ed By., (/ Date( t.'.J/I- (..) > ( DIJ" Iv:nd T..<(! Jg, )

Subject . C C.. v, . ( I . '. I I: L:; .

System,."'t -c''gi-

Checked By

Job No

Date

File No;r 9 I

Analysis No, r I I Rev, No. Sheet No.2 7

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1005 OC

TABLE Or CONTENTS QXDN 361106

SECTION

1.0

2.0

3.0

4.0

4.1

4.2

4.3

4.3.1

4.3.2

4.4

5.0

5.1

5.2

5.3

5.4

5.5

6.0

TITLE

Requalification CertificateSQRT Forms

Table of Contents

Requalification Analysis

Conclusions

Summary of Results

Analysis

Introduction

Calculations

References

Appendices

Response Spectra

Nalkdown Sheets

Valve Local Coordinate Systems

SRM Sheets

Final Pipe-Mounted EquipmentResponse G-levelsDrawings

NO OF PAGES

66 +Appendices

21

Revision 3

TABLE OF CONTENTS

CON'TQIDI 361106

SECTION TTTLE NO OF PAGES

7.0

7.1

7.2

7.3

7.4

Transmittals, Prior Calculationsand Reports

Communication Reports & Correspondence

Old Regualification 6 SQRT Forms

BXF Report

McPherson Associates Analysis

37

98

75

SECTION 4.0

REQUALIFICATION ANALYSIS

4I 4 O4 OW

Pt

I


CalculationCoverSheet

Project Job No. 82044

E ui ment Seismic & H drod namic RequalificatioA'" 'T.01/FClient

Washin ton Public Power Su ply SystemSubject

Gale. Set No. ]No. of Sheets

Seismic Qualification of 24" Cylinder Operated Butterfly ValvesQID 361106, EPN ifICSP-V-3,4,5,6 & 9, and CEP-V-3A & 4A

Statement of Problem

The equipment qualification was performed based on calculations usingvalve and operator response g-levels transmitted by the A/E,(Finalpiping loads dated 3/31/83) .

Sources of Data

See sheets 4.3.65 and 4.3.66

Sources of Formulae & References

See sheets 4.3.65 and 4.3.66

Remarks

None

Originators

J. Rakowski

Checkers

D. Searle

L. Kaner

Distribution

WPPSS-2

Project File-1

Revision No.

Supersedes Calculation Set No.

Revision 2

M. Scott

f005 00

LC FernandeApproved By:

~P+Date:

Ii

t /yg'Xg


CalculationSheet

Project

Subject

Prepared

By.'hecked

By;

Date

Date

System Job No. Fite No.

Analysis No. Rev, No. Sheet No.

CONTENTS

4.1

4.2

4.3

4.3.1

4.3.2

4.4

Calculation Cover Sheet

Conclusions

Summary of Results

Analysis

Introduction

Calculations

References

rccs cc


CalculationSheet

project

Subject

System

Analysis No. Rev. No.

Prepared By:

CheckedBy.'ob

No.

Sheet No,

File No.

Date

Date

SECTION 4.1

CONCLUSIONS


CalculationSheet

Project .WPPSS Equipment SeismicH drod namz.c Re ualification

Subject BIF Valves/Miller Operators

Prepared By, Oate 6'9 83

Ã. ~ay, ~ 4, 6/9/83System

CEP 6 CSPAnalysis No,

361106Rev. No.

Job No.82044

Sheet No,4.1.1

File Jlo.1T.01.F

CONCLUSIONS

Seven 24-inch BZF,Butterfly valves with Miller Air Productscylinder operators have been analyzed for structuralintegrity and operability for the plant, specific seismicand hydrodynamic piping loads transmitted from Burns andRoe. ,These piping loads are in the form of air operatorresponse G-levels (Section 5.5, dated March 31, 1983) .

The valves will be qualified after incorporating thefollowing modifications:

1). Remove the existing operator bracket attach-ment bolts (A-307) and replace with an A-325or A-490 bolt.

2) Reinforce the operator support ears with theaddition of shear plates as shown on page4.3-48 or 4.3-54 of 361106, Rev. 3 (this report) .


CalculationSheet

Project Prepared By; Date

Subject Checked By: Date

System

Analysis No, Rev. No.

Job No.

Sheet No.

Fite No.

SECTION 4.2

SUMMARY OF RESULTS

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CalculationSheet

WPPSS MECHANICAL EQ

Subject 24" Butterfly ValvesSystem

CSP it'r CEP

Prepared By

Checked By;

Job No.82044

Date'3z, 33 aolas

File No.OT.01.F

Analysis No.36110

Rev. No. Sheet No. 36 1 1 06 -~Z-

SUMMARY OF RESULTS

Parametric data for the seven subject valves inthis report, is given in Table 1.1. Results ofthe requalification analyses, which include acomparison of calculated stresses to the allowablesare given in Table 1.2. Allowablestresses for the various material types are givenin Table 1.3.

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SubjectII

Checked By, Date8 55

System

Analysis No.361106

Rev. No.

82044File No.

OT.01/F

3@/lb/ -4.z-

SUMMARY TABLE 1.3ALLONABLESTRESSES

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Since operability is required, the stresses for thefaulted condition will be kept below yield. Thetable below is based on AISC criteria and the yieldstresses at temperature (340'F) from PG. 9 of REF. 4for conservatism.

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ANALYSIS

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CalculationSheet

Pro ect Prepared By:GPSS Mechanical E ui ment Qualification ""1 10

Artalvsis No.361106

Rev. No.

Subject24" Butterflv Valves

System

Checked B i 2 ) Date. XJ..~'.~(

82044 'T.01/FSheet No.

361106 "4.>-I

EQUIPMENT REQUALIFICATION FOR QID 36110

BIF 24" CYLINDER OPERATOR BUTTERFLY VALVES

4.3.1 Introduction

The seven valves in this file are classified accordingto the parametric data given in Summary Table 1 ~ 1.

Since hydrodynamic loads apply in certain cases, fatigueanalyses were provided for components with the higheststress ranges.

The calculated stresses are based on valve and operatorG-levels calculated from the piping analysis and re-

'eivedfrom Burns 6 Roe. Since theseloads were initial-ly too high to qualify all EPN's the response G-levelswere subsequently recalculated with some of the con-servatisms removed from the piping analysis. In ad-dition, an SRSS analysis was set up in a computer pro-gram for each valve EPN in its specific orientation inthe piping system (see Section 5.4). Each computerprogram (Appendix A) is compiled and hence not subjectto subsequent change unless recompiled (and documented).

The method calculates stress from the north, vertical,and east component of operator response g-levels. TheSRSS is taken at the stress level and operating loadsdue to seating torque force and dead weight are latercombined by an absolute sum. Valve ear bending stresscomponents due to any one response g-level componentare combined by an absolute sum.

1000 00


CalculationSheet

'CVSS Mechanical Equipment Qualification ' "'2~ 1/10/83Sub e~t2k'utterfl Valves

Checked By ~ 1 i J Dateje m,I./~~SystemCSP & CEP

Job No.82044

File No.OT.01 F

Rev, No.361106 - g,g g

The computer analysis addresses only the more highlystressed components in the valve operator assembly.Separate analysis is given for the remaining compo-nents using a simpler approach with upper bound loads.This applies to all valve operator EPN's in QID 361106(24" Valve/8" cylinders) and QXD 361104'(30" valves/10"operators). Hand calculations which check selected por-tions of oomputer output gt-e, shown in Appendix C.

Appendix B of this section describes the air operatormass/stiffness model which was incorporated in thefinal piping analysis for calculation of operator re-sponse g-levels. The computer program includes an op-tion for using the valve ear forces and moments whichare directly output from the piping analysis with thevalve/operator model included. This was not finallyutilized, however, to qualify the subject equipment.

The equipment locations and elevations were taken fromthe PAID's in section 6.0. Natural frequency calcu-lations are given for the air operator assembliesin Section 4.3.2.1.

Preliminary analyses were performed which showedthat, for operator response g-levels greater than ap-proximately 3 g's, the air cylinder spring preloadforce would be exceeded and hence some disk flutterwould occur when the valve is in the open position.The calculation in section 4.3.2.2 shows that the mag-nitude of the valve disk flutter vibration angle dueto upper bound g-levels which occur in the hydro-dynamic frequency range is approximately 6 degrees.This flutter was evaluated to have no detrimentaleffect'n system safety function as noted in Reference5.

Valve operability was addressed in the following manner.For the valves with Use Code 2, operability after theevent can be assured by demonstrating that faulted con-dition stresses remain below elastic limits (seeSummary of Results.

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CalculationSheet

Proiect Prepared By:WPPSS Mechanical- E ui ment ualification 1 10 8Subject I Checked B g r Date24" Butterfl F v ..:-X.iA r, .: -Q,."rgSySterh Job No. File No.

Rev. No. Sheet No.361106

For valves CSP-V-3 and 4, which must operate from opento fail closed during an event, the following additionalevaluations were made:

1) Dynamic flow torques were assessed per Ref. 3and found to be less than the seating torquewhich controlled the equipment ~tresses.Furthermore these flow torques tend to movethe valve disk toward the fail-closed position,as noted in the above report.

2) The details of BIF drawing 206 767> parts ofwhich are shown in figures 1.1 and 1.2, allowthe following conclusions to be made for valveoperability:A) Figure 1.1 shows that thrust bearings are

part of the shaft bearing design. Thisdesign prevents lateral movement of thedisk in the direction of the shaft to eli-minate interference with the valve bodywhen closing. Further, it is noted onPage 26 of Ref. 3 that frictional torquesin the shaft bearing system are negligible.

B) Figures 1.1 and 1.2 show a circular valvecross section having an internal rim withinwhich the valve seats, in the closed posi-tion. The only mechanism remaining to af-fect valve closing which can be postulatedis out-of-round distortion of the sectiondue to DBE piping loads and dynamic loadson the valve.

These loads were accounted for in Ref. 4 in the overallvalve sizing calculations, where analysis showed thatthe stress intensity in the 0.5 inch thick valve bodyremained below 1.2 Sri, or approximately 0.8 of yield.Stress contribution from dynamic loads on the valveand operator were relatively small. Further, as shownin the figures:

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The valve seat forms a heavily reinforced section madeup of the valve body, internal hub and external flanges(including the mating flange of the piping). Hence thestress levels in this section are much lower than inthe valve'ody and hence no distortion of the sectioncould occur to affect seating'f the valve. Valveflange dimensions are given below. Note the relativelylarge internal radial clearance of 1/8 inch.

2 Stress analysis of the valve extended structures aregiven in this report. Air operator operability isaddressed in QID 018001.

The design data used in the analyses are given inSummary Table 1.1 (pipe-orientations and elevationsare taken from the appropriate PAID's in Section 6.0).Other pertinant data is given below.

1) Spring preload per communication reportin Section 7.0 of QID 018001 are:

Fail Open Preload =350'inal

= 1850ijj

Fail Closed Preload = 15009Final = 30008

2) Cylinder C.G.'s shown on the following sketchesrepresent data received from BIF in the communi-cation report of Section 7.0 of QID 018001.

3) Closing torque values are taken from Ref. 3.

4) Valve component dimensions: (Ref. Feb. 10, 11/83communication report - Section 7)/Flange: width = 3.5", thickness = 1.78"Radial Clearance Disk/Seat 1/8"

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82044File No.

OT.01 F

4.3.2 CALCULATIONS

4.3.2.1 NATURAL FREQUENCY CALCULATTONS

Perform. natural frequency calculations for the fol-lowing four operator configurations:

Grou I - Fail 0 en

EPN's CSP-V-5 6> and 9

Case |: Valve Open

Case I|: Valve Closed

Grou II - Fail Closed

EPN's CSP-V- 3 and 4 and CEP-V-3A and 4A

Case I Valve Open

Case II Valve Closed

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Job No,

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OT.01 F

RB 41572.5 25+ 1364.99 25

= 12754.44 + 1042.85 = 13797.297.67 19 '

0> = . 6—= .000476 rad13797.29

B 29~106Deflection at Point "A"

SA'ue to eB.000476(14.46)

.0069

Total SA = .0069 + .000032 = .0069

V = —= 72306.998/TN5004..00691fn =—

(72307) (386.4) = 42.12 Hz3

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CalculationSheet

Subject24" Butterfl Valves

SystemCSP and CEP

Checked B

Job No,82044

Protect Prepared By(WPPSS Mechanical E ui ment ualificati , Date

""slsolisFile No,

OT.01/FAnalysis No„

361106Rev No. Sheet No.

361106 -+. Q-

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361106 - Q-g - 7

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QN88 Mechanical Equipment Qualification "( 1/10/83Subiect24" Butterfl ValvesSystemCSP and CEP

Rev. No.c~

Checked 8: Date5 5d/89

Job No. File No.82044 OT.01 F

Sheet No.361106 -A.5 ZZ

4.3.2.3 STRESS ANALYSIS

The procedures for the analysis of the subject valvesare outlined below:

Recalculate the valve appurtenance stressesaddressed in Ref. 4 using response g-levelsfrom the final piping analysis. Incorporatethe current seating torque given in Ref. 3.Compare stresses to the appropriate percentage(s)of yield strength as, indicated in Summary Table 1.3.

2. Perform a fatigue analysis on significantlystressed components. Determine allowablealternating stress ranges from AISC 8th Edition,Appendix B, noting commentary.

The fatigue analysis is to be performed only for thoseEPN's subject to;hydrodynamic loads. The number ofrespective .load cycles is given below,

-LOAD COMBINATIONS G,STRESS CYCLES

The following table lists the load combinations andthe number of expected stress cycles for each com-bination. 'From the design criteria)

Combination ~Ccles1. SRV Alone 13500-200=13300 cycles2. OBE+SRV 50

3. SRV+AP+CHUG 140

4. SSE+SRV+AP+CHUG 10

Note: Load combination g4 with 150 cycles can beused to conservatively bound combinations3 and 4.

10CS CC

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CSP and CEPAnatvsis No.

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SystemCSP and CEPAnalysis No,361106

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Project Prepared Byf h DateMPPSS Mechanical E ui~ment ualification 1 10 83

Subject24" Butterfl V lv s

System

Checked B:

Job No. File No,a 50/es

Rev, No.361106 -g +-pg

Disc

The stressesRef. 4 to beload. SincePSI will notcelerations,

!in the disc were shown on page 51 ofdue almost entirely', to the pressurethe stress found in Ref. 4 of 3871change significantly for the new ac-the disc is acceptable.

Ta er Pins

The stress in these pins is due only to the seatingtor ue. The stress in Ref. 4 a e 53 is 10753q p g Ipst and is therefore acceptable.I For rhe new, lowerseating torque, the stress becomes 8710 PSI.

Analysis for: Drive Rod, cylinder bushing pressure,valve ears and valve ear bolts.

Method I: Use element forces and moments outputfrom the piping analysis (Summary Table1.1) and the absolute sum of stresses.The conservatism of SRSS summing of thecomponent stresses cannot be assuredbecause the independence of the sixelement forces (/moments) cannot be de-termined without. analysis of modal par-ticipation.

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Project Prepared Byp Mechanical -Equipment Qualification 1/10/83


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SystemP dCP

Job No,82044

File No.OT.01 F

Rev. No, Sheet No'361106 - g Q- gg

Method Il: Use the north, east and vertical operatoraccelerations output .from the pipinganalysis. Absolute sum for stresseswith each component then SRSS over re-sults for N,E and V.

Note t; Analysis of the distribution of stress on4 valve ears to predict the maximum tensilestress cannot confirm a maximum value lowerthan the absolute sum of the elemental ten-sil stresses due to the six forces (fromone acceleration direction, N,E or V). There-fore the absolute sum will be used at this level.

Note 21 Add stress due to the vector sum of deadweightplus seating torque force after above SRSScombinations are performed. (ABS)

Note 3: 10" A/0 parameters are shown for use in QXD361104.

Anal sis of Seatin Tor ue Forces

1) Seating Torque loads control the stress in thevalve lever arm, keyway, shaft and taper pins. Thesestresses were less than allowables for the valves ofseating torque given in Ref. 3, for all valves.2) For valve EPN's which are Fail-Open with Use-Code 2, no seating torque forces are applied duringthe faulted and upset conditions (CSP-V-5,6).

3) For the Fail-Closed valves, the forces at thetrunnion pins are shown below, along the cylinderaxis, for +2-axis g-loading:

~2, ~ ~iscn c!evis/valve skid

I I I ~

cn sac.~AalVe CarS

~eisrr ic./i7Mre&ic F~ f'rem oPer~rirr a. - cu'/8 dlrCcdDhf

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System Job No. File No.

Rev. No, 361106- cf.p-gy

As the bracket deflects in +2, under dynamic loads,the seating torque force is releived. The extentof relief depends on the relative stiffness of thebracket and valve ears relative to the valve seat.Since the steel backets and ears are very stiff inthis direction, little relief can be expected.Hence seating torque forces will be added as anABS sum to the valve ears. However, seating torqueforce will oppose operator weight when the bracketshangs downward from horizontal pipes.

0 erator Drive Rod

Drive rod dynamic stress is due only to g becauseg and g forces are taken out by trunnion pins.Ald seating torque stresses. 7. IZS

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Job No82044

File NoOT.01 F

Analysis No.361106

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Proiect Prepared By:/WPPSS Mechanical E ui ment uglification 1 10 83

SubjectII

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Job No.

rye,~ hP <&/ / Oate

File No.0

Analvsis No.361106

Rev. No. Sheet No.361106- .'5" 2

4~/ U set Condition Stresses

Th'e cylinder drive rod and valve ears were separatelyanalyzed for upset condition loads for the EPN's andassociated response g-levels noted below. All othercomponent faulted stresses are less than the upset al-lowables except for taper pins and keyway bearing stress.No additional analysis was performed for these compo-nents because the stress is controlled by the seatingtorque only. The allowable stress for the bracket boltsalso holds for upset conditions per the AISC manual,8th Edition. Bolt fatigue is considered as presentedin Section>.3.5.

Upset g-levels (per revised B&R piping analysis, Sec. 5.5)

EPN N

CSP-V-3CSP-V-4CSP-V-5CSP-V-6

1.731.140.97

1.64

1.601.401.401.44

0.961.501.710 '9

Component stresses are given in Table 1.2.

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SubjectII

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System Job No,82044

File No.

0Analysis No.361106

Rev. No. Sheet No. - 4.3-45

Section4,>.5 — Fati ue Anal sis

Discussion

The operator and bracket assembly are not part of the pressureboundary, therefore, the fatigue analysis will be performed inaccordance with Appendix B of the AISC Manual for Steel Con-struction. The following assumptions apply to the. fatigueanalysis.

1) Faulted stresses (based on piping-analysis accelerations)will be used. This is necessary to insure operabilityafter a design basis event.

2) The actual stresses used will be the ones calculatedin Section g.3.

3) If the alternating portion of the stress has been cal-culated separately only this part will be used. If theoperating loads (i.e. seating torque effects) are al-ready included in the stress analysis it will be con-servative to use the calculated stress value. As longas no failures occur, the operating stress does notneed to be extracted.

4) The allowable s'tress will be based on Table B3 of Appen-dix B in the AISC Manual of Steel Construction.

S) A factor of 1.S will be applied to the allowable be-cause of the low number of cycles. (Per Section 1.7of the Commentary'on the AISC Manual).

6) The actual stress range is taken as 2 times the maxi-mum stress for components subject to alternatingtension and compression.

Iced Cd


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System

5'BbF. Rev, No.

Job No.82044

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'61106- g,+- Qcf.

7) Bracket bolting is assumed to be properly tightened and willnot be considered for fatigue per Section B3.1 of the AISCManual.

The table on the following page gives the calculated stress range,stress category, and allowable for the critical components. The fol-lowing page gives excerpts from Appendix B of the AISC Manual showingthe descriptions of the relevent stress categories.


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Pr t Prepared By:I P W Date$8VSS Mechanical E ui ment Qualification, ') 4P( 1/10/83

Subject24" Butterfly Valves

System

Rev. No.z

Job No. File No.

'361106-Q >-g~

Checked By Date8 b

Fati ue Anal sis (cont.)

ITEM

TRUNNION PIN

DRIVE ROD MAX

SUPPORT EARS

STRESSTYPE

STRESS(PSI)

4108

SEE TA

SEE TAB

STRFSS STRESSRANGE (PST) CATEGORY

21

LE 1.2

E 1.2

1.5 x ALLOW(FROM AISC)

HAIN SHAFT$ 1278064

19,~M+1 12

90000

NOTES:

(I} Assume shear stress on nominal area of a studtype shear connection.

Note that this comparison includes all of the load combinations in oneconservative comparison using the maximum stress and the total numberof cycles ([3 x 4478] + 60 = 13494 cycles).

>Ocs.00

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Sheet No,

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3< jlo(-<.

S ZS 0~1;

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4J Z' H en lfjRROM.

GeneralCondi ~

tion

Plainmaterial

Built-upmembers

hlechani-callyfastenedconnec-tions

httach.ments

Situation

Base metal with rolled or cleaned sur-faces.

Base metal and weld metal in mem-be'rs, without attachments, built-up ofplates or shapes connected by contin.uous full.or partial. penetration groovewelds or continuous filletwelds parallelto the direction of applied stress.

Calculated flexural stress, Is, in basemetal at toe ofwelds on girder webs orflanges adjacent to welded transversestiffeners.

Base metal at end of partial lengthwelded cover plates having square ortapered ends, with or without weldsacross the ends.

Base metal at gross section of high-strength. bolted friction.type connec.tions, except connections subject, tostress reversal and axially loaded jointswhich induce out.of-plane bending inconnected material.

Base metal at net section ofother me-chanically fastened joints.

Base metal at net section of high.strength bolted bearing connections.

Shear stress on nominal area of stud-type shear connectors.

Kind of

Stress'or

Rev.

Tor Rev.

T or Rev.

Tor Rev.

Tor Rev.

Tor Rev.

Tor Rev.

S

StressCate-gory.(See

TableB3)

D

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REFERENCES:

D-207110-H, D-207110-G,(Valve Data Sheets)

A-206767,18", 24" & 30" Butterfly Valve - General

C-26096,"Certified Dimension for Model A-83-B Cylinder"

2. WPPSS Unit 2 Drawin s:

CSP-807-81.08

CSP-809-1.2

CEP-625-3.4

CEP-625-1.2

D.220-0310

Containment Purge Air Supply

Suppression Pool Vacuum Breaker .

From Reactor Nozzle X-67 to SGT-Fu-lA, 1B

From Reactor Nozzle X-67 to SGT-Fu-lA, 1B

Support and Erection isometric-TR64(Johnson Controls)

3. BIF Report TR-27234 and TR-27235, "Dynamic Torque Calculation ofButterfly Valve; Sizes 24 and 30 inch", dated November 10, 1982.

4. Report JTR-74-7 by McPherson Assoc., Tnc., "Design 6 SeismicAnalysis 24" Cylinder operated Butterfly Valve." (Rev. 1) 1/5/76.

5. WPPSS letter to Cygna Energy Services, GE-02-RWH-018, 12/17/82.

1ccs co

CalculationSheet

projectWashin ton Public Power Su 1

Prepared By: DateS stem L.C. Fernandez 5/27/83

Subject CheckedBy.'quipmentSeismic/Hydrodynamic Requal. ~. ~~a g~,, Date

y/q~/o~g

CSP 6 CEP 82044 OT.01.F~tHy5%'Ne'. Rev. No. Sheet No.

QID 361106 2 4. 3. t'(o

SECTION 4.4REFERENCES (CONTINUED):

r~i L-.,;~ ~j./'Z,/c~~~J r/q/~< y

6. Cygna Energy Services: Communications Report, R. Ricappito,BIF Valve, and J. Rakowski, CES, "BXF Valve Dimensions",2/11/83.

7. Cygna Energy Services, Project Manual Design Criteria,DC-1, Rev'. 1, November, 1982.

8. Cygna Energy Services, Equipment Qualification WalkdownVerification Forms, Revision 1, dated 1/5/83.

9. WPPSS, WNP-2, Safety Related Mechanical Equipment ListSummary Sheets, dated 2/10/83.

10. "AISC Manual of Steel Construction", American Instituteof Steel Construction, 8th Edition, 1980.

11. Preliminary Transfer of Final Burns & Roe Piping Loadsfor CSP-V-1,2,3,4,5,6 and CEP-V-3AG4A, received 4/13/83.

12. Cygna Energy Services, "Equipment Seismic and HydrodynamicRequalification of 30" Cylinder Operated Butterfly Valvesfor CSP-V-', 6 2, and CEP-V-1A, .G 2A," File No. OS.01.F,QID No. 361104, Revision 1, June,.

1983.'3.

Cygna Energy Services, "Equipment Seismic and HydrodynamicRequalification for 8", 10" and 12" Bore Air CylinderOperators," File No. 1P.01.F, QID No. 018001, Revision 0,May, 1983.

14. USNRC, "Standard Review Plan, NUREG-0800"

1000 00

APPENDIX A

COMPILED PROGRAMS AND RESULTS FOR

CSP-V-3

CSP-V-4

CSP-V-5

CSP-V-6

CEP-V-3A

CEP-V-4A

4 4' -( ~ c 4 ~

i i '1 "J<~ kl "I II

'I

J~

sbasic csp34tm

-BASIC Compi 1er Version 5.4b

0001:000002:000003!000004:000005!000006:000007'000008:000009:000010:000011:000012:000013:000014:000015:000016:000017!000018:000019:000020:000021!000022:000023:000024:00.'l25:00026:00

0027:000028:000029:000030:000031 $ 000032: 000033:000034!000035:000036:000037:000038!00„0039!000040'000041!000042:000043:000044!000045:000046:000047:000048:000049:000050!00

'51: 00v052:000053:000054:000055:000056.'00

resto! e 2read l rod, 1 cg, x, ph i, 1 ave, ab 1't, 11, 1 2restor e 3read fst2,ca,ia,cb,ib,aa,abrestore 4read wao,wbr,el,e2,e3,e4,e5restore 5read lrodo,lcgo,ldr,d,abushrestore 6read a(1,1),a<2,1),a<3,1),a(1,2),a<2,2),a(3,2)r estor e 7read a<1 s3> ra<2,3),a(3s3) sav<1),av(2),av<3>text 0,8c INPUT GLOBAL ACCELERATIONS 5i npu t b(1), b(2), b(3)pr inttext O,h INPUT DATA hpr intprint "GLOBAL G-LEVELS

ATT~ ~f L~, 0 7Bi.o SZb4

FlLEI;Q. OWbf

GHLRT"'0 BJ—

"ib(i) sb(2) tb(3)LES = ",;a(1,1),a<2,1),a(3,1)

REM~++++ BIF VALVE AND AIR OPERATOR SEISMIC STRESSREM+%%% 4 ++++%+: +++% CSP-Vj'AO-3/4REM++SAME ORIENTATION FOR EPN 3h4, SAME PARAMTERS, VARY G'SREMvar i,j,k = integervar lrod,lcg,x,phi,lave,abl t,li,l2,ei,e2,e3,e4,e5 = realvar fst2, ca, ia,cb, ib,aa,ab,dl,d2,ci, ii,c2, i2=realvar lrodo, 1 ego, 1 dr,d, abush, pbush=realvar fcof, fco, ma,mb, siga, sigb, fcdr, fcdrf,maf, mbf=realvar dear, fcear, fr, f11, f22, la, c i 12, c i 21, st t3, semi=realvar sem2, se t3,sesi, ses2,sr, taui 1, tau22, tauear,aear=realvar b'tens, taubl t, se t3f, semi f,.sem2f, fcear f, frf, f 11 f=! ealvar f22f,stt3f,sesif,ses2f,srf,tauif,tau2f,taurf=realvar taubf,btf, dsr,dtaur,dtaub,dbten,dsa,dsb,dpb=r ealvar sdraf,sdr bf,pbushf, tau11f, tau22f=realvar wao,wbr, f tr i,watr 1, si, si f, s2, s2f,mi,mi f,m2=r ealvar m2f,t3,t3f,tt3,tt3f,lbr,wtot=realvar bs1,bs2,bt3,bmi,bm2,btt3=real ~

dim r eal av(3)dim real wa(3)dim r eal wb<3)REMREM +++ BURNS 7 ROE EAR FORCES ARE bsi etc TURN ON WITH K=1+~+REMREMdim real a(3,3)dim real b<3)dim real glc<3,3>1 —data 7;5, 10, .75, 1.$ 5, 1.25, .72 data 25,14.46,.531,53.,7.125, ~ 31,1.5,2.53 data 1150 , 875,.46,.648,.138,2.41,1.44 data 399,277,5.25,8.5,28.5,15.,6.8755 data 40.,10.96,26.5,30.5,2.0756 data 90.,90.,180.,0.,90.,90.7 data 90 ~ s180 ~ r90 ~ s1'80 '90 ~ s90 ~

REM DATA 657 FOR VALVMGLOBAL-GORIENTATIONS AND WEIGHT VECTORrestoreread di,d2,ci,i'i,c2,i2

cs +34I 'UT GLOBAL ACCELERATI OhlS

? .66,2.99,3.76

INPUT DATA

GLOBAl G-LEVELS " = 2,66NORTH UECTOR ANGLES = 5'0VERTICAL VECTOR ANGLES= 0 5'0EAST VECTOR ANGLES = 90WEIGHT VECTOR ANGLES = 180

2.5'5'0

901805'0

3.76180

9090

LOCAL G-LEVELS

-1.43433E-53 '6

-1.43433E-5

-'1''.01471E-5 '"" 2;95'.,1 '1471E;5, -1.14059E-5-„.2.66 -1.14059E-5

II

OPERATING DP IUE 'OD STRESS AT AOPEPATIhlG DP, I VE ROD STRESS AT BOPERATING CYLINDER BRG PRESSUREOPcRATIhlG VALVE EAR TEl lSI LE STROPERATING VALVE EAR SHEAR STRESOPERATING EAR BOLT SHEAR STRESSOPERATING EAP, BOLT TENSILE STR

5525.528542.57

-98.46463795.21244.5'o225'63.252ol5.8o

D .,AMI C COMPONEhlTS

DRIVE ROD TENSILE STRESS AT A 15094.5DRIUE ROD TENSILE STRESS AT 8 23086.2BUSHING PRESSURE 294.409VALVE EAR TENSILE STRESS 14765.9VALVE EAR SHEAR STRESS 967.76EAR BOLT SHEAR STRESS 11706.8EAR BOLT TENSILE STRESS 14225'.2

, FIXED PLUS DYNAMIC COMPOhlENTS

DRIVE ROD TENSILE STRESS AT A 20620.1DRIUE .ROD TENSILE STRESS AT B 31628.7PUSHING PRESSURE 35'2.874VALVE EAR TENSILE STRESS 18561.1VALUE EAR SHEAP. STRESS 1212.72EAR BOLT SHEAR STRESS 14670EAR BOLT TENSILc STRESS 16845.1

CVGW~A~At-HiHFMTJoe xo. bz'osFLENo.< .dl i=

SHEEV NO.4.e.

O.qI ti'~'JT GLOBAL ACCELERATIONS

? '. ~6)2.99,3.76

INPUT DATA

GLOBAL G-LEVELS 2.66NORTH VECTOR ANGLES = 90VERTICAL VECTOR ANGLES= 0 90EAST VECTOR ANGLES = 90WEIGHT VECTOR ANGLES = 180

2.99909018090

3 ~ 76180

9090

LOCAL G-LEVELS

DRIVE ROD TENSILE STRESS *T ADRIVE ROD TENSILE STRESS AT BBUSHING PRESSUREFAR WELD TENSILE STRESSEAR WELD SHEAR STRESSE*R BOLT SHEAR STRESSEAR BOLT TENSILE STRESS

15094.523086.2294.40916435.22053.2411706.814229 '

FIXED PLUS DYNAMIC COMPONENTS

DRIVE ROD TENSILE STRESS AT A 20620.1DRIVE ROD TENSILE STRESS AT B 31628.7PUSHING PRESSURE 392.874E*R WELD TENSILE STRESS 20773.8EAR WELD SHEAR STRESS 2572.96EAR BOLT SHEAR STRESS " 14670EAR BOLT TENSILE STRESS 16845.1

-1 '1471E-5 2.99 , -1.43433E-5-1.01471E-5 -1.14059E-5 -3.76-2.66 -1 '4059E-5 -1.43433E-5

OPERATING DRIVE ROD STRESS AT A, 5525.52OPERATING DRIVE ROD STRESS AT B 8542.57OPERATING CYLINDER BRG PRESSURE -98 '646OPERATING E*R WELD TENSILE STR 4338.59OPERATING EAR WELD SHEAR STRES 519.72OPERATING E*R BOLT SHEAR STRESS 2963.24OPERATING EAR BOLT TENSILE STR 2615.86

Db...+MI C COMPONENTS

CVGMA

JQB NO.~PILE MQ

SHE+i NO~

I t<+UT GLOBAL *CCELERATI ONS56E2.99,3.76

INPUT DATA

GLOBAL G-LEVELS 2.66NORTH VECTOR ANGLES = 90VERTICAL VECTOR ANGLES= 0 5'0EAST VECTOP. ANGLES = 5'04IEIGHT UECTOR ANGLES = 180

2.95'0

901805'0

3 ~ 76180

5'090

LOCAL G-LEVELS

-1.43433E-S-3.76-1.43433E-5

"-1".01471E-'5 2.5'9-1,. 0,14?1E-.5,'-1 . 140S9E-5-2. 66 -1 . 14059E-5

W

OPERATING DRIVE ROD STRESS AT AOPERATING DRIVE ROD STRESS AT BOPERATING CYLINDER BRG PRESSUREOPERATING VALVE EAR TENSILE STROPEPATING VALVE EAR SHEAR STRESOPERATING EAR BOLT SHEAR STRESSOPERATING EAR BOLT TENSILE STR

5525.528542.57

-98.4646375'5.21244.96225'63.252615 '6

si -906.782s2f= 1150t3f=-2.57873E-3ml f~-7906. 1 5m2f=-6234. 1

t t3f=-12328. 8

DYNAMIC COMPONENTS

DRIVE ROD TENSILE STRESSDRIVE ROD TENSILE STRESS

'BUSHING'RESSUREVALVE EAR TENSILE STRESSVALVE EAR SHEAP, STRESSEAR BOLT SHEAR STRESSEAR BOLT TENSILE STRESS

sld= 2711.27s2d= 2541.76t3d= 175'8.16mid= 59281.6m2d= 22662 'tt3d= 68555 '

AT A 15094. 5AT B 23086.2

294 '0914765.9967.7611706.814229.2

FE.ENQ.E+~< <EHEE7 NO. ~~

F IZED PLUS DYNAMIC COMPONENTS

DPIVE ROD TENSILE STRESS AT A 20620.1DPIUE ROD TENSIl E STRESS AT B 31628.7PUSHING PPESSURE 392.874VALVE EAR TENSILE STRESS 18561.1VALUE EAR

MISHEAR

STPESS 1212 '2

EAP, BOLT SHEAR STRESSEAP. BOLT TENSILE STRESS

s1 t= 3618. 06ts2t= 3691.76t3t= 1798.16ml 0= 67187 . 8m2 28896.7tt3t= 80884 '

1467016845.1

cspSQI'' UT GLOBAL ACCELERATIONS? .96,3.17.4.19

INPUT DATA

GLOBAL G-LEVELS 2.96NORTH VECTOR ANGLES = 90VERTICAL VECTOR ANGLES= 0

*

90EAST VECTOR ANGLES = 904IEIGHT VECTOR ANGLES = 180

3.17909018090

4 ~ 19180

9090

LOCAL G-LEVELS

-1 . 1291'5E-5 '3. 17 '1.59836E-5;,,1 ~ 1 291 5E-„5;. -l.;20926E-5 -4 ~ 19

2 . 96 -1 . 20926E-5 -1 . 59836E-5

OPERATING DRIVE ROD STRESS AT A 5525.52OPERATING DRIVE POD STRESS AT B 8542.57OPERATING CYLINDER BRG PRESSURE -98.4646OPEPATING VALVE EAR TENSILE STR 3795.21OPERATING VALVE EAR SHEAR STRES 244 '62OPERATING EAR BOLT SHEAR STRESS 2963.25OPERATING EAR BOLT TENSILE STR 2615.86

D. AMIC COMPONENTS

DRIVE ROD TENSILE STRESS AT ADR IVE ROD TENS I LE STRESS AT BBUSHING PRESSUREVALVE EAR TENSILE STRESSVALVE EAR SHEAR STRESSEAR ~ BOLT SHEAR STRESSEAR BOLT TENSILE STRESS

16003. 224476312 ~ 133157431034.2912511.615776.8

FIXED PLUS DYNAMIC COMPONBWS

DRIVE ROD TENSILE STRESS AT A 21528 ~ 7DPIVE ROD TENSILE STRESS AT B 33018 ~ 6PUSHING PPESSURE 410. 597VALVE EAP. TENSI LE STRESS 19538. 2VALVE EAR SHEAR STRESS 1279.26EAR BOLT SHEAR STPESS 15474.9EAP. BOLT TENSILE STRESS 18392.7

p33INPUT GLOBAL *CCELERATI ONS?; '6,3.17) 4.19

I NP UT DATA


,3.17909018090

4.19180

9090

LOCAL G-LEVELS

—l.12915E-5 3.17 -1.59836E-5-1.12915E-5 -1.20926E-5 -4 '9-2.9o - -1.20926E-5 -1.59836E-S

OPERATING DRIVE ROD STRESS AT AOPERATING DRIVE ROD STRESS AT BOPERATING CYLINDER BRG'RESSUREOPERATING EAR WELD TENSILE STROPERATING EAP. WELD SHEAR STRESOPERATING EAR BOLT SHEAR STRESSOPERATING EAR BOLT TENSILE STR

D'. <MIC COMPONENTS

5525.528542.57

-98.464o4338.59519 '22963.242615.86

DRIVE ROD TENSILE STRESS AT ADRIVE ROD TENSILE STRESS AT BBUSHING PRESSUREEAR WELD TENSILE STRESSEAR WELD SHEAR STRESSEAR BOLT SHEAR STRESSEAR BOLT TENSILE STRESS

16003. 224476312.13317548.32194.412511.615776.8


DRIVE ROD TENSILE STRESS 'AT ADRIVE ROD TENSILE STRESS AT BPUSHING PRESSUREEAR WELD TENSILE STRESSEAR WELD'HEAR STRESSEAR BOLT SHEAR STRESSEAR BOLT TENSILE STRESS

21 528. 733018 ~ 6410.59721886.92714.1215474.918392.7

~pg gp 82cl44

|:ILKMO DP.e(.Psv"-=-i Np.=A-'7

esp/4I NPOT GLOBAL ACCELERATIONS

? 96,3.17,4.19

INPUT DATA

GLOBAL G-LEVELS 2.96NORTH VECTOR ANGLES = 90VERTICAL VECTOR ANGLES= 0 90EAST VECTOR ANGLES = 904IEIGHT VECTOR ANGLES = 180

3 ~ 17909018090

4 ~ 19180

9090

LOCAL G-LEVELS

-1 ~ 12915E-5 3.17— -1.59836E-51, 1291 5E .'5 ~ '1 '2092oc 5 4 19

-2.. 96 ',; .::" -1 . 20926E-5 -1 . 59836E-5

OPERAT I t }G DRIVE ROD STPESS AT AQPERAT I } }G DR I VE 'OD STRESS AT BOPEPATING CYLINDEP. BRG PPESSUREOPERATlt'}G VALVE EAP. TENSILE STP.OPERATING VALVE EAR SHEAR STRESOPERATING EAR BOLT SHEAR" STRESSOPERATING EAR BOLT TENSILE STR

5525.528542.57

-98.46463795.21244 '622963.252615 '6

sl -906.782s2i- 1150t3$ =-2.57873E-3ml$=-7906.15rn2$ =-6234.1tt3$ =-12328.8

DYNAMIC COMPONENTS

'PIVE ROD TENSILE STRESS AT A, DRIVE ROD TENSILE STRESS AT BBUSHING PRESSUREVALVE EAR TENSILE STRESSVALVE EAR SHEAR STRESSEAR BOLT SHEAR STRESSEAR BOLT TENSILE STPESS

sid= 2874.49s2d= 2832.44t3d= 2000.96mid= 65975.4rn2d= 24418.8tt3d= 72951.2

16003.224476312.133157431034.2912511,615776.8

CVQMAATTACHMEN'7

JOB NO 8ZdMFtt.a No. ~<>~'<SHEET MO.

F .ED PLUS DYt }AMI C COMPONENTS

DRIVE POD TENSILE STRESS AT A 21528.7DRIVE POD TENSILE STRESS AT B 33018. oPUSHING PPESSURc 410.597VALVE EAR TEt'}SILE STRESS 19538 'VALVE EAR SHEAR STRESS 1279.2oc*R RAI T RHFAR RTRFRR 1%4r4.o

EAR 80LT TENSILE STRESS

s1 t= 3781 . 28s2t= 3982.443t= 2000 '61t= 73881.5

m2" - 30652.9tt .= 85280

18392 '

CYQMAAYYACHSEM7sos xo.2~~~FlLKRg ~~01.FSHEET MQ.

esp GQ4

INc'UT GLOBAL ACCELEPATI QNS QQER GE-PC'/? '. r'0

s 1 . 97, 1 ~ 71

INPUT DATA

(c,zg~~~r c „lS~- 7-~~

GLOBAL G-LEVELS 2.8NOPTH VECTOP, ANGLES = 90VERTICAL VECTOR ANGLES= 0 90cAST VECTOR ANGLES — 90idEIGHT VECTOR ANGLES = 180

1.97909018090

'.71180

9090

LOCAL G-LEVELS

-6.52313E-6-1 .71-6.52313E-6

.-'1 . 0 68 1, 1,E-,5.," . ~, 1,. 97'"',1. 0681 1E-5 -7. 51495E-6

'-':". 8 ' -7. 51 495E-6" 'I 0 ll,

OPERATING DRIVE ROD STRESS AT AQPEPATING DRIVE RQD STPESS AT BOPEPATING CYLINDER BRG PRESSUREOPERATING EAR MELD TENSILE STROPERATING EAR MELD SHEAR STRESOPERATING EAR BOLT SHEAR STRESSOPERATING EAR BOLT TENSILE STR

5525.528542.57

-98.46464338.59519.722963.242615.86

D'. iMIC COMPONENTS

DRIVE ROD TENSILE STRESS AT A 9945.23DRIVE ROD TENSILE STRESS AT B 15210.7BUSHING PRESSURE 193.975EAR MELD TENSILE STRESS 10668.6EAP. MELD SHEAR STRESS 1296.94EAR BOLT SHEAR STRESS 7394.64EAR BOLT TENSILE STRESS 14365 F 1

FIXED PLUS DYNANIC COMPONENTS

DRIVE RQD . TENSILE STRESSDP. IVE ROD TENS I LE STRESSPUSHING PRESSURE

R MELD TENSILE STRESSEAR WELD SHEAR STRESSEAR BOLT SHEAR STRESSEAR BOLT TENSILE STRESS

AT A 15470.8AT B 23753.2

292.4415007 '1816 '610357.916980.9

s p~1,~ ggJpa xo A~~ss.s No.SHEET <<1 A-Ib

~ ~

sp Q4INPUT GLOBAL ACCELERATIONS

?"1 l4,1.40,1.5ItlPUT DATA

Q pS'E'7 EQ Jc-'bP~


1 ~ 4909018090

1.5180

9090

LOCAL G-LEVELS

-4.34875E«6 1.4 -5.72204E-6-4.34875E-6 -5.34057E-6 -1.5-1 ~ 14 -5.34057E-6 -5.72204E-6

OPERATING DRIVE ROD STRESS *T AOPERATING DRIVE ROD STRESS AT BOPERATING CYLINDER BRG PRESSUREOPERATING EAR WELD TENSILE STROPERATING EAR WELD SHEAP, STRESOPERATING EAR BOLT SHEAR STRESSOPERATING EAR BOLT TENSILE STR

5525.528542.57

-98.46464338.59519.722963 '42615 '6

Y'AMIC COMPONENTS

DR IVE ROD TENS I LE STRESS AT A 7067. 68DRIVE ROD TEtlSILE STRESS AT B 10809.6BUSHING PRESSURE 137 '5EAR WELD TENSILE STRESS 7558.92EAR WELD SHEAR STRESS 940. 809EAR BOLT SHEAR STRESS 5364. 13EAR BOLT TENSILE STRESS 6129 '4

FIXED PLUS DYNAMIC COMPONEt'lTS

DRIVE ROD TENSILE STRESS AT A 12593 'DRIVE ROD TENSILE STRESS AT B 19352 'PUSHING PRESSURE 236. 315EAR WELD TENSILE STRESS 11897.5EAR WELD SHEAR STRESS 1460.53EAR BOLT SHEAR STRESS 8327.37EAR BOLT TENSILE STRESS 8744.9

CVC~ll'fld%A~ ~ACRE'.".R7

sbasic csp5tm

S-BASI C Comp i l er Ver s i on 5. 4b

v001:000002:000003:000004:000005:000006:000007$ 000008:000009:000010 000011:000012:00

,.; .,0013$ 00.,00,14: 000015 $ 00

-0016:000017:000018: 000019:000020 $ 000021: 000022: 000023:000024:00n025:00

326:000027$ 000028:000029$ 000030:000031:000032:000033:000034:000035:000036:000037:000038!000039:000040:000041$ 000042:000043:000044:000045:000046:000047:000048:000049".000050:00

~51:00. a52 F 000053:00

read wao,wbr,ei,e2,e3,e4,e5restor e 5r ead lrodo, i ego, 1 dr,d,abushr estore'read a(1,1), a(2, 1), a(3, 1), a<1,2), a<2,2), a<3,2)restor e 7read a(1,3),a(2,3),a(3,3),av(1) )av(2),av(3)tex t O,h INPUT GLOBAL ACCELERATIONS 5input b( 1),b(2),b(3)printtext 0,8c INPUT DATA h

ATE"CHMENT

JOB NO ~264~FILE Np ~QT.O

SHEEi i'JC. A-IZ

REM+++++ BI F VALVE AND AI R OPERATOR SE I SMI C STRESSREM%%%%+%% i+:w%%w%% CSP-V/AO-5REMvar i,J,k = integervar l rod, 1 cg,x,phi, 1 ave,abl t, 1 1,12,ei,e2,e3,e4,e5 = realvar fst2, ca, i a,cb, ib,aa, ab,di,d2,c 1, i i,c2, i 2=realvar lrodo, 1 ego, ldr,d, abush, pbush=realvar fcof, fco, ma,mb, siga, sigb, fcdr, fcdrf,maf, mbf='realvar dear, fcear,fr, f1 i,f22, la, ci12,ci 21,stt3,semi=realvar sem2, se t3, sesl, ses2, sr, taui 1, tau22, tauear, aear=realvar btens, taubl t, set3f,semi f,sem2f,fcear f, frf,filf~realvar f22f,stt3f,sesif,ses2f,srf, tauif, tau2f, taurf=r ealvar, taubf-, bt f, dsr, dtaur, dtaub, dbten, dsa, dsb, dpb=realvar sdr af, sdrbf, pbushf, taui 1 f, tau22f~r ealvar wao,wbr, ftrl,watr i,si,s1f,s2,s2f,mi,mi f,m2=realvar m2f,t3,t3f,tt3,tt3f,lbr,wtot=realvar bsi,bs2,bt3,bml,bm2,btt3=$ ealdim real av(3)dim real wa(3)dim real wb(3)REMREM +w+ BURNS 7 ROE EAR FORCES ARE bsi etc TUPIK ON WITH K=1+++REMREMdim real a(3,3)dim r eal b(3>dim real glc<3,3>1 data 7.5, 10, .75, 1.95, 1.25, .72 data 25,14.46,.531,53.,7.125,.31,'1.5,2.53 data 0 ~ i ~ 875s ~ 46s ~ 648s 138~2 '1$ 1 ~ 44 data 399,277,5 '5,8.5,28.5,15.,6.8755 data 40.,10.96,26.5,30.5,2.0756 data 42.5,47.5,90.,90.,90.,0.7 data 47.5,137 ',90.,180.,90.,90.REM DATA 6%7 FOR VALVE/GLOBAL-G ORIENTATIONS AND WEIGHT VECTORrestor eread di,d2, cl, i 1, c2, i 2$'estore 2read lrod,lcg,x,phi,lave,ablt,l1,12restore 3read fst2,ca,ia,cb,ib,aa,abr estore 4

UT GLOBAL ACCELERATIONS? .96,3.44)5 '2

INPUT DATA

GLOBAL G-LEVELS 2 '6NORTH VECTOR ANGLES = 42.5VERTIC*L VECTOR ANGLES= 90EAST VECTOR ANGLES = 47.5WEIGHT VECTOR ANGLES = 180

3.4447.590137. 590

5.4290

09090

h

LOCAL G-LEVELS

2.18234 -1.31225E-5 3.661691.99974 -1.31225E-S -3,.99606

-1.12915E-5 3.44 -2.06756E-5

OPERATING DP IVE ROD STRESS AT AOPERATING DRIVE ROD STRESS AT BOPERATING CYLINDER BRG PRESSUREOPERATING VALVE EAR TENSILE STROPERATING VALVE EAR SHEAR STRESOPERATING EAR BOLT SHE*R STRESSOPERATING EAR BOLT TENSILE STR

D..AMIC COMPONENTS

5048 ~ 357721.14

-98.46464664.25297.6143600 '71340 '9

DRIVE ROD TENSILE STRESS AT ADRIVE ROD TENSILE STRESS AT BBUSHING PRESSUREVALVE EAR TENSIL'E STRESSVALVE E*R SHEAR STRESSEAR BOLT SHEAR STRESSEAR BOLT TENSILE STRESS


21519. 632912 '419.72420190.51,312.911588219507

DRIVE ROD TENSILE STRESS AT A 26567.9DRIVE ROD TENSILE STRESS AT B 40633.9

'USHING PPESSURE 518.189VALVE E*R TENSILE STRESS 24854.8VALVE EAR SHEAR STRESS 1610.53EAR BOLT SHEAR STRESS 19482.2EAP. BOLT TENSILE STRESS 20847.7

ATTACHMENTaoswo. ~~44va.exa ~<W FSHEET tlO.

csp5UT Gl OBAL ACCELERATIONS

? >6;3.44,5.42

I NPUT DATA

r >Q ~Rb ~ J q t b; iC -';:

GLOBAL G-LEVELSNORTH VECTOR ANGLESVERTICAL VECTOR ANGLES=EAST VECTOR ANGLESWEIGHT VECTOR ANGLES

2 '642.59047.5180

3.4447.590137.590

5. 4290

09090

LOCAL G-LEVELS

3.66169-3.99606-2.06756E-5

,,2 . 1 8234 ..; -1 . 31 225E-51 ~ 99974 . -1.31225E-5

'-'1 .12915E-5 3 44'H ~ ~

OPERATING DRIVE ROD STRESS AT AOPERATING DRIVE ROD STRESS AT BOPERATING CYLINDER BRG PRESSUREOPERATING EAR MELD TENSILE STROPERATING EAR MELD SHEAR STRESOPERATING EAR BOLT SHEAR STRESSOPERATING EAR BOLT TENSILE STR

5048 '57721.14

-98.46465107.51631.4313600.171340.69

D, WMI C COMPONENTS

DRiVE ROD TENSILE STRESSDRIVE .ROD TENSILE STRESSBUSHING PRESSUREEAR MELD TENSILE STRESSEAR MELD SHEAR STRESSEAR BOLT SHEAR STRESSEAR BOLT TENSILE STRESS

AT A 21519.6AT B 32912.8

419.72422736.72785.5215882I 9507


DRIVE POD TENSILE STRESS AT ADRIVE ROD TENSILE STRESS AT BPUSHING PRESSUREEAR WELD TENSILE STRESSEAR MELD SHEAP. STRESSEAR BOLT SHEAP, STRESSEAR BOLT TENSILE STRESS

26567.940633 '518 '8927844'.23416 '519482 '20847.7

boa wo.MC~Od

PILSNER.

~+I <SHEET Ho.dl «L.

I } r'UT GLOBAL ACCELERATIONS'7 96)3 ~ 44s5 ~ 42

INPUT DATA

GLOBAL G-LEVELSNORTH VECTOP. ANGLESVERTICAL VECTOR ANGLES=EAST VECTOR ANGLESWEIGHT VECTOR ANGLES

2 '642.59047.5180

3.4447.590137. 590

5.4290

0op90

LOCAL G-LEVELS

2 ~ 18234 -1 ~ 31225E-5 3. 661691 . 99974 -1 . 31225E-5 -3. 99606

-1 ~ 12915E-5 3. 44 -2.06756E-5

OPERATING DRIVE ROD STRESS AT AOPERATING DRIVE ROD STRESS AT BOPERATING CYLINDEP. BRG PRESSUREOPERATING VALVE EAR TENSILE STROPERATING VALVE EAR SHEAR STRESOPERATING EAR BOLT SHEAR STRESSOPERATING EAR BOLT TENSILE STR

si -906.782s2$ =-2.57874E-3t3%=-2.57873E-3ml f= 9.89667E-2m2$ =-6234. 1

tt3j=-22103.8

5048 ~ 357721 . 14

-98.464o4664.25297 '143600 '71340.69

DYNAMIC COMPONENTS

DRIVE ROD TENSILE STRESS AT A 21519.6DRIVE ROD TENSILE STRESS AT B 32912.8BUSHING PRESSURE 419.724VALVE EAR TENSILE STRESS 20190.5VALVE EAR SHEAR STRESS 1312.91EAR BOLT SHEAR STPESS 15882EAR BOLT TENSILE STRESS 19507

sld= 3865.34s2d= 3020.7t3d= 2325.44mid= 76145m2d= 31 3o9. 7tt3d= 84539.5

F „,ED PLUS DYNAMIC COMPQl }ENTS

OBHQ 8ZOMFILE IIO.SIIEn'II. A'«

DRIVE ROD TENSILE STRESS ATDRIVE ROD TENSILE STPESS ATPUSHING PRESSUREVAI VE EAR TENSILE STPESSVALVE EAP. SHEAR STRESS

A 2o567.9B 40633 '

518.18924854 'lol0 ~ 53

~rI t'lPUT GLOBAL ACCELERATI Ot'lS

'? ~ o7,1 ~ 4,1.71

I NPUT DATA

j3 PSEUD

GLOBAL G-LEVELS?lORTH VECTOR ANGLESVERTICAL VECTOR AtlGLES=EAST VECTOP, ANGLESWEIGHT VECTOR *tlGLES

.9742.59047.5180

io447.590137.590

1.7190

09090

LOCAL G-LEVELS

~ 715158 -5 '4057E-6 1 ~ 15526'''. 655321': '-5. 34057E-o -1 . 26075-, -.3.70025E-, 6 1.4 -6.52313E-6

'OPERATING DRIVE ROD STRESS AT AOPERATING DRIVE ROD STRESS AT BOPERATING CYLINDER BRG PRESSUREOPERATING EAR WELD TEtlSILE STROPERATING EAR WELD SHEAR STRESOPERATING EAR BOLT SHEAR STRESSOPERATING EAR BOLT TENSILE STR

5048. 357721 . 14

-98.4o465107.51631.4313600.171340.69'~

'AMI C COMPONENTS

DP.IVE ROD TENSILE STRESS AT A 6859.18DRIVE POD TENSILE STRESS AT B 10490 ~ 7BUSHING PRESSURE 133.784

R WELD TEtlSILE STRESS 7323.31EAR WELD SHEAR STRESS 892.936EAR BOLT SHEAR STRESS 5091 . 16EAR BOLT TENSILE STRESS 7599.75


DRIVE ROD TENSILE STRESS ATDRIVE ROD TENSILE STRESS ATPUSHING PRESSUREEAR WELD TEt'ISILE STRESS=AR WELD SHEAR STRESS

R BOLT SHEAR STRESSEAR BOLT TENSILE STRESS

A 11907.5B 18211.9

232.24912430.81524.378691 . 338940. 43

sbasi c csp6tm

S-BASIC Compiler Version 5 'bJOI '00

0002:000003:000004:000005:00000620000072000008:000009:000010:000011:000012:0000132000014:0000152000016:000017:000018:00001920000202000021:000022:000023:000024:000025:00

126200v 027: 000028:000029:000030: 000031: 000032: 000033 2 00003420000352000036:0000372000038:0000392000040:000041:00004220000432000044:0000452000046:000047:000048:000049:000050:00nn51:00

522000053:0000542000055:000056:00

read fst2,ca, ia,cb, ib,aa,abrestore 4read wao,wbr,ei,e2,e3,e4,e5res tor e 5read lrodo, 1 ego, 1 dr,d,abushr es tore 62 ead a(1 s 1) sa(2s 1) sa(3»1) sa(1,2)»a<2»2) sa(3»2)*restore 7r ead a< 1, 3), a(2, 3), a(3, 3), av (1), av (2), av (3)text 0»h INPUT GLOBAL ACCELERATIONS 8c

input b<1) sb<2) sb<3)printtext 0,6 INP,UT DATA hpr intpr i n t "GLOBAL G-LEUELSpr int "NORTH VECTOR ANGLES

CVGNAATTACH1icNTJOB NO. 0

RLENO. ~T Oi

sHf s No.

"»b(1)sb(2>sb(3>";a(1,1),a<2,1),a(3,1)

REM+»s+++ BIF VALVE AND AIR OPERATOR SEISMIC STRESSREM»s»s~»s». ~~». ~~~».».s. ~ CSP-VyAO-6»s~»s»s~» ~»s~~~»s~»s»'+» + ss~ss~~~~»sREMvar 1 s J sk = integervar lrod, leg,x,phi, 1 ave,abl t,11,12,el,e2,e3,e4,e5 = realvar fst2, ca, i a,cb, ib,aa,ab,di,d2,cl, i i,c2, i2=r ealvar 1 rodo, 'i cgo, 1 dr, d, abush, pbush=realvar fcof, fco, ma,mb, si ga, s i gb, fcdr, fcdrf,maf, mbf=r ealvar dear, fcear, fr, f 1 1, f22,1 a, c i 12, c i 21, st t3, semi=realvar sem2,set3,sesi,ses2,sr, taul 1, tau22, tauear,aear=r ealvar b tens, taubl t, se t3f, semi f, sem2f, fcear f, frf,f11 4 =realvar f22f,stt3f,sesl f,ses2f,srf, taul f, tau2f s taurf=realvar taubf,btf, dsr, dtaur, dtaub, dbten, dsa, dsb, dpb=realvar 'dr af,sdrbf,pbushf, taui 1 f, tau22f~r ealvar wao,wbr, ftri,watri,sl, sl f, s2, s2f,mi,ml f,m2=r ealvar m2f, t3, t3f, t t3, t t3f, 1 br,wtot=r ealvar bsl, bs2, bt3, bml, bm2, bt t3=realdim real av<3)dim real wa(3)dim real wb<3)REMREM +»s»s BURNS 7. ROE EAR FORCES ARE bsl etc TURN ON WITH K=1»s+»sP.EMREMdim r eal a(3,3)dim real b<3)dim real glc(3,3)1 data 7.5, 10, .75, 1.95, 1.25, .72 data 25,14.46,.531,53.,7.125,.31,1.5,2.53 data 0 ' ~ 875s ~ 46» ~ 648s ~ 138»2 '1sl ~ 44 data 35'5',277»5 '5»8 '»28 '»15 '6 '755 data 40.,10.96,26.5,30.5,2.0756 data 5'O.s90 ~ st »0 '90 '90 ~

7 data 5'0 '0 '5'0 ~ s180 ~ s90 ~ s90 ~

REM DATA 6h7 FOR VALVE/'GLOBAL-G ORIENTATIONS AND WEIGHT VECTORrestoreread dl,d2,cl,i i,c2,i2restore 2read 1rod,'icg,x,phi,lave,ablt,11,12restor e 3

Pl I II I,

0060: 000061: 010062: 02'0063: 020064:020065:01'')66:00367:Oi

0068:010065':000070:000071: 000072: 000073:000074:000075:000076:000077:010078:010079:010080:000081". 000082: 000083: 000084: 000085:000086:000087:000088:000089".000090:000091:00

5'2: 00v093:000094:000095:00005'6:00005'7:00005'8:000095':000100:000101:000102:000103!000104:000105:000106:000107'000108:000105'.000110:000111:000112:000113:000114:000115:000116:00'7:00

18:000115':000120:0001 21: 000122: 000123:000124:00ni oR.nn

ATTACHVi=MTsos NO.~MAFiLE NQ.QX 4~i

SHEETRO. 4 ~

for i=i to 3for j=l to 3;

a<j,i)=a<j',i)+2.+3.1416/360.glc(j,i)=b<i)icos(a(j,i))

nextnext ifor j=l to 3av ( j ) =av ( j ) +2. +3. 1416/360 .next Jprinttext 0,& LOCAL G-LEVELS 4pr intprint gl c(1,1),gl c(1,2),gl c(1,3)print glc(2,1),glc(2,2),glc(2,3)pr in t gl c(3,1), gl c(3,2), gl c(3,3)REM WE I GHT COMPONENTSfor j=i to 3wa(j)=wao+cos(av(j))wb(j)~broncos(av(j))next

'ph'i=phi+2.+3.1416/360.la='lave/2'„c112=c1/i

2c i 2l=c2/i 1

aear=l 1 +12REM CALCULATE EAR FORCES USE BhR LOADS AS OPTION LATERREM FIXED COMPONENTS ARE ALWAYS THERE1 br= 1 r od+1 cgwatr 1=1 br+wa(1)/1 rodslf=wb<1)+watr 1

w t o t~wao+wbrs2f=wb(2)+wa(2)+f st2t3f=wa(3)+wb<3)mi f=-<wa(2)+wb(2)+fst2) +e5-wa(3) +(e3+ 1 cg)-wb(3) +e4m2f=(watr 1+wb(1) ) +e5-wa(3) +e2-wb(3> +elt t3f=watr 1+e3+ <wa(2)+ fst2) +e2+wb< 1 > we4+wb(2> we 1fcdrf~l cg+wa(1)/1 r odmaf~fcdr f+(lrod-13.5)mbf~fcdr f+7.125sdraf=f st2/aa+abs(maf +ca/1 a)sdrbf=f st2/ab+abs(mbf +cb/lb)fcof=lcgoxwa(1)/1 r odopbush f=fcof+< 1 dr+d)/(d+abu sh)REM STRESSES FROM FIXED COMPONENTSdeat =(dl+dl+d2+d2) ++.5se t3f=abs( t3f/(4+aear ) )semi f=abs(ml f/(2+d2+ae ar > )sem2f =abs<m2f/(2wdl +ae ar ) ) CYfcearf=t t3f/(2+dear)frf=x+fcearff i if=-<fcearf+sin(phi )-frf+cos(phi) )f22f=fcearf icos(phi )+fr f+sin< ph 1 )st t3f=abs< f 11 f+1 a+c i 12)+abs( f22f +1 a+c i 21 )se s1 f=abs( sl f+c i 12+1 a/4. )ses2f=abs(s2f+ci 21+la/4 'srf=se t3f+seml f+sem2f+sesl f+ses2f+st t3fREM EAR SHEARtaul 1 f=abs(si f/<4+aear) )+abs< f 1 1 f/aear )tau22f=abs(s2f/(4~aear) )+abs( f22f/aear)taurf=( tau1 1 f+taul 1 f+ tau22f +tau22f ) ++ ~ 5taubf=taur f+aear/abl tREM E*RBOLT TENSIONbtf=(se t3f+seml f+sem2f ) +aear/abl tprintpr int"OPERATING DRIVE ROD STRESS AT A ";sdrafnr i n & ~~ AocpbTTMf'ptlJc Inn QTpccc 6T R "

crier

h4

V 4 V ~ V V

01 26: 000127: 000128!00'0129!000130:000131! 00"132: 00

i33:000134 0001 35: 000136! 0001 37: 000138! 000139! 000140! 000141:000142: 000143: Oi0144! 010145: 0101.46! 010147: 010148! 0 1

01 49: Oi0150: 0 1

0151: 010152! 0 1

0 1 53: 010154! 010155! Oi0156: 010157!01

58: 01!59:Oi

0160:010161! 010162! 010163: 010164! 0 1

0165:010166!010167!010168!010169:010170! 010171! 010172'010173:010174:010175:010176:010177:Oi0178:010179:Oi0180! 010181:010182: 01~'3: 01

84:0001 85: 000186: 000187: 000188: 000189! 000190: 00'n! 01 ~ nn

P ~ ~ ~ ~ s vo 0 ~ 4 ~ ~ 4 ~ 1V 8 ~ l4 V I ~ 'I'VV V I ~ % ~ VV ~ I ~

print"OPERATING CYLINDER BRG PRESSUREprint"OPERATING VALVE EAR TENSILE STRprint"OPERATING VALVE EAR SHEAR STRESprint"OPERATING EAR BOLT SHEAR STRESSprint"OPERATING EAR BOLT TENSILE STRpr intREMREM CALCULATE VARIABLE COMPONENTSREMdsr~O. f

dtaur =0.dtaub=0.dbten=O.dsa=0.dsb=0.dpb=O.for j=i to 3fc o= 1 c go+wao+g 1 c ( 1, j ) 11 rodopbush=f co+< l dr +d)/(d+abush)f tr1=1br+waowgl c<1, j)/1 rodsi=f tr 1+wbr +gl c(1, j)s2=wtot+glc(2,j)t3=wtot+glc(3,J)mi=-wtot+glc(2,j)+e5-wao+glc(3,J>+(e3+m2=(f tr.i+wbr+gl c(1, j ) >+e5-(wao+e2+wbr+tt3=ftriwe3+wbr+glc(i,j)+e4+glc(2,J)+(fcdr=lcg+wao+glc( l,j)r'irodma= fc dr+( l r od-1 3. 5)mb=f cdr+7. 125si ga=ma%cM i as i gb=mb+cbl i bREM CALCULATE EAR TENSIONse t3=abs( t3r'(4+ac ar > )semi=abs(mit'(2wd2+aear) )sem2=abs(m2/(2+di +aear > )fcear =t t3/(2%dear)5 r=x+fcearf 1 1=-(fcear+sin(phi )-fr icos(phi ) )f22~% cear+cos<phi )+fr+sin(phi )st t3=abs( f11+1 a+c i 12)+abs( f22+1 a+c i 21)sesi=abs( si +c i 12+1 M4. )ses2=abs(s2+c i 21+1 al4. )sr ~se t3+semi+sem2+sesi+ses2+s t t3REM EAR SHEARtaui i~abs( si/(4. +aear > >+abs( f11''aear )tau22=abs< s2/< 4. +aear ) )+abs( f22/aear )tauear=( tau11+tau11+ tau22+tau22) w+. 5taublt=tauear+aear/'abltREM EARBOLT TENSIONbtens=(se t3+semi+sem2) +aear/abl tdsa=dsa+ s i ga+s i gadsb=dsb+si gb+s i gbdp b=dp b+ p bu sh +p bushdsr=dsr+s! +srdtaur=dtaur+ tauear+taueardtavb=dtaub+ taubl t+ taubl tdbten=dbten+btens+btensnext jREM CQMBINE STRESSESdsa=dsa++.5dsb=dsb++.5dpb=dpb++ ~ 5dsr=dsr++.5dtaur=dtaur++:.5dtaub=dtaub++.5rlh 0 on .rib 4 or WS

%J ~ ht I

";pbushf"Isrf"; taurf"; taubf";btf

lcg)-wbr+glc(3,J)+e4ei)+glc(3,j)waowe2+wbr+el)

gyGRAATTACHE!BI".!

0192: 000173!000194: 00'01 5'5: 000196! 00015'7:00

198:00E 5'5': 00

0200:000201:000202! 000203:000204:000205:000206!000207:000208!000209:000210:000211 200" ' '0212!'000213:000214'00"' 0215!00

-0216:000217'000218:00021 5'! 000220: 000221 $ 000222!000223:00

'.24! 00225$ 00

AT A";dsaAT B";dsb

";dpb'dsr

";dtaur";dtaub";dbten

ONENTS &

AT A";dsaAT B";dsb

" ldpb"Edsr";dtaur";dtaub";dbten

++ww+w End of program +++++w

printtext 0,& DYNANIC CONPONENTS &printprint "DRIVE ROD TENSILE STRESSprint "DRIVE ROD TENSILE STRESSprint "BUSHING PRESSUREprint "VALVE EAR TENSILE STRESSprint "VALVE EAR SHEAR STRESSprint "EAR BOLT SHEAR STRESSprint "EAR BOLT TENSILE STRESSds

aci�ds

a+ abs ( sdr af )dsb=dsb+abs(sdt bf )dpb=dpb+abs( pbush f )dsr~dsr+abs(srf )dtaur=dtaur+abs( taur f )dtaub=dtaub+'abs( taubf )dbten=dbten+abs(btf )printtext 0,& FIXED PLUS DYNANIC CONPprintpr i'nt "DRIUE ROD TENSILE STRESS.pr.int "DRIVE ROD TENSILE STRESSprint "PUSHING PRESSUREpt.i'nt "UALVE EAR TENSILE STRESSpr int "VALUE EAR SHEAR STRESSprint "EAR BOLT SHEAR STRESSprint "EAR BOLT TENSILE STRESSend

ATTACHE'ENT

gpss No 5'Zbd

FllENO. 0 .blEHEEi NO.~

~ ~ ~

csp6INPUT GLOBAL ACCELERATIONS11.39.3.33,5.85

Il~rUT DATA

GLOBAL G-LEVELS11.39'ORTH

VECTOR ANGLES = 90VERTICAL VECTOR ANGLES= 0 90EAST VECTOR ANGLES = 90

3.339090

0

5.850

90

LOCAL G-LEVELS

-4.34494E-5 3.33-4.34494E-5 -1.27029E-5

11.39 -1.27029E-S

-2.23loE-55.85

-2.2316E-5

OPERATING DRIVE ROD STRESS AT AOPERATING DRIVE ROD STRESS AT BOPERATING CYLINDER BRG PRESSUREOPERATING VALVE EAR TENSILE STROPERATIIIG VALVE E*R SHEAR STRESOPERATING EAR BOLT SHEAP, STRESSOPERATING E*R BOLT TENSILE STR

5048.357721.14

-98.46464664.25297.6143600.171340.69

E

DYNAMIC COMPONENTS

R " ROD TENSILE STRESSDRxv'E ROD TENSILE STRESSBUSHING PRESSUREVALVE EAR TENSILE STRESSVALVE EAR SHEAR STRESSEAR BOLT SHEAR STRESSEAR BOLT TENSILE STRESS

AT A 16811AT 8 25711.4

327.88717822.11154 '213963.o57543


DRIVE ROD TENSILE STRESS AT *DRIVE ROD TENSILE STRESS AT BPUSHING PRESSUREVALVE EAR TENSILE STRESSVALVE 'EAR SHEAR STRESSEAR BOLT SHEAR STRESSE*R BOLT TENS I LE STRESS

21859. 433432.5426.35222486.41451.9317563.758883.7

~TTACHQgg<yJQBNo. Bzo4cf,<ALE NO. ~dd~llSHEET MO. A Z5

~ ~

csp6T GLOBAL ACCELERATIONS

,39.3.33,5.85

INPUT DATA

GLOBAL G-LEVELS 11.39NORTH VECTOR ANGLES = 90VERTI CAL VECTOR ANGLES= 0 90EAST VECTOR ANGLES = 90

3. 339090

0

5.850

90

LOCAL G-LEVELS

-4.34494E-5 3.33 -2.2316E-5-„4 . 34494E-,5,—,1 . 27029E-5 5. 85

1'1~ 39 -1 . 27029E-5 -2. 231 6E-5

~ * IIp ~ ~ - ~

*

OPERATING DRIVE ~ ROD STPESS AT A 5048. 35OPERATING DRIVE ROD STRESS AT B 7721.14OPERATING CYLINDER BRG PRESSURE -98.4646OPERATING EAR WELD TENSILE STR 5107.51OPERATING EAR WELD SHEAR STRES 631.431OPERATING EAR BOLT SHEAR STRESS 3600.17OPERATItlG EAR BOLT TEhlSILE STR 1340.69

D><AMIC COMPONENTS

DRIVE ROD TENSILE STRESSDRIVE ROD TENSILE STRESSBUSHING PRESSUREEAR WELD TENSILE STRESSEAR WELD SHEAR STRESSEAR BOLT SHEAR STRESSEAR BOLT TENSILE STRESS

AT A 16811AT B 2571'1 ~ 4

327.88721586.22449 '513963 '57543


DRIVE ROD TENSILE STRESSDRIVE ROD, TENSILE STRESSPUSHING PRESSUREEAR WELD TEhlSILE STRESSEAR WELD SHEAR STRESSEAR BOLT SHEAR STRESSEAR BOLT TENSILE STRESS

AT A 21859.4AT B 33432.5

426.35226693.73080 '817563.758883.7 JOB RO.~~4

Fn.e WC.~SHEETXO.~<- <

spaI t"~UT GLOBAL ACCELERATI ONS

.35',3.33,5.85

INPUT DATA

GLOBAL G-LEVELS 11.39NORTH VECTOR ANGLES = 90VERTICAL VECTOR ANGLES= 0 90EAST VECTOR ANGLES = 90

3 '3905'0

0

5. 850

5'0

LOCAL G-LEVELS

-4.34494E-5 3.33-4.3445'4E-5 -1.27025'E-511.35'1.27029E-5

-2.2316E-55.85

-2.2316E-5

OPERATING DRIVE ROD STRESS AT AOPEPATING DRIVE ROD STRESS AT 8OPERATING CYLINDER BRG PRESSUREOPERATING VALVE EAR TENSILE STROPERATING VALVE EAR SHEAR STRESOPERATING EAR BOLT SHEAR STRESSOPERATING EAR BOLT TENS! LE STR

5048.357721 . 14

-98.46464664.2525'7 '143600 . 171340. 65'

i"'--906. 7822. -2.57874E-3

t3f=-2. 57873E-3ml f= 9.89667E-2m2f=-6234. 1

t t 3f=-221 03. 8

DYNAMIC COMPONENTS

DRIVE ROD TENSILE STRESSDRIVE ROD TENSILE STRESSBUSHING PRESSUREVALVE EAR TENSILE STRESSVALVE EAR SHEAR STRESSEAR BOLT SHEAP. STRESSEAR BOLT TENSILE STRESS

sld= 3019.58a2d= 3954.6t3d= 7699.63mid= 2.44083E+5m2d= 58968.3tt3d= 78875.3

AT A 16811AT B 25711.4

327.88717822 F 1

1154 '213963.657543

=D PLUS DYNAMIC COMPONENTS

DRIVE ROD TENSILE STRESS AT A 21859.4DRIUE ROD TEt'lSILE STRESS AT B 33432.5PUSHING PRESSURE 426.352VALUE EAR TENSILE STRESS 22486.4VALVE EAR SHEAR STRESS 1451.93EAR BOLT SHEAP. STRESS 17563.7

EAR BOLT TENSiLE STRESS

sit= 3926 '6=-Zt= 3954.6t3t= 7699.64mlt= 2.44083E+5m2>= 65202 'tt = l.00979E+5

58883.7

II JT GLOBAL ACCELERATIONS EQgQ g f-gQy? 11.37,3.18,5.83

INPUT DATA

GLOBAL G-LEVELS 11.37NOPTH VECTOP. ANGLES = 90VERTICAL VECTOR AIIGLES= 0 90EAST VECTOR ANGLES = 90

3. 189090

0

5.830

90

LOCAL G-LEVELS

-4 '3731E-5 3.18-4 '3731E-5 -1 ~ 21307E-5

11.37 -1 ~ 21307E-5

-2.22397E-55.83

-2.22397E-5

OPERATING DRIVE ROD STRESS AT AOPERATING DRIVE ROD STRESS AT BOPERATING CYLINDER BRG PRESSUREOPERATING EAR MELD TENSILE STROPERATING EAR MELD SHEAR STRESOPERATING EAR BOLT SHEAR STRESSOPERATING EAR BOLT TENSILE STR

D'AMI

C COMPONEIWS

5048.357721 . 14

-98.46465107.51631 .4313600 ~ 171340.69

DRIVE ROD TENSILE STRESSDRIVE ROD TENSILE STRESSBUSHING PRESSUREE*R MELD TENSILE STRESSEAR WELD SHE*R STRESSEAR BOLT SHEAR STRESSEAR BOLT TENSILE STRESS

*T A 16053.7AT B 24553.2

313. 117209672365.9613489.857426.5


DRIVE ROD TENSILE STRESSDRIVE ROD TENSILE STRESSPUSHING PRESSUREEAR MELD TENSILE STRESSEAR MELD SHEAR STRESSEAR BOLT SHEAR STRESSc R BOLT TENSILE STRESS

AT A 21102.1*T B 32274.4

411.58226074.52997.391709058767.2

c&p6I hlPUT GLOBAL ACCELERATI ONS Q Pg Q ('P 2.69,3.09,1.48

Its> JT DATA

GLOBAL G-LEVELS 2.69NORTH VECTOR ANGLES = 90VERTIC*L VECTOR ANGLES= 0 90EAST VECTOR ANGLES = 90

3 ~ 099090

0

1.480

90

LOCAL G-LEVELS

-1.02615E-5 3.09-1.02615E-5 -1 ~ 17874E-52.69, ,. -1 '7874E-5

-5.64575E-61.48

-5.64575E-6

OPERATING DRIVE'OD" STRESS AT A 5048.35OPER*TING DRIVE, ROD,;,STRESS AT B 7721.14OPERATING CYLINDER BRG PRESSURE -98.4646OPERATING EAR WELD TEl'lS I LE STR 5107. 51 ~

OPERATING EAR WELD SHEAR STRES 631 . 431'PERATINGEAR BOLT SHEAR STRESS 3600 . 1 7

OPEPAT ING EAR BOLT TENS I LE STR 1 340 .

69'YNAM

I C COMPONENTS

DP.;: ROD TENSI LE STRESSDR IVE ROD TENS I LE STRESSBUSHING PRESSUREEAR WELD TENSILE STRESSEAR WELD SHE*R STRESSEAR BOLT SHEAR STRESSEAR BOLT TENSILE STRESS

AT A 15599 'AT B 23858.3

304.25616110.81976.811127114173.8


DRIVE ROD TENSILE STRESS AT A 20647 'DRIVE ROD TENSILE STRESS AT B 31579.4PUSHING PRESSURE 402. 72EAR WELD TENSILE STRESS 21218.3EAR WELD SHE*R STRESS 2608.24=AR BOLT SHEAR STRESS 14871.2EAR BOLT TENSILE STPESS .15514. 5

J08 NG.ZtFc4C~

FlLE NQ ~~d. t=

SHE TRQ.MWW

Pl I II i Wl 1 VIII V4VIVli PIIWVI I 4 yOVi I t )4ViC I gOVi4)

sba ic cep3atm

S-BASIC Compi 1 er Versi on 5.4b

701:00v002:000003:000004:000005:000006:000007!000008:000009:000010:000011!000012:000013:000014!000015!000016:000017!000018:000019!000020:000021:000022:000023:000024:000025:00"026:00

J27! 000028: 000029:000030:000031:000032:000033:000034:000035!000036:000037!000038!000039:000040:000041!000042:000043:000044:000045:000046!000047:000048:000049!000050:000051!00

i52t00..a53!000054 000055:000056:000057:000058!00

read lrod,lcg,x,phi,lave,ablt,lrestor e 3read

fst2,ca,ia,cb,ib,aa,ab'estore

4read wao,wbr,ei,e2,e3,e4,e5r estore 5read lrodo, 1 ego, l dr,d,abushrestore 6read a(1,1), a(2, 1 >, a<3,1), a(1,r estore 7read a(1,3), a<2,3), a<3,3>, av (1text 0,& INPUT GLOBAL ACCELERATi npu t b(1), b< 2), b< 3)pr in

t'ext 0,& IliPUT DATA &printprint "GLOBAL G-LEVELSprint "NORTH VECTOP. AliGLESprint "VERTICAL VECTOR ANGLES=print "EAST VECTOR ANGLES

i,l2

2), a(2, 2), a< 3, 2)

), av(2), av(3)IONS &

"; b< 1), b(2), b(3)ia(1)1>,a(2,1),a<3,1)

"la(1 t2) sa(2~2) sa(3<2>")a(1,3),a<2,3),a(3,3)

CYGRAATTACHMENT~os wo.FiiE XO. < ~

SHEET NO. WM~

REM+++++ BIF VALVE AND AIR OPERATOR SEISMIC STRESSREM~+~w++w++w+++++ CEp-V/AO-3A +wwww++++++++w+ww+w++++++REMvar i, j,k = integervar lrod,lcg,x,phi,lave,abl t,l1,12,el,e2,e3,e4,e5 = realvar fs t2, ca, i a y cb

>i b, aa, ab, di, d2, c 1, i 1, c2, i 2=real

var ir odo, l cgo, l dr,d, abush, pbush=r ealvar fcof, fco, ma,mb, si ga, si gb, fcdr, fcdrf,maf, mbf=realvar dear, fcear, fr, f11, f22, l a, c i 12,c i 21,st t3,seml=r ealvar sem2, se t3, sesi, ses2, sr, taui 1, tau22, tauear, aear=r ealvar btens, taub) t, se t3f,semi f,sem2f, fcearf, frf,flif=realvar f22f, st t3f, sesi f, ses2f, sr f, taui f, tau2f, taur f=realvar taubf,btf, dsr,dtaur,dtaub,dbten,dsa,dsb,dpb=t ealvar sdraf,sdr bf,pbushf, taui if, tau22f=realvar wao,wbr, f tr i,watri,si,sif,s2, s2f,mi,mi f,m2=r ealvar m2f s t3s t3f s tt3s tt3f s ib!'swtot=realvar bsi,bs2,bt3,bmi,bm2,btt3=realdim real av(3)dim real wa(3)dim real wb(3)REMREM +++ BURNS 7 ROE EAR FORCES ARE bs1 etc TURN ON WITH K=1+++REMREMdim real a(3,3)dim r eal b(3)dim real glc(3,3>1 data 7.5s 10s ~ 75s 1 '5< 1 ~ 25< ~ 72 data 25,14.46,.531,53.,7.125,.31,1.5,2.53 data 1150.~.875s.46s ~ 648s ~ 138s2 ~ 41si ~ 4

data 399,277,5.25,8.5,28.5,15.,6.8755 data 40.,10.96,26.5,30.5,2.0756 data 90 '90 A >0 '90 '0 A >90 '

data 180.,90.,90.,90.,180.,90.REM DATA 6&7 FOR VALVE/'GLOBAL-G ORIENTATIONS AND WEIGHT VECTORrestorer ead di, d2, c 1, i 1, c2, i 2restore 2

Compilation comp) ete

ce aINPUT BLOB*L *CCELERATIONB PER-4-B4 ( . RI ~)? 4 '7,1.2o,.S6INPUT DATA

GLOBAL G-LEVELSNORTH VECTOR ANGLESVERTICAL UECTOR ANGLES=EAST UECTOP. ANGLESWEIGHT VECTOR ANGLES

4.57909018090

1 ~ 2690

090180

.860

905'090

,, LOCAL.,G-,LEVELS,"~

~-1.74332E-5 " -4.80652E-6 -.S6., 1;,,1 . 74332E-,5, 1 . 26 '3. 28064E-6

„ 4.57 -4 '0652E-6 ~ -3.28064E-6

OPEPATING DRIVE POD STRESS AT A 477.15'8OPEPATING DRIUE ROD STRESS AT B 821.458OPERATING CYLINDER BRG PRESSURE -3 '5613E-4OPERATING VALVE EAR TENSILE STR

1136.52'PERATINGVALVE EAR SHEAR STRES 89.1706OPERATING EAR BOLT SHEAR STRESS 1078.68OP~~ATING EAR BOLT TENSILE STR 525.595

sl f=-3. 4591E-3s2f= 474t3f=-2.57873E-3ml f=-3258. 67m2f=-5.29623E-3tt3f= 4929.17

DYNAM!C COMPONENTS

DRIVE ROD TENSILE STRESSDRIVE ROD TENSILE STRESSBUSHING PRESSUREVALUE EAR TENSILE STRESSVALVE EAR SHEAR STRESSEAR BOLT SHEAR STRESSEAP. BOLT TENSILE STRESS

sl d= 779. 831s2d= 851 . 76t3d= 3089.31mid= 5'7498.om2d= 22785tt = 19965.7

AT A 4341 '7AT B 6640.18

84.67954711.31285.5'353458.8922999.3

JQB No.~~FILE NO.~CT' ~

SHEET VO.M~~

FIXED PLUS DYI'iAMIC COMPONENTS

DP.IVE ROD TENSILE STRESS AT A 4818.7oDRIVE ROD TENSILE STRESS AT B 74o1.64PUSHING PRESSURE 84.6799

VALVE EAR TEtISILE STRESSVALUE EAR SHEAR STRESSEAR BOLT SHEAR STRESSEAR BOLT TENSILE STRESS

~

~

31 t= 7?9.835s2t= 1325.76

3089.32mls= 1.0075?E+5m2t= 22785tt3t= 24894 '

5847.84375.1064537.5723524.9

JoaMo ~8Z 4pgpgp STOICsvsevwo.8->~

Ccnpilatian cceplete

cep3SLOBAL ACCELERATICNS

? 4.5711.26)0.86

INPUT DATA

GLOBAL G"LEVELS = 4.57NORTH VECTOR ANGLES = 90

VERTICAL VECTOR ANGLES= 90

EAST VECTOR NGLES = 180

MiiGHT ViCTOR ANGLES = 90

1.2690

0

90

180

,860

90

90

90

LOCAL G-LEVELSqlI~I ', ': -v

-.1,'74332E"5 -4.80652E-6 ,-.86-1.74332E-5 1.26 -3.28064E-6

4.57 '4.80652i-6'" -3;28064E-6

OPERATING DRIVE ROD STRESS AT A 477.198OPERATING DRIVE ROD STRESS AT 8 821.458OPERATING CYLINDER BRG PRESSURE

-3,75613'PERATING

EAR MELD TENSILE STR 1326.01OPERATING EAR MELD SHEAR STRES 189.188OPERATING EAR BOLT SHEAR STRESS 1078.68OPERATING EAR BOLT TENSILE STR 525.595

DYNANIC CONPNENTS

DRIVE ROD TENSILE STRESS AT A4341.57,'RIVE

ROD TENSILE STRESS AT B 6640.18 ',

BUSHING PRESSURE 84.6795EAR MiLD TENSILE STRESS 6247.02EAR MELD SHEAR STRESS 606.65EAR BOLT SHEAR STRESS 3458.89EAR BOLT TENSILE STRESS 22999.3

FIXED PLUS DYNANIC CNPlNBffS

DRIVE ROD TENSILE STRESS AT A 4818.76DRIVE ROD TENSILE STRESS AT B 7461.64PUSHING PRESSURE 84.6799EAR MELD TENSILE STRESS 7573.03EAR MELD SHEAR STRESS 795.838EAR BOLT SHEAR STRESS 4537.57 ,EAR BOLT TENSILE STRESS 23524.9

sbasic cep4atm

-BASIC Compi 1er Version 5.4b

0001:00OOO2:0O0003:000004:000005:000006:000007'000008:000009:000010:0000112000012:000013:000014:000015:000016:000017'000018:000019:000020:000021: 000022: 000023: 000024: 00

l25'00u026'000027:000028:000029:000030:000031:000032:000033:000034:000035:000036:0000375000038:000039:000040:000041:000042:000043:000044'000045'000046:000047:000048:000049:00nO5O:OO

f51:00u052:000053,:000054:000055:000056:000057:000058:00

read l rod, leg, x, ph i, 1 ave, ab1 t, 1 1, l 2restore 3read fst2,ca,ia,cb,ib,aa,abrestore 4read wao,wbr,ei,e2,e3,e4,e5re tore 5read lrodo,lcgo,ldr,d,abushnestor e 6read a< 1, 1), a(2, 1), a(3, 1), a(1,2), a(2,2), a<3,2)restore 7read a(1,3),a<2,3),a<3,3),av<1),av(2),av(3)text o,h INPUT GLOBAL ACCELERATIONS hinput b,b(2>,b< -)printtext o,h INPUT DATA 6pr intprint "GLOBAL G-LEVELS lb< 1 ) )b(2) fb(3)pr int "NORTH VECTOR ANGLES = ";a(1,1>,a(2,1>,a(3,1)pr i nt "VERTICAL VECTOR ANGLES= " la(1 >2) ~ a(2 s2> ~ a(3s2>print "EAST VECTOR ANGLES = ":a(1.3) .a(2.3) .a(3.3)

ATTACHMENT

408 NO.

FILE NO. OT 0SHEET',:.O.~~

REM++++~ BIF VALVE AND AIR OPERATOR SEISMIC STRESSREM%%%%%%%%%%%%%%% CEP-V/AO-4A %%%%%%%%%+%%%%%%%%%%+i:%%OF+

REMvar i,J,k = integervar lrod,lcg,x,phi,lave,abl t,l1,12,ei,e2,e3,e4,e5 = realvar fst2, ca, ia,cb, ib,aa,ab,di,d2,ci, i1,c2, i2=realvar 1 rodo, 1 ego, l dr, d, abush, pbush=realvar fcof, fco, ma,mb, si ga, si gb, fcdr, fcdrf,maf, mbf=r ealvar dear, fcear, fr, f11, f22, 1 a, c i 12,c i 21, st t3,semi=realvar sem2, se t3, ses1, ses2, sr, tau11, tau22, tauear, aear=r ealvar btens, taubl t, set3f,semlf,sem2f,fcearf, fr f,f11f=realvar f22f,stt3f,sesi f,ses2f,srf, tauif, tau2f, taurf=realvar taubf, btf,, dsr,dtaur, dtaub, dbten, dsa, dsb, dpb=r ealvar sdraf,sdrbf,pbushf, taui 1 f, tau22f=realvar wao,wbr, f tri,watr1,si,si f,s2,s2f,mi,mlf,m2=realvar m2f, t3, t3f, t t3, t t3f, 1 br,wtot=realvar bs 1, bs2, b t3, bm 1, bm2, b t.t3=r e a ldim real av(3)dim real wa(3)dim real wb(3)REMREM ++< BURNS 7 ROE EAP. FORCES ARE bsi etc TURN ON WITH K=1+++REMREMdim real a(3,3)dim real b(3)dim real glc(3,3)1 data 7.5, 10, .75, 1.95, 1.25, .72 data 25,14.46,.531,53.,7.125,.31,1.5,2.53 data 1150.s.875'.46< ~ 648s ~ 138>2 '1si 44 data 399,277,5.25,8.5,28 ',15.,6.8755 data 40.,10.96,26.5,30.5,2.0756 data 90.,-38.,52.,90.,52.,142.7 data 180 ~ s90 ~ s90 ~ s90 ~ s 128 ' 38

'EMDATA 657 FOR VALVMGLOBAL-GORIENTATIONS AND WEIGHT VECTORrestoreread di,d2,ci,ii,c2,i2restore 2

0059:00OC'60:000061'000062:Oi0063:020064:020065:02066:Oi

U067r000068:010069:Oi0070: 000071: 000072: 000073:000074:000075:000076:000077'000078:010079:010080:010081:00

: ~ 0082:000083!000084:000085:000086:000087:000088:000089:000090:00"091:00

392r000093:000094:000095:000096:000097:000098:000099:000100r000101!000102:000103:000104:000105:000106:000107:000108:000109:000110:000111:000112:000113:000114:000115:000116:00

17:00vl 18r000119:000120: 000121:000122:000123:0001 24:00

se t3f=abs< t3f/(4+aear ) )semi f=abs (mlf/(2+d2+ae ar ) >

sem2f=abs(m2f/(2+di+aear))fcearf=t t3f/(2%dear)frf~x+fcearff 1 1 f=-< fcearf +sin(ph i >-frficos(phi ) )f22f~fcear ficos(ph 1 )+frf+s 1 n < ph i )st t3f=abs(f 1 1 f+1 a+c i 12)+abs(f22f+1 a~re i 21)sesl f=abs< si f+c i 12' a/4. )ses2f =abs( s2f +c i 21 +1 a/4. )sr f=se t3f+semi f+sem2f+sesl f+ses2f+ st t3fREM EAR SHEARt au 1 1 f=abs( si f/<4+ac ar ) ) + abs( f 1 1 f/ae ar )tau22f=abs(s2f/(4+aear) )+abs(f 22f/aear >

taur f=( taul 1 f~taui if+ tau22f +tau22f ) ++.5taubf=taur f+aear/abl tPEM E*PBOLT TENSI Oilbtf=(se t3f+seml f+sem2f ) +aear/abl tpr int

A~P{ HiNEMT

pr int "WEIGHT VECTOR ANGLES = ";av(l),av(2),av(3)printfor i=i to 3for j=i to 3

a< j, i )=a(j,, i >+2.+3.1416/360.gl c(j, 1 )~b( 1 ) +cos<a(j, i ) )

next Jnext i

for j=l to 3av ( j ) =av ( j ) +2. w3. 1416/360 ~

nextpr inttex t O,h LOCAL G-LEVELS hprintpr int glc(l, l),glc(1,2),glc(1,3>pr int gl c(2,1),gl c(2,2>,gl c(2,3)print gl c(3,1),gl c<3,2),gl c(3,3)REM WE I GHT COMPONENTSfor j=i to 3wa(j)=wao+cos(av(j>),wb( j ) =wbr +co's< av ( J > )next Jphi=phi+2.+3 ~ 1416/360.la=lave/2cii2=ci/i2c i 21=c2/i 1

aear=ll+12REM CALCULATE EAR FORCES USE BhR LOADS AS OPTION LATERREM FIXED COMPONENTS ARE ALWAYS THERE1 br =1 rod+ 1 cgwa tr 1 = 1 br ~a(1 )/1 rodsi fm=wb< 1 ) +watr 1

wtot=wao+wbrs2f=wb(2>+wa(2>+ fst2t3f~a(3)+wb(3)ml f~»<wa<2)+wb<2)+f st2) +e5-wa(3) +< e3+ 1 cg) -wb(3) +e4m2f=(watrl+wb(1) ) +e5-wa(3) +e2~b(3) +elt t3f~atr I +e3+(wa(2>+f st2>+e2+wb( 1 ) +e4+wb(2) +elfcdr f=lcg+wa(1)/1 rodmaf=fcdrf+(lr od-13.5)mbf=fcdr f+7.125sdr af=fst2/aa+abs<maf ~ca/1 a)sdrbf~f st2/ab+abs(mbf +cb/lb)fcof=l cgo+wa(1)/1 rodop bush f=fcof+< 1 dr+ d)/( d+abush)REM STRESSES FROM FIXED COMPONENTSdear=(dl+dl+d2+d2>++.5

01 25: 000126: 000127: 000128:000129:000130:00nl31:00

132:000133:00Oi 34: 000135! 000136:000137:000138:000139:000140:000141:000142:000143:000144:Oi0145'01Oi 46: 010147:010148:010149:010150: 010151: 010152:Oi0153: 010154:010155:0101 56:01

157:01~158: 010159: 010160:Oi0161:010162:Oi0163:010164:010165:010166:010167:010168:010169:010170:010171:010172:010173:01

";sdraf";sdrbf";pbushf";srf"; taurf"; taubf";btf

pr int"OPERATING DRIVE'OD STRESS AT Apr int"OPERATING DRIVE ROD STRESS AT Bprint"OPERATING CYLINDER BRG PRESSUREprint"OPEPATING VALVE EAR TENSILE STRprint"OPERATING VALVE EAR SHEAR STRESpr i n t"OPERATING EAR BOLT SHEAR STRESSprint"OPERATING EAR BOLT TENSILE STRprintREMREM CALCULATE VARIABLE COMPONENTSREMdsr=0.dtaur=0.dtaub=0.dbten=0.dsa=0.dsb=0.dpb=o ~

for j=l to 3fco=lcgoxwao+glc<i,j)/irodopbush=fco+<ldr+d>/<d+abush)ftri=lbr+wao+glc(l,j)/lrods1=f tr 1+wbr +g l c (1, j )s2=wtot+glc(2,j)t3=wtot+glc(3,j>ml=-wtot+glc(2,J>we5-wao+glc(3,j>+<e3+m2=( f tr 1+wbr+gl c(1, j > ) +e5-<wao+e2+wbr+t t3=f tr 1 +e3+wbrwql c < 1, j ) +e4+gl c(2, j >+(fc dr= i cg~ao+gl c (1, J )/l rodma=fcdr+(lrod-13.5)mb=fcdr+7.125siga=mawca/iasigb=mb+cb/ibREM CALCULATE EAR TENSIOi'iset3=abs(t3/(4+aear))semi~abs(mi/(2+d2+aear))sem2=abs(m2/(2+dl+aear))fcear=tt3/<2+dear)fr=x+fcearf11=-< fcear+s in(ph i )-fr+cos(ph i ) >

f22=fcear icos(phi )+fr+sin(phi )st t3=abs(f 1 1 +1 a+c i 12)+abs(f 22+1 a+c i 21)ses 1 =abs < sl +c i 12+1 a/4. )ses2~abs( s2+c i 21+1 a/4. )sr ~se t3+seml+sem2+sesi+ses2+st t3REM EAR SHEARtau1 i=abs( si/(4. +aear) )+abs< f11/aear )tau22=abs(s2/<4. waear) )+abs(f 22/aear )tauear=( taui 1 +taul 1+ tau22+tau22) ++. 5

1 cg) -wbr+ql c ( 3, j ) +e4e 1 ) +ql c(3, j )wa owe 2+ wbr we 1 )

0174: 010175: 0 1

0176:010177'010178:010179:Oi0180:010181: 01nl 82:01

!83:0101 84:010185!000186:000187:0001 88:000189:000190:00

taubl t=tauear+aear/abl tREM EARBOLT TENSIONbtens~< se t3+seml+sem2) +aear/abl tdsa=dsa+si ga+si gadsb=dsb+sigb+sigbdpb=dpb+pbush+pbushdsr=dsr+srwsrdtaur=dtaur+tauear +taueard t aub=d t aub+ t aub 1 t + t aub 1 tdbten=dbten+btens+btensnext JREM COMBINE STRESSESdsa=dsa++.5dsb=dsb++.5dpb=dpbw+.5dsr=dsr++.5dtaur=dtaur ++ .5

ATTACHMENTJOB NO.

FILENO. Q .6EHEET HQ 8.

0191: 0001<2! 000193: 000194 '00195:000196:00n197:00

i98!000199:000200:000201r000202:000203:000204:000205:000206:000207:000208:000209:000210:00'' -0211-: 000212: 000213:00

'214:000215: 000216:000217:000218:000219:000220:000221:000222:00

223:00224:00

0225:000226:00

AT A";dsaAT 8";dsb

";dpbdsrS


ONENTS h

AT A";dsaAT B";dsb

";dpbI dsl


End of progr am w+++++

d t aub=d t aub++. 5dbten=dbten~+.5printtext Q,h DYNAMIC COMPONENTS hpr intprint "DRIVE ROD TENSILE STRESSprint "DRIVE ROD TENSILE STRESSprint "BUSHING PRESSUREprint "VALVE EAR TENSILE STRESSprint "VALVE EAR SHEAR STRESSprint "EAR BOLT SHEAR STRESSprint "EAR BOLT TENSILE STRESSdsa=dsa+ abs( sdr af )dsb=dsb+ abs( sdr bf )dpb=dpb+abs(pbushf )dsr=dsr+abs(sr f )dtaur =dtaur+abs( taur f )d t aub=d t aub+ abs ( t aub f )dbten=dbten+abs(btf )pr inttex,t -Q,h'IXED PLUS DYNAMIC COMPprintprint "DRIVE ROD TENSILE STRESSprint "DRIVE ROD TENSILE STRESSprint "PUSHING PRESSUREprint "VALVE EAR TENSILE STRESSprint "VALVE EAR SHEAR STRESSprint "EAR BOLT SHEAR STRESSprint "EAR BOLT TENSILE STRESSend

CYGNAATTACHMENTJOB NO. ZO 4RLEXO OT.blSHaEv No.k

~ ~

ep4aINPUT GLOBAL ACCELERATIONS

'? '5,1.34,.86INPUT DATA

GLOBAL G-LEVELS 3 '5NORTH VECTOR ANGLES ' 90VERTICAL VECTOP ANGt ES= 90EAST VECTOR ANGLES = 1804IEIGHT VECTOR ANGLES ~ 90

1.34-38

5290

-128

.865214 2

90-38

LOCAL G-LEVELS

-1.27792E-5 -5.11169E-6 —.862.63983 .824984 -3.28064E-62.06246 -1.05594 -3.28064E-6

OPERATING DRIVE ROD STRESS AT A 477.198OPERATING DRIVE ROD STRESS AT B 821.458OPERATING CYLINDER BRG PRESSURE -3.75613E-4OPERATING VALVE EAR TENSILE STR 1946.57OPERATING VALVE EAR SHEAR STRES 128.033OPERATING EAR BOLT SHEAR STRESS

1548.79'PERATING

EAR BOLT TENSILE STR 4771.17

D.'MIC COMPONENTS

DRIVE ROD TENSILE STRESS ATDRIVE ROD TENSILE STRESS ATBUSHING PRESSUREVALVE EAR TENSILE STRESSVALVE EAR SHEAR STRESSEAR BOLT SHEAR STRESSEAR BOLT TENSILE STRESS

A 4341.57B 6640. 18

84.67955948.81379 '114587.2413246.5

F IXED PLUS DYNAMIC COMPONENTS

DRIVE ROD TENSILE STRESS AT A 4818.76DRIVE ROD TENSILE STRESS AT 8 7461.64PUSHING PRESSURE 84.6799VALVE EAP. TENSILE STRESS 7895.38VALVE EAR SHEAR STRESS 507 '44EAR BOLT SHEAR STRESS 6136 ~ 03EAR BOLT TENSILE STRESS 18017. 7

ATTACRh3ENYJpBNp. ~i~+4FILENP ~dt0/ F.SHEET Np

~

~ ~

~A>B>cep4a

INP GLOBAL ACCELERATIONS35sl ~ 34s ~ 86

INPUT DATA

.GLOBAL G-LEVELSNORTH VECTOR ANGLESVERTICAL VECTOR ANGLES=EAST VECTOR ANGLESWEIGHT VECTOR ANGLES

3 ~ ~5909018090

1 ~ 34-38

5290

-128

.865214290

-38

LOCAL G-LEVELS

-1.27792E-5 -5.11169E-6 —.86, 2.63983 „, .824984 -3 '8064E-6

2.06246 „-1.05594 -3.28064E-6

~ OPERATING.'DRIVE ROD STRESS AT A 477.198OPERATING DRIVE ROD STRESS AT B 821.458OPERATING CYLINDER BRG PRESSURE -3.75613E-4OPERATING EAR MELD TENSILE STR 2592.98OPERATING EAR MELD SHEAR STRES 271.64OPERATING EAR BOLT SHEAR STRESS

1548.79'PERATING

EAR BOLT TENSILE STR 4771.17

D~ 'ANIC CONPONENTS

DRIVE ROD TENSILE STRESS AT ADRIVE ROD TENSILE STRESS AT BBUSHING PRESSUREEAR WELD TENSILE STRESSEAR WELD SHEAR STRESSEAR BOLT SHEAR STPESSEAR BOLT TENSILE STRESS

4341 . 576640. 1884 . 67957493 '2804.5474587 '213246.5


DRIVE ROD TENSILE STRESSDRIVE ROD TENSI LE STRESSPUSHING PRESSUREEAR WELD TENSILE STPESSEAR MELD SHEAR STRESS

'ARBOLT SHEAR STRESSEAR BOLT TENSILE STRESS

AT A 4818.76AT B 7461 '4

84.679910086.11076 '96136.0118017.7

EFFT

B) cep4aINPUT GLOBAL ACCELEPATIONS

>s 3 '5si ~ 34s ~ 86

INPUT DATA

GLOBAL G-LEVELS 3.35NORTH VECTOR ANGLES = 90VERTICAL VECTOR ANGLES= 90EAST VECTOR ANGLES = 180MEIGHT VECTOR ANGLES = 90

1.34-38

5290

-128

.865214290

-38

LOCAL G-LEVELS

-1.27792E-5 -5.11169E-6 —.862.63983 .824984 -3.28064E-62.06246 -1 ~ 05594 -3 '8064E-6

OPERATING DRIVE ROD STRESS AT AOPERATING DRIVE ROD STRESS AT BOPERATING CYLINDER BRG PRESSUREOPERATING VALVE EAR TENSILE STROPERATING VALVE EAR SHEAR STRES

PER*TING EAR BOLT SHEAR STRESSP,'TING EAR BOLT TENSILE STR

477.198821 .458

-3 '5613E-41946.57128.0331548 '94771 .17

slf=-3.4591E-3s2f = 733. 811t3f= 532. 695mi f=-21 826. 4m2f=-3818.52t t3f= 6791 . 56

DYNAMI C COMPONENTS

DRIVE ROD TENSILE STRESS AT A 4341.57DRIVE ROD TENSILE STRESS AT B 6640.18BUSHING PRESSURE 84.6795VALVE EAR TENSILE STRESS 5948.81VALVE EAR SHEAR STRESS 379E211EAR BOLT SHEAR STRESS 4587.24EAR BOLT TENSILE STRESS 13246.5

s 1 d= 779. 831s2d= 1869.64t3d= 1566.33mid= 59205.9m2+- 12442.3

23258.6

ATTACHMENTqOE NO.LZOet

JFE.ENO. STS~ F

SHEET NO.~2

FIXED PLUS DYNAMIC COMPOIIENTS

DPIVE ROD TENSILE STPESS AT A 4818.76DRIVE ROD TENSILE STRESS AT B 7461.64Rl IRHT Nfi PRFRRI IRF Ad.4799

VALVE EAR TENSI LE STRESSVALVE EAR SHEAR STRESSEAR BOLT SHEAR STRESSEAR BOLT TENS I LE STRESS

Gi t= 779. 835s2" 2603.45t3 2099.02mit= 81032.3m2t= 16260.8tt3t= 30050.1

~ ~

7895.38507.2446136 '318017.7

APPENDIX B

VALVE/AIR OPERATOR MODEL FOR

FINAL PIPING RESPONSE G-LEVEL CALCULATION.

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SECTION 4.2

SUMMARY OF RESULTS


CalculationSheet

WPPSS Mechanical Equipment Requalif ication "'.C. Fernandez, 6/13/83Subject Checked By: ~~/Date

30" linder ated Butterfl Valves M.A. Scott 6/13/83System

CAC 6 CEP'tttttat~ Rev. No.

Job No. File No.82044 OS.01.F

Sheet No.

4.1 Conclusions

Four 30" BXF butterfly valves with Miller Fluid Power cylinderoperators have been analyzed for structural integrity

and'perabilityto the seismic and hydrodynamic piping analysisloads. These Burns and Roe piping analysis loads are in theform of operator response g-levels. (see Ref. 9) .

All four EPN's, i.e., CSP-v-l, CSP-V-2, CEP-V-1A and CEP-V-2Aqualify with the following modifications:

1.. Manufacturer supplied A-307 bolts must bereplaced with A-325 bolts.

2. Shear plates must be added to reduce the ear weldstress (see sheets..4.3.30 through 4-3.48 ).

Valve operability was also demonstrated (see p. 4.3.20) whilecylinder operability is addressed in QXD No. 018001.

100e 00


CalculationSheet

WPPSS Mechanical EquipmentSubject 30" Butterfly Valves

CSP 6 CEP 82044File No.

OS.01.F

J.E. Rakowski 3/25/83Checked By: Date

~~Pc-c~ C /~/ ~m

Analysis No.361104

Rev. No. Sheet No.4.2.1

SUMMARY OF RESULTS

Parametric data for the four subject'alves inthis report is given in Table 1.1. Results ofthe regualification analyses, which include acomparison of calculated stresses to the allowablesare given in Table 1.2. Allowable stresses for thevarious material types are given in Table 1.3.

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Project Prepared By: .DateWPPSS Mechanical E ui ment Qualification J.E. Rakowski

" "'50" Butterfly Valves Checked By: Datet .C'. I-~" ~Wc, ~/~ /c"-

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AnalYsis No. 36] lp4 Rev. No.I

82044Sheet No.

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NPPSS EQ '.E.Rakowski 3/25/83checked By:

C g F'ace

System

Analysis No,36110 4

Rev. No,

82044Sheet No.

~ ~

OS. 01/F

SUMMARY TABLE 1.3ALLOWABLESTRESSES

Since operability is required, the stresses for thefaulted condition will be kept below yield+. Thetable below is based on AESC criteria and the yieldstresses at temperature (340'F) from PG. 9 of REF. 4for conservatism.

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CalculationSheet

NPPSS Mechanical Equipment Requalification " L.C. Fernandez 6/13/83Subject

301I

SystemC Sr CEP

Checked By: Dateated Butter f1 Valves M.A. Scott 6/13/83

Job No, File No.82044 'S.01.F

QID 361104Rev. No.

1Sheet'No.

4.3.1

EQUIPMENT REQUALIFICATION FOR QID NO. 361104

BIF 30"CYLINDER OPERATED BUTTERFLY VALVES

4.3.1 IntroductionThe four valves in this file are classified according tothe parametric data given in Summary Table 1.1.

Since hydrodynamic loads apply (Ref. 7) fatigue analyseswere provided for components with the highest stress range.

The analysis method calculates 'stress from north, verticaland east components of operator response g-levels. Theseg-levels ar'e the result of the Burns ij'- Roe piping analyses.(Ref. 9)

An SRSS analysis was set up in a computer program for eachvalue assembly in its specific orientation. The SRSS istaken', at the maximum stress level due to seismic g-loading.Operating loads due to seating torque force and deadweight are combined with the seismic stress by absolutesum. 'alve ear bending stress components due to any oneresponse g-level component are combined by absolute sum.

100s tO


Calculat|onSheet

'QNSS Prepared By. DateMechanical Equipment Qualification J.E.Rakowski 1/10/83Subject30" Butterfl Valves

Checked By„ t „ i ~ DateL. ( . t ~i~ tie'A.ti'/-7Ir3

SystemCSP & CEP

Job No.82044

File ttro.

OS~01 F

"N'VP84 Rev. No.1

Sheet No.4 3

The computer analysis addresses only the more highlystressed components in the valve operator assembly.Separate analysis is given for the remaining compo-nents using a simpler approach with upper bound loads.This applies to all valve operator EPN's in QID 361106(24" Valve/8" cylinders) and QXD 361104 (30" valves/10"operators). Hand calculations which check selected por-tions of computer output is shown in Appendix C.

Appendix B of this section describes the air operatormass/stiffness model which was incorporated in thefinal piping analysis for calculation of operator re-sponse g-levels. The computer program includes an op-tion for using the valve ear forces and moments whichare directly output from the piping analysis with thevalve/operator model included. This was not finally

'tilized,however, to qualify the subject equipment.

The equipment locations and elevations were taken fromthe P&ID's in section 6.0. Natural frequency calcu-lations are given for the air operator assembliesin Section 4.3.2.1.Preliminary analyses were performed which showedthat, for operator response g-levels greater than ap-proximately 3 g's, the air cylinder spring preloadforce would be exceeded and hence some disk flutterwould occur when the valve is in the open position.The calculation in section 4.3.2.2 shows that the mag-nitude of the valve disk flutter vibration angle dueto upper bound g-levels which occur in the hydro-dynamic frequency range is approximately 6 degrees.This flutter was evaluated to have no detrimentaleffect'n system safety function as noted in Reference5.

Valve operability was addressed in the following manner.All valves have a Use Code of 1-3. 't is noted thatthe g-levels pertaining to CSP-V-2 envelope CEP-V-1A andCEP-V-2A.

O.IIIIIIIIIIIIIIIIIIIIIIIIIIIIII

CalculationSheet

Prospect

Prepared By; DateVPPSS Mechanical E ui ment ualification J.E.Rakowski 1 10Subject

ButterfChecked By: Date

L 0a 4 JAl&ILGe ~ l '76 ~

System

Sf@4'ev. No

Job No.

Sheet No,4 3 3

Fite Qd.

RJ3~'or

valves CSP-V-3. and 2, which must operate from opento fail closed during an event, the following additionalevaluations were made:

1) Dynamic flow torques were assessed per Ref. 3and found to be less than the seating torquewhich controlled the equipment ~tresses.Furthermore these flow torques tend to movethe valve disk toward the fail-closed position,as noted in the above report.

2) The details of BTF drawing 206 767> parts ofwhich are shown in figures 1.1 and 1.2, allowthe following conclusions to be made for valveoperability:A) Figure 1.1 shows that thrust bearings are

part of the shaft bearing design. Thisdesign prevents lateral movement of thedisk in the direction of the shaft to eli-minate interference with the valve bodywhen closing. Further, it is noted onPage 26 of Ref. 3 that frictional'torquesin the shaft bearing system are negligible.

B) Figures 1.1 and 1.2 show a circul'ar valve'cross section having an internal rim withinwhich the valve seats in the closed posi-tion. The only mechanism remaining to af-fect valve closing which can be postulatedis out-of-round distortion of the sectiondue to DBE piping loads and dynamic loadson the valve.

These loads were accounted for in Ref. 4 in the overallvalve sizing calculations, where analysis showed thatthe stress intensity in the 0.5 inch thick valve bodyremained below 1.2 Sm, or approximately 0.8 of yield.Stress contribution from dynamic loads on the valveand operator were relatively small. Further, as shownin the figures:

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CalculationSheet

8'LES Mechanical Equipment Qualification " '" "'J.E.Rakowski 1/10/S3Subjec!30 'utterfly Valves

Checked By.'atel.e. FSystemCEP and CSPAnalysis No, Rev. No.

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Job No,82044

File No'.

OS.01 FAnalysis No.

361104Rev. No Sheet No. 4 3

The valve seat forms a heavily reinforced section madeup of the valve body, internal hub and external flanges(including the mating flange of the piping) . Hence thestress levels in this section are much lower than inthe valve body and hence no distortion of the sectioncould occur to affect seating of the valve. Valveflange dimensions are given below. Note the relativelylarge internal radial clearance of 1/8 inch.

2. Stress analysis of the valve extended structures aregiven in this report. Air operator operability isaddressed in QZD 018001.

The design data used in the analyses are given inSummary Table 1.1 (pipe-orientations and elevationsare taken from the appropriate P&ZD's in Section 6.0) .Other pertinant data is given below.

1), Spring preload per communication reportin Section 7.0 of QZD 018001 are:

Fail Closed Preload = 2800

Final = 4800

2) Cylinder C.G.'s shown on the following sketchesrepresent data received from BZF in the communi-cation report of Section 7.0 of QZD 018001'.

3) Closing torque values are taken from Ref. 3.

4) Valve component dimensions: (Ref. Feb. 10, 11/83communication report — Section 7)

Flange: width = 3.88nr thickness - 2.625"Radial Clearance Disk/Seat 1/8"

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CalculationSheet

Pr'oject Prepared By.'ateWPPSS Mechanical E ui ment Qualification J.E. Rakowski 3/25/83

Subject „lE

30" Butterfl Valves "Checked By„~l. C, F ~~rI.;c

Dated/0 P ICE~

SystemCSP and CEP

Analysis No.361104

Rev. No.

Job,No.

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Subject30" Butterfly Valves Checked By: DateL C F~ c "tzvbS

SystemCSP and CEP

Job No,82044

File o,OS.01/F

Rev. No,Analysis No. Sheet No. 4 3 /\361104

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'0n Butterfly Valves

ESP and CEP

Checked By„ /} 1 /

'82044

4, >D.,iQ

OS.01/PAnalysis No.

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SystemCSP and CEP

Analysis No.361104

Rev. No.

Subject30" Butterfly ValvesJob No.

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Analysis No.361104

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Project Prepared By: DateWPPSS Mechanical Equi ment Qualification J.E. Rakowski 3/25/83

Subiect30" Butterfl Valves

Checked By DateI- .0. 4~t ~kr "I&tr'rS

SystemCSP and CEP

Analysis No,

361104Rev..No,

|

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Sheet No. 4

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e'S

Mechanical EquiPment Qualification ' J.E. Rakowsgi 1/10/83Subiect30" Butterfl Valves

Checkec Sy:L ~ F

~, Oate

SystemCSP and CEP

Analysis No36110 4

Re .No,

Job No, File No82044 O.S.01 F

Sheet No.4 3 14

~ad-'l -!'-!~=C'!3$ /6 3

4.3.2.3 STRESS ANALYSIS

The procedures for the analysis of the subject valvesare outlined below:

2.

3.

Recalculate the valve appurtenance stressesaddressed in Ref. 4 using response g-levelsfrom the Burns a Roe piping analysis. Incorporatethe current seating torque given in Ref. 3.Compare stresses to the lower yield strengthsin Summary Table 1.3.

If faulted condition stresses exceed the upsetcondition allowable stresses, repeat the analy-sis for the affected components using upsetaccelerations from the piping analysis.

Perform a fatigue analysis on significantlystressed components. Determine allowablealternating stress ranges from AISC 8th Edition,Appendix B, noting commentary.

~ tj

The fatigue analysis is to be performed only for thoseEPN's subject to hydrodynamic loads ~ The number ofrespective load cycles is given below.

LOAD COMBINATIONS & STRESS CYCLES

The following table lists the load combinations and.the nubmer of expected stress cycles for each com-bination. (From tHe design criteria)

Combination ~Cc leel. SRV Alone 3 (4500) =135002. OBE+SRV 50

3. OBE+SRV+Chugging 20004. SSE+SRV+Chugging/

SSE+AP 10

Note: Load combination N4 with 15560 cycles can beused to conservatively bound all combinations.

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ProjectWPPSS -Mechanical Equi ment

l'repared By: Date3 25 83

Sublect30" Butte fl V v

'hecked By. r Datel- C. /~mar 4I2..

SystemCSP and CEP

Analysis No.361104

Re,No)

Job No. File N6. I

2Sheet No.

4 3 15

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SystemCSP and CEP

Job No.82

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Analysis No. Rev. No, Sheet No.4 3 j

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Analysis No361104

Rev. No,

Subtect30" Butterfl Valves

SystemCSP and CEP

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Job No.

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0'Obtect

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System 4 Job No. File No. ~CSP and CEP

Analysis No361104

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Project Prepared By: DateWPPSS Mechanical Equipment Qualification J.E. Rakowski 3/25/33

Subject 30" Butterfly Valves c. .i~w~lwc( r/2rir5System


361104Re . No.

Job No. File No.82044

St)ee(No. 4 3 ]9

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Prorect Prepared By.'ateWPPSS Mechanical Eoui~ment ualification J.E. Rakowski 1 10 83

Suhiect30." Butt rf1 Valves

System Jot'o. File Nor.

Checked By: Datej .( . I'~neer g(rr l//2q/ca

Rev. No.~

Sheet No.4 3 20

Disc

The stressesRef. 4 to beload. SincePSI will notcelerations,

in the disc were shown on page 51 ofdue almost entirely to the pressurethe stress 'found in Ref. 4 of 4540change significantly for the new ac-the disc is acceptable.

The stress in these pins is due only to the seatingtorque. The stress in Ref. 4, page 53, is 11265PSI and is therefore acceptable. For the new, lowerseating torque, the stress becomes 8985 PSI.

Analysis for:'rive Rod, cylinder bushing pressure,valve ears and valve ear bolts.

Method It Use element forces and moments outputfrom the piping analysis (Summary Table1.1) and the absolute sum of stresses.The conservatism of SRSS summing of thecomponent stresses cannot be assuredbecause the independence of the sixelement forces (/moments) cannot be de-termined without analysis of modal par-ticipation.

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CalculationSheet

Project ~'repared By: QateMechanical .Equipment Qualification J.E. Rakowskz 1/10/83Subject30'utterfl Valves L.C. F~~~ q/tqj+System

d PRev, No

Job No.

Sheet No.

82044File No)

OS.01 F

Method IIt Use the north, east and vertical operatoraccelerations output from the pipinganalysis. Absolute sum for stresseswith each component then SRSS over re-sults for N,E and V.

Note!: Analysis of the distribution of stress on4 valve ears to predict the maximum tensilestress cannot confirm a maximum value lowerthan the absolute. sum of the elemental ten-sil stresses due to the six forces (fromone acceleration direction, N,E or V). There-fore the absolute sum will be used at this level.

Note 2: Add stress due to the vector sum of deadweightplus seating torque force after above SRSScombinations are perfoimed. (ABS)

Note 3: 10" A/0 parameters are shown for use in QID361104.

Anal sis of Seatin Tor ue Forces

100d Oc

1) Seating Torque loads control the stress in thevalve lever arm, keyway, shaft and taper pins. Thesestresses were less than allowables for the valves ofseating torque given in Ref. 3, for all valves.

2) For valve EPN's which are Fail-Open with Use-Code 2, no seating torque forces are applied duringthe faulted and upset conditions (CSP-V-5,6).

3) For the Fail-Closed valves, the forces at thetrunnion pins are shown below, along the cylinderaxis, for +2-axis g-loading:

t2 LaQld Mta

an clevis/va.lvc s4&I

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Proiect Preparea By. DareWPPSS Hechanical E ui ment ualification J.E. Rakowski ] /10/83

Subject" Bu terf v Valve

System Job No.

l . C. F~)t,ut 'I jrz+j/~>File No.

OS'NY78'4Rev. No, Sheet No. 4 3

As the bracket deflects in +2, under dynamic loads,the seating torque force is releived. The extentof relief depends on the relative stiffness of thebracket and valve ears relative to the valve seat.Since the -steel backets'and ears are very stiff inthis'direction, little relief can be expected.Hence seating torque forces will be added as anABS sum to the valve ears. However, seating torqueforce will oppose operator weight when the bracketshangs downward from horizontal pipes.

0 erator Drive Rod

Drive rod dyanmic stress is due only to g becauseg and g forces are taken out by trunnion pins.A3d seating torque stresses. 7.I25

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Project Prepared By'ateWPPSS Mechanical Equi ment Qualification J.E. Rakowski 3/25/83

Sublect 30" Butterfly ValvesSystem

CSP and CEP

Checked By: / ~ F' Da'e

g/~ltd< g

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Analysis No.361104

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sheet No, 4 3 24

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Prepared By: DateJ.E. Rakowski 3/25/83

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Subject30" Butterfl

SystemCSP and CEP

ValvesJob No. File No.

OS.01

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Rev, No.I

Analysis No. Sheet No361104 ~ ~

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Subject,30" Butterfl

'J,

Valves L. t.'=e.~«System


361104Re.No.

~

Job No.2

Sheet No, 4 3 27

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Checked By:, ~ . Date. (., I . - ' rt x t r l ~I r.i ~ (( 6ISeZ

SystemCSP and CEP

Analysis'o3 11

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Job No,

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Project Prepared By-WPPSS Mechanical E ui ment Qualification J.E 3/25/83

Subject30" Butterfl

SystemCSP and CEP

Analysis No.361104

Valves

Rev. No.I

Checked By:L ~ F

'a«@~I ~t~

Job No. File No.

82044StteetNo. 4 3 29

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CalculationSheet

WPPSS ~hanical Ecpxiprent ~lification ~ M.A. Scott ~ 6/15/83Subject Checked By.'~gW Oate

30" linder rated Butterfl Valves 6 .d. Fernandez 6/15/83System

P dgagl-'ysii eat

QID 361104Rev. No.

Job No.82044

Sheet No.4.3.30

File No.OS.Ol.F

Section 4.3.4 — Ear Support Weld Stress

Comparison of a similar file (QZD No. 361106) to this file noted theunconservative assumption of considering the bracket support ears tobe a guided cantilever (fixed-fixed) . The resulting ear weld stressesexceeded the allowable stresses. The ear weld stresses can be loweredby the addition of- shear plates to stiffen the whole assembly. Theresulting weld stresses (both existing and modified) are to be keptwithin the fatigue allowable stress, i.e., Q stress range. Theallowable fatigue stress range from AISC for fillet welds in shearwith less than 20000 cycles of loading is:

SR = (1.5)(15000)=22500 PSIThis includes the 50% increase due to fewer than 20000 cycles. Theweld stresses are calculated using faulted loads. These loads produceless than one percent of the total 15560 cycles of faulted/hydrodynami~loading. Since the upset and emergency conditions are considerablylower in magnitude, small margins of overstress in fatigue will betolerated for faulted stress levels. The following allowables willbe adhered to in the ear weld stress calculations.Allowable stress for welds for faulted conditions:

liow 1.6 (0.3) Fu = 28800 PSI

Allowable stress for welds subject to fatigue.allowable stress range of AISC Appendix B:

=1. 25 (1. 5) (15) = 14 KSIfat 2

This is 4 the

1.25 = 25% increase due to previous comments

1.5 = 50% increase due to AXSC commentary

'lees.00

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CalculationSheet

ProjectNPPSS Mechanical

Prepared By: ~Ac Dateification M.A. Scott 6/15/83Subject Checked By: Q(p Date

30" linder ated Butterf1 Valves L.C. Fernandez 6 15 83System

CSP. and CEP

QID 361104Rev. No.

Job No.82044

Sheet No.4;3.31

File NoOS.01.F

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Subject30" Butterfl Val es

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Job No.

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File No.


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„ProjectWPPSS Mechanical ' '

Subject30" linder rated tte f

Prepared By: ~a+~r batelification M.A. Scott 6 15 83Checked By: Date

VSystem

CSP and CEP

Rev. No.

Job No.82044

Sheet No.

File No.OS. 01.F

2

CalculationSheet

Project Prepared By.'GVOateWPPSS Mechanical Equi@rent Bequalification M.A. Scott '/15/83

Subject Checked By: prQ Date30" linder ated Butterfl Valves L.C. Fernandez

SystemCSP and CEP

QID 361104Rev, No.

Job No.

Sheet No.~ ~ 3

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NPPSS Mechanical Bpiipnent Requalification M.A. Scott ~ 6/15/83Subject 30" Cylinder Operated Butterfly Valves

Checked By: ~ateL.C. Fernandez 6 15 83

SystemCSP and CEP

Acne~~.QID 361104

Rev. No.

Job No.82044

Sheet No.4 3 35

File No.

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ProjectWPPSS Mechanical

Prepared By. ~t~w+ tDatet alification M.A. Scott ~' 15 83Subject '0" linderSystem

CSP and CEP

QQD 361104Rev. No.

Job No.82044,

Sheet No.~ ~

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'" NPPSS Mechanical Equignent Requa1ification "'.A. Scott ~'/15/83

AR~CP,ID 361104

Rev, No.

Subject30" Cylinder Operated Butterfly Valves

SystemCSP and CEP

Job No.82044

S eetNo.4 3 37

Fite No.OS. 01.F

Checked By.'ate. L.C. Fernandez 6/15/83

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WPPSS Mechanical Bpipnent Requalification "'.A. Scott+~+ 6/15/83Subject e Checked By: ~~ Oate30" Cylinder Operated Butterfly Valves L.C. Fernandei 6/15/83System

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DWPPSS Mechanical Equipment ~lification '.A. Scott '/15/83

Subject30" Cylinder Operated Butterfl Valves

Checked By'. OateL.C. Fernan8ez 6/15/83

SystemCSP and CEP

ID 361104Rev. No.

Job No.82044

Sheet No.4 3 40

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QID 361104Rev. No.

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Job No.82044

Sheet No.4 ~ 3.41

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WPPSS Mechanical Equiprent Requalification '.A. Scott"" '~, 6/15/83Subject Checked By: +C~Date

30" linder ated Butterf1 Valves, L.C. Fernandez 6 15 83System

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QID 361104Rev. No.

1

Job No.82044

Sheet o.4 3 42

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Project Prepared By: ~„'i,DateWPPSS Mechanical Equipnent Hequalification M.A. Scott ""4 6/15/83

Subject30 II linder

Checked By; Dateated Butterfl Valves L.C. Fernanddz 6 15 8

SystemCSP and CEP

~n5~M%HQID 361104

Rev. No.

Job No.

Sheet No.~ ~

File No.

Tdr o)s'L2O WWS c 4 WD o ( PR ~/4CQP —„Q- 10. + -DlPc~77Cr J /~ C~dcA-755.rf

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Subject30" linder

SystemCSP and CEP

Checked By: ~Daterated Butterf1 Valves L.C. Fernandez

Job No. File No.

QID 361104Rev. No. Sheet No.

4.3.44

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hasted~QID 361104

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Subject30u

Checked By: Oatelinder ated Butterfl Valves L..Fdz

Sy'tem

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Job No.

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Subject30" Cylinder Operated Butterfly Valves

SystemCSP and CEP

Job No.82044

Fiie No,OS.01.F

Checked By: ~ DateL.C. Fernandez 6/15/83

QID 361104Rev. No. Sheet No

4.3.47

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t, lification M.A. Scott Wt 6 15 83Subject

30" linder Operated Butterfl ValvesSystem

P

Checked By:L.

Job No. Fite No.

ate

%6iaijsm+a=.ID 361104

Rev. No. Sheet No/4 3 48

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CalculationSheet

Pro'tectWPPSS Mechanica c i Prepared By. Date

Z.E. RakowskiSubject

rr

System Job No: File No82044 0

Z]'-le"

Analysis No361104

Rev, No.1

Sheet No~ ~

Section 4.3.5 —Fati ue Anal sis

Discussion

The operator and bracket assembly are not part of the pressureboundary, therefore, the fatigue analysis will be performed inaccordance with Appendix B of the AISC Manual for Steel Con-struction. The following assumptions apply to the fatigueanalysis.

1) Faulted stresses (based on piping-analysis accelerations)will be used. This is necessary to insure operabilityafter a design basis event.

2) The actual stresses used will be the ones calculatedin Section 4.3.

3) If the alternating portion of the stress has been cal-culated separately only this part will be used. If theoperating loads (i.e. seating torque effects) are al-ready included in the stress analysis it will.be con-servative to use the calculated stress value. As longas no failures occur, the operating stress does notneed to be extracted.

4) The al3owable stress will be based on Table B3 of Appen-dix B in the AISC Manual of Steel Construction.

5) A factor of 1.5 will be applied to the allowable be-cause of the low number of cycles. (Per Section 1.7of the Commentary on the AISC Manual).

6) The actual stress range is taken as 2 times the maxi-mum stress for components subject to alternatingtension and-compression.

icos 00


CalculationSheet

Protect Prepared By.'ateJ.E.Rakowski

Subtect Butterfl ValvesSystem Job f4o.

82044File No.

0 .01 F

g. c ~ F~~~ ~ j~Q jg~Q

SBb Rev. No Sheet No.4 3 50

7) Bracket bolting is assumed to be properly tightened and willnot be considered for fatigue per Section B3.1 of the AISCManual.

The table on the following page gives the calculated stress range,stress category, and allowable for the critical components. The fol-lowing page gives excerpts from Appendix B of the AISC Manual showingthe descriptions of the relevent stress 'categories.


CalculationSheet

Prepar'ed By: OateWPPSS Mechanical E ui ment ualification J.E. Rakowski 1/10/83

Sobject3'0" Butterflv Valves

System Job No.

L., C. F~m~i~', p jL~ (E3

File No.

'5L'|'Mp4 Rev, No. Sheet No 4 3 51

Fati ue Anal sis (cont.)

ITEMSTRESS

TYPESTRESS

(PSI)STRESS

RANGE (PSI)STRESS

CATEGORY1.5 x.ALLOW(FROM AISt")

TRUNNION PIN

DRIVE ROD MAX

SUPPORT FARS

410

SEE TA LE 1.2

SEE TAB E 1.2

MAIN SHAFT91277158

1825414316

90000

NOTES:

(/) Assume shear stress on nominal area of a studtype shear connection.

/

Note that this comparison includes all of the load combinations in oneconservative comparison using the maximum stress and the total numberof cycles ( 3. x 4500 + 2000 + 60 = 15560).

1006 00

Calculation SheetPrepared By Date

zs a. J k. ik~IIIIIIIIIIIIIIIIIIIIIIIIIIIIII

Project 'r

50 o'rT -'p r I + VC

Sysrem

Analysis No. +4'll+ + . Rev, No

Job No File No

Date

ly / SZ.

azQR4- Qs elSneet No.

4.3.52

DENT;

I HE j t9$ LE 8 Ei o ~ 9 +5 BEEN ~H DEADER 'F 2 n&IPPG'Pfb~x 5 oF 7 H e Hx'sc Qt4Hex t. aP ZTEFcC onsrauc rx on. TH E c.pjsEZ uS Eg g as H pj's aC>

Ld z'v H <e RRRouJ.

GeneralCondi-

tion

Plainmaterial

Built-upmembers

hiechani ~

callyfastenedconnec-tions

httach.ments

Situation

Base metal with rolled or cleaned sur-faces.

Base metal and weld metal in mem.hers, without attachments, built-up ofplates or shapes connected by contin-uous full.or partial. penetration groovewelds or continuous filletwelds parallelto the direction of applied stress.

Calculated flexural stress, fs, in basemetal at toe ofwelds on girder webs orilanges adjacent to welded transversestiffeners.

Base metal at end of partial.lengthwelded cover plates having square ortapered ends, with or without «aidsacross the ends.

Base metal at gross section of high-strength. bolted friction.type connec-tions, except connections subject tostress reversal and axially loaded joints

. which induce outwf-plane bending inconnected material.

Base metal at net section ofother me.chanically fastened joints.

Base metal at net section of high-strength bolted bearing connections.

Shear stress on nominal area of stud.type shear connectors.

Kind ofStress'

or Rev.

T or Rev.

T or Rev.

Tor Rev.

Tor Rev.

Tor Rev.

Tor Rev.

StressCate-gory(See

TableB3l

B

D

B

~~ (g0 QQb)

~ (~~,s 5


CalculationSheet

ProjectWPPSS Mechanical E ui ment

Prepared By:ualification 3/25/83Subject Checked By: Date

30" Butterfl Valve '. C. Fe ~~ q/„qI'it~System

CSP and CEPAnalysis No 361104 Rev. No.

Job No.82

Sheet No.4 3 53

File No.

4 ' REFERENCES

1) BXF Drawings

Drawing IA-206763

Revo DescriptionGeneral Arrangement

CEP-625-10

CEP-625-11.12 H

From Reactor NozzleX-3 to SGT-FU-1A, 1B


C-26095 Model A-83B Cylinder

A-206767 Valve Assembly

DOC-D-220-0310-IR-66 Tube errection iso-metric

D-207110 Valve Data Sheet

M-144

CSP-807-3.4

General Arrangmentlan mis level

Containment purgeair su 1 s stem

tcos.00


CalculationSheet

WPPSS Mechanical Equipment Qualifica~tVon J.E. Rakowski 3/25/83Subject 30" Butterfl ValvesSystem

CSP and CEPJob No, File No.

OS.01/F

Checked By: DateI-.c'. Fe.~~~~, +/:~„'~ ".

Anatysis No.3 6 ] 1 0 4

Rev, No.1

Sheet No.4 3 54

Reference cont'n

Formulas for Natural Frequency and Mode Shapes,Robert D. BlevinsVan Nostrand Reinhold Company1979 Edition

3) BIF Report TR-27234 and TR-27235, "Dynamic TorqueCalculation of Butterfly Valve; Sizes 24 and 30 inch",dated November 10, 1982.

4) Report TR-74-8 by McPherson Assoc., Inc., "Design &Seismic Analysis 30" Cylinder operated Butterfly Valve".(Rev. 1) 12/31/75.

5) WPPSS letter to Cygna Energy Services, GE-02-RWH-018,12/17/82.

6)

7)

8)

WPPSS, WNP-2 SRM Equipment List Summary Sheets dated2/10/83.

Cygna Energy Services, Equipment Qualification WalkdownVerification Form dated 7/14/82 and 7/19/82.

Cygna Energy Services, "Project Manual Design Criteria,"DC-1, Rev. 1, 10/82.

9) Burns and Roe Revised Piping Analysis Loads forCSP-V-1 and 2 (dated 4/12/83) and CEP-V-lA and 1B(dated ll/15/82) .

10) Communications Report, R. Ricappito of BIF and J. Rakowskiof CES, nB1F Valve Dimensions", 2/ll/83

'l000 Oo

APPENDIX A

COMPILED PROGRAMS AND RESULTS FOR

CSP-V-1

CSP-V-2

CVGNAATTAC>!iAC,ViT

V OS IIO.~«<FILE No ~0~. oI. F

SHEE7IIO.~4'

sbasi c csp12tm

S-BASIC Comp i 1 er Version 5.4b

uooi:000002:000003:00OOO4:OO0005:000006:000007:000008:000009:000010ioo0011:000012:000013:000014:000015:000016:000017:000018:000019:000020:000021: 000022:000023:000024:00

= "025:00326'00

0027:000028:000029:000030:000031:000032:000033:000034:000035:000036:000037:000038:000039ioo0040ioo0041:000042:000043:000044'000045'000046:000047:000048:000049:000050:00

'151'00vu52:000053:000054:000055:000056:000057'000058:00

r estore 3r ead fst2,ca, i a,cb, ib,aa,abres tor e 4read wao,wbr,ei,e2,e3,e4,e5restore 5read lr odo,lcgo,ldr sd,abushr estore 6read a< 1, 1), a(2, 1 >, a(3, 1), a(1, 2), a(2,2), a< 3, 2)restore 7r ead a< 1,3), a(2,3), a(3,3), av(1 >, av(2), av < 3)text 0 rh INPUT GLOBAL ACCELERATIOt iS 8c

i npu t 6< 1), b(2), b(3)printtex t 0 s8c INPUT DATA 8c

printprint "GLOBAL G-LEVELS ";b(1> sb(2) sb<3)print "tiORTH VECTOR AhiGLES = ";a(i, l),a(2,1),a(3,1)pr i n t "VEPTICAL VECTOR ANGLES= "; a< 1 s 2) s a< 2 s 2) s a< 3 s 2)

Aii.~~.CH~'."r'QB

NQ.9~~t'-ILE hs0 os. 0 t. F

SH=.KV JQ. < '«

REtlJJ++++ BIF VALVE AtiD AIR OPERATOR SEISI"iIC STRESSCSP-V/'AO-1/2

REt"t+++++++++++++++ 10 IhiCH AO PARAMETERSREt'1

var i,j,k = inteoervar 1 rod, 1 cg,x,phi, 1 ave,abl t,11,12,el,e2,e3,e4,e5 = r ealvar fst2, ca, ia,cbs ib,aa,ab,dl,d2,cl, ii,c2, i 2=realvar lrodo, 1 ego, 1 dr,d, abush, pbush=r ealvar fcof, fco, ma,mb, siga, sigb, fcdr, fcdrf,maf, mbf=realvar dear, fcear, fr, f 1 1, f22,1a, c i 12,c i 21,st t3, seml=r ealvar sem2,set3,sesl,ses2,sr, taul 1, tau22, tauear,aear=realvar btens, taubl t, se t3f, semi f, sem2f, fcear f, f r f, f 11 f=r ealvar f22f,stt3f,sesl f,ses2f,srf, tauif, tau2f, taur f=r ealvar taubf, btf, dsr, dtaur, dtaub, dbten,dsa, dsb, dpb=realvar sdraf,sdrbf,pbushf, taui if, tau22f=r ealvar wao,wbr, f tr1,watr1,si, si f, s2, s2f,mi,mi f,m2=realvar m2f, t3, t3f, t t3, t t3f, 1 br,wtot=realvar bsisbs2sbt3sbmlsbm2sbtt3=r ealdim real av(3)dim real wa<3)dim real wb(3)RENREM ss+ss BURNS 7 ROE EAR FORCES ARE bsi etc TURN Ohi WITH K=is'++REMREI"1

dim real a(3,3)dim r eal b(3)dim real glc(3,3)1 data 9.5,,10.5, .88, 3.94r 1.50,1.342 . data 25,21.50,.488,48.,4.8S,.627,1.75,3.03 data 1847 't 875s i6s ~ 648s ~ 138s2 ~ 41si 44 data 593.,321.,S.25,8.5,28.5,15.,7.755 data 40 ~ s16 ~ 2Ss26 ~ 5s43 ~ s2 ~ 0756 data 135 ~ s90 ~ r135 ~ s90 ~ r180 ~ r90 ~

7 data 45 ~ s90 ~ r135 ~ r90 ~ s0 ~ s90 ~

REM DAT* 657 FOR VALVMGLOBAL-GORIENTATIONS AND WEIGHT VECTORrestor er ead dl,d2,cl, i l,c2s i 2restore 2read lrod,lcg,x,phi,lave,ablt,11,12

oo592ao0060:000061:000062:000063:010064:02

~065:O2~')66:02

~0672010068:000069:Oi0070:010071: 000072: 000073: 000074: 000075:000076:0000772000078:00OQ79:010080:010081:Oi0082:000083:0000842000085:000086:000087:0000882000089:000090200

091:00392:00

0093:000094 000095:0000962000097:000098:000099:000100:000101:0001022000103:000104:000105:000106:000107:000108:000109:000110:00Oili:0001122000113:000114:000115:000116:00

2~ 17:00218200119:00

0120:00- 0121:000122:000123:00o124:ao

";a<1,3),a(2,3),a<3,3)";av(i),av(2>,av(3)

CVGiNAATTACH»'ATJ08 ~'10. ~So~Fli.E NO. O~

SHEET N0,M4~

p r i n t " EAST VECTOR ANGLESpr int "WEIGHT VECTOR AiiGLESprintfor i=1 to 3for j=l to 3

a( j, i ) =a( j, i ) +2. ~3. 141 &'360 .glc(j,i)=b(i)icos(a<j,i)>

next jnext i

for j=i to 3av < j ) =av ( j ) +2. +3. 1416/360 .nextprintt e x t 0, h LOCAL G-LEVELS 8c

printpr int ql c<1,1),gl c(1,2),gl c<1,3)print gl c(2,1),gl c(2,2),ql c(2,3)pr i n t gl c (3, 1 >, gl c (3,2), gl c(3,3)REM WE I GHT COMPONENTSfor j=i to 3wa( j )~ao+cos(av( j) )wb( j )=wbr icos(av( j ) )n.ex t jph i =ph i +2. +3. 141 &'360 .1 a= 1 av e/2c i 12=c lli 2c i 21=cd'i 1

aear=l 1 +12REM CALCULATE EAR FORCES USE BhR LOADS AS OPTION LATERREM FIXED COMPONENTS ARE ALWAYS THERElbr=lrod+lcgwa tr 1 = l br ea�( 1) 11 rodsi f=wb( 1 )+watr 1

wtot=wao+wbrs2f=wb(2)+wa(2)+ fst2t3f=wa(3)+wb(3>mi f=-(wa<2)+wb<2)+fst2) +e5-wa(3) +< e3+ l cg>-wb(3) +e4m2f=(wa tr 1+wb< 1) ) +e5~a(3) +e2-wb(3) +e 1

t t3f=watr 1 +e3+ (wa< 2)+ fst2) +e2+wb< 1) +e4+wb(2) +e 1

fcdr f=lcg+wa( l )t'1 rodmaf=fcdrf +< l rod-13.5)mbf=fcdr f+7. 125sdraf=f st2/aa+abs(maf +cali a)sdrbf=f st2r'ab+abs<mbf+cbJ'ib)fcof=l cgo+wa<1)/ir odopbushf=f cof +( 1 dr+d)f'(d+abush)REM STRESSES FROM FIXED COMPONENTSdear=< di wdi+d2+d2) ++. 5se t3f=abs( t3f/(4+aear) )semif=abs(mif/(2+d2+aear>)sem2f =abs(m2f 1( 2+di +ae ar ) )fcear f=t t3f/'(2+dear)frf=x+fc ear ff1 if=-(fcearf+sin(phi )-frfwcos(phi ) )f22f=fcear f+cos(phi )+frf+sin(phi )s t t3f=abs( f11 f+I a+c i 12>+abs( f22f +1 a+c i 21)sesi f=abs(sl f+c i 12+1 a/4. )ses2f=abs(s2f +c i 21+lax'4. >

sr f=se t3f+semi f+sem2f+sesi f+ses2f+st t3fREM EAR SHEARtau 1 1 f=abs(sl f/(4+aear > )+abs( f 1 1 fi'aear)tau22f=abs(s2f/(4~aear ) )+abs< f22f/aear)taur f=( taui 1 f+taui 1 f+ tau22f +tau22f ) ++ ~ 5taubf=taurf+aear/abl tREM EARBOLT TENSIONb t f= ( se t3f+ semi f+ sem2f ) +ae ar J'ab 1 t

0125:VU0127:000128:00

'0129! 00Oi 30: 000131: 00"132:00

'33: 00I .84!000135:000136! 0001 37: 000138! 0001 39: 000140!000141: 000142: 00Oi 43: 010144:010145!010146!010147:010148:010149! 010150! 01Oi 51: 010152: 010153! 010154: 010155: 010156! 010157!01

~8!019:01

0160!010161:Oi0162! 010163: 010164: 010165:Oi0166!01.0,1 67! 0 1

0168! 010165'! 0 1

0170 2010171! 010172: 010173! 010174: 010175: 010176! 010177: 010178!010179:010180:010181! 010182! 01A1 Q3 ~ Of

4!000185:000186:0001 87: 000188! 000189! 000190! 00

pr i n t "Ul hKA I lNU UYLINDE,K BKG f Kh.SbUKhprint"OPERATING VALVE EAR TENSILE STRprint"OPERATING VALVE EAR SHEAR STRESprint"OPERATING EAR BOLT SHEAR STRESSprint"OPERATING EAR BOLT TENSILE STRprintREMREM CALCULATE VARIABLE COMPONENTSREMdsr~O.dtaur=O.dtaub=0.dbten=0.dsa=O .dsb=O .cip b=o ~

for J=l to 3fco=lcgo+wao+glc(l,j)/lrodopbush=fco+(ldr+d>/<d+abush)ftrl=lbr+wao+glc<l,j)/irodsl=f trl+wbr +gl c(l,j)s2=wtot+alc(2,J)t3=wtot+glc(3,J)mi=-wtot+glc(2,J)+e5-wao+glc(3,J)+<e3+m2=( f tr 1+wbr +g1 c < 1, J ) ) we 5-(waowe 2+wbr +t t3=f triwe3+wbr+gl c( l,j) +e4+gl c(2,J >+(fc dr= 1 cg+wao+gl c (1, J )/1 rodma=fcdr+<lr od-13.5)mb=fcdr +7. 125s i ga=ma+ca/i as i gb=mb+cb/ 1 bREM CALCULATE EAR TENSIONse t3=abs( t3/(4+aear > )seml=abs(ml/(2+d2+aear) )s em2=abs(m2/( 2+0 1 + ae ar ) )fcear =t t3/(2+dear )4 r=x+fcearf 1 1=-( fcear+s in(ph i ) -fr+cos(ph 1 ) )f22=fcear icos(phi )+fr+sin(phi )st t3=abs( f 1 1 +1 a+c i 12)+abs( f22%1 a+c 1 21 )ses1 =abs( si +c i 12+1 a/4. >

ses2=abs( s2+c i 21+1 a/4. )sr=se t3+semi+sem2+sesl+ses2+st t3REM EAR SHEARtau 1 1=abs( sl/(4. +aear ) )+abs( f 1 1/aear )tau22=abs(s2/(4.+aear > )+abs< f22/aea! )tauear ~( taul 1 +tau11+ tau22+tau22) ++.5taubl t=tauear+aear/abl tREM E*RBOLT TENSIONbtens=(se t3+semi+sem2) waear/abl tdsa=dsa+s i ga+s i gadsb=dsb+sigb+sigbdpb=dpb+pbush+pbushdsr~dsr+sr +srdtaur=dtaur+ tauearwtaueardtaub=dtaub+taublt+taubltdbten=dbten+btenswbtensnext JREM COMBINE STRESSESdsa=dsa++.5dsb=dsb++.5dpb=dpb++ ~ 5dsr=dsr++.5dtaur=dtaur++.gdtaub=dtaub++.5

lpousnf" 'srf"; taurf"; taubf";btf

lcg)-wbr +glc(3,J)+e4el ) +gl c<3,J

)'ao+e2+wbr+el>

8 gO.~~~JO

fllKgO.TNO

0192: 0001'F3: 000194: 00

"01 95: 000196:00

197:0098:0099:00

v~00:000201:000202:000203:000204:000205:000206:000207:000208:000209:000210:00021 1: 000212:000213:000214:000215:000216:000217:000218:000219:000220:000221: 000222:00223:00

~4:005:00

AT A"AT B"

I dsaIdsbI dpbI dsl;dtaur;dtaub;dbten

ONENTS h

AT A"tdsaAT BNidsb

"ldpbr dsl


End of program

printtext 0, h DYNAMIC COMPONENTS 5pr intpr i n t "DR I VE ROD TENSILE STRESSpr i n t "DR IVE ROD TENS I LE STRESSprint "BUSHING PRESSUREprint "VALVE EAR TENSILE STRESSprint "VALVE EAR SHEAR STRESSprint "EAR BOLT SHEAR STRESSprint "EAR BOLT TENSILE STRESSdsa=dsa+ abs ( sdr a f )dsb=dsb+abs(sdt bf)dpb=dpb+abs(pbushf)dsr =dsr+abs(sr f )dtaur=dtaur+abs( taur f )d t aub=d t aub+ abs( t aub f )dbten=dbten+abs(btf )printtext O,h FIXED PLUS DYNAMIC COMPprintprint "DRIVE ROD TENSILE STRESSprint "DRIVE ROD TENSILE STRESSprint "PUSHING PRESSUREprint "VALVE EAR TENSILE STRESSprint "VALVE EAR SHEAR STRESSprint "EAR BOLT SHEAR STRESSprint "EAR BOLT TENSII E STRESSend

CYGNAA i rwcvr@EnvJOB NO.~<'~<FlLE NO.

SHEET NO.~>.AE

cspiINPUT GLOBAL ACCEI ERATIONS

'P 2.26,3 '2,2.8INPUT DATA

GLOBAL G-LEVELSNOPTH VECTOR ANGLESVERTICAL VECTOR ANGLES=EAST VECTOR ANGLESWEIGHT VECTOR Al'lGLES

2 '6135904590

— 3. 629018090

0

2.81359013590

LOCAL G-LEVELS

-1.59807 -1.38092E-5 . 1.97989-8.62121E-6 -3.62 -1.06811E-5-1 '9807 —1.38092E-5 —1.97991

OPERATING DRIVE ROD STRESS AT A '66.432OPERATING DRIVE ROD STRESS *T B 1319.35OPERATING CYLINDER BRG PRESSURE -7.15824E-4OPERATING VALVE EAR TENSILE STR 2111.01OPERATING VALVE'EAR SHEAR STRES 293.896OPERATING EAR BOLT SHEAR STRESS 2460.85OPERATING EAR BOLT TENSILE STR 1625.1

DYNAMIC COMPONEllTS

SCC SfRCTQ 1,3 3o - 4:E.<'aEAR BOLT SHEAR STRESSEAR BOLT TENSILE STRESS


703910524.9

DRIVE ROD TENSILE STRESS AT A 28384.4DRIVE ROD TEI'lSILE STRESS AT B 43412 ~ 2 ~'~'>'4(g'-'"c'~ C6g ."i lr<wA .'.~BUSHING PRESSURE 477.447

EAR BOLT SHEAR STRESSEAR BOLT TENSILE STRESS

>me-.sa—9499.86121 50

DRIVE ROD TENSILE STRESS AT A 29150.9DRIVE ROD TENSILE STRESS AT B 44731.6PUSHING PRESSURE 477 '48

CVG~~~A

Jos zo.~~FiLs Nosvaa'o. ~s4'

cs@2

~ ~

EUT GLOBAL ACCELERATIQtlS'26,3.62,2.8

INPUT DATA

GLOBAL G-LEVELSNORTH VECTOR ANGLES

'ERTICAL VECTOR ANGLES=EAST VECTOR ANGLESWEIGHT VECTOR ANGLES

2.2o135904590

3 '29018090

0

2 ~ 81359013590

LOCAL G-LEVELS

-1 .59807 -1.38092E-5-8 '2121E-6 -3.62-1 .59807 -1.38092E-5

1.97989-1.06811E-5-1.97991

OPERATIflG DRIVE ROD STRESS AT AOPERATIf'lG DRI'VE ROD STRESS AT BQPERATIflG CYLINDER BRG PRESSUREOPERATING EAR WELD TENSILE STROPERATIt'IG EAR WELD SHEAR STRESOPERATING EAR BOLT SHEAR STRESSOPERATING EAR BOLT TENSILE STR

766.4321319 '5

-7.15824E-43090.43735.1242460.861625.1

W I C CQMPOt lENTS

DRIVE ROD TEt ISILE STRESS AT A 28384 ~ 4DRIVE ROD TENSILE STRESS AT B 43412.2BUSHING PRESSURE 477.447maua -e a=Ed—zan smcss —vis~~ + <Cc~ g,'i '875

; ~R-WEf=&—SHEAR .rrREAR BOLT SHEAR STRESS 7039EAR BOLT TEf'lSILE STRESS 10524.9

FIXED PLUS DYNAMIC COMPONENTS CVQ<4ADRIVE ROD TENSILE STRESS AT ADRIVE ROD TENSILE STRESS AT BPUSHItlG PRESSURE~R-MEt.-D—7 EhEAR'WEL~~EAR BOLT SHEAR STRESSEAR BOLT TENSILE STRESS

29150. 944731.6477.448

28~&6-9499 ~ 8612150

JOB &!0.~„(~~ ~~ ~05.6(.

g.s,A7gfaacT QQ.

c=p QINPUT GLOBAL ACCELERATI Ot'lS

'? 1 '4s3 ~ 54fl 9

I t lPUT DATA

GLOBAL G-LEVELS 1.44NORTH VECTOR At'lGLES = 135VERTICAL VECTOR ANGLES= 90EAST VECTOR ANGLES = 45WEIGHT VECTOR ANGLES = 90

3.54'9018090

0

1.91359013590

LOCAL G-LEVELS

-1.01824 -1.3504E-5-5.49316E-6 -3.54-1.01824 -1.3504E-5

1.3435-7.24792E-6-1.34351

OPERATING DRIVE ROD STRESS AT AOPERATIt'lG DRIVE ROD STPESS AT BOPERATING CYLINDER BRG PRESSUREOPERAT I t lG VAL'VE EAP. TEtitSI LE STROPERATING VALVE EAR SHEAR STRESOPERATING EAR BOLT SHEAR STRESSOPERATING EAR BOLT TENSILE STR

766.4321319.35

-7.15824E-42111.01293.8962460.851625.1

DYNAMIC CONPONENTS

DRIVE ROD TENSILE STRESSDRIVE ROD TEt'lSILE STRESSBUSHIt'lG PRESSURE

EAR BOLT SHEAR STRESSEAR BOLT TENS I LE STPESS

AT A 18806*T B 28762.8

316.332P Cm SWe,VS %.3.~~ -II"%.~

5077.947164.63

FIXED PLUS DYNANIC CONPONENTS

DRIVE ROD TEt'lSILE STRESS AT A 19572.5DRIVE ROD TENSILE STRESS AT B 30082.1PUSHING PRESSURE 316 '33MA~EAR-TSttS.FQ~7RESS "'868. 59

~tNE-EA~HEA~7RES8— - 900~48-'ARBOLT SHEAR STRESS 7538.79

EAR BOLT TENSILE STRESS 8789.72

CVQblAATTACH)BEiil,

JOB NO. f~'pp+

FILfNO. OS.PI ~ P

SHffTNO. "~.~f

c IQ2UT GLOBAL ACCELERATIONS

'4s354)1 9

INPUT DATA

GLOBAL G-LEVELS 1.44NORTH VECTOR ANGLES = 135VERTICAL VECTOR ANGLES= 90EAST VECTOR AllGLES = 45WEIGHT VECTOR Al'lGLES = 90

3.549018090

0

1.91359013590

LOCAL G-LEVELS

-1.01824 -1.3504E-5 1.3435-5.49316E-6 -3.54 -7.24792E-6-1.01824 -1.3504E-5 -1.34351

OPERATIl'lG DRIVE. ROD STRESS AT AOPERATING DRIVE ROD STRESS AT BOPERATING CYLINDER BRG PRESSUREOPERATIl'lG EAR WELD TENSILE STROPERATING EAR WELD SHEAR STRESOPERATING EAR BOLT SHEAR STRESSOPERATING EAR BOLT TENSILE STR

766.4321319.35

-7.15824E-43090.43735.1242460.861625.1

'INIC CONPONENTS

DRIVE ROD TENSILE STRESS AT A 18806DRIVE ROD TENSILE STRESS AT B 28762.8BUSHING PRESSURE 316 '32

~R-IdELD—SHEAR-SFRESS ——+SM.;R2.EAR BOLT SHEAR STRESS 5077 ~ 96EAR BOLT TENSILE STRESS 7164.63

F IXED PLUS DYt lANI C COMPONENTS

DRIVE ROD TENSILE STRESS AT A 19572.5DPIVE ROD TENSILE STRESS AT B 30082.1PUSHING PRESSURE 316. 333

~-WELD.—TENSI-l-E-STRESS—=—1-1 506-..3-

EAR BOLT SHEAR STRESS 7538.81EAR BOLT TENSILE STRESS 8789.72

JOB RO

PILE HO. ~ S'"SHSZVHO.~4

APPENDIX B

VALVE/AIR OPERATOR MODEL FOR

FINAL PIPING RESPONSE G-LEVEL CALCULATION.

JGE NG. ~

SaENG. OSSA F

SHEET NG

f 0 ~ ~ ~ /p

J J /w P'

SECTION 5.0

APPENDTCES

CONTENTS

5.2 Walkdown Sheets

g~ Q+&E' 9~c ~~~)

5;3

5.5

5.6


g~ (QPwz&i SE++Tf >c)

Revised 'burns and RoePiscina Analysis Accelerations

Load Comparative Sheets

EQUIPIiEhT QUAL'1CATIONWALKDOWli VERIF 1 CATIOI'I FOR! 1 PAGE 1 OF

EPN 0 SP-'/-

BLDG IR

MiFR c9//-MODEL( 6&5

4~ PSI 8 84D

"~D/COPPPONENT EL 5O&SERIALS / I "7Z+g- (

QIDP Bt'COORDS 4S/7 Co~r ~;MAT'L5l < Q -'75

LBS SIZE~@

YOKE ORIENTATION

I TO AXIS OF PIPE ( )

// TO AXIS OF PIPE ( ), I/'i/V[n

YOKE LENGTH(FLANGE TO FLANGE)

MOUNTING CONDITION

NO OF BOLTS

BOLT TYPE~g ~//s

BOLT 0 //4-(uY 'JC

WELD TYPE 8 SIZE ~cA~)c ~ Ci:~ z'3Z7

PIPE MOUNTED YES (vi) N (

PERYiANENT OBSTRUCTION (WITHIN 2 ")................ YES ( ) NO ( QIS COMP BETWEEN CONT S; 1ST ANC (FULL 6 WAY ANC) YES (g) NO ( )

DO MULTIPLE SUPPORTS EXIST BETWEEN CONT 6 COMP YES ( ) I'10 ()()

Z

TYPE SIZE

GLOBAL CO-ORDINATESYSTEM

OPERATOR EPN 4- '/MODEL NO

VALVE STEM ORIENTATION

MANUFACTURER r'zz<~SERIAL NO

ORDER NO

MOTOR EPN

MODEL NO

ID NO INS CLASS

MANUFACTURER

SERIAL NO

1-PHASE ( ) 3-PHASE ( ) AC DC

TYPE OF CONDUIT CONNECTION: RIGID ( ) „FLEX (Q)

NOTES: 1. Definition (N/F = Not. Found)

~4'4'iA CC ~~«7 <Vi7CWC Z~,~," D) 7CQQQIDdD~~«d> ~rc w'~/D~'. /zDC~JririeArio~

7~t'~ ~cu ''

PREPARED BYI ~(SIGNATURE)

onJZc.d

DATE~Ps a REVIEWED BY ZC&anmnn&r DATE~>l jg(SIGNATURE)

FeRAn~OC2-

C:a ic ulaiionSheet

F'rotf ot Prepareo By Date

Eg ulk. r/Oc /Checked By Date

d.SP- U'-/*h lyk';;

c

Rev No

Job No,

Sheet No2 0

File No

c r

f ~. ~

~ e

t I

/ey

QVC J -'41cceJXp

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PAGE 1 OF

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PAGE 3 OF

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5. 5 REVISED BURNS 6 ROE

PIPING ANALYSIS ACCELERATIONS

QJ!,'>

i~ ~!!fear«> r,'„

Sub5ectx W. 0. 3900/4 000%lashing ton Public PowerN4P-2Qualification of Ncchant.'ounted Equipnent; ForvZnfoxma tion

Su ppl y S ye ter"..

ical Pipearding of

MAY 11 f983,.P

R f CEIQrFDI!|/Al '! J )f83

I' ~

CYGNA-RICHLggo '--:"-

~ I

April 29, 1983DNPP-83-07 6

!fr. L. T. HarroldAssistant DirectorWashington Public Powe3000 George VaohingtonRichland, Vashington 9

r Supply SystemMay

9352

~ g,

Attention: hlr. B. A. lfolmbc:rgr

References:

'„MQ+.o,i. '. ~ ~

%laic>

Gentlemen:

(a) >7PBR-03-17, Bated 3/16/93.{b) WPBP;S3-20, Gated 4/12/83.(c) MPHR-83-29, datod 4/12/83.

'(d) Te3.ecopy, B. A. Holmherg toJ. J. Vere>crber, dated 4/4/83

sos wo.~8p.c +0os.o{. FF!!.a!40.~

SHeET No. g.5, I

I /i

r

~ I

.,''C. W.rn, ~

i"..tg.!

'h

~ I

;, \

Xn response to the request of references (a) > (b), {c)and (d), this letter ia fcr:rarding rePined valve accelerations.The valve acceleration sheets for the five {5) CSP valvesrepresent the second iterati.on of the refincraent task.. Valve .',sheets for the other four {4) valves represent the firstiteration of the refinement task. - Please inform the Noodbury:.",.-Office if efforts should bc r.-ade to rer1uce accelerationsfurther.

~ I

+ei<~A;~:':>'-" O'JV/BPM/es:" i~i;;;j~:g,<-',! Att

Ve ry truly your s,

QR )caps twL ctCi.'I ED BY J. J. Vr2',DERSEP

John J. VerderberPro5ect Engineering Manager

~ ~

I

~ I

'~". A,~""r"

0:"'C:

Hr. >1. S. Chin - DPA — 3 ~r/1QHr. J. Z. Rhodes - VPPSS - 1 xr/l

P. Buck - E,"Pp"S - l ~./1 .'lail Drop ."'75

ATTACHE1ENT

Ak

Data forwarded with BRNP-83-078, dated April 29, 1983

Valve Kale. No.

SP-V-(~SP V-2 .~

CSP-V-3CSP-V-4CSP-V-5RCIC-V-31RHR-V-17BRHR-V-53AREER-,V-53B

125125125125125107312931

8. 148.148.148.148.148.148.148.148. 14

.129

.129

.129

.129

.129

.112A

..121~ 62C. 121B

CVGMAATTAChV~Eii-'7

JGB NG.

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rot: Tp! c j (Jcgg.~ gL,<,u Ev T

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A = p<g = so,3 iN (1g) =':,[z. i~c = u."(s)

10"s 00

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Jabwo. oa+~4 FleNo. i/Sheet No.

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Date8,!Zd'h5

File No.Gt ~ col ~

Analysis No., Rev. No.44I/O", 8 ting@ >.Io I IC>4-',.3- l~ I 3,

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j'a'r* ea r,

2.S

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g Cggrg~g4e r

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f'o L

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T. = 7.9( )r'ac)'

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'I 0} VE l C| 4A <C'I 0 r L ~«trttrAQ.'l . Jr'4';-ct- ."Irg ''.''s!""

System „

Analysis hto. Rev. No..5( I la I d I 4 6

bZD44 d t. 01 /t-'.;t >lgj - -! ='-(Big

I=tgt td!=„7

7,1~5~ 7

g8 I rg!I (g g f..'-.5 Vcr=- LF"==,,%~I~ ~lWs

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+ SllJI.FtQe

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gZ, - Il< Z„„= —..s~ I.o 88+)Vj

A=mt, ="=.qS N (

I00S 00

7.1 H~

g C.

q,OCjt ~f.,)H'l

5g!!IFq ~o ~C. =.at=7

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= —r =.Pr c- D V (C .u.~ (":0 "

( p g =-,cr: -')

Jjl!IC /J

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!!+=',78

ill (2'I )5'rY = 3+'E-'3 = g lI ~.g<)

.2( g.t1+.et>

APPENDIX C

SAMPLE HAND CALCULATIONS

TO CHECK PROGRAM

CEP-V-3A

~ y I 4 V \ ~

~ v 'I ~ N t ~: ~

nbi f Cc P V'-INPUT GLOBAL ACCELEPATI Ct l$

? 13.89,1.66,1.04It'lPUT ANGLES OF NORTH VECTOR

? 90,90,0INPUT ANGLES OF VERTICAL VECTOR

90 0 r90INPUT ANGl ES OF EAST VECTOR

? 0,90,90

I t lPUT DATA

CalculationSheet

Prepared By

Checked B

"" 'e.os@

Oate

5 RlOT:0 i(~=

GLOBAL G-LEVELS 13.89NORTH VECTOR ANGLES = 90VERTICAL VECTOR Al'lGLES= 90EAST VECTOR ANGLES = 0 90

1 '690

090

1.040

90

5C I Io(.-C -i

-5.29861E-5 -6.33239E-6-5.29861E-5 1.66

13 '9 -6.33239E-6

1.04-3.96728E-6-3.96728E-6

INPUT AtlGLES OF MEIGHT VECTOR? 90,180,90

LOCAL G-LEVELS

%Pl MPCE. CHECl< CALC 5

<A R TL.VSl<E H~ZE>5

TPF - (F T-e~)~V.~ -m> ~~.~—(tlS'o -age)+ bS: 27)~S Z>

'TgF 9031. ) tc --~~~~ I<~%

OPERATING DRIVE ROD STRESS AT AOPERATING DRIVE ROD STRESS AT BOPERATING CYLINDER BRG PRESSUREOPERATING VALVE EAR TENSILE STROPERATIl'lG VALVE EAR SHEAR STRESOPERATItlG EAR BOLT SHEAR STRESSOPERATING EAR BOLT TEllSILE STR

glc(i,j)= J=-S.29861E-5 ~1

fcdr = -1.22282E-2siga= -.267492si gb= —.409114Fc due to T3=-5.71181E-2-fii= 2.73638E-2f22=-5. 85968E-2ds a= . 071 5S2dsr= 3.3257E+7dbten= 4.86604E+9glc(i,j)= j=-6.33239E-6 2fcdr= -1.4614E-3siga= -3.19681E-2sigb= -4.88934E-2Fc due to T3= 321.752f 1 1 0' 43 (p)gg~ pAr E)f22= 33 . 082dsa= .072574dsr= 3.7607E+7dbten= 4.86759E+9glc(i,j)= j= 1.04 3fcdl = 240. 013s i ga= 5250 . 28s i qb=, 8029. 99Fc due to T3= 919 ~ 516f11=-440.516f22= 943.322Ac.a= 2 PSr'REF+7

10CO 00

F„= -.~>~T)F = -~+Fez. = l-i 4'3+T-F = Zdg

SNlr=f-"5'A t I~Sy .7> I+J~o>~7 (~5y t -'5

477.198821.458

-3.75613E-41136.5289.1706

'078.68

525.595

TC TqL t)NP EAR E.~5tt.r- ~ASS=f2I. t++fZ'll=.II%I vS~II37 '.Qg

Ctl Pc<@ p~'zri(u+ wvs) r, n» la-~=as

t5Ir

'(( 55: zs.z+ zn» I oqw<r)/~='7I9

= $ ZC PiT

Ml, due dc'uad tl»»dl~g= l~llakwr+-FST )pep

Q(/~d ~ r ~g259 - d.». I rZw (0 g lD':lZ.S

rd'l» $ du 8 ~ (tJ>flit = (~A<>+Jl r 7')y+'1.!,(4l4

+gee ~ ~~~ — 4>~ ~i.tg ~7.iz.~ c7i P5

CalculationSheet

'"'"'PP ss- E< Prepared By; / . Datec.- v 3wSubject Checked By: Date-c

(

System gyp'~pAnalysis No. Rev. No.

5 ZC44 'V.gI-Sheet No.

M I lob - -Z

CR KCK -X Q TEASDALE. O'T12$ )5 CALC 5:~ ~

— 154

4c 3ZX

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Sot- T w&Huiog C.H-C'<~ (Vd T >! A) )

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ICC0.00

SECTlON 5.0 QZDI 361106

APPENDICES

CONTENTS

5.1

5.2

5.3

—5-.4

5.5

Response Spectra

Walkdown Sheets


aces IP~ (go~ruisrRAriJw)

Final Pipe Mounted EquipmentResponse G-Levels

Revision 3

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160.00

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r; )UIPMENT QUA3 3FI CA TIO"hAL1:DO')iN VERI' CATIOl: 1'OR".

~ ravw a VI

'<Illllllilltllllllllllllllllll

>:ODf 9„„-&-A/'> PSI S 2r~

YOKE ORIENTATION

FLOOR EL )/;ICONPOh'= N"T EL~itSERIALS + i 3.~.

NOUNTINC CONDITION

C)IDII.,'.. l l '(-

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PgrTsL > ~g ( fLBS (/r" SIZE

>='S)'.E

CLASS A/rr

TO AXIS OF PIPE ( ~// TO AXIS OF PIPE ( Q

I g I(YOKE LENGTHEN - 2(FLANGE TO FLANGE)

NO OF BOLTS ~V~BOLT TYPE X,/J. BOLT r/ /fAVELD TYPE 6 SI ZE

PIPE 1:Ou.:TED YES(g-NO ( )

I' RY&NENT OBSTRUCTION (VITHIN 2 ") YES ( ) NO ( 4

, S CONP BETNEEN CONT 6 IST ANC (FULL 6 'IV~Y ANC} YES ( ) NO ( ) h'/F'rQ MULTIPLE SUPPORTS EXIST BETWEEN CO1'T 6 COMP YES ( ) NO ( ) t 'fF

g~r )/

GLOBAI, CO-ORDINATESYSTEM

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VALVE STEM ORIENTATIOI):

ERATOR ZP1 &~am~»~~Dr.L NO

SIZE

OP. EPN + $ /6 /7d//0

1"D3'UFACTURER

SEPIA NO

ORDER NO

RA ~& Y~UFACTURER

ATTICH"";iS= ~)!:

JOB NO.BcLQ-FILE NO.CKC~~SHEEVWO.iM I

DEZ NO

NO INS CLASS

SERI',1 NO

I-PHASE ( ) 3-PHASE ( } AC DC

'"~NTS: Def inition (N/F = Not Founa)c'sP- ~ 4~-3

op pip~ jr~ +y+ &~~~'y~g~~ ~owy4 L&K 7u ~h~pp/AJPf~A'T,

.:P~ D BY/z 'ATE%/r'-, : RIEYVED .BY W K— DATE~~b'I(SIGNATURE) (SI N .TUFE)

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Re.No.

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ProspectWPPSS Mechanica1 E uiomenSubiect24" Butter+1v Valves

System

a P~ oPrepared Bv'ate

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MOUNTING CONDI Tp pN

NP PF BOLTS

BOLT TY'PE

HELD TYPE & SIZEBOLT ql

PIPZ MOUNTED YES ( ) Np ( )

PERi~iANENT OBSTRUCTION (WITHIN 2 ") YES ( ) NO ( )IS COMP BETtsEEN CONT & 1ST ANC (FULL 6 NAY ANC) YES ( ) Np ( )DO MULTIPLE SUPPORTS EXIST BETNEEN CONT & COMP YES ( ) NO ( )

GLOBAL Cp-ORDINATESYSTEM

PZRATOR ZPN

iODEL NpYPZ

iOTOR EPN

~ODZL NP

SIZE

VALVE STEM ORIENTATIpl)',

MANUFACTURER

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NO OF BOLTS

BOLT TYPE BOLTq'ELD

TYPE 6 SZ ZE

PIPE hiOUNTED YES ( } 1:O ( }

PER! LRNEtilT OBSTRUCTION (hITHIN 2 ") YES ( ) NO ( )

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DO 1/!ULTIPLE SUPPORTS EXIST BETWEEN CONT & COYiP YES ( ) NO ( )

GLOBAL CO-ORDZ t~!ATESY STEYi

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Subject~ R. 0. 3900/4000Washington Public Power SunplWt)P-2Qualification of?|ounted Equipnent

'nformation:<c '.,

!ir. L. T. HarroldAssistant Director

""'r'-.p'~'~'.~i.."Washington Public Po~<er Supp.."-s=.",.;.:",9'r -" 3000 George Washington May

Pichland, Washington 99352

:"i'-", . ". References:vP cq~ ~

''F,,'E r$N'r

Gentlemens

(a) WPBR-03-17, dated 3/16/8 3 .(b) WPBR-83-20, dated 4/12/83.(c) f&HR-83-29, dated 4/12/83.(d) Telecopy, B. A. Holmberg to

J. J. Verderber, dated 4/4/03;Ih

0 ~

Xn response to the request of references (a), (b), (c)and (d), this letter io fcr:rarding refined valve accelerations.The valve acceleration sheets for the five (~) CSP valves

".j'';:a".~,,". ~ represent the second iteration of the refinement task.. Valve .',~<'!>;'~",'~,, sheets for the other four (4) valves represent the first'-:".„'jji",~c.';g.",;.;. iteration of the ref inc@rent task. Please inform the Woodhury

.'.",.'fficeif efforts should be r."+de to rec1uce accelerationsfurth r

Very truly yours,

ORIG,~„L SIC~rICO GY 3 3 ~r~DEASEP

i Ebi

~ I ~ I

John J. VerderberProject Fngineering Manager

CC: Hr. W. S. Chin — BPA — 1 r/1QHr. J. 7.'. Rhodes - WPPSS — 1 ~;/1

p. Buck - 5"Ep<S - 1 ~./1 ~tai3. f>rop ~r75

ATTACHMENT

Data forwarded with BRWP-83-078, dated April 29, 1983

Valve I Kale. No.

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QZDg 361106

7.0 TRANSMITTAL, PREOR CALCULATlONS

AND REPORTS

CONTENTS

7.1

7.2

7.3

7.4

Communication Reports

Old Requalification and SQRT Forms

BIF Report: Dynamic Torque Calculationsof Butterfly Valve (Excerpt) *

McPherson Associates Report:Design and Sei'smic Analysisof 24" Cylinder-OperatedButterfly Valve. (Excerpt) *

*NOTE 1See Cygna Energy Services Project File; "EquipmentSeismic and Hydrodynamic for 24" Cylinder OperatedButterfly Valves", File No. OT.Ol.F,'XDS 361106,Revision 3, June, 1983 for complete report.

Revision 3

6.0 Drawings

QID=: 361106

DRAWINGS SUBi~fITTED TO SUPPLY SYSTEM

IN ORIGINAL PACKAGE

Johnson Controls

D-220-0310-IR-64 Rev 0

Flick-Reedy Corp

C-"26096 Rev 0

BIFD-207110-H Rev B

D-207110-G

A-206767

Rev A

Rev C

Bovee 6 CrailCSP-807-8.10

CSP-809-1.2

CEP-625-3.4

Rev 4

Rev 4

Rev 6

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QIDN 361106

7.1 Communication Reports a Correspondence


CommunicationsReport

Company:

Project:

Subject:

CBS'elecon 0 Conference Report

Job No.

Date: f3

Time:

Participants:

jl- tUK I AC. StOQ5

4-gb-

Place: g g~

of C

CP p-

Item

z./ tot

Comments

F+ j

Req'd Action 8y

5iF .VA4VE FL AQ &6 Pie&,N sion s

4 'gtc,~~l. d.e). cL.

25

Z.iz.S

'5l

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ATTACHMENTJO8 HO.SIilLENO. ~+.SH"=Bi NO.~7' I

Signed:

Distribution:

Page of

Washington Public Power Supply SystemP.Q. Boy.968 3030Georae Washington Way Richland, SVashtnoton 99352 (509) 372-5000

December 17, 1982GE-02-RWH-82-018

Cygna Energy Services141 Battery StreetSuite 400San Francisco, CA 94111

Attention: Hr. T. Wittig, Project thanager

Subject: NUCLEAR PROJECT 2CONTRACT C-0892

'l

Investigation of the CSB and CEB systems shows that during a dynamicevent the systems are not degraded in any way by the butterfly valvesfluttering. Therefore, all work on Work Release Nos. 14 and 17 whichaddress valve stability should be terminated.

R. W. Hickman - 575Senior Engineer,Equipment qualification

RWH/sms

cc: F. Khanachet, Cygna Richland

R ECElVEDL'=Can j982

CYG«'A-RICHLAND

Joe ~O.~™FILENO.~slRET No'



CR-030

company: CES

Project:WPPSS

X3 Teiecon O Conierence Report

82044

7 29 82Subject: Time: 9:40 A.M.

Participants:

/ID 361110 - 18" BUTTERFLY VALVE

Dick Hickman

Hal Reeser

R 'DAOI Supply System

oi CES, SDAO

ot

Comments Req'd Action By

I called Dick re. dynamic instability of BIF valve while inopen position. I also requested permission to contact GE re.use of aulted or upset allowables for RHR valves'

Dick said we should complete the requalification analysisof the valves and flag the dynamic instability issue as aseparate subject that will require Supply System actionfor resolution.

o Supply System has granted a contract to BIF for operabilitystudies on their valves. The contract admistrator at BIFis John McDonald (401/885-1000). Our action should be todetermine the scope of the BIF study and to make certainthat we do not overlap our efforts with theirs. Also weshouId attempt to assure~hat our work does not conflictwith the BIF effort.

o Dick said we may contact GE direct. Our contact at GE forthe decision on faulted or upset allowables is: ArianDeVault (408/925-2208).

*ACTION: Rajan, this resolution should be documented viarevised criteria in our Project Manual.

H. Abolhoda

MD Rajan*

pTT qCI;MEINT

IO™0FILE HO. DT.rst F

SHEET NC. f.I.T

H. Reeser Page 1-oi 1

"'" ""'"'. Wittia, H. Abolhoda, F. Khanachet, P. Guglielmo, B. Schla fer, M. Rajan,

J. Minichiello, P. Patel, Project Files (SD), (SF), (RB)


CommunicationsReportCR-027

Company:

Project:

sttbject:

WPPSS

XI Telecon

Time: P.M ~

0 Conference Report

sob wo 92OQ6

Date: 7/20/82

Participants:

APPLICABILITY OF HYDRODYNAMIC LOADS

W. SchlaferH. Reeser

Piece: SDAO

of CES, SDAO

CES, RBOof

of

Item Comments Req'd Action By

2.

3.

The Hydrodynamic Load Column in the WPPSS SRM list is knownto have errors. A "non listing is not to be trusted.

For packages in analysis Cygna will trace down the P 8 ID todetermine the applicability of hydrodynamic loads to linemounted equipment.

To accomplish this, Cygna will:Al

a. Check the line routing to.see if it penetrates theprimary containment. If not, hydrodynamic loads donot apply. Rt.E

SHEb. If the line penetrates the primary. containment, hydro-

dynamic loads will apply unless:

1. An anchor point appears first in that line, or

2. The line first connects with floor mounted equipmentoutside the, primary containment and it is sufficientlysturdy to eliminate the propagation of pipe linehydrodynamic loads beyond it.

GNAACHM:-H

"I'.

fuff rI.

O. op.o i. I-

NO.Z.I~

If a line mounted equipment fails to qualify due to hydro-dynamic loads, estimate it's fragility level. This informa-tion will be used by WPPSS when they receive the 8 8 R finalpiping analysis and examine actual pipe accelerations.

WS/sak

W. Schlafer Page of

1020.00

L. Kammerzell, J. Read, P. Guglielmino, J. Minichiello, P. Patel, M. Rajan,

H. Abolhoda,~RE~ P. Curry, H. Reeser, T. Wittig, F. Khanachet

l j s j


CommunicationsReportCR-027

Company: CES Telecon 0 Conference Report

project:

Subject:

Participants:

WPPSS

APPLICABILITY OF HYDRODYNAMIC LOADS

Job No.

Date:

Time:

Place:

of

of

of


5. For packages whose analysis is complete and where hydrodynamicloads were not considered because the SRM said nNou:

a. Review the line as in 3 (first page of this tel'econ).

b. If we feel hydrodynamic loads really do apply; send amemo to the S. S. indicating the package may need'revfork.

c. Send memo to F. Khanachet requesting supply system con-currence that hydro loads do apply and added analysis isrequired.

p "t'gP CH

„iOB«.~V'r.~I ~ fFas« ~

~gFP~ ho.~

signed: W. Schl a ferDistribution:

1020 00

Page of



CR-023

Company:

project:

Subject:

Participants:

WPPSS

Hydrodynamic Loads

g) Telecon

J. Minnachiello

0 Conference Report

82046

Jul 20 1982Time:

g A~San Dieao

of F

of

of

Item . Comments Req'd Action By

2.

3.

During the conversation we discussed the following:

If attenuation data on hydrodynamic loads are not available,one does not have any choice but to take into account hydro-dynamic loads on all line mounted equipments.

One should use 1.5X peak acceleration unless the systemfrequency (line plus equipment) indicates otherwise.

If the equipment satisfies the allowable stress limits, thenone should perform fatigue analysis using the fatigue designcurves given for Class 1 components. To calculate thefatigue damage for normal operation (excluding all dynamicevents) one might take a conservative approach by assumingthe calculated stresses are equal to the allowable stresslimits.

fr f(» B 's >~

>T I,~CH;»~H.r

JO2 BO.~r~rn.a No.

~~~~'~-=-

vo ~~I~

signed: P. K. Patel Page 1 of

Distribution: H. Reeser, L~~AueR> Rajan, H. Abolhoda, P. Curry1020 00

-'IFJuly 7, 1982 CYGAA

Sygna Energy Service225 Stevens StreetSolana Beach, CA 92075

Attention: Mr. "Bill" Schlafer

.IOB XO. ~~<<PILE VQ 0 o( C

SHEET HO.~~ ~ I

I V

Subject: Butterfly Valves for NuclearApplications with IEEE QualificationRequirements

Dear Sir:This information is provided in response to your recent phonecall.l. Enclosed please find some catalog information describingBIF's line of butterfly valves, including our current

models as well as our new Model 0668 design (which willshortly replace our 0652 and 0658 models).2. The following are our best estimates for bud et, our oses

~onl of what it would cost to replace the valves and oper-ators originally furnished to WPPSS in the 1970's (whichdid not require IEEE qualifications) with valves and oper-ators that are fully qualified to IEEE-382-1972, IEEE-323-1971 and IEEE-344-1975

't

is almost impossible to obtain prices from IEEE quali iedactuator vendors without a detailed specification showingexactly what is required; therefore, these are our bestguestimates of what the replacements would cost. Theycould be high or low by 10 to 20$ , depending upon thewording used in the engineer's resultant specification.Replacements for Valves Furnished Ori inall on N-27232

14 — 18" BV's with electric oper-ators (See NODS — ll/1/79) $ 40,000 ea. if qty.

or $ 25,000 ea. if qty.Re lacements for Valves Furnished'Ori inall on N-27233

2 — 18" BV's with spring to ~o encylinder operators

$ 60,000 ea. if qty.or q45,000 ea. if qty.

", 600 OIVISION ROAD ~ WEST WARWICK,RI 02893 ~ BOX 21 7 ~ ~01.885.1000CABLE:BIFWRWKRI ~ TWX 710.382 0402 ~ ELFX 827 631

Sygna Energy ServiceJuly 7, 1982Page 2

Replacements for Valves Furnished Ori inall on N-27234

4 — 30" BV's with spring to close $ 75,000 ea. if sty.cylinder operators or 660,000 ea. if qty.

Replacements for Valves Furnished Ori inall on N-27235

4 — 24" BV' with spring to close $ 60,000 ea. if sty.cylinder operators or 550,000 ea. if qty.Re lacements for Valves Furnished Ori inall on N-27236

3 — 24" BV's with spring to ~o encylinder operators

$ 60,000 ea. if sty.or $ 50,000 ea. if sty.

Ne trust that this information will be of some help to you, andare sorry that our prices cannot be more precise.Sincerely,

eorge E. SayerBV Sales Applications Engineer

Enclosures: 650.20-4BPD-668-45-1BPD-668-1NODS-1 1 /1 /7 9

ATTACH[.hler„"MY

JOB BO.f2oqg'ILE

FIG. or sI pBHB:T FIG. I 5

A ottt: or cattaaat. stcam coaaoaaztott

BUTTERFI Q, VALVES.MODEL '6C8l2 .'2+ THRU SHAFT

PARTS .

a

I2

'

7 II

+ IS

ITEM 22 IIEET 2 3SHRUNK f. SEALEDWITII LOCKTITE

WECHANCZLLV RrraIHED ADJuSTABLESEAl

~IIELD IRREPLACEABLE WITHCUT . 8

REHovWG VALVE mom PIPE LWE.3 ~

tT EM 5 SECURED WITH5 wvLott IHsetar

IO

I2

l4l5l6l7I8

20

22

..SECT ION A-A

'ATERIALVALVE BODYRUBBER SEATCLAMP I NG R I NGCLAMP ING R ING LOCKHALF DOG POINT SET SCREW

SHAFT BEARINGSTUFFING BOX PACKINGSTUFFING BOX GLANDHFX HEAD CAP SCREWOPERATOR SHAFTHAt F DOG POIhll SET SCREW

YALYE DISCWASHERDISC P INKEYHEX NUTTHRUST COLLARTHRUST BEAR ING COVERHEX HEAD CAP SCREW0-R INGTHRUST BEAR INGDISC SEATING RING

ALTERNATE AOJUSTABLE VEEPACKING

MATER I ALCAST IRON ASTM AI26 CL BBUNA-N ASTM 02000TYPE 304 ST. ST'LTYPE 304 ST. ST'LTYPE 304 ST. ST'LREINFORCED TEFLON BRZ ORPHENOLIC BACKEDVEE P ACKING BUNA-NCAST BRONZE ASTM B62TYPE 304 ST. ST'TYPE 304 ST. ST'LTYPE 304 ST.- ST'LCAST IRON ASTM A48 CL40 ORDUCTILE I RON ASTM A536 GR. 65-45-12TYPE I8-8 ST.ST'LTYPE 304 ST.ST'LST'LTYPE 304 ST. ST'LTYPE 303 ST. ST'LCAST IRON AS Tidal AI26 CL BTYPE 304 ST. ST'LBUNA-NRE I NFOR CED TEFLONTYPE 3IG ST ST'L

AlTACHMEI~T

7-r-82 METERS-FEEOERS~ONTROI S

BPD 668 rS-l

A UNIT OF GENERAL SIGNALITEM 5 SECURED

5 WITH NYLOKINSERT

2

AWWA BUTTERFLY VALVESMODEL 0668 30" THRU l20

~

'~ PARTS

7

19

l2

15

05 aI

XKZXlLTHRUST ADJUST-

MENT PARTS"

l3 6II

MECHANICALLY RETAINED ADJUSTABLE SEATF I ELD R EP LACEABLE WlTH OUTR EMO V I N G VALVE FR OM P I P ELINE

ITEM 27 HEAT SHRUNKAND SEALED WITH LOCKTITE

czuuLJLa'(FOR 30'HRU 48'.V) 'FOR 54'HRU l20'.V;)'

TEM MATER I ALI VALVE BODY2 RUBBER SEAT3 CLAMP ING R ING.4 CLAMP I NG R ING LOCK5 HALF DOG POINT SET SCREW6 SHAFT BEARING7 STUFF IN G BOX P ACKING8 STUFFING BOX GLAND9 HEX HEAD CAP SCREWIO OPERATOR SH P,.=TII STU HA T

l2 VALVE DISC'3 WASHERI4 DISC P INI5 KEYl6 HEX. NUTl7 THRUST COLLARI8 THRUST BEARING'OVERI9 HEX HEAD CAP SC EW20 0-R I NG2I THRUST BEAR ING22 THRUST ADJUSTING SCREW23 JAM NUT

MATERIALCAS T I RON AS Tidal Al26 CL BBUNA-iV AS TiVI 02000 ~

TYPE 304 ST. ST'LTYPE 304 ST. ST'LTYPE 304 .ST. ST'LREIN ORCED TEFLON BRZ ORPHENOLIC BACKEDVEE P ACK I NG BUiVA-NCAST BRONZE ASTi'A B62TYPE 304 ST: ST'LTYPE 304 ST. ST'LTYPE 304 ST. ST'LGAST IRON ASTM A48 CL40 ORDUCTILE IROI'I ASTiil A536 GR. 65-45-12TYPE l8-8 ST.ST'LTYPE 304 ST.ST'LST'LTYPE 304 ST. ST'LTYPE 303 ST. ST'LCAST IRON ASTM AI26 CL BTYPE 304 ST. ST'LBUNA-NP. E I NFOR CED TEFLON P HENOL I C B ACKEDTYPE 304 ST. ST'LTYPE 304 ST. ST'L

24 THRUST BEAR ING PLATE25 SEAL26 HEX HEAD CAP SCREW27 SEATING EDGF

STEEL ASTM A36S ILICOI'IE RUBBERT'(PE 304 ST. ST'L

'(PE 3I6 ST.ST'LJO

Ml %1»

I-I5-82 MEYERS-FEEDERS~ONTROLS

Fll.gag ~o7. ~SiiE~,'i0.7'I:lo.

SPD-668-I

LIMtrpttpuz

(~i,i j,,:~>' 1. /

'

k~<. ~~,:., ',":;,sMaPL %ha~

LIMITORQUE CORPORATION ~ P. O. BOX 11318 ~ LYNCHBURG, VIRGINIA 24506

/ .>y

'

IEEE 323 (1974) and IEEE 382 (1972)NUCLEAR QUAUFICATIONDATAFOR SAFETY RELATED SERVICE

THREE PHASE ONLY D.C.

Design Life

Ambient Temperature(Continuous)

Ambient Humidity

Aging

Total Radiation(40 yrs, Integrated)

SeismicRof: IEEE344

Nuclear Containment(See Option 8 Price Adders)

40 years (2000 cycles)

140'F

60.100%

Motor Stator only180'C tor 100 hours

2.04x10'ads

"6.0 g's (SMB/SB)" 3.0 g's (SMB/HBC)""6.0 g's (SMB/HBC)

~ ~ ~

~ ~ ~ ~

Outside Containment(Standard Prices) t t40 years (2000

cycles)'20'F

30 100%

Entire Unit165'F for 200 hours at100% relative humidity

2x10'ads

6.0 g's (SMB/SB)3.0 g's (SMB/HBC)6.0 g's (SMB/HBC)

Containment-Inside or Outside(See Option 8 Price Adders)

40 years (2000cycles)'20'F

30.100%

Motor Armature, Field'oils, 8, Brush Box only180'C for 100 hours

1.0x10'ads

t6.0 g's (SMB/SB)" '3.0 g's (SMB/HBC)" 6.0 g's (SMB/HBC)

'mber of transients

I'ransient Temperature

Test Humidity

Profile

Length ot Test

Completed Test Date

340'F (BWR)300'F (PWR)

100% (saturated)

PWR/IEEE382 73,Page 12, Table 1

BWR/IEEE382.73,Page 12, Table 2

30 Days

PWR-September 1974(600456)BWR-September 1972(6000376)

250'F

100% (saturated)

ANSI (yot to be published)

15 Days

February 1975(600461)

340'F

100% (saturat

Special

25 Hours

October 31, 19(80009)

)~77ACHK~E~t 7

'During BWR test, 500 cycles Wore used as a design life per IEEE382,

During PWR test, 2000 cycles were used as a design lite of which 500 wore Incorporated prior to test and 1500 atter test.

During test for outside containment, 200 cycles were Incorporated while the actuators were being aged, and 1800 wereadded prior to Irradiating.

During D.C. test, all 2000 cycles were Incorporated prior to frradlatlng.

"As of 7/26/75, seismic tests were completed to IEEE344-1975 for both SMB and SB units to 6.0 g's vertical and 3.2 g'shOrizontal. Since no cross coupling was noted between axes, the test qualities the SMB/SB to 6.0 g's In both vertical andhorizontal axis. Maximum g level dwells ln each of the three axes qualify the units tor any mounting position. (SeismicQualification Report No. 80021). Qualification extends through 35 Hz.

t tStandard Class-8" insulated motors only.

"Standard units without spur attachments.

""Standard units with seismic support bracket and without spur attachments.

NOTE: SMC.04 and SMC 05 actuators are qualified for -Outside Containment" service per above levels based on theirsimilarity to the SMB actuator.

NODS ~ 11/'I/79



Company: CES

Project:

WPPSS

M Telecon 0 Conference Report

82046/CR-019Date: 7/] /8

Subject.'articipants:

W. SchlaferHarkness

Hydrodynamic Loads for LineMounted Equipment

Time:

SDAO

of Bechtel Norwalk CA

CESi SDAO

of

Item Comments

Callid the Seismic Qualification Working Group todetermine their current criteria for line mountedequipment subjected to hydrodynamic loads.

Req'd Action By

2. Their current test requirements for in line equip-ment subjected to hydrodynamic loads are:

a) One SSE + SRV Event: Required Input Motion(RIM) of sine beat testing at 1/3 OctaveIntervals from 1 to .200 Hertz >each for 15seconds at 6.0 g.

b) Two OBE + SRV Events: Required Input Motion(RIM) of two sine sweeps at 1 Octave/Minutefrom 2 to 200 to 2 Hertz at 2/3*6.0 g = 4.0 g.

c) In-Plant Vibration: Required Input Motion ofsine sweep testing at 2 Octaves/Minute from5 to 200 to 5„Hertz for 90 minutes at .75 g.

3. This type of environment is distinctly more severeand more correct than that proposed in the NPPSSinterim dynamics criteria memo 5 856. EventuallyWPPSS will need to be informed of curren 'rypractice such as this.

WS:lgn

ACHMENT

JOB NO.

FiLS NO. Df.o(.F

SHE"-T NO.~I'~

W. Schlafer Page 1 of 1'"" "" "Messrs. Eammerzell, Read, Reeser, Nittig, Minichiello, Guglz.elms.no,

Bosch, ~~eh Patel, Ra jan, Abol oaa r urry



Company: CES

Project:

WPPSS

i5 Telecon 0 Conference Report

Job No 82046/CR-018Date: 6/29/82

Subject:

Participants:

EQ of BIF Butterfly ValvesQID 361104, 361106

John Henry

12205Place: SDAO

of

John Henry Associatesof

of


Called John Henry because he was the engineer whoapproved the original seismic calculations for BIFButterfly Valves.

2.

3.

His recollection of these analyses was vague butdid mention they, as consulting engineers, nevertried to assure operability. Operability wasthe manufacturer's responsibility.

\

He recommended testing a similar valve.

g, I, ACHI~.EElA~ !

JQS NO.

SS.=- HO.~>."SHEET NO.

BS:lgnSigned Bill Schlafer Page 1 of

1020.00

L. Eammerzell, J. Read, H. Abolhoda, 222~gsj~~ P. Patel, P. Curry

2 r



Company:

Project:

CES

NPPSS

tK Telecon 0 Conference Report

82046 CR017

6/29/82Subject:

Participants:

EQ of BIF Butterfly ValvesQID 361104, 361106

Bill SchlaferGeorge Sayer

Time: a.m.Place: SDAO

of CES S

BIF, 401-885-1000of

of


Called George Sayer, the BIF sales agent to get abudget price for BIF 18", 24nr 30" air-operatedbutterfly valves and an 18" motor actuatedbutterfly valve. These valves are similar to onesin WPPSS QID files but do not use the same air-actuators. The original BIF valve serial numbers (forreference) are N-27234-F, N-27235-F, N-27236-F andN-27232-1.

2. He required a few days to work out a price and willalso send descriptive brochures.

C vG ~g 'Q

.q"pAr HMb MT

JOB HO )go~FlLs NO. Oyo(.F

SH=aV NO.~I

BS:lgn

Bill Schlafer Page1

of

P. Patel, P. Curry1020 00



Company:

Project:

CES

WPPSS

H Teiecon o Conference Report

82046/CR016Date: 6/29/82

EQ of BXF Butterfly Valves QID 761104,361106 Piace: SDAO

'Bill SchlaferAllan Berger

CES, SDAOof

BIF 401-885-1000of

of'tem


Called Allan Berger, a BIF engineer, to gettechnical drawings for the 18", 24" and 30" air-operated butterfly valve actuators.

2. Requested drawings of Miller air cylinders showingdetails ofa) Cylinder dimensionsb) Piston dimensionsc) Rod/piston connections

3. Conversation indicated

BS:lgn

a) There is a bearing and seal around the pistonrod where it exits the cylinder

b) The piston rod fits through a clearance hole inthe, piston and is bolted on.

c) No seismic functional tests have been done onthe Miller air cylinder

d) For dimensional data to verify functionaloperability of the motor actuated valve, con-tact Limitorque in Lynchburg, Vir

Q~/GNA,.~T-,„;gHMENT

JOB NO.~r

fargo~

pf'.ol.FrlLP. FIO.

GHEKT NO. ZL

Bill Schlafer Page 1 of 1

Distribution;

10t0 00

L. Kammerzell, J. Read, H. Abolhoda~"H+Xe , P. Patel, P. Curr


To: gg/ C

MemorandumPROJECT MEMO: ~P

~.Oc (

Oate:

From:

Subject: MISSING DATA REQUEST

Job No: 82046NPPSS

Copies:

Project File

0 gA'-~~///zr,' /.Sup7;

,-'/f/A/6 > g 6I ( Q/ZL.Eg

lORA-w/A& 8- z.l/ Z3o vg 2 E(~PI(

yN-w'/,rC~ 8 - > t'/ ~ - ~- (ClPp/5

tI,,I .

JOB tqpFIl.E tqO. 0T',o(.F:

SHEc=.T gO ~~~(

NOTE: Please sign and return the attached copy of this memora~as acknowledgement of receipt of this memo. THANK YOU. ~

Received by:

Date Received:

Memorandum


To:P . Gugl ielminoJ . Nin ich iello>,

June 17 , 19 8 2

W. Schlafer, PZ.'atel 82046/SDM-003

Subject:Analysis for Operabil tyT+>t HgEpT

JOB NO.~~or~I I:

FiLKRO.~gHEEY NQ.

opies: L. KammerzellJ. ReadH. ReeserG. Shipway (Wyle)T. WittigProject File

ln order to assess operability by analysis of mechanicalequipment which can be modelled to correctly predict itsstress and deformation responses 'relevant to operation,the following criteria are to be considered in conjunc-tion with Section 3.E.1 of the Design Criteria.If an equipment in Group II is expected to perform duringthe seismic and/or hydrodynamic event then the followingrequirements shall be met:

I

(1) Elastic displacement calculations shall be performedto assure non-interference between mating parts, and

(2) The calculated stresses shall be within theallowable stress limits.

If the calculated stresses for any service loading aresuch that permanent deformations might have occurred dueto high allowable stress limits, a displacement analysisas in (3) shall be performed.

(3) A comprehensive elastic-plastic analysis should beconducted in these cases to assure non-interferencebetween between mating parts.

For an equipment in Group I which is expected to operateafter the seismic and/or hydrodynamic event then thefollowing requirements shall be met:

(4) Total stresses in the part must be limited to ayield strength of the material, OR

'(5) Satisfy the requirements of Group II equipment.

WS:lgn

s =sir



Company:

Project:

Subject:

WPPSS

Wyle Data Bank

8 Telecon 0 Conference Report

82046/CR-014Date 6/16/82Time: a.m.Place:

ParticiPants: W. Schla fer

G. Shipway

CES, SDAOof

Wyle, Norcoof'f


Asked George to initiate a search in their testingdata bank for seismic or seismic/hydrodynamictests on BIF 18", 24" it; 30" Butterfly Valves. G ~ Shipway

2. These valves are in QID files 361106 and 361104.

3. George is skeptical test data exists for thosebutterfly valves experiencing the extended fre-quency range of the hydrodynamic event.

P.TT AC'r'hi=I"

'S:lgn

Signed:

Distribution:W.Schlafer Page of

L. Eammerzell, J. Read, H. A o o a, . see, roy ect: 3.J.e

4 4 C J I cllllllllj!I!ill!!!!Illllllll

;:-"; EC '.-I V",= D

gfJI'1 fy d

tr is~P I"tI'~l f ',t -( -"

CommunicationsReport (~~~ e~™~

CompanyI r nw Itiv1 > Telecon 0 Conference Report

Profe !~ ~ ~ Job No.kauipfttent Seismic/Hydrodynamic Requalifi- '2044

r gati 6./1 5/8 2Subject Interim Dynamic Loads C

Pwticit o riParticipants'

r ro man

Jim Foreman

4

JoBNo~FiLE

No.~~'ime

1 1 00

Richland Office

of n

Nyle Laboratoriesof

of

Item Comments

Joe Braverman of Burns and Roe was contacted bytelephone on June '15, 1982 to get a clarificationon the subject criteria for use in the Requalifi-cation of Equipment for Seismic and Hydrodynamiceffects.

Rep'd Action By

Joe concurred that the accel eration va1 ues shown inthe table of the attachment to the conference notewere intended to be used for rigid line mountedcomponents only and not for flexible components.i.e., those having natural frequencies below thecutoff frequency. To be consistent with B6R re-commendation for qualification of line mountedcomponents by test would indicate that for the anaysis of flexible line mounted components a staticload would be applied at the C.G. of the extendedstructure equal to theamplification factor for sinsusoida1 motion at a justifiabl e damping value.For example, for an SSE condition the amplifica-tion at 3tt damping would be 50 divided by 3 = 16-7This loading may be in some cases present a veryconservative loading on the line mounted componentA somewhat more realistic input motion would be

Signed: Page1

"3

Distribtition'tandard Di ~tri hut i on rfg ol @~et ~ . «tc~ . <Et r~f

llfillllllllllllllllllllllllll


Company: Cy<na/Qlyl e Telecon

ProjectEquipment Seismic/HydrodynamicReaualification

Subject'nterim Dynamic Loads Criteria andFatiaue Criteria

D Conference Report

Job No. 820446/15/8211:00

Place: Richland Of jceParticipants."

Joe Braverman O'Yof Burns and Roe

Item

Jim F A~ACHig~<~tj7 of ta V T

dOB No, r'logeof

C .~OI.8H FT Xr .f.

Req'd Action By

continuous sine beats of 12-15 ocsillations perbeat as recommended by the IEEE-382 draft "Ameri-can Standard of Safety Related Valve Actuators".The amplif'ication for a 15 oscillation sine beatat resonance for 3K damping is approximately 11.5.

If the static loadings given above show an over-stressed condition or deflections which wouldcause operational malfunction, the alternative todevelop a more realistic approach would be to per-form in. situ testing from which the data could beused to develop response spectra at valve locationThe in-situ tests would allow the determination

of the natural frequencies and mode shapes ofa sufficient part of the piping system along withthe valve and extended structure to validate themathematical models used to generate responsespectra'at the valve location and/or componentlocations on the extended structure. The responsespectra at component locations allow direct com-parisons with component test data. It is feltthat a combined test and analysis would be a feas-ible and cost effective approach.

Signed.' xi''tandard Distribution

1020 00

Page of

c~ c. s t. i cc s t F


&Ull I I I I Uj j jf 'ct L(uj jS

Report

D Conference ReportTeleconComPanyCyqna/Ny1 eProfect Job No. 82Q44

Eouipment Seismic/Hydrodynamic Reauali- Date; 6/15/82cSubject Ff,

Interim Dynamic Loads Criteria andFatigue Criteria

Time.. 11 - PP

Pfttce'i ch1 and OfficePanicipants:

Joe Braverman , Burns and Roe

Jim Foreman « 4 le Laboratories

of

Item Comments Rett'd Action By

Burns and Roe is checking to see if fatigue cri-teria have been developed for b7Ãp-2 and will noti-fy Cygna/Nyle not later than June 17, 1982 if such

criteria exists. CYGNE»A

ATTACHiM~~AIT

coo NO.QQ~«FILE NQ.

SHEET NO.

Signed: +~~

Distribution:

'c:tanya-.d Distribution1020 00

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Company:

Project:

Subject:

CES

WPPSS

Teiecon D Conference Report

82046/CR-008Date: „6/11/82Time:

Qualification of Line Mounted Equip. Piece: SDAOParticipants':

H. Reeser CES, RichlandofW. Schlafer

ofCES, SDAO

of


The new work authorization had not yet been re-leased. Use the Initial Analysis EQ-12-3000number for the week-ending Friday 6/11/82.

2.

3.

Hal recommends that as a result of using our bestengineering judgment in the qualification of linemounted equipment, it is more prudent to fail a fewitems first before presenting WPPSS with our concern for a more well defined position on linemounted equipment qualification. At that time, wcan present a'lanned approach for additionalanalytical and/or in-situ testing to be conductedwhich. will yield data needed for a more accuratedefinition of the dynamic input to line mountedequipment.

An examination of the preliminary horizontal OBEand SSE response spectra outside the containmentbuilding for a frequency of 8Hz, indicate that the'

levels from Attachment 1 (of the Interim DynamicLoads Criteria) to be used in the static analysisof line mounted equipment not affected by hydro-dynamic loads, may already have a multiplicativefactor incorporated in them. This factor may notyet still address the issue of a possible resonancecondition of the line mounted equipment whichwould result in even higher g levels for use inanalysis.

YOND< TACHMEHT8 iXO.~+~

LE NO.

z TN0.~7'."

Signed: W. Schlafer Page 1

Distribution: L. Kammerzell, J. Read, H. Reeser, J. Minichiello, P . Guglielmino1020.00 P.K. Pate3

IllllljlllllllljllllIIIIIIIIII


company: CES R "Telecon Ci Conference Report

Project:

Subject:

Participants:

WPPSS Equipment gualification

Response Spectra I| WPPSS E.g. Documents

H. Reeser

J. Forman

W. Schlafer

"o '82046/CR-005

June 8 . 1982Time:

Place:SDAO

CES, Richlandof

Hyle (CES, Richland)

CES, SDAO

Item Comments Req'd Action 8y

2.

3.

Hal has asked Jim Forman to help Cygna obtain. the followinginformation form WPPSS or from similar data availablewithin Hyle:a) Separate SRV Response Spectra for use in fatugue stress

analysis.b) Time histories used in deriving the SRV response spectra

for use in determining the number of significant stresscycles and duration. of an SRV loading.

c) The number of SRV events.d) The number of significant stress cycles and duration

of the hydrodynamic loads (AP/Chugging) associatedwith the LOCA event.

The large compilation of Response Spectra for OBE, SSE andcombined hydrodynamic events recently received. by the BAO,SDAO and the SFAO are to be considered preliminary.

spectra to'be used for analysis/testing.

Hal is also sending the WPPSSa) FSAR Section 3.10 and Appendicesb) The 2/12/82 submittal to the HRC concerning Equipment

qualification.

wqg G Qg's, fiiC~& e

gy-f .„CHi.fjt-it F

'l,ott'iLi:NO.~

7. (,$ oSiiEF., i'iO.~

Signed: Page of

Kammerzell, Read, Patel, Rsleh Rajan, Abolhoda, Curry, tlinichiello, Guglielminoimo.oo Reeser, PROJECT FILE



Company:

Project:

Telecon

WPPSS Equipment qualification

0 Conference Report

'2046/CR-004June 8, ]g82

Subject:(}ID File Review

Participants:P. Gu lielmino

W. Schlafer

Time: am

Pface: SDAO

of BAO

of SDAO

of

Item Comments Req'd Action 8y

2.

3.

In the revietf of a AID file, if errors in other thanseismic analysis are discovered which adversly affect theequipment's qualification, these too must be noted andcorrected or justified.If the error is such that the equipment can still bequal ified, note the error and the fact it does not advers lyaffect qualification, but avoid the expense of alteringthat portion of the analysis.

Both Peter and myself feel that a better defensibleposition needs to be investigated for the loads usedin the analysis of line mounted equipment.

p, vT>QC+ti.,z" fil t

JOB HO.~~Fll.E NO.

7. I.3ISHEET NO.

Signed: W. Schlafer Pageof'""

"''ammerzell. Read. patel. Hsie@ Raian. Abolhoda. Curr . Minichiello. ReeserPROJECT FILE



company: CES

Project:

Telecon

Subject:

Participants:H R

W. Schlafer

WPPSS Equipment qualification

0 Conference Report

'8204 R-00June 3, 1982

Time:

Place:

of

CES, San Diego

of

Item Comments Rett'd Action By

2.

3.

Hal questioned his immediate contact at WPPSS, DennisArmstrong, about the number of SRV events and number ofcycles. Their reply was "we don't know".

Hal has suggested that Cygna investigate these issues,formulate a position, and then get WPPSS concurrence.

'inceWPPSS has generated combined response spectra forseismic and SRV events, I suggested to Hal he obtainseparate SRV response spectra and time histories fromwhich they were derived. This will help in determiningthe length an SRV event and the number of significantcycles. The number of SRV events is more difficult todetermine and possibly needs a more thorough'nderstandingof the BWR's systems.

Hal will be our contact in Richland to submit our ActionPlan and cost estimates for approval.

HGR

Q'tf'QUA~ r. AcHME~~T

.>0- >>0.

p>LE NO

EHEET >>0. 1 I 12

1

Signed:W. Schlafer ."f.w Page ol

Distribution:

1020 00

I'ammerzell, Read, Patel,~Brreh, Rajan, Abolhoda, Curry, Guglielmino,

Ilinichiello, Reeser, PROJECT FILEWS:ib

llllllllllillllllllllllllllll.

COf f ft I IUiRICatlOf1~

¹pot'otnpan~

Ftofec!

CESX Tetecon o Con'.etence Re por.

Joo No, 82044

4NP-2 Eouioment "Ouali ication 4 / '7 P. / A 0

Subfec!,

F arnot pants

Tinte''eldsize at %'alve Flange/Ear interface

Richland

Don Searle

R1 Ck Ri C29'D1 tool

of

CES/RBO

ElF /t0l-885-1000

of

Iten. Contfnents

Reouested ano received information concerning tneattachment of the rectangular shaoed "ears" to thevalve body flanges.

Pick info med mc tha- all of these items- vere af-: xed to the valve fl-tge by means o we" ding.

Rea'o Action By

a) 0.3l')

0.3T":la..ge

llet weld three si3 '/Groove welc onface.

oes~ 1"sn %v~sn

R-"e" ence: B ~ G" a~ iso: P.'~27"'34, Pi'7"J.ssemb ' D av lng: A-2GC/Q7

ATTACH~AF-'4T

JC3 NO.oi. ~(,F"ILKNO.

3HMT NO.'t <.35

S cnec > ~~.~,Jg Race 0

v,,an a c -,e - ~ . fr,.:s t ong ..'.. ScG t; R ~ f'.1cK:ian,"-rc-'ect .. ='' e,t-'-:D. SearLe G== ice

Sub)ect

Date:

Place:

Purpose:

Pres nt:

Notes:

July 16, 1974nce Notes No. 258

,Jgg g 7~yndrickson

~~ ~~>A-RlP%„'g'jgPPerryMHroncichDMurphyHRehCVesy (PT&O)RLukenRECampJHaganHDoonRWoodwardJBlas (2)HSybi1JO'DonnellAWChamos

Confere

'-0- 2808Washington Public Power Supply SystemWPPSS Nuclear Project No. 2Contract No. 68

!a"a-Jii:lych.",-';<1.,974~ -"-'-<,

B ~ X.F ~

Providence, Rhode Xs land

Rem, '...::, nmmenee~n Bm'aa1hanMa1 nn'. annnnan 'meeBCO"iT"tde V'in~ t fee a an B

B.I.F

MGooamanSFoxJVZalavadiaDSheikhBBedros'anRBa ldwin.EFerrari (6)MKahnpfdb

Burns and Roe

D, SheikhJ. V. Zalavadia

OCCOcca* Part Time

lCi ..CO CP

1. Documents to BIF

BVGFa)AATTACHMENT

Burns and Poe Comments on Q.A. Manual-Burns and Roe letter BRBIF-68-74-011, da tedMarch 19, 1974.

J.P. Cunningham - Product Engr-Butterfly Valves*T. Masse — Engr. Product Mgr. — Butterfly Valves*G-F- MacDonald -- Director Nuclear Q .A.'*T. Wolfe — Marketing anager - Butterfly Valves

2. Seismic Calculations — B&R Comments

Burns and .Ro~~e'ES'"

JOB NO.~~+na.B No.BBePT NO.

a. C~ha ~e~mar, xa ~." TM~~„,"=:!'>6;-'" ~~~w~hicb='acrm~g~g~;-

.„Xro'n " '~~eB pter ontract Specif ication.b. ubmit the ~g4 „Ohab+~~pgre,mriW~TZ.:P~~r~"™~>

c. Submi" the calculations for the detail of seating torquevalue, used in design calculations

~ I

f . Submit;.'p cjo~~ti'-there.~wohu:1d:;:be> no'W'oss „of"fuacWon-.,du~ing.'xa'n'd .ref t'ei:thee jr'esecsr'ibemd-'seismicd't~banc~a'll:eritrhone>d in™pacrag'rar'h''"~3'"of'hepecific.-xtion. The seismic calculations include

stress an lysis only. The analysis for strain/deformationis also'required as a proof that there will be noloss of function.

g. Submit analy is or proof that radiation will not~adve slv a feet the yield point of the material.Submit analysis and design for. 72" and 84" valvesconsidering normal. load with the combination of >>

SSE stresses shall be maintained within the normalallowable working stress limit as mentioned inparagraph 3.3.1.1 of specification. 'h

3. Mandatory Testincr for Seismic Qualifications

~W~~for.,m'56ik~;.™sMi%eRQs+%te, ~R~eatwo ned;ih-:".~4"„,,~~pea&'EH5'M+in. 5l~eQXxe'5 'tea>"'t'>th'eyx.~b'av~-a.lready.-'~~'.~:tested the same type of equipment for greater accelerationothan Burns and Roe specified and that they will subthe test: data for Burns and Roe review and approval

4 ~ Stardvne tlodel used in Seismic CalculationsP TTACHMEh

I>Rlmmx, „., Lh,ln' mcco1XX!rnernnsmn~oe:".command's

the<"SZMM~~535"d~Yi's5~oP,."84''aRB+3Y'. <VETves.~~~~!1&0>4'

sosh . '3 n 1 T"Xm~>~~ r

',QQB NO.~~FILE NO

SHEET NO.'7. (.3<

6.

7.

':",oe~dgas 'o .,r-, „..,.. ha.t~-halva hv,.s~w-i@=...QP. A. C'V'LLIggjg~peo &Le~a-i:"'- <>>cia>eeI'xmenL CX>>Ied~>i>i~i>In>Ceje'C Xr~m>>~pr .B~„:; re'o TVedgbag;: 6Ke~g„.,ea'nRot~nÃl'@Mrna'l%Qj ro%'~.'tiff>s, SpV t<~™

Chey~wW~L'C..-l: te~~v~a~;;the-dt im'e -d j=-.Ieakage"..;.t'es.t;.- x,n~I.'.the-~pi.<EMaC~8&Beeui'.a~'aa~~Ra~ii'~eetOr"..~i@'i t '>hem ".COn gaia>C t>-Scpecifi'ca t ion'--'requ'irem'enl ts'.

W5U e.--'Ec'.centi&'&'bC-&Can'd<.r~..~~~~@~ pMme>1AM

" AIFeKdFd~oxcce orL — — h'ehh:ebould'„-cones. 'e -doubleeccen~~~o~tQ~Mnder." v~1~;id'esi:.gnfzi~trunnn ion pi:rp,ins t cad"-.- o f.—,„"thes~naing1e~ccerj~hc x t>y~cons i dered;"„i~. -30 ";:24 "va ives. 'w-.-,'EXp~~ieecL~Lo~ggo: t+e -„"ro5'lcm ...'~~","~i"

M~maa1 Breauermxe'~6f<WS™~4-.7;:and:;.30 "~ Valves ",'

Bu ns and Roe asked B1F to submit the natural fundamentalfrecuency of 18", 24", and 30" valves. B re;

'<T:.~at~>Lt'„..~~

. C~g scop .,of,, her"6t, ".Ph + 'll'ih&M'M+-:i6-~Yid@k&e~ega'rQi.'ri j&dcK'0"=YiVT<1 "ccats t .nr this

1 1an:.i Roe state; > th;:t a;L'. 'L.vl:.:wl:;~ the).rql!ctat cn nd after !'PPSS's approv.-l Br>ms ..nd:.',re '~> 51h;Ot-'. fy B>F i ~ a(MltAhDna I WOX><..l S Ou Cn>>r)ZC(is (B '' slrOr!I'>'!.; F c-I ~, ll-h o l 'rh! le <'> '>> <37.: l>v t- '>

< lr()o!l<n that tho co:>t <'L

see r, ~ ~ ~ se h/ 'ppaeehh ae

additiona'ork w'l be $ 300.00) .

General-BIF Comments

BIF indica,ted as follows:

a. If operat'on or acc'dental temperature is high, thcrubber seal should be on valve disc, correctly specifiedby Burns and Roe, instead of valve body. Rubber sealif on valve body, is fixed by glue, which cannot resisthigh temperature. Rubber seal on valve disc is fixedin-between metal pieces.

b. If water or any other fluid is supposed to flow in thepipe, the shaft in the valve should be vertical. Thevertical shaft would mean C.G. of pressure due to fluidwill'be on the axis and hence much less driving forceis -remi ed to operate the valve . But in case of airor steam it makes no difference.

9. ualitv Assurance Hanual-

Burns and Roe stated that Burns and Roe comments on BIFQuality Assurance Hanual was mailed to BIF on Harch 19, 1974(BRBIF-68-74-011) and was classified "Not Approved". Theresponse to these comments has not been rece'ved as of this"date. BIF stated that the BIF Plant is on vacation for.2 weeks (Ju ly 1 thru Ju ly 12) . I lr. HacDona, ld will s tar tupdating QA Hanual on July 15 and he e..pects to complete byJuly 19, 1974. BIF will revise their Q.A. Hanual and/orprovide necessary supplements to the manual as per Burnsand Roe comments. Bu ns and Roe comments were discussed.Hr. HacDonald will call Hr. Sheldon Paige of Burns and Roeon July 15, for the clarification of the following Burns andRoe comments:

a. Corrective actionb. Audit of Purchase Regs./P.O.'s/change ordersc. Complian'ce to supplier Quality Control Progrd. Compliance to Lower Tier Procuremente. Welding Process Sheet Form N-152 (BIF) and t

of Contract Specification 17A-30 and 17A-31

10. Inservice Insaection Recuirements

fQPPS~2oC4

PILH NO.~ggKET NO:

Burns and Roe auestioned regarding the requirements of"calibration blocks" in accordance w'th the draft of the1974 Edition of ASHE Section XI, Article I-3000 "Prep rationfor Calibrat'on" for Inservice Inspection. BZF stated thatthe special calibration blocks are not required. They willsubmit detailed method of Inservice Inspection with StandardCal.ibration blocks.Zt~- 0:"i~~3 t~ '~:- L-.;- '3'.R

Decisic;n on B, guoLatiol')n ca ':: Lat .ons on nc tu

12 e'

tern

Owed to B&R bv-.',-8 P.

a.; Suzvxssz.on o~ev'C"M'sexsr;.~E'XeaMMons as'-per:-"3 tern Mo'."e-"'2'".!3~aadeP''above".' ",."

b. Suhmissi.on of revised Q;A. Manual (Item Ho. 9)

Inservice Inspection Recuirements (Item hTo." 10)

JJV/JV2/dc~i

~~dÃe<"

prepared by).~

Submitted by Q6~0e~

cc: Mr. J. E. Noolsey — WPPSS -3Mr. P. C. Otness — BPA -1

CPG($ :~$

PTTP,{'H'MEN~

„)OG <tLO.~.yl. F

Fl- g,NOHP"-7 NO.

e

~ e e ue ~~ I 9 ~

QIDg 361106

7.3 BIF Report

B I F A UNIT OF GENERAL SIGNAL1600 DIVISION ROAD

WEST WARWICK, R.I. 02893

QUALIFICATION OF PRIMARY CONTAINMENT BUTTERFLY ISOLATION VALVESUNDER LOCA CONDITION.

DYNAMIC TORQUE CALCULATION OF BUTTERFLY VALVE

PREPARED FOR:


VALVE SIZES 30", and 24"WPPSS CONTRACT NO. 68BIF ORDER NO.: PN27234 & PN27235WPPSS IDENTIFZCATZON NO. CSP-V-1 & 2, and

CSP V 3 & 4

Prepared by.-

Date:

Checked by:

Date:

Debeadra K. Dae

Qov. 10 19 62

Dezso Szila i

REPORT NO. TR-27234 AndTR-27235

Al i ACHMEQY

TABLE OF CON~c TS

SECTION

1 ~ Summary

2. Dynamic torque tables

3. Ref erences

4. Analytical Procedure and Flow Data

5. Analysis for 30 inch valve(I) a. Hand Computation of several test cases for air flow 25

b.'omputer results and comparision with hand computation 28

(II) c. Hand computation of several test cases for steam flow 40d. Computer results and comparision with hand computation 42

6. Analysis for 24 inch valve(III) e. Hand computation of several test cases for air flow 53

f. Computer results and comparision with hand computation 55

(XV) g. Hand computation of several test cases for steam flow 67h. Computer results and comparision with hand computation 69

7. Appendix 80

a. WPPSS Calc.No. M-02-83-08-0, Sheets 1 thru 9b. LOCA Temp. Curvec. LOCA Pressure Curved. WPPSS Letter dated 10/22/82e. BIF Flow Loss Coefficient K plotf. BIF dynamic torque Coefficient CT plot

'SUMfMRY

This report contains the„ dynamic toraue analysis of two butterflyvalves of sizes 30, and 24 inch. The analysis is performed forLOCA (loss of Coolant Accident) per'WPPSS Specification, reference

1 on page six of this report. The analytical procedure and the

assumptions are outlined in the section beginning on page seven.

Dynamic torcue calculations have been performed for two media,

namely, air and saturated steam for various angles of opening ofthese valves.

The results of the analysis tabulated on page two through fiveof the report indicate that the dynamic torcrues developed under the

specified flow conditions are less than the design toraues used inthe. original Seismic and Stress analysis o these valves. Therefore

the valves are safe against the action of dynamic torcrue in the

event of a LOCA.

O'II'GNAAT i ACHMKST~~ ~PoRLE NO ~oT o F...SHEET 40. 2

SUK LORY OF RESULTS

T3.mes

1.0

1.5

2.0

2.5

3.0

3.5

4.0

4.5

Table — 1

Angle Wdegas

90(Full open)

78.75

67.50

56.25

45. 00

33.75

22.50

11.25

30 Inch Valve, airflowDynamicTorquein-lb11020

23098

18138

14747

12428

10780

8014

3972

5.0 9. 0 (Full'losed) 0 0 * TNet= 22174 in-lb

* At full closed position the dynamic torque is zero and the net

torque is due to seating and bearing friction.NOTE: The design torque used in the Seismic analysis report

I

No. TR-74-8 by McPherson Associates for this valve is27800 in-lb. Therefore the design is safe.

SUMMARY OF RESULTS

TimeS

1.0

1.5

2.0

2.5

3.0

3.5

4.0

4.5

Table - 2,

Angle Wdegas

90(Pull open)

78.75

67.50

56.25

45. 00

33.75

22.50

11.25

30 1rch Valve Steam- flowDynamicTorquein-lb

11032

23175

18142

14668

12424

10580

7809

3867

5.0 9. 0 (Pullclosed) 00* TNet= 22174 in-lb


torque is due to seating and bearinc friction.

SU?&fARY OF RESULTS

Times

Table — 3E

Angle Wdeg.

inch Valve; Air flow

DynamicTorquein-lb

1.0

1.5

2.0

2.5

3.0

3.5

4.0

4.5

90(Full open)

78.75

67.50-

56.25

45. 00

33.75

22.50

11.25

9. 0 (Fullclosed)

5525

11692

9095

7428

6239

5430

4043

2020

0.0 * TNet= 13808 in-lb


torque is due to seating and bearing friction.

Note: The design torcue used in the Seismic analysis report

No. TR-74-7 by McPherson Associate for this valve is~

': '70/>in-lb. Therefore the deisgn is safe.

A t iACHMESY~ m,~PO<~qFtLE HO ~ot o F..SHEET HO. S

SUMMARY OF RESULTS

e TimeS

Table — 4

Angle Wdeg

24 Inch Ualve, Steam flow

DynamicTorquein-lb

1.0

2.0

2.5

3.0

3 5

4.0

4.5

5.0

90 (Full open)

78.75

67.50

56. 25

45.00

33.75

22.50

11.25

9. 0 (Fullclosed)

5425

11394

8921

7213

6109

5202

3842

1902

p 0 * TNet= 13808 in-lb

.* At full closed position the dynamic torque is zero and the net

torque is due to seating and bearing friction.

REFERENCES

WPPSS Specification 2808-68, Calc. No. liE-02-83-08-0, Sheets1 thru 9, dated 10/8/82.

LOCA Temperature Curve Fig. 6.2-2.LOCA Pressure Curve Fig. 6.2-3.

ANSI/AWWA C504-80, AWWA Standard for Rubber-Seated ButterflyValves. American Water Works ASsociation, Colo.

Beard,C., Final Control Elements, Valves and Actuators, FirstEdition, Rxmbach Publications, 1969.

Hutchison J. W. ISA Handbook of Control Valves 2nd EditionTorque and Sizing Calculation for BIF Butterfly Valves, No. D-214590,dated 1/9/ 5 for WPPSS Contract 468.

B I F Test Report for Dynamic Torque and Head Loss Tests of CastIron Streamline Disc versus Fabricated Flat Plate Disc datedMay 13, 1974.

B I F Test Report iTR-0650-43, Hydrocynamic and Headloss Test of12" - 150 Lb. Butterfly Valve with directly connected short radiuselbow upstream, dated 2/24/82.

B I F Drawings: 30 inch Valve General Arrangement Drawing A-20676324 inch Valve General Arrangement Drawing A-206764

QID4~361106

7.4 McPherson Associates Analysis

'

~ ~

I

0

~ ~

BXF A UNIT OF GcCKRAL SIGNAL1600 DIVISION ROAD

NEST NARNXCK, R.X. 02893

DESIGN A'K) SEZSiMC ANALYSZSOF

24 CYLINDER OPERATED BUTTERFLY VALVEFOR

WASHINGTON PUBLIC PO~ SUPPLY SY~AND 0

BURNS AND ROE

CUSTOMER P.O NT 68

'BZP 5EO . "R~hO'MS-U-0708,'236-U-0808.

I ~ 0

B r S PN27235-1 th~ '4PN27236-1 theo '3

REPORT NO. TR-74-7PREPARED BY McPHERSQN ASSOCIATES, ZNC.

APPRO~~ BY 3 7 7(f'

I/5I7+ ~I@~ 1~

DESIGN ANDSEISMIC ANALYSIS

OF24" CYLINDER OPERATED

BUTTERFLY VALVEA-206765

22 February 1974

Prepared For:

BIF 1

A Unit of General Signal Corporation

Prepared By:

Thomas M. RileyJohn R. Henry

A Unit of Generai Gisnp Co'rpfrationPurchase,Orf er Nq 8+468-68

M he son''Associates, Inc.aport No. TR 74 7-- -<eLta»J» les

~ . ~

408 No.'PILE NO.

OHEKT N

RP~) 9..ol. F

McPherson Associates, Inc.400 Totten Pond Road

Naltham, Massachusetts 02154

4C MS «~5 ~~tel

400 TOTTER PONO ROAO ~ WALTHAM.MASSACHUSETTS 02154

DESIGN ANDSEISbll C ANALYSIS

OF24" CYLINDER OPERATED

BUTTERFLY VALVEA-206765

BIFA Unit of General Signal'orporation:

Purchase Order No. 84908-63 40E HO. E~~>"'I

PLE Ho. ~O. o i.P'HEET

ND. ~~

(~X()

V'cPhersonAssociates, Inc.Report Ho. T R74- ~7- RSV- | i'd/~)/vs

FOR 24" VALVES

BIF Contract No.

68

BIF S.O. No.

N 27235-FN 27236-F

Valve Tax No's

CSP-V-3CSP-V-4CEP-V-3ACEP-V-4ACSP-V-5CSP-V-6

REVl S lOH RECORD

NUS REPORT TR-74-7

REVfSlON 1 12/31/75

Page 3

Page 5

a) Hat'1 was ASTM A-126 s A-48b) Allowable Stress Yalue corrected

a) 'rive Lever was.8-184005"6b) Clevis was D"146578

Page 9 a) Hat'1 was ASTM A-126, Class C 0b) Corrected yield stress allowab ec) Deleted ASTM A-48

Page 32 a) Ref. drawings were " 840054 pD-t 578

>agas 33, 33, 36 < 37 ~ 4 X ('x~a) Hat'1 wa~M A-32& '

b) Corre Cad'Stress AQcwab le

JOB NO.~B~'~

PLE NO O&.ol V

ONE ET NO. +

Section 1.0

QlTRODUCTlON

The purpose of th's report is to determine the structuraladequacy of a 24" . Butterfly Valve Ass emb 3y when s ub jected

to seismic accelerations as described. in Reference '1 and

to insure the valve design is in accordance with Reference

o this report. CVGNAATTACHMENT

The se"'smic plus operating analysis is performed in accord-

ance with Nzshington Public Power Supply System Specifica-V ~tron No. 2808-68, Reference 1, and all applicable information

as described in Sec ion 4,0 of this report..

Section 2.0

'SENARY OF RESULTS

Q)

) K~ ~

~ ~

'hy Q)r'

~tt ~

~ ~ ~

~ ~

~ ~

~ I t ~

ST~(WW~ETET t'l 74 SuaJEETCHKD, SY.A .. QATAR..Z d~

<cg~ V.V'v.c' rt~ h R'$

t

SHEET NS. S S -Sldd8 Nd.

3~A

C4fWP&CLl7

0 ~

.R<QQi4Q P<QL

'

~"< ' et TX 0 0"J~ gQ

Cgt.S 5Q~Cu. IJ) sf

+VCC C'menSeu (r i') a hhT<CS SL

7SI'ffg C.C ay =flfoo (5g L-7T'St,I I

zz flz( Sy flfodo C Ilsl-010 0

S AhtI C 5~= 3bSSO fPPIA-3G )w . c~ = zg ~ C4sssf

a ef iS Pie

bccvC l-v~

YHAz po+ "EhPd

Bhfiolup p.~

P= ff3G C .S 5y-- ff'00 (B-Z

II = 4S< <a C ~~ = 4S~ (Z .

16~$ 1K 'Ey ~ z8~, (5)

~t z,7 ~ sy, c~~z.~~ (><-

ONAA EST401 fIO.~<><~

. O~SI.V,'Hs

No.Q->

SlkhS- S,

78M Px)5,

Vhhue'my

GLAIR t=M~~

M~V KEaa~~c Cevcg

S3r,'

~~ ~

a.7=.1axa7 <,I.a- z7,«> («,, ~ ~s.z. - K a'nfl' s Issso I tt sE -. j

1+~tt IO Ss +~HIf S lES 0 (SS E7'

'-f."~» 1> <>c.~ a ~ * IoE=T ( s ~Hits)mWK&HC%N C Q~)Z ~py

~ ~

+ICRLl+5$ C +~M~ QL3f /

tee pars To ST'P- -s5 )g~wq<l~

C

~ SH

3~ ~

~ I

Section 3.0

CONCLUSIONS

I ~ ~

HcPhers on Ass ocia es, Inc. concludes that all components forthi 24" Butterfly Valve, as analyzed in this report, meet therequirements'of all governing specifications for seismic and

operating considerations as de ined in References 1, and 3 ofthis report.

mSHa~E>'ILEHD.~O. o I. F

SHEET HO. ~

'

TABLE OF CONTENTS

Section No. ~Pa e

:Table of Contents

Certification

1.0

2.0

3.0

4.0

Introduction

Summary of Results

Conclusions

References 0 S

CYGMAA'rTACHMENies wo. '~>'>~<

Pgg gQ,~O'0 I'F'aavND.Q-~

Dc'eeeer gee cree See

6.0 Analysis 10

6.l.

6.2

6.3

Cylinder Operator;Ns emb

c(XCylinder Support Eracke~

Clevis Assembly an Drive Lever

14

23

6.4

6.5

6.6

Valve Body Support "Ears" and AssociatedHardware

~ ~

Shaft and Disc Assembly and 'AssociatedHardware

Valve Si "ing and Stress Analysis ConsideringCombined Operat'ng and Seismic Conditions

38.

. 46

Certification

McPherson Associa es, Inc. certifies tha the 24" ButterflyValve, A-206765, as shown on the customer drawings was

analyzed in accordance with Nashington Public Power SupplySystem Specification No. 2808-68 and to the best of our

Knowledge and belief, meets the requirements of Paragraphs

3.2, 3.3, and 3.5.2.4 of this document and Reference 3 ofSection 4.0 of this report. meso. '»"«

p~~ gg ~O ol ~F.oHEav no. C+

Xr/h. v

John: R.(Fenzy~~) FRegis t'er ed'Qr ofess ional Engineer

qMass.'. Regis"-ation No. 25929

Section 4.0

RFFERFNCES

l. Nashington Public Power Supp y System Specification No.Z808" 68.

2. BIF Drawings

Drawin No. Revision Descript on

A-900523A-900524A-900339A-900340A-208293

~ B-&00521,B-900522S. Z'I>8~b

CD pe Ql'LQ)'2+ I

D-206661

3 ~

5.

6.

. M-206765 B 24" Butterfly Valve-GeneralArrangementsBody, FabricatedBody,.hfachiningDis c, Fabricated ~~Disc, Machined,

. Cylinder Support BracketOperator Shafts.Drive LeverClevis ..',>' ~)Miller C Tinder<>

Section XXI, Nuclear Power Plant Components, AShfE Boilerand Pressure Vessel Code, 1971 w'th,Addenda.

+)'v'Virgil

Moring Faires, Design of hfachine Elements, 4thEd" tion, The MacNillan Co., N.Y.', 1965.

Raymond J'. Roark,. Formulas;.So Stress'nd Strain, 4thEdition, McGraw Hill Book Co., 1955.

Laddish Catalog No. 5S.

~E gC EPOS

SLEWED. <~oi S''

OHEET NO.G

7 ~ Grinnel, Piping and Engineering, 3rd Edition, 1971.

8. 1963 Supplement to Sc=ew Thread Standards for FederalServices s

9 ~ Baumeister ff Marks, Standard Handbook for MechanicalEngineers, 7th Edition, hfcGraw Hill Book 'Company.

h ~ical Engineers Handbook.

S T M. Standards - Part 2.

Handbooks

~ ~o and Goodier, Theory oZ Elasticity, 3rd -dition,'cGzaI( Hill Book Co., 1910.

1 ~d Smith, Advanced Mechanics OZ Materials,ad Sd tion, John Wiley 4 Son, Enc., 1966.

cry>s Handbook, 17th Edition, The Industrial Press,zcHznery364.

„-tion yrZT, Pressure Vessels, Division 2 alternativeles, p.S.~l.E. Boiler and Pressure Vessel Code,<1971.

nubble P»hler.shing Co., otanaara tiara- at'cs>Les, Tve3.=th edition.

ler=can "fational Standards Xnstxtu e .- Document B16.5tied "Steel Pipe Planges and P3.anged Pittings."

.. 'y'q( V:~ ~

~ ~ ~

J ~ ~~ ~ ~ ~ ot

yIgg R209V

SCX WO. <~ of ~

Q4EET NO. ~~

~ ~ ~ ~

p ~

g ~ ~'

& ~

~ ~ ~ ~

~ ~ ~ ~

~ ~ 4 ~

~ 0 ~ ~

~ ~

~ HIKQMRu.

~ ~ ~ ~

~ ~ ~

~ ~

~ 0

~ ~ ~

gg ~ ~ '~ '

~ I~ ~ I

~ ~~ ~ ~ ~ ~

~ ~ ~

MMM

M

~ ~

'".~ IIIIIIIIIIIIIIIIIIIIIIIIIIIIII

FinalQualificationReport

PROZZCT: Equipment Seismic and Hydrodynamic RequalificationO'OB NO: 82044

CALC NO- OS.01.F

CLIEVl: Washington Public Power Supply System

QID NO- 361104

TITLE: Equipment Seismic and Hydrodynamic Requalification of30" Cylinder Operated Butterfly Valves:

CSP-V-1 and 2CEP-V-lA and 2A

PREPARED BY:

REVIEWED BY:

APPROVED BY:

M.A. Scott

/L.C. Fernandez PC+~w >a&.

JF. Khanachet

6/15/83DATE

6/15/83DATE

6/15/83DATE

REVISION:

QID=:. 361104

REVISION STATUS LOG

~'ev.

No. Date

Preparedby

Reviewed.by

Approvedby CygnaEnergy

Services

Approvedby

M'PSS Descrzptxon

0 2/16/83 R. HsiehH. AbolhodaJ. Rakowski

Original. Issue

L. Fernandez

1 6/15/8Scott

Pi 8L. Fernanctez, tl

evised tocorporate

ddition of shearlates

Revision+1 1.1


REQUALIFICATIONCERTIFICATE

WNP-QZD 361104

COMPONKNT NO1 -V- gp -V-2 P-V-2A

CDMPDNKNTDKscRIPTIDNs" vlinder Ooerated But ter f1 Valves

MANUPACTURKR1

KQUIPMCNT CLASSIPICATIONi gJ ACTIVE Q PASSIVE

A-206763

SEISMIC QUALIPICATIONRCPORT REPKRENCEs

C gna Energy Services, "Equipment Seismic and Hydrodynamic Requalifica-tion of 30" Cylinder Operated Butterfly Valves," File No. OS.01.F,QID No. 361104, Revision 1, June, 1983.

ikRE UIRED ACTION: 1) Re lace A-307 Ear Bolts with A-325 bolts.

2) Addition of shear plates, see sheets 4.3.30to4.3.48 for additional details.

THK ABOVESEISMIC QUALIPICATIONRCPORT5 HAVC BKKN RKKVALUATEOIN ACCORDANCE WITH

THC CURRENT NRC SC15MIC CRITERIA!

I ICEE STANOARO5 244 {197$)

2 U5NRC RKQULATORYCUIOKS 1.92, I 144

2a 5TANDARD RKVICW PLANS ~Ma 5 14a ISED

4, NURCC&$$ 4

This equipment is qualified asa assembly when the air cylindersare completely qualified addressedin QID f018001.

THC ABOVC COMPONENT HAS BCKN POUND ACCEPTABLE POR PCRPORMINQ ITS INTENOCD SAPETY RKLATED PUNCTION

WHEN SUSPECTED TO THC PLANTSPCCIPIC VIBRATORY LOAO5

PREPARED BV

R EV IKWCD 6 Y

APPROVED BV

J.E. Rakowski 8 ~~4~ Da iA./D5~ p/r ~ i ~~HM.

DATE3 25 83

OATK !OATK

941 12574

Revision 1 2.1

WASHlNGTON PUBL1C POWER SUPPLY SYSTEMB S

J c fllllllllllllllllllllllllllllll

I PLANT NAME: WNP-2

Qualification Summary of Equipment

TYPE

QIDN 361104Ref. Mo.

NSSS: GE Burns & Roe BwR 5, Mark III I ~ COMPONENT NAME:

I ~ SCOPE: Q NSSS

y V.COMPONENT Np CSP-V-1 & 2

CEP-V-1A & 2A

2 MOPEL NLf4BER. A-206763 PUANTITY:

5G VENDCR: BIF .

4 IF THE CCMPONENT I S A CABINET OR PANELS NAME AND MODEL NOG OF THE OEV ICES I NCLUOEO

N/A

PHYs IOAL pfscR IPT I pN + APPfARANcf Butter f1 Valve with 1 0 " C 1 0 erat

b. DIMENSIONS: 30" Nominal D' t r1208 — Valve Assy; 914 — Operator & Bracket

6. LCCATION: BUILDI NGs

ELEYATIDN. 508 'CSP) and 588 'CEP)

T, FIELD NIONTING CONDITIONS: Q BOLT (NO SIZE )

WELD (LENGTN )

B y SYS'EM IN wHICH LOCATEp Containment Supp ly Purge Systems (CSP )

Containment Exhaust Purge Systems (CEPFUNcTIpNAL pfscRIPTION; Primar Containment isolation revention ofof the release of radioactive material to the environment.

c. IS THE EPUIFMENT REQUIRED FOR: Q HOT STANMY Q COLD SHUTPONN

Q BOTH Q NEITHER

9 PFRTINENr RfFERENcf pfSIGN spfcIFIcATIpN~ WPPSS Spec . 2808-68

I I I ~ IS EOUIFMENT AVAILABLE FOR INSPECTION IN THE PlANT: g YES NO

PAGE I OF 5

Revision 1 2.2

Qualification Summary of Equipment (Continued)QIDI 361104

Ref. NoI V EQUIPMENT QUALIF ICATION METHOD:

TEST

QUALIFICATIONREPORT:

X ANALYSIS Q C(NBINATION OF TEST Ij ANALYSIS

Equipment Seismic and Hydrodynamic Requalification of 30" C linder 0 crated Butterfl Valve*

(No., TITLE 6 DATE) File No. OS.01.F, June, 1983

coMPANY THAT PREPARED REPQRT: C na Ener Services

coMPANY THAT REYI EwED REPQRT: Washin ton Public Power Su ol S stems*Plus original valve analysis

V, VIBRATION INPUT:

I LOADS CONSIOEREO: e SEISMIC ONLY

bo HYDRODYNAMIC ONLY

c X CQMBINATON OF (e) AND (b)

2 METHOD OF CO4BINING RRS: ABSOLUTE S(H X SRSS OTHER (SPECIFY)

REQUIRED RESPONSE SPECTRA (ATTACH THE GRAPHS) .. Section 5. 1 of ID 361104

4 ~ DAMPING CORRESPONDING TO RSS: OBE SSE

5 ~ REQUIRED ACCELERATION IN EACH DIRECTION: ZPA [jj] OTHER (SPECIFY) SeotiOn

OBE S/S ~ F/8 a

F/B ~

6 WERE FATIGUE EFFECTS OR OTHER VIBRATION LOADS CONSIOEREOT

[j] YES NO

IF YES, DESCRIBE LOADS CONSIDERED AND HOW THEY. WERE TREATED IN OVERALL QUALIFICATION FRO(RAM:

The calculated stress ran es were com ared to theAISC allowables, as the structures analyzed were not

part of the pressure boundary.

~ NOTE: IF MORE THAN ONE REPORT, C(HPLETE I TEMS IV THROUGH Vl I FOR EACH REPORT

PAGE 2 OF 5

2.3

Qualification Summary of Equipment (Continued)QIDN 361104

Ret. No.

V I IF QUALIFICATION BY TEST THEN COMPLETE~: N/A

I.Q SINGLE FREQUENCY MULTI-FREQUE CY RANOCM

2» SINGLE AXIS MULTI-AXIS Q SINE BEAT

3 NO OF QUALIF ICATION TESTS: OBE SSE OTHER (SPECIFY)

4. FREQUENCY RANGE ~

5» NATIRAL FREQUENCIES IN EACH 0IRECTI ON (S IOE/S IOE, FRONT/BACKS VERT ICAL):

S/S R F/B R R

6 METHOO OF OETERMI NING NATURAL FREQUENCIES:

Q LAB TEST IN SITU TEST Q ANALYSIS

7 TRS .ENVELOPING RRS USING MJLTI-FREQUENCY TEST: Q YES (ATTACH TRS I RRS GRAPHS) Q NO

8» INPUT g-LEVEL TEST! OBE S/S R

SSE S/S

F/B R

F/B R

R

9» LABORATORY MOUNTING:

BOLT (NO., SIZE I IIELO (LENGTH ) Q10» FUNCTIONAL OPERABILITY VERIF I EO: Q YES NO NOT APPLICABLE

I I ~ TEST REULTS INC(.UOING MOOIFICATIONS MAOE:

OTHER TEST PERFORMEO ( SUCH AS AG I NG OR FRAG I L I TY TESTE I NCLUO ING RESUI TS)

NOTE: IF QUALIFICATION BY A CCMBINTATION OF TEST ANO ANALYSIS, ALSO COI4oLETE ITEM Vl I.

PAGE 3 OF 5

Revision 1 2.4

Qualification Summary of Equipment (Continued)

Vl I ~ IF QUALIFICATION BY ANAI.YSIS, THEN COMPLETE:

QiD~< 361104Ref. No

I ~ METHOD OF ANALYSIS:

STATIC ANALYSIS

Q DYNAMIC ANALYSIS

EQUIVALENT STATIC ANALYSIS

TIN' STORY RESPONSE SPECTRLH

2G NATIRAL FREQUENCIES IN EACH DIRECTION (SIDE/SIDEP FRONT/BACK, VERTICAL):

13' Hz F/B 11 45 Hzv ) 100 Hz

3 MODEL TYPE:

3O Q 2D ID . Fl TE ELEME T g BE Q CLOSED FORM SOLUTIO

4e Q COI4DUTER CODES:

FREQUEM Y RANGE AND NO OF MODES CONSIDERED:

Q HAND CALCULATIONS

OTHER5. ETHOD OF COIB I G 0 IC ESPOHSES: Q SO LTE SLH Q SESS [g (SPECIFY)

6 DAN ING: OBE SSE BASIS FOR THE OAHPIHG USED:

7 SUPPORT CONSIDERATIONS IN THE MODEL

B MAX, CRITICALDEFLECTION

Q 0.01"LOCATIOH

Valve disk radialdeflection

8. CRITICAL STRU TIRAL ELEMENTS: GOVERN I NG LOAD

OR RESPONSE

A, IOEHTIFIGATIOH LOCATIDH COIBI IIATIOH

Operator Drive Cylinder on FatigueRod CSP-V-1 Stress

CSP-V-2 Range

Ear Weld Support Ear FatigueCSP-V-1 Stress

Range

SEISMICSTRESS

TOTAL

STRESS

STRESS

ALLOIABLE

86,82657,526

90,00090,000

26 F 554 28 F 000MAXIM'LLOWABLE

DEFLECTION TO ASSlHEFUNCTIONAL OPERABILITY

approx 1/8" radialclearance

NOTE: Calculations based on accelerations for CSP-V-1 and 2 willprovidean envelope for CEP-V-1A and 2A. See Table 1.1 of Section 4.3 forrelative required accelerations for CSP and CEP valve operators.

~sed on calculation using Revised Burns and Roe Piping AnalysisAccelerations, April, 1983;

PAGE 4 OF 5

Revision 1 2.5

Qualification Summary oi Equipment (Continued)QIDN 361104

VIII. REFERENCES

1) BIF Drawings

Drawing IA-206763

Revl DescriptionF General Arrangement

CEP-625-10

c CEP-625-11.12

From Reactor NozzleX-3 to SGT-FU-lA, 1B


C-26095 Model A-83B Cylinder

A-206767 Valve Assembly

DOC-D-220-0310-IR-66 0 Tube errection iso-metric

D-207110 F Valve Data Sheet

M-144

CSP-807-3.4

General Arrangmentlan mis level

Containment purgeair su 1 s stem

References continued on page 2.6

" ~ c w~~~ i D~N .~ ~/~/~~Date

~/~~

Pago 5 of 5

THXS PAGE NOT USED.


CalculationSheet

project Prepared By. DateWPPSS Mechanical Equipment Qualification J.E. Rakowski 3/25/83

Subtect 30" Butterfl ValvesChecked By;

')-.C. I=~ +/~ lzzSystem

CSP and CEPAnatysis No'61104 Rev, No.

Job No.

Sheet No.2.6,

File No.Os.ol/F

Reference cont'n

2) Formulas for Natural Frequency and Ytode Shapes,Robert D. BlevinsVan Nostrand Reinhold Company1979 Edition

3) BIF Report TR-27234 and TR-27235, "Dynamic TorqueCalculation of Butterfly Valve; Sizes 24 and 30 inch",dated November 10, 1982.

4) Report TR-74-8 by McPherson Assoc., Inc., "Design &

Seismic Analysis 30" Cylinder operated Butterfly Valve".(Rev. 1) 12/31/75.

5) WPPSS letter to Cygna Energy Services, GE-02-RWH-018,12/17/82.

7)

6) WPPSS, WNP-2 SRM Equipment List Summary Sheets dated2/10/83.

Cygna Energy Services, Equipment Qualification WalkdownVerification Form dated 7/14/82 and 7/19/82.

8)

9)

Cygna Energy Services, "Project Manual Design Criteria,"DC-l, Rev. 1, 10/82.

Burns & Roe Revised Piping Analysis Loadsfor CSP-V-1 and 2 (received 4/13/83) and CEP-V-lA and1B (dated 11/15/82) .

10) Communications Report, R. Ricappito o f BIF and J. Rakowskiof CES, "BIF Valve Dimensions", 2/ll/83

ll) Cygna Energy Services, "Equipment Seismic and HydrodynamicRequalification Calculation No. OS.01.F", QID No. 361104,Revision 1, May, 1983.

rccs Oc

7IIIIIIIIIIIIIIIIIIIIIIIIIIIIII

F,o,ec, WPPSS, tvNP-2 Seismic/Hydrodynamic

CalculationSheet

Freoa e" By DaieL.C.Fernandez 4/29/83Svo~ec: Ghee«ea By

IIDaie'l,—.

Systpcc

Analya a No361104

Fle ~ Nc

Joo No82044

Shee: Nc

Foie NoOS. 01

UPSET COND1T10N G-LEVELS

EPICS

CSP- V -1

Cep- V-20.76 1.36 0.88

0.66 1.33 0.79

-e FAULTED CONDI T1ON G-LEVELS ( RWuIREb)6 AND 10 1NCH AIR CYLINDER OPERATORS

EPN

CSP-V -1

CSP- V -2

HYDRLDS ELEV 'R'

50B. 00

Y 508.00

2.26 3.62 2.80

1.44 3.54 1.90

CEP- V -lb Y

CEP- / -2A Y

586.00 1.93 2.23 1.85

588.00 0.96 2.11 1.16

From Revised Burns and Roe Piping Accelerations, see Section 5.5.

le~A cc

TABLE OF CONTENTS QlDg 361104

SECTION TITLE NO OF PAGES

1.0

2.0

3.0

4.0

4.1

4.2

4..Pg. 4.3.1

Pg. 4.3.8

Pg. 4.3.53

5.0

5.1

5.2

5.3

5.4

5.5

Requalification CertificateSQRT Forms

Table of Contents

Requalification Analysis

Conclusions

Summary of Results

Analysis

Introduction

Calculations

References

Appendices

Response Spectra

Walkdown Sheets


SRM Sheets

Revised Burns & Roe Piping AnalysisAccelerations

6.0 Drawings

Revision 1

TABLE OF CONTENTS

CON'TQIDN 361104

SECTiON TITLE NO OF PAGES

7.0

'7. 1

7.2

7.3

7.4

Transmittals, Prior Calculationsand Reports

Communication Reports

Original Requalification and SQRT Forms

BIF Report *

McPherson Associates Analysis*

*Note: Excerpts from report included in specifiedsection. For complete report see CygnaEnergy Services File No. OS.01.F, QID 361104,"Equipment Seismic and HydrodynamicRequalification of 30" Cylinder OperatedButterfly Valves," Revision 1, June, 1983.

Revision 1


Equipment Seismic and HydrodynamicRequalification

ClientWashington Public Power Supply System

Subject

Job No. 82044File No. 0S 0 1 FGale. Set No.

1

No. of Sheets 8 3

BIF 3 0 " Cylinder Operated Butterfly Valves ,QZDN 3 6 1 1 0 4EPNS : CSP-V- 1 , 2

CEP-V-1A , 2A

Statement of Problem

Seismic and Hydrodynamic Requalification of CSP-V-1, CSP-V-2,CEP-V-1A, CEP-V-2A to Burns and Roe Piping Analysis Loads.

Sources of Data

See References pages 4.3.53 and 54.

Sources of Formulae ft References

See References pages 4.3.53 and 54

'he

equipment requalification was performed based on calculationsusing Revised Burns and Roe Piping Analysis Accelerations,April, 1983. (See Section 5.5)

Originators Checkers Distribution Revision No.1

JE Rakowski

H. Abolhoda

R. Hsieh

LC Fernandez

MA Scott

DE Searle

Project File-1 Revision 0, 7/23/82Approved By: ~ P, Date:

~ p,

i~

Supply System 2 SuPersedes Calculation Set No.

100$ .00

ttT

C5 BIIIIIIIIIIIIIIIIIIIIIIIIIIIIII

CalculationSheet

Protect

Subtect

System

Prepared By

Checked By

Job No, File No,

Date

Date

Anatysis No. Rev No. Sheet No

CONTENTS

4.1

Calculation Cover. Sheet

Conclusions

4.2 Summary of Results

4.3

4.3.1

4.3.2

4.4

Analysis

Introauction

Calculations

References

1006 00


CalculationSheet

Project

Subject

System

Analysis No Rev, No,

Prepared By;

Checked By,

Job No,

Sheet No

File No.

Date

Date

SECTION 4.1

CONCLUSIONS

rctjs cc

V

SUPP l.1LJR Tl<ANSIlllTTALFORI'Il

AREA WITHINHEAVY BORDER TO BE COMPLETED BY SUPPLIER)

To THK ATTENTIDNoF Denn is Arms tron3 p p p G PP NIZJgiT PfJRCH PFOPGQNQ UYfg CON RAC$ AD I ~ )

sU JKcT Eouio . Seismic H drodvnamic Re u 1' '

C na Ener ServicesADDREss. 1200 Jadwin Suite 565 Richland HA

THE FOLLOWING PUBI ICATIONS/DRAWINGSARE SUBMITTED FOR:

@APPROVAL Q REVIEW " Q INFORMATION Q DISTRIBUTION

NO.OF PRINTS OF EACH NO OP REPROOOCIEL OF E CH

SUBMITTKDBY: t

TITLE:

PAGE ~ OF ~l

2 NEW 0 RK SUBMITTAL

RKQUKSTKD DATEOF RETURN:

CONTRACT NO:

PO NO)

WORK ORDER NO:

SPEC. NOg

SUBVENDOR: CONT.JP.O, NO,: SPEC, SECT NO>

ITEMNO,

PUBLICATION0 RDRAWING NO.

RKV.NO, PUBLICATIONOR DRAWING TITLE MANUFACTURER

WPPSSACTION

T-6 1 4 3

COMMENTS< (USE ADDITIONALSHEET, IF REQUIRED) TO BE REVIEWED BY

R EIVKO BY: IPURCHASING ONLY)II HAMROVED E4Y:

TRANSMITTED BY: IPURCHASING ONLY)

TITLE

ACTION LEGENOcA ~ APPROVED FOR PUBI.ICATION

AN m APPROVKO AS NOTEO FOR FABRICATIONP ~ I P PT SSS

I ~ INFORMATIONONLYNA ~ NOT APPROVED

'- ~k>llllllllllllllllllllllllllllll

FINALQUALIFICATIONREPORT

PROJECT: Equipment Seismic 5 Hydrodynamic Requalification

JOB NO.: 82044

CALC. NO.: 1P.01/F

CLIENT: washington Public Power Supply System

QID NO.: 018001

TITLE: Equipment Seismic 5 Hydrodynamic Requalification8", 10" and 12" Bore Air Cylinder OperatorEPN 8CEP-AO-lA, 2A REA-AO-1', 2

CEP-A0-3A, 4A ROA-A0-,1, 2CSP-A0-1, 2CSP-AO-37 „4, 5, 6, 9

PREPARED BY:

REVIEWED BY:

APPROVED BY:

REVISION:

1001.00

REVISION STATUS LOG

ReviNo. Date

Preparedby

Reviewedby

Approvedby Cygna

EnergyServices

Approvedby

NPPSS Description

1 0 REQUALIFICATION CERTIFICATION

1.1



WNP- QID 018001

cOMPDNENTNO, CSP-,A0-3 4

8" Bore Air Cylinder Operators

MANUPAcTURKR Miller Fluid Power Cor

KQUIPMKNTCLASSIFICATIONt gg ACTIVE Q PASSIVE

MOOKI NOt A83

SEISMIC QUALIFICATIONREPORT REFERENCKt

C a Re ort 1P.Ol/F, QID 018001

WPPSS Seismic Qualification of 8" and 10" Bore Miller Air0 erator.

ENVIRONMENTALQUALIFICATIONREPORT RKPKRKNCKt

Remarks': Parts of the air operators such as the drive rod, trunnion'ns brackets and clevis were evaluated as art of the

res ective valve ID acka es.These o erators do not ualif until the operability dem-

onstration described in Section 4.3.2 has been performed.

THKABOVESKI5MICAND

THK CURRENT NRC SKI5MICANO

QUAIJPICATION REPORT5 HAVE BREN RKKVAL,UATKDIN ACCOROANCK WITH

CRITKRIAt

I~ IKKKSTANOARO5 244 (l57$ I,

2 U5NRC REGULATORYOUIOK5 I%2, I~ ISO

Se 5TANDARO REVIEW PLANS-2&~i2 IOo~4~~%I

This certificate applies only to theoperator which was evaluated as partof the valve assembly. Followingcompletion of the valve requalifica-tion (QID 361106), the certification

willbe revised to address the entireassembly.

THKABOVE COMPONENT HAS BEEN FOUND ACCEPTABLE FOR FERFORMINQ IT5 INTENDED 5APKTY RELATED FUNCTION

WHEN 5UBIECTKD TO THK PLANTSPECIFIC VIBRATORY .LDAos subj ect to the aboveremarks.

PRKPARKO BY3. E . RA&o~S&I

APPROVED BY

t$2 l2$7$

ki4d~ la +S~~ln, ~ I ~4~ A ~vdSOATS+ peggyDATE / ')

1.2

WASKNGTQNPUBLIC POWER SUPPLY SYSTEMIC


WNe- QID 018001

coMPDNKNT Noi CSP-AO-1 2

cDMPDNKNTDKscRIFTIDN3 10 Bore Air C linder 0 erators

MANUFAOTURER, Miller Fluid Power Cor

KQUIPMKNTCLASSIFICATIONs QX ACTIVE Q PASSIVE

MODELNO(

SKI5MIC QUALIFICATIONREPORT REFERENCE:

or 1P.01 F ID 018001WPPSS Seismic ualification of 8" and 10" Bore MillerAir 0 erator.

KNVIRONMENTALQUALIFICATIONRKPOR'T RKFKRKNCKl

Remarks 1: Parts of the air operators such as the drive rod, trunnionins, brackets and clevis were evaluated as part of the

respective valve QID packages.Remarks 2: CSP-A0-1,2 are not qualified until the operability demon-

stration described in Section 4:3.2 has been performed.

THK ABOVESKI5MICAND'HK

CURRENT NRC SEISMIC ANO

QUALIFICATIONRKPORT5 HAVE BEEN RKKVALUATEDIN ACCORDANCE WITH

CRITERIAc

'I IEEK STANOARD5 244 (I$75)

2e U5NRC REGULATORYQUIOK5 Io$2, I~ IOO

Se 5TANOARD REVIEW PLAN5 SAW 2 I0+410t

4 fCctlRKISNNEE

This certificate applies only to theoperator which was evaluated as partof the valve assembly. Following com-pletion of the valve requalification(QID 361104)., the certification willbe revised to address the entire as-sembly.

THKABOVE COMPONENT HAS BEEN FOUND ACCEPTABLE POR PKRFORMINQ IT5-INTENDED5AFETY RELATED FUNCTION

WHEN SUBJECTED TO THK PLANTSPKCII IC VIBRATORY,remarks.

PREPARED BYJ. 2 RAtc~OSIc I N (4.~ IAA>5c~A

REVIEWED BY

LDAD5) sub ject to the above

DATE

a4'PPROVED

BY( ~v PCi/>,i~r~,,v w

$ 44 I2574

OATKV )

1.3WASHINGTONPUBLIC POWER SUPPLY SYSTEM


WNP QID 018001

COMPONENT NOs

coMPDNKNT DKscRIPTIDN( 8" Bore Air C linder 0 erators

Miller Fluid Power Corp. A83MODKLNOs

EdIUIPMKNTCLASSIPICATIONs"

g] ACTIVE Q PASSIVE

SEISMIC CIUALIPICATIONREPORT RKPERENCKj

C na Re ort 1P.01/F, QID 018001

WBP6S Seismic ualification of 8" and 10" Bore MillerAir 0 erator.

ENVIRONMENTAL.QUAUPICATIONREPORT REPERKNCEt

Remarks 1: Parts of the air operators such as the drive rod, trunnionins, brackets and clevis were evaluated as part of the

respective valve QID packages.

THKABOVE5KISMICAND

THK CURRENT NRC 5KI5MICAND.

dIUALIPICATIONRKPORT5 HAVE BEEN REEVALUATEDIN ACCORDANCE WITH

CRITERIA>

2e U5NRC REGULATORYOUIDE5 le$ 5, 1 ~ IDO

I ~ IKKKSTANDARD5 544 (1 $75), This certificate applies onlyto the operator which was evalu-ated as part of the valve as-

st STANDARD REVIEW PLANS SA>e 5 10' sembly. Following completionof the valve requalification

4 NCOR$1~~ (QID 361106), the certificationwill be revised to addressthe entire assembly.

THKABOVE COMPONENT HA5 BEEN POUND ACCKPl'ABLEPOR PERPORMINO IT5 INTENDED 5APETY RELATED PUNCTION

WHKN 5UBJECTKD TO THK PLANT SPECI PIC VIBRATORY, ~ ~ LOADS

PREPARED BYQ E ~p, wan (~~g~

REVIEWED BY

DATK

+pwca

DATE

APPROVED BY I<+ IVr 1' -'ides') i$ $ $~1$ $ 15

DATE

1.4WASHINGTONPUBLIC POWER SUPPLY SYSTEM


WNP- QID 018001

coMPDNENT Not CEP -AO-lA 2A

coMPDNKNTDKscRIFTIDNt 1 0" Bore Air C 1 inder 0 erators

Miller Fluid Power Corp.

KCIUIPMKNTCLA5SII ICATIONt gg ACTIVE Q I ASSIVK

A83 (2A), A83B (1A)MODELNO(

SKI5MICdUAIJFICATIONREPORT REFKRKNCKt


WPPSS Seismic Qaulification of 8" and 10" Bore MillerAir 0 erator.

ENVIRONMENTALQUALIFICATIONREPORT REFERKNCEt

Remarks: Parts of the air operators such as the drive rod, trunnionins, brackets and clevis were evaluated as part of the re-

spective valve QID packages.

THK ASOVKSEISMIC AND

THK CURRENT NRC SEISMIC ANO

0IUAIJFICATIONRKPORT5 HAVE SEEN REEVALUATEDIN ACCORDANCE WITH

ITKRIAt

I ~ IKKKSTANOARD5 544 II%75),

USNRC REGULATORYOUIOKS I%Sr I~ IOO

Sr 5TANDARO REVIEW PLANS 5AAr5 IOr~4 OWN~

This certificate applies only to theoperator which was evaluated as partof the valve assembly. Following cornpletion of the valve requalification(QID 361104), the certification willbe revised to address the entire as-sembly.

THE ASOVK COMPONENT HA5 SEEN FOUND ACCKFTASLE fOR PKRFORMINO IT5 INTENDED 5AFETY RELATED FUNCTION

WHEN 5USIKCTKDTO THK PLANT5PKCIFIC VIBRATORY '- LOAO5

PREPARED SYRtl <C k.l

REVIEWED SY

APPROVED SY+ti'tif ilt.rt r

$ 4$ r I 251$

(4 c3~ /A/

OATS

1.5

WASHINGTONPUBLIC POWER SUPPLY SYSTEM


WOP ~ QXD 018001

coMPDNENT Not CEP -AO-3A 4A8" Bore Air C linder 0 erators

Miller Fluid Power Corp.

KCLUIPMENTCLA55IF ICATI ON s KjACTIVE Q PASSIVE

MDDKL,ND A83 ( IA), A83B (3A)

SEISMIC GUAuPICATION REPORT RKFERENCKt

1P.01 F ID 018001

Seismic uglification of 8" and 10" Bore Hilleror.

ENVIRONMENTALGUAIJFICATIONREPORT REFKRENCKt

Remarks: Parts of the air o erators such as the drive, rod, trunnionins brackets and clevis were evaluated as part of the

res ective valve QID ackages.

THE ABOVESEISMIC AND

THK CURRKNT NRC SEISMIC AND

GUAIJPICATION REPORT5 HAVE BEEN REEVALUATEDIN ACCORDANCE WITH

CRITERIA s

I~ IKKKSTANOARD5 344 1197$ )

USNRC REGULATORYGUIDES 1A2e 1+100

S~ STANDARD REVIEW PLANS SA&e 5 IOe~4lfUlCKIDBRS'his

certificate applies only to theoperator which was evaluated as partof the valve assembly. Followingcompletion of the valve requalifi-cation (QXD 361106), the certificatiowill be revised to address the entireassembly.

THE ABOVE COMPONKNT HAS BEEN I OUND ACCEPTABLE FOR PERFORMING IT5 INTENDED SAF'KTY RELATED FUNCTION

WHEN SUBIKCTKDTO THE PLANTSPECIFIC VIBRATORY~ ~ LOAO5,

PREPARED BY%.&l ~id U~ i'WS~7VW

REVIEWED BY

APPROVED BY...1 4 ~r I'-/d�zc .--.

c91&�I�257

QzY 83DATE >7 &ZOATK /~7/.- i

1. 6



WNP- QXD 018001

coMPDNENTND, REA-AO-1 2 ROA-AO-1 2

coMPDNKNT DKScRIPTIDN< 12" Bore Air C 1 inder Operators

MANUFAcTURER Miller Fluid Power Corp .

EQUIPMENT CLA$5IFICATIONt Q ACTIVE Q PA55IVK

MOOKt.NOtA83

SEISMIC QUALIPICATIONREPORT RKFKRKNCKt


WPPSS Seismic Qualification of 8" and 10" Bore MillerAir 0 erator.

ENVIRONMENTALQUALIFICATIONRKPORT REFERENCE

QUALIFICATIONRKPORT5 HAVE BKKN RKKVALUATEDIN ACCORDANCE WITH

THK CURRENT NRC SKI5MICANO CRITERIA'

~ IKKESTANOARO5 244 (I97$ )

2 U5NRC REQULATORYQUIDK5 IA2o I~ I00

2~ 5TANDARO RKVIKWPLANS'$5&v 2 IOe~4

THKABOVE COMPONKNT HA5 BEEN POUND ACCEPTABLE FOR PERFORMINQ IT5 INTENDED 5AFETY RELATED FUNCTION

WHKN SUBJKCTKD TO THK PLANTSPECIFIC VIBRATORY LOAO5

PREPARED BYWiden>

RKVIKWKDBY

APPROVED BY0-, 'iJ '<, 'i v

944 12970

DATEW zan

DATKz7

DATE

2.0 SQRT FORM(S) AND REFERENCES

GOBKJE,IIIIIIIIIIIIIIIIIIIIIIIIIIIIIII

WASHlNGTON,PUBLlC POWER SUPPLY SYSTEM

Qualification Summary of Equipment

I PLANT NAME. ~P- 2 TYPE

Ref. No.

GE z AiE. Burns & Roe 5-Mark IICEP-A0-3A, 4A

C~NENT NO. CSP-AO-3 4 5 6 9

I NSSS:

coINoowENT NAME 8 Bore Air C 1 inder

I ~ SCOPE: NSSS

2'DDEL NU4BER. A83B QUANTI TY:

VENDOR'T.F4 IF THE CQ4%WENT IS A CABINET OR PANEL, NAME ANO MODEL NO OF THE DEVICES INCLUDED:

N/A

5 PHYS ICAL OESCR I PT ION: a, APPEARQCE:

b DIMENSIONS: 8" Dia. x 1.

WE I GHT: 3 lb s ~

LocATIow BUILDING Reactor Bu '

ELEVATION. 475 ' 4

13.

13

13

7 FIELD MOUNTING CONDITIONS: BOLT (NO S(ZE

P NELS (LENGTH )

8. a.

b

CO

sYsTEM IN wHIcH LocATED: CEP ~ Containmen hCSP; Containment Supply Purge System

FUNOTIDNAL DEscRIPTIDN.Primar Con tainmen I o '

of the release of radioactive materi@ po @IIS THE EQUIFMENT REQUIRED FOR: HOT STANCBY COLO SHUTDOWN

BOTH Q NEITHER

9. PERTINENT REFERENCE DESIGN SPECIFICATION:

I I I. IS EOUIFMENT AVAILABLEFOR INSPECTION IN THE PLANT: X YES Q NO

see wPAGE I OF 5

2.3

Qualification Summary of Equipment (Continued)QID 018001

Ref. No.

, I ~ S INGLE FREQUENCY Q MULTI-FREQUENCY RAND(H

2o SINGLE AXIS MULTI-AXIS Q SINE SEAT

NO OF QUALIFICATION TESTS: OBE SSE OTHER (SPECIFY)

4 FREQUENCY RANGE

5 NATIRAL FREQUENC I ES I N EACH 0 I RECT I ON ( S I OE/S I OE E FRONT/BACKE VERT ICAL)

S/S ~ F/8 EE

6 METHOD OF OETERMI NING NATIRAL FREQUENCIES:

Q LAB TEST IN SITU TEST ANALYSIS

7 TRS .ENVELOPING RRS USING HJLTI-FREQUENCY TEST: Q YES (ATTACH TRS 4 RRS GRAPHS) Q NO

B. INPUT g-LEVEL TEST: CBE S/S ~

SSE S/S EE

F/8 ~

F/8 EE

go LABORATORY MOUNTI NG:

EOLT (NO., E IZE I Q IIELO (LEIIOO(

10o FUNCTIONAL OPERABILITY VER IF I EO: Q YES NO Q NOT APPLICABLE

11 ~ TEST REULTS INCLUDING MODIFICATIONS MADE:

12 OTHER TEST PERFORMED (SUCH AS AGING OR FRAGILITY TEST, INCLUDING RESULTS):

"NOTE: IF QUALIFICATION BY A CCMBINTATION OF TEST ANO ANALYSIS, ALSO CG4 LETE ITEM Vl I.

PAGE 5 OF 5

'kFAULTED COND I T I ON G-LEVELS8 AND 10 INCH AIR CYLINDER OPERATORS

EPN

CSP-AO-1

CSP-AO-2

CSP-AO-3

CSP-AO-4

CSP-AO-5

CSP~O-6

HYDRLDS ELEV '' G'S

V

V 5OB.OO 4.4O 6.51

Y 508.00 4.95 6.45

Y 481.00 5.72 3.82

Y 478.00 4.65 4.06

Y 475.00 9.35 5.75

E

4 '9+ +

3.72

7 '56.57

Y 480.00 9.35 5.57 1.46

3.s4 goy

3 33 i

«Qg'z,0t

'A': B.7&

p.j7 > . 4. (g

CSP-AO-9

'EP~O-1

EP-AO-2

CEPQO-3A

CEP-Ail-4A

Y

Y

490.00 2.57 1.73 2.67

588.00 1.27 1.77 1.23

588.00 0.78 1.77 1.02

495.00 13.89 1.66 1.04

495.00 10.95 1.50 1.10

4.g7

3.35

rVQ I

I

/JQi Z( co~

+Transmi t ted from the f inal p i ping anal vs is,see Sect i on 5.5.

++These va) ves are required to fai l-closeddur ing a DBE, change Use Code to "1,3" .

~ETC AQQ<r.fkg-,r&J'r-duCrr.jy A? 6 JrVCD gddd'diJ6 qQgr yd.-r~~~~< l4Q MOOA8Udky ~~CC)u(~ T~+l<J d'~l yd'dd L f. "gP~g~

~d'~>~(~>>SSJ. ZEE ZC'Q. K.S/QiD 6/d 00/

4kdld

2.5

AlL aiIIIIIIIIIIIIIIIIIIIIIIIIIIIIII


Qualification Summary of Equipment/ID 018001

I~ PLANT HAKEEWNP-2 RoI. No.

lo. HSSSI 2o A/E!

I I~ cosFPoNENT NAKE. 0" Bore Air linder

Burns g Roe 5 - Mark IIBNRCEP-A0-1A, 2A

CyerwENT NO. CSP-AO-1 2

'I ~ SCOPE:

2o ICDEL HLNBER:

YEN'!

NSSS BOP

A83B

BIF

OUANTITY:

4o IF '%E CO4%NKHT IS h CABINET OR PANELS HAKE AHD KOKL HOo OF THE DEVICES IHCLVDEDL

N/A

PHYs IcAL DfScR IPTIDHL I APPfARjgcf li drical 13

b D IKENS I OHS:

c lC I GHT!

10EE dia. x, 64" ion (excludes the drive rod

593 lbs. - c linder, 321 lb. - bracket

13

13

LocATI oH QJ I LDIHG Reactor Bui1ding

ELfyh'TIDH. 508 'o 5607

7 FIEIO OIUIITINO COfOITIOMSF QX BOLT (IIO SIZE )

HELD (LEHGTII )

Bo Oo SYSTEK IN WICK LOCATED: CEP Containment Exhaust Pur e S stemCSP; Containment Supply Purge System

bo FVICTIONAL OESCRLPTIOH:

Co

the release of radioactive material to the environmIS THE EOUIPKEHT REOUIRED FOR: Q HOT STAHCBY Q COLD SHUTDCNH

Q BOTII Q NEITHER

nt.

9o PERTLHENT REFEREM K DESIGN SPECIF ICATIOH: 68

I I I~ LS E UIFKENT AVAllhBLE FOR INSPECTION IN THE PLANT: Q YES Q HO

(See Walkdown)PAGE I OF S

2.6


EOUI PMENT DUALIF ICATION METHOD:

QID 018001Ref. No.

TEST ANALYSIS CO4BINATION OF TEST 4 ANALYSIS

pty L IF IGATI0N REPDRT ~ Re ualification Anal s is of ID 0 1 800 1

(Nos E TITLE a DATE): OP. Ol/F, Februar 1983

coMpANY THAT pREpARFD REPDRT: C a Ener Services

coMpANY THAT REYI EwED REPCRT Washin ton Pub lie Power Su 1 S s

tern

V VIBRATION INPUT:

I LOADS CONSIDERED: es Q SEISMIC ONLY

be Q HYCROOYNAMIC ONLY

c Q CCMBINATON OF (e) AND (b)

2 METHOD OF CCMBI NING RRS: Q ABSOLUTE SLH

3. REOUIRED RESPONSE SPECTRA (ATTACH THE GRAPHS):

Rj SRSS OTHER ( SPECIFY)

Section 5.1

4 DAMPING CORRESPONDING TO RSS: OBE

5 REQUIRED ACCELERATION IN EACH DIRECTION: Q ZPA

Attached F/B .

SSE S/s Attached F/B

sss ~2

Q 0THER (sPEGIFY) Sec. 5 ~ 4

ss

6 WERE FATIGUE EFFECTS OR OTHER VIBRATION LOADS CONSIDEREDT

Q YES NO

IF YES, DESCRIBE LOADS CONSIDERED ANO HOW THEY. WERE TREATED IN OVERALL DUALIF ICATION FROOIAM:

For those EPN's which are sub'ected to h drod amic loadin s

13

the fati ue anal sis on critical locations will be erformed

to comply with the requirements of AISC, Section 5, A endix

B. Total number of h drod namic stress c cles is e ual to

15560.0 cycles (10 x 6 (OBE/SSE) + 3 x 4500 (SRV) + 2000.0 c cl s

(chugging).

~NOTE: IF MORE THAN ONE REPORT, CCMPLETE ITEMS IV Tl+OUGH Vl I FOR EACH REPORT

PAGE 2 OF 5

2.7

Quaiification Summary of Equipment (Continued) qID py8ppy

Yl~ IF UALIFICATION BY TEST THEN C~LKTE»: N/A

I Q SINGLE FREQUE~ Q MULTI-FREQUEJCY Q RANDCH

2oQ SINGLE AXIS Q l4JLTI-AXIS Q SINE BEAT

Ref. No.

3 NO OF QUALIF I CAT(OI TESTS: CBE SSE OTHER (SPECIFY)

FREPUENCY RANGE

5H NATlRAL FREQUENCIES IN EACH DIRECTION (SIDE/S IOE, FRONT/BACXE VERTICAL):

S/S ~ F/B %

6, METHOD OF DETERMINING NATLNAL FREQUENCIES:

LAB TEST Q IN Sl TIJ TEST Q ANALYSIS

7 TRS .ENVELOPING RRS USING MULT INFREQUENCY TEST: Q YES (ATTACH TRS 4 RRS GRAPHS) Q NO

8 INPUT g-LEVEI. TEST( CBE S/S %

SSE S/S %

F/B %

F/B %

Y %

9» LABCRATORY )CUNT I NG:

IIOLT (HO, SIZE ) Q IIELO (LEHOTH )

IOH FUNCTIONAL OPERABILITY YERIF I ED: Q YES Q NO Q NOT APPLICABLE

I I~ TEST REULTS INCLUDING MOOIF ICATIONS MADE:

I2H OTHER TEST PERFORMED (S(CH AS AGING OR FRAGILITY TKST, INCLUDING RESULTS):

NOTE: IF PUALIFICATION BY A ClHBINTATION OF TKST AND ANALYSISE ALSO COMPLETE ITEM Vl I ~

PAGE 3 OF !

2.9


IF QUAL IF ICATION BY ANALYSIS, THEN C(HPLETE:

QID 018001Ref. No.

I METHOD OF ANALYSIS:

STATIC ANALYSIS

DYNAMIC ANALYSI S

2 NATURAL FREQUENCIES

13.0 Hz F/B Bs11.45 Hz v 100 Hz

QX EQUI VALENT STATIC ANALYSI5

Q TIME-HISTORY RESPONSE SPECTRLH

I

IN EACH DIRECTION (SIDE/5 IDEE FRONT/BACK, VERTICAL):

13

10

3P MODEL TYPE:

4 / C~UTER CODES:

Q FINITE ELEMENT Q BEAM Q CLOSED FORM SOLUTION

FREQUEICY RANGE AND NO OF MODES CONSIDERED:N/A

MAND CALCULATI ONS

OTHER

5 NETNOO OF COIBININO OYNANIC RESPOIISES: Q ABSOULTE SIN Q SASS Q ISPECIFY)

SSE BASIS FOR THE ROPING USED:Id*

6o OAH ING: OBE

7 SUPPORT CONSIDERATIONS IN THE MODEL

13

„~SB CR I T ICAL STRLCTlRAL ELEMENTS:

A IDENTIFICATION

Drive Rod

GOVERN I NG LOAD

OR RESPONSE SEI SHIC

I SCAT ION COIBI NATION STRESS

(Range)Operator Fatigue/Fault+ 86824

CSP-V-1

TOTAL

STRESS

STRESS

ALL(%ABLE

90,000 PSX

B HAX CRITICALDEFLECTION I.CCAT I ON

HAXIHLH ALLQfABLE

DEFLECTION TO ASSURE

FUST IONAL OPERA B I L I TY

Operability to be demonstrated by test for CSP-AO-1 & 2.**AirOperator bushing stress ) 200psi

* Final Response accelerations from piping analysis were used.A

PAGE 4 OF 5

FAULTED CONDITION G-LEUELS8 AND 10'INCH AIR CYLINDER OPERATORS

G'SV

HYDREPN LDS ELEU '' E

4.89

3 '27 '56 '7

CSP-AO-1 Y

CSPMO-2 Y

CSP-AO-3 Y

CSP-AO-4 Y

CSP-AO-5 Y

CSP-AO-6 Y

508. 00 4. 40 6. 51

508.00 4.95 6.45

481 .00 5.72 3.82

478,00 4.65 4.06

475.00 9 '5 5.75 7.72

480 .00 9.35 5.57 1 .46

Z,4&

3 Cc)Z

3.s4

Z,6'.l73.7&

4.fQ

5.Q3 5

344, s4Z

'SP-AO-9

CEP-AO-1

EP-AO-2

CEPS-3A

CEP-A0-4A

Y 490.00 2.57 1.73 2.67

Y 588.00 1.27 1.77 1.23

Y 588.00 0.78 1.77 1.02

Y 495.00 13.89 1.66 1.04

Y 495 F 00 10 '5 1.50 1 ~ 10

4.57

3. 35

I>@<

(.34

+Transmi t ted from the f inal p i p in9 anal ysi s,see Sec t i on 5. 5.

++These val ves are r equir ed to fai l-closeddur ing a DBE, chanpe Use Code to '1,3" .

~ +~ + A~~<""~4 7(c'4~~ QNAPczc "37 4 8J/g~g rvpiNg g~lgc.veil~~~<=~~~< l4"-, 4yorbduiky ~Maoris 724'-rrt/T rgL. pqgpgg~~~ oo«(~>>«J. roe tea. s s/are oieoo i

y/gg/p

2. 10

AkIIIIIIIIIIIIIIIIIIIIIIIIIIIN

VfASHlNGTON PUBLlt POV/ER SUPPLY SYSTEM

Qualification Summary of, EquipmentQID 018001

~LANT NANERts5P-.2 RI5. llo.

lo. NSSS5Buxns g Roe

2 VE

SCOPE: NSSS g OOF

CCHQHENT NO,I I. c~ENT NANE: 12EE Bore Air linder

PNR

5 - Mark IIIIIRREA-AO-l, 2ROA-AO-1 2

2, FIDEL NLHBER: A83B

BIF

OLIANTITY.

io IF TIIE COPONENT IS A CABINET OR PANEL, NAXE ANO ICOEL NOH Of THE DEVICES INCLVDEDI

N/A

S PHYS ICAL DESCRIPT IONI I APPEARAICEI lindrical 13

DINENSICNsI 12 dia. v 46. 83(E ion excludes the drive rod 13

C lC I IOHT5 583 lbs. - cylinder, 586 lb. - bracket

QJ I LDINQReactor Bui1ding

13

ELEYATIDNH 578 'o 597f

T FIELD IOIIIITIHO COIOITI(RHI QX COLT (IHL SITE )

Q IIELO (LEHCIH I

C3

I SYSTEM IN NH IcH LocATED REA Reactor Bui1ding

Exhaust

Air (HVAC) SystemROA; Reactor Building Outside Air (HVAC) System

FIIIcTIDNALDEscRIPTIDN Reactor Buildin Containment Atmosphere Control andprevention of the release of radioactive material to the environment.

C IS THE EOHIH(EHT REOHIREO FCII: Q IOT STIR(ST P COLO SHI/(SOIR

KI ROTI( ( IEA) QX EERIER (ROA)

9, PERTINENT REFEREN-E DESIGN SPECIFICATION: 68

III~ IS E VIRULENT AVAILABLE FOR INSPECTION IN THE PLANT: Q YES Q NO

(See Walkdown)PAGE I OF 5

'.11


Ref. No.

EOU I FMENT QUALIF I CAT I ON METHOD:

TEST

QUAL IF ICATION REPORT:

Q ANALYSIS C(HBINATION OF TEST 4, ANALYSIS

ualification Anal sis of ID 018001

(No., TITLE a onE>: OP.Ol/F, February 1983

COMPANY THAT PREPARED REPORT: Ener Services

coMPANY THAT REYI E)(ED REPDRT WashLn on Public Power S 1 tern

V VIBRATION INPUT:

I LOADS CONSIOEREO: a. Q SEISMIC ONLY

b Q HYCROOYNAMIC ONLY

c. X CCMBINATON OF (e> ANO (b)

2, METHOD OF C(NBINING RRS: ABSOLUTE SW Q SRSS OTHER (SPECIFY)

REQUIRED RESPONSE SPECTRA (ATTACH THE GRAPHS):

4 ~ OAR ING CORRESPONDING TO RSS: Q OBE

5 REQUIRED ACCELERATION IN EACH DIRECTION: Q ZPA

CBE S/S ~ 1.0

SSE

Q] DTHER (sPEGIFY) Sect. 5.

6, HERE FATIGUE EFFECTS OR OTHER VIBRATION LOADS CONSIOEREDT

YES NO

IF YES, DESCRIBE LOADS CONSIDEREO ANO HON THEY. MERE TREATED IN OVERALL QUALIFICATION FROGRAM:

13

r PN' d h d m a din

the fati ue anal sis on critical loacations will be erformed

to corn 1 with the re uirements of AISC, Section 5, A endix

B. Total number of h drod namic stress c cles is e ual to

15560.0 c cles 10x6 OBE SSE + 3x4500 SRV + 2000.0 c cles

(chu in ).

~ NOTE: IF MORE THAN ONE REPORT, C04PLEVE ITEMS IV 7k%OUGH Vl I FOR EACH REPORT

PAGE 2 OF 5

2.12

Qualification Summary of Equipment (Continued) QID 018001

V I ~ IF UALIF ICATION BY TEST THEN CO@'LETE+: N/A

I Q 5 NGLE EQUEICY Q MULTI-F EQ ECY Q ANKH

2 Q SINGLE AXIS Q MULTI AXIS Q SINE BEAT

Ref.

NQ, OF QUALIFICATION TESTS: OBE SSE OTHER (SPECIFYI

4 ~ FREQUENCYRANGE',

NATIRAL FREQUENCIES IN EACH DIRECTION (SIDE/SIDE, FRONT/BACKS VERTICAL)!

S/5 ys F/B ~ V RS

6 METHOD OF DETERMINING NATINALFREQUENCIES'AB

TEST Q IN SITU TEST Q ANAI.YSIS

7 TRS .ENVELOPING RRS USING MULT INFREQUENCY TEST) Q YES {ATTACH TRS 4 RRS GRAPHS) Q NO

8P INPUT 9-LEVEL TEST: CSE S/5 ~

SSE 5/5 ~

F/B ys

F/B ~

V RS

9y LABORATORY )OUNT I NG: a----IOO FUICT IONAL OPERABI L ITY VER IF I ED: Q YES Q NO Q NOT APPL ICABLE

11 ~ TEST REULTS INCLUDING MODIFICATIONS MADE:

)2y OTHER TEST PERFORMED ISLCH AS AGING OR FRAGILITY TESTy INCLUDING RESULTS):

NOTES IF QUALIFICATION BY A CCMBINTATION OF TEST AND ANALYSIS, ALSO COMPLETE ITEM Vl I ~

PAGE 3 OF !

'2.13


Ref. No.

(', IF DUALIF ICATION BY ANALYSIS, THEN CCHPLETE:

I ~ MFTHOD OF ANALYSIS:

Q STATIC ANALYSIS

Q DYNAMIC ANALYSIS

Qg EOUI VALENT STATIC ANALYSIS

T IME-HI STORY Q RESPONSE SPECTRIN

13

2 NATlRAL FREPUENCI ES

s/s 10. 81

IN EACH DIRECTION (SIDE/SIDEB FRONT/BACK, VERTICAL):

F/B 52. 0 v 100

3 MODEL TYPE:

Q 3D Q D Q E E EM g E CLO ED O UTIO

4 Q COMPUTER CODES:

FREOUEM Y RANGE AND NO OF MODES CONSIDEREO:

HAND CALCUlATIONS

5H METHOD OF CCHBI NING DYNAMIC RESPONSES: Q6H DAIL ING: OBE SSE

7H SUPPORT CONSIDERATIONS IN THE MODEL

N/A

OTHER

ABSOULTE SIP4 Q SRSS Q lSPECIFY)

BASIS FOR THE OhH ING USED:

e-Mounted

13

BH CRI 7 ICAL STRlCTlBAL ELEMENTS- GOVERN I NG LOAD

OR RESPONSE

LCCATIOH COIBI HATICHA IDENTIF ICATION

SE I SMI C

BTHBBB

TOTAL STRESS

STRESS ALLIABLE

Tie Rods

Drive Rods

Operatingthreaded end faulted

13683psi 20000 psi31',172 psi 86,400 ps'3

8 MAX CR I T I GAL

DEFLECTION LCCATIOH

MAXI MLM ALLIABLEDEFLECTION TO ASSLRE

FUNCTIONAL OPERABILITY

* Final response accelerations from piping analysis were used.PAGE 4 OF 5

2.14

Qualification Summary of Equipment (Continued) QID 0180»

Vill. REFERENCES

1. 'V&IE Boiler and Pressure Vessel Code", American Society of Mechanical Engineers1974 Edition with Winter 1974,Addenda. Section III, Division 1, SubsectionsNC and Appendicies.

2. U.S. Atomic Energy Comnission Regulatory Guide No. 1.61, October 1973.

3. Response Spectra Plots. From Design Input Document No. 82045 DID 001.

4. NNP-2 Safety Related Mechanical Equipment List, SRM02. Dated 9/9/82, Section 5.4.

5. "Project Manual for WPPSS Equipment Seismic and Hydrodynamic Requalification",cygna Energy servi'ces,'ev. 0, Dated b/8/Bz. Including Desi'gn'l.rxteria 1K-1.,

6. Cygna Energy Services Project Memorandum, 82044/027SF, dated 9/9/82.

7. WPPSS WNP-2, FSAR Table 3-7.1.

8. Cygna Energy Services Equipment Qualification Walkdown Verification Formsfor EPN's CEP-A0-1A, CEP-AO-ZA, CEP-V-3A, CEP-V-4A, CSP-V-l, CSP-V-2,CSP-V-3) CSP-V-4, CSP-V-S, CSP-V-6) CSP-V-9.

9. American Institute of Steel Construction, 'Manual of Steel Construction", 8thEdition, AISC, New York, NY.

10. Equipment Seismic 5 Hydrodynamic Requalif ication, QID 8361104. File OS.01/F.

11. Equipment Seismic g Hydrodynamic Requalif ication, QID 8361106, File OT.01/F.

12. Equipment Seismic 5 Hydrodynamic Requalification, QID 8361102,

13. Cygna Calculation, Equipment Requalification, QID 018001, File 1P.Ol.F.

Completed By g

Rovlowotl ByJ.E. Rakowski

Date

Pape 5 ol 5

3.0 TABLE OF CONTENTS

TABLE OF CONTENTS QID 018001

SECTION TITLE

1.0

2.0

3.0

4.0

4.14.24.34.4

5.0

Requalification CertificateSQRT Form(s) and References

Table of Contents

Calculations - Cygna RequalificationAnalysis

ConclusionsSummary of ResultsAnalysisReferences

Appendixes to Requalification Analyses

16

6

43

5.15.25.35.4

5.56.0

Response SpectraWalkdown SheetsSummary SheetsLoad Comparative sheets for REA and ROAAir CylindersBurns 6 Roe telex final piping G-levelsDrawings used for Requalification

6

23

16

7.0 Prior Calculations and Transmittals usedfor Requalification

SECTION 4.0


R ~ J a 1


Project

E ui ment Seismic H dClient

Washin ton Publi S stem


ID 018001'20'P.01 F

Gale. Set No.

No. of Sheets

Sub jec!Dynamic Qualification of 8, 10 and 12 inch Bore Air Cylinder Operators.

Statement ot Problem

The equipment qualification was performed based on calculations usingthe air operator response g-levels transmitted by the A/E, currentto 12/31/82.

Sources of Data

References, Section 4.4

Sources of Formulae 5 References

Cygna Design Criteria DC-l, Rev. 0

Remarks

None

Originators

J. Foie

Rakow

Checkers

R. Casassa

Distribution Revision No.

Supersedes Calculation Set No.

Approved By: ate:


CalculationSheet

Project

Subject

Prepared By:

Checked By:

QID 018001Date

Date

System Job No. File No.

Analysis No. Rev. No. Sheet No.

CONTENTS

Calculation Cover Sheet

4.1 Conclusions

4.2 Summary of Results

4.3 Requalification Analysis

4.3.1 Introduction4.3.2 Cylinder Operability4.3.3 Analysis

4.4 References

APPA>tx A,IC

'lees 00

IIIIIjjjjjjjjIIIjjjjjjjjjjjjjj

CalculationSheet

project

Subject

Prepared By:

Checked By

Date

Date

System Job No. Fite No.

Analysis No, Rev. No. Sheet No.

SECTION 4.1

CONCLUSIONS


CalculationSheet

projectWPSubjectRe ualificationSystemBIF Air 0 eratorsAnalysis No. Rev. No.

Prepared By:

CheckedBy.'ob

No.

Sheet No.

File No.

Date

Date2 83

CONCLUSIONS

This QID demonstrates seismic and hydrodynamic qualification of the8, 10 and 12 inch bore diameter cylinder operators identified inSection 4.2.

Summary Table 4.2.2 presents these comparisons and shows requirementsfor the bolting material in the 8 and 10 inch cylinders.

1. Cylinders CSP-A0-1,2,3 R 4 must be qualified for anactive function and require a representitive opera-bility demonstration as described in Section 4.3.2of this report.

This should be performed using the, values of air operator loads inQTD 361104 and 361106.

QID packages 361101 and 361102 document qualification of the valvesassociated with the 12 inch air cylinder in this report for the seis-mic loads which they experience. No fatigue analysis is requiredfor these cylinders because no hydrodynamic vibration is experienced.These cylinders were shown to quali'fy with A307 bracket bolting forthe actual response g-levels calculated in the piping analysis.This qualification package will be complete when a satisfactoryoperability test is performed and documented herein. Tt has beenconcluded in this report that the standard A307 "earbolts" shouldbe replaced with A325 material type bolts on the'" and 10" aircylinders only.

1005 00

HHHIHHHHHHHHHHHI

CalculationSheet

ProjectWPPS E iSubiectRe ualificationSystemBIF Air 0 erAnatvsts No,018001

Rev. No,0

Prepared By:

Checked By.

Job No.

Sheet No,

Fi(e No.

Date

Date

SECTION 4.2

SUMMARY OF RESULTS


CalculationSheet

project

SubjectR

Prepared By:

Checked By:,

Date

4 rs85System Job No

82044File No.

1P. 01 FAnalysis No.018001

Rev. No.018001 - 4..Z../.

4.2 SUMMARY OF RESULTS

Summary tables in'this section present calculated stressesin comparison to allowables for the 8, 10 and 12 inch air cyl-inder operators. Trunnion pin, drive rod and bracket bolt cal-culated stresses for the 8 and 10 inch air cylinders were takenfrom QID 361106 and 361104, respectively. These calculationswere performed on the valve/operator assembly using the SRSSmethod and the actual piping response g-levels to eliminateunnecessary conservatism in the higher-stressed components. Theair operator components addressed in this'eport are not highlystressed and were analyzed using simpler techniques with generallyhigher envelope loads having greater margin. See Section 4.3.1for more information.

The following summarv tables note corresponding g-levelsand 'ooerator components.

r 008 to

i-~ 'tPIa Pig


CalculationSheet

SubjectRe ualification cheeaeahe:gg

'Date p Z~ QSn~

SystemBIF Air 0 eratorsAnalysis No. Rev. No.

Job No.82044

Sheet No.

File No.

—4.2. 2

1P. 1

TABLE 4.2.1

AIR CYLINDER REQUIRED G-LEVELS

I

ST.ZE EPN ELEVATION REQ'D G'S — GLOBAL*X(N) Y(VERT) Z(E)

8

8

8

8

8

8

8

10

10

10

10

12

12

12

12

CSP-AO-3CSP-AO'-4

CSP-AO-5

CSP-AO-6

CSP-AO-9

CEP-AO-3A

CEP-AO-4A

CSP-AO-1

CSP-AO-2CEP-AO-1A

CEP-AO-2A

REA-AO-1

REA-AO-2

ROA-AO-1

.ROA-AO-2

481

478

475

480

490

497

497

500

500

500

500

597

597578

578

2.662.962.96

11.392.574.573. 35

2. 26

1.441.930.961.001.001.001.00

2. 99

3e173. '44

3.331.731.261.343.623.542 '32.110.600.600.600.60

3.764.195. 712

5. 85

2.670.860.862.801.901.851.161.001.001.001.00

Refer to final piping G-levels in Section 5.5 and QTD361104 and 36110b.

1000 00

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CalculationSheet

Project Prepared By: DateWPPSS E i eismic H drod namic Re ual. J.E. RakowSubjectRe ualification

Checked By: Date f2'gSystem

Aoalvsis No.018001

Rev. No.

Job No.

Sheet No

File No.

018001 - d..Z

TABLE 4.2.2(continued)

Remainin 8" Bore Air 0 erator Com onente 'h~14 =6:

Cylinder:SI = 12,056 psi c 18,000 psimax

Tie Rods:

ft = 6099 psi < 20,000 psi

Support Bracket (Bearing):F = 2299 psi ( 32400 psi

P

Total Stress:= 7492 psi e 21,600 psi

Shear Stress:691 psi ~ 14,400 psi

Weld:f = 789 psi < 21,000 psi

Fatigue:f = 1579 psi ( 45,000 psi

O.K.

O.K.

O.K.

O.K.

O.K.

O.K.

O.K.

Remainin 10" Bore Air 0 erator Com onents ~6 =5:h v—Cylinder:

max

Tie Rods:

18,000 O.K.

10,000 psi

1008 00

f = 6614 psitSupport Bracket (Bearing):

f =2287 psi 32,400 psi

O.K.

O.K.

6 J r a tIIIIIIIIIIIIIIIIIIIIIIIIIIIIII

CalculationSheet

Project

SubjectRe ualification

Prepared By: Dater 83

SystemBIF Air 0 erators

Job No.8204

File No.1P.

Analvsis No.018001

Rev. No. Sheet No.018001 - cf..2. S

Total Stress:= 4830 psi 21,600 psi

TABLE 4.2.2(continued)

O.K.

SUMMARY OF RESULTS

Shear Stress:Weld:Fatigue:

"T = 346 psi w 14,400 psi , O.K.f 832 psi ~ 21,000 psi O.K.N/A (Allowable stress range= 45 ksi for welds).

12" Bore Air 0 erators Com onentsCylinder:

Tie Rods:

Support Bracket;(Bearing):Total Stress:Shear Stress:Weld:Drive Rod (Tensile):Trunnion Pins (Shear):

SImax

ff

p

f

4267 psi ~ 21,600 psi283 psi ( 14,400 psi3445 psi < 21,000 psi31,172 psi ~ 86,400 psi2,515 psi ~ 11,840 psi

O.K.0.K.O.K.O.K.O.K.

3439 psi ( 18,000 psi O.K.

13681 psi ( 20,000 psi O.K.

1775 psi ( 32,400 psi O.K.

Support Bracket Bolts (A307): gh=g = 1.54:h v (I.rS~Tensile: 12,598 psi w 30,000 psi O.K.Shear: 6,339 psi ( 1$ ',000 psi O.K.

1000 00

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CalculationSheet

WPPSS EQSubject

II

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Analysis No,'0'1 v001=Rev. No.

82044File No.

OT.01/F

'18001 - c$ .2. &

Prepared By: DateJ.E..Rakowski 4 22 8

Checked By. J g g J Dale +(

SUMMARY TABLE 1. 3

ALLOWABLESTRESSES

Since operability is required, the stresses for thefaulted condition will be kept in the elastic range. Thetable below is based on AISC criteria and the yieldstresses at temperature (340'F) from PG. 9 of REF. 4for conservatism.

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SubjectReaualificationSystemBIF ir 0Analysis No, Rev. No.

Prepared By:

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Job No.8204

Sheet No.

File No.

Date

Date

1P. 1

Section 4.3


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CalculationSheet

project

Subject

Prepared By: Date

checked 8y: / g~ + Date +/System Job No. File No.

Analysis No.018001

Rev. No.018001 4.~. l tI

4.3.1 INTRODUCTION

The analyses herein address specific parts of the 8, 10 and12 inch diameter Miller Air Products air cylinder operatorsidentified in Section 1.0 of this QID. The remaining struc-tural components of the operators were addressed in the asso-ciated* valve dynamic qualification pakcages. Refer toTable 4.3.1.

d 8 and 10is calculation.

The analyses in this QID were performed with envelopingg-levels. Table 4.2.1 summarizes the required g-levelsfrom the piping analysis. The air operator mass-stiffnessmodel incorporated in the piping analysis to calculateresponse g-levels on the more Beverly loadeinch operators is riven in Appendix A of th

4.3.2 CYLINDER OPERABILITY

The cylinders designated as EPN CSP-A0-1.2,3,4 must operateduring an DBE from open to fail-closed.. While seatingthe valve disk during a DBE, the air cylinders must havesufficient capacity to overcome the seating torque of thevalve plus the frictional forces in the bushing and cylin-der. The following table compares the required seatingtorque forces and minimum cylinder spring preloads givenin QID 361106 and 361104 for the 8 and 10 inch cylinders.

sizequzre

Seatin Fore* SprangPreload

Residual CapacityTo Overcome Frictio

8ff

10"1150 lb.1847.lb.'500

lb2900 lb

350 lb.1053 lb.

+ QID's 361106, 361104 and (361101 R 361102) for the 8, 10and 12 which operators respectively.

100s Co

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ProjectWPP S

Prepared By: Datei . eismic H drod amic Re ual. J..E'. Rakowski 4 22 83Subject Checked By: g ~ i / Date J /System

Analysis No.018001

Rev'. No.

Job No.82044

File No.1P. 01 F

018001 —4. 3,2. 5

4. 3. 2 CYLINDER OPERABILITY (CON ')Ability of the spring to fully close the valve depends on thecoefficient of friction.between the sliding surfaces of thecylinder, namely the drive rod and bushing, and the pistonand cylinder.Although upper limit bushing pressures due to load reactionwere given by Miller Air Products for consideration of shaftwear, (Section 7.0, Ref. 5a and 5b) this alone is not asufficient criterion because piston friction in the cylinderis not accounted for.Therefoxe, it is recommended that one 8" air operator(CSP-AO-3 or 4) be fieldtested'to verify operability sincethis size has approximately only 25 percent the residualcapacity of a 10 inch. operator. Dynamic plus static bush-ing pressures for these operators are calculated in QID's361106 and 361104 and these may be used as a guide to speci-fy the simulated test g-level on the end of the air cylinderby consideration of the bushing. reaction equation in Ap-pendix B of this calculation. The test load should beapplied in the direction which tends to rotate the cylinderabout the trunnion pin axis. Bushing pressures for boththe 8 and 10 .inch operators must be considered in compari-son to the'elative residual capacity, of the 8 and 10 inchcylinders so that both sizes axe covered by. this test.

4. 3. 3 ANALYSIS

4.3.3.1 12 inch operator assembly frequency*.

100s 00,

Similar calculation for the 8 and 10 inch assemblies aregiven in QID 361106 and 361104.

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"

Pl STOM:

(Qg.gay $ ,5+ 4.375)( M'5) &9 ~ 6

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Date

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ProjectWPPSS E ui ment Seismic H drod

Prepared By: Dateamic Re ual. J.E. Rakowski 4 22 83

Subject Checked By: Date~ ~ g+

System'nalysis

No Rev. No.

Job No.82044

File No.1P.01 F

ol~ t—B.B.s,36

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SubjectRe ual

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0

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d.3.z.z7

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g g I, Iq to I+)= . 334

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System

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Job No.82044

DateO

File No.1P.01 F

Analysis No1 1

Rev. No. Ol't Ml- 4.9.3.36

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+. Ztt'-',lS.7>)0.Z)

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Proiect Prepared By: DateWPPSS E ui ; Seismic H drod amic Re ua1. J.E. Rakowski 4 22 83Subject

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System


Job No,82044

File No.1P. 01 F

Dl b~ I —c2.P,3 gg

p~t-w gN E+ A. ~ F mo ~R.l~w vzc INmztq:

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Sheet No

dr8oor-

Date

Datel2- S-82

Q+ REFERENCES

1. 8" Cylinder, Dwg. No. C-26096, Flick-Reedy Corp.



4. BIF Report TR-74-7, Rev. 1, Dated 1/5/76.

5. Cylinder Support Bracket, 8" x 15" Cylinder Operator., Dwg. No. A-208293.

6. Cylinder Support Bracket, 10". x 15" Cylinder Operator, Dwg. No. A-208195.

7. Cylinder Support Bracket, 12" x 15" Center Trunion Mtd. Miller Cylinders.Dwg. jj A-208274.

8. Manual of Steel Construction,

9. Cygna Calculation, 82044, QID:(

10. Cygna Calculation, 82044, QID

AISC, 8th Ed.

361106, Dated 12/7/82, Rev. 2.

361104, Dated 7/23/82, Rev. 0.

QID 018001

APPENDIX A

SUMMARY OF A/0 MODEL

USED IN PIPING ANALYSIS

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04/06/83 BURNS L AOE ItiCMASIIINGTOti PUBL'IC POMKH SUPPLY SYSTEH

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PAGE 532

DATA DATE 04/06/83

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6. 0 DRAYINGS USED FOR PXQUALIFICATION

Contents

BIF Drawing A-208293, Cylinder Support Bracketfor 8 x 15 Cylinder Operator, 24" Valve.

BIF Drawing A208195, Cylinder Support Bracketfor 10 x 15 Cylinder Operator, 30" Valve.

BIF Drawing A-208274, Cylinder Support Bracketfor 12 x 15 Cylinder Operator, 30" Valve.

'

Fli~V, - Reedy Corp. Drawing C-26095, CertifiedDimension for Model A83B Cylinder, 10" Bore,57 5/8" Stroke.

Flick - Reedy Corp. Drawing C-26096, CertifiedDimension for Model A83B Cylinder, 8" Bore,46 3/8" Stroke.

FliCK - Reedy Corp. Drawing C-26093, CertifiedDimension for Model A83B Cylinder, 12" Bore,40" Stroke.

BIF Drawing A206759, General Arrangement of(2), 12"xl5" Cylinders - Spring loaded, 84"(valve).BIF Drawing'A206760, General Arrangement of(2), 12"x15" Cylinders - Spring loaded 72"(valve).Miller Fluid Power Drawings 7505, 7505 A-D,Series 8, SRE Air Cylinder Cross Section—(General Arrangements Showing Seals).

QID 018001

7.0 PRIOR CALCULATIONS AND TRANSMITTALSUSED FOR REQUALIFICATION

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Company: (;ES ijI Telecon" o' Conferepce eport

Project: t4os,r ~2}II4g~b-f4oe,

Washington Publ i c Powem4upp~~st'.em. ~:J

' «)0 6 82

Subject:

/ID inf018001 and 0180 'Acr-4pera@r)"-' "wpi'ec: ~--gD~O

Participants:Ole Konstantinow~WE «J««JJ ~

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I called 0)eg 'ibo&uMR detailed informa'trop„."of 'thehir'ylinderoper~aor" (P', 8" hand.lg-'~.Eo~e)„'for.,'.the 18",24";

1. The air and spring cyli;nder»6p'er'htor,,is'not.in„theMiller's catalog and,it,.~i s.a. special —

design~'P.

2. The sizes of the air cylinder's...are,:: ~fw

OD ~~ 'ID

10n bore,.... '10'A25".;.,'~; . -= 9.;9K .": .'

6n . bore--- ~28,5,".' '5'.SPj'«JVJJ««

ru 4.

The matef'i'al is equivalent4to'"ASTM A519': '~w«a«~JJ« ~««w a w a a«VJ Jv ~ J«JJa

- ~ .3. Miller Fluid Power does.not calculate the GG lo'cation'f'he

ai» cylinder. In oftrJ case, BIF calculated„ tlieJ Ctl '",

1 ocatio „of„+e+." 8"",'rjd 3a', M~yl'inders>.J '~k '4,,'J

p»'.

The'pring inside the cylinder..yas designed"bywti3ers,and there is no record in the file 'indicating'who desj.gn'edthe spring, MFP ordered, the spring'ith this infoRnation;preload, final„"VdSf> Itforf< 'ftVoRep

5. Oleg gave. e ncaa.l-sye~tyf.'' -company which~dt.sigrted ,most ofj'their hir-sp~;cylindeC's'iiot necessagi3> <heone h wdofgesd-ntbee;spri gs onf,

IIELD

6018001 and'rgg)8009).J

6.'leg prhmised to seiul'fse':scmes'ketches of theicraf ra'rjd '9c

spring ~yonder ctes<ign.'

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.7. Basically, ihg. assembly. of,.the„ingegpa] components of anajr-s'pqing.,cy]ipder.Be";,j pre]opded,.corn'pressed spring

-.w'it)-a'concentrate.,jp'ring stpp'ybe'(welded'to the endcap.plhtqf'os'nerend-„ofittje„piston".':. An'd.with a series

,„. „"of concenti;a<p.,rings *on the'other. e'rid,.of,Khe piston,'.,-(Setweeg:phe';pistonrland..the end,,pl'a*'te)" to keep the spring

„... in,coIIIpressjop.'j;he„piston,".i,s,tgadj„; fr.om,iron'. and is'.;:threaded „'into (he drive ro«d"our.;pistoh.',jod, The piston

is"able to 'take 'the'hrust« 0rom the 'air,.;.pressure.

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Ln apse the,drive rod:js removed-in~the„direction whichcauses ther,'pistoii to'bear'."on. th'„.end. p'(ate,*(through the

,cqncentrtate rings) and assej;i;s'a.'hrust.on..'this end plate,.'he'hretads.on-'tIIe~p'i,jason.,wi11 elope ..iIeqce the same magni-

. .' tude„of. this.'hruusk.~ ~ A,ske)ch of g e.',air=spring cylinder...: operator.'is as'6'ei.ow': , '",

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Req'd Action By

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Blstrtbutlon

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Company: CES0 r r ~ a mors, r.....„A,.Jemooa...„....... "".' „„9't C~~nrerencm~Report

project: Job No. 82044Washington Public Power Supply System

wow wire 44 ~e~ ~err PAN Awe ee'oteew 8 Par

Subject r

/ID ¹018001 and 018009-'sAO ——Participants: —Rick-R~ cap&o.

nd iisteh-

of H%F

CESSDAO'f

Item

2.

Gomments-

Dwg. ¹C-26096'rawn'ry,F1ickrReldy'orpnoration',(I'1iller FluidPower Div.), indicated'that„both.the "fait. "c'toshdu (CSP-V-3,4and CEP-V-3A a 4A), and the-"fail: open'-''design',{CSP-,V-5, 6)have the samytspriftg preloa'd (1 '500-'¹) 'and'he„-final Toad(3,000 9). (Npte that CS'P-9'-,9 'Ifa>1 opens'was n'o't mentionedin C-26096),. "It tJ(as'poiih'ted out'in '/ID ¹361106 that th'"fail open" operator"'asshmbly"droes "ttot have-enough'air pres-sure to close'he butterfly valve. if the 'sttring'final,,load 1

is equal to 9'000¹.'-

Rick went'hirough''the"BIF"record award cnonfiriiii d 'that the in/or-mation containelqin'w'g." ¹C'-'26096 'fs.ihcorrrec't". 'Therae shouldbe two types'f ski'inrg'ene.foi',the "fail'cl'ose" ;'design whichhas a sprin'g jYrelOrad of 1'500¹'ndifiiia1 load-of 3,000¹; theother type o7 s)nhg is 'fora"the "fail open" desig'n which hasa spring preload of 350¹ and a sprfng,.'final load of'1,850¹.For the fail open desig~ with a 70.psig air pressure and a;"

piston area 'o'-50:3 .jn'.,-'; a pressure force of 3,521¹ couldbe exerted on -the„piston. -This is sufficient to overcomeboth the spring...final..load (],/50'.,and. the;seating torque

'orceof 1„478¹,-,'l6ck aTso .'pointed'ut that all'he valvesand its ai'r",cyTiiiher ope'razors-jtave+een -tested for theoperability (to open-and close).- From thts Telecon is cantbe concluded"than"t-the valves, EPN'.¹CSP-V-5,6,9 (the fail opendesign) which'PPSS ajTe'ad(I rFc'eivEd; are properly designedexcept the reco'rd of the spring forces (inside the aircylinder). are not show'n 'correct'ly. Rick indicated he willisend me the required information to clear up the springforces problem.

Rick will also send me the support brackets of the 6", 8" i

and 10" bore air cylinders.r

ReqMAction By

Signed:

Oistributlon:

1030.00

coy rerrrr 6 %4'wwH r eaerrerr areal m Ae'&w444 AA1%%a %r r% err ~ I ~ Ir+r A r ne Kerr e

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Company:

Project:

*~ Itj Teiecon x ct Conterence Report

Job No.

Subject: < E )E

QID f01mjOT-.:antn ISm'ime:<EMl 1 dt E % < piece'.

Participants:".~r 1C,


3 ~ I

EA'„'

i4.

Ritk"and I'-discusied'th'e: locations-"of tTie CG'of the 6", 8"and 10" bore air cyl'inders'-'(Vor'both'-'the""fai'I closed" andnfail open" designs). We concluded that the CG locationsof the 6" bore air cylinder'fai'1 op'e'n«des'ign, Dwg. 8A-206762) and the 10n bove air cylinder'fail closed design,Dw'g;«8A'-206763)'l".e probably torrent. (cag';t'.find the" calcs).However, for the 8" bore;. air~ cylinder, Dwg. PA-206764 (failclosed design) and'wg.- imIA-206765 (fail open design), bothhave the identical CG location"yn.,the,gylingens.;

There are possibly two mistakes „about <he; CG.;location on the8" bore air cylinder. First, the "fail closed" and "failopen," designs could not hav'e the same CG .location becausethe "spr'ing and'the. spring storpi tu%e're'.lo'cated o'n 'theopposite-and of the"cyAnder'o'f""the 'tW<o 'QeEsigns.'ote thatthe spring and the spring stop tube are located at theop'p'oui te'end." of. the air'rr1j t~" ~tI;<he'"two.'"designs have adiffer'ent'ocation 'o'f th' air'~hl'et "(at"<he."opposite end).

Second, the CG of the 6" and 10." bove c'ylinders pre bothloBte'd'near'he center of 'the air cyl'in~Ier".E ""Hot'lever,, the8" bore air cylinder has its'B'located'bbut 9~'ff the'copter of„, the,Fylinder toward the,far end (away .from the sup-j'ovt. b "acket)'.„ Pick'w'IT@ se'arch ..for.'the caTc'uTations of the'CG loca/ion's"of tlte'ai'r 'cylind6 s. "" K,he'failed "to findthyrse"'ca'1„'culatioris;- he.pr'okised Cb. i4'nd, me a'=letter statingthat the"CG '-loca't'idn oY'the 'f"'"b'ore'fr'rcyfindev" h'ave boththe "fail open and fail closed designs and can be assumed tohave the same proportion as that of the corresponding 6" borecylinder (fail open design) and the 10" bore cylinder (failclosed design), respectively.The time needed to close or open the butterfly valve is approimately two seconds (estimated).

Sighed:

Oistribution:

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Communicaboas;=,.-,=-.-:.—;—.-.

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Company:

Project:

Telecon

Washington Public-Power Supply System

"0 Conference Report

o No. 82044Date: 10/6/82

Subject Time: 10:50 A.M.(ID 8018001, 018009.;(Air Cylinder Operator) Pia'e'- " '"'DAO '-

='articipants:

Dave Pf1am

Ra ond Hsieh

f Co i1 S eci al t Co .

CES/SDAO

of

Item

2.

3.

4,

~ -Comments

Dave exp)ained,toI me ghat,the,,spjing,manufacturer Hses the.following rulies'.'i',."'designsngi'the»spgng's': ', „'..',a. For low cycle„..spring'esign:.. „;:, .

grist

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x=f0.45 Fu'Fb-"'='ultimate:"tensile: Stren'gtlT'f>t'";-

" '~~ "~«b!'ateria'])'

b. FOr high'r CJJCle Spy!ing deSign: ir ".r."«. ""I, " ',.'t.!'-'0.3

to" 0;35'Fu -: '«; 3a,'I ot«', .'!„:?c t;b ~ f~ -!max-.

3PDave indicated::i'fr hef lffere,ifesi gnsyg. the'se, spry ngs'f„ th'e as rcylinder for W)PSS,ten y'ea'rs,'ago;.he wil;1, use these safIIe,rules

I

The most comiIIon,used,,'material for the. sprsng,wpj,ch 'Cojl;;Specialty „provides.,to Hjl,.per,rFluid. Power', is AISI 51608'.Whichhas an Fu of 196 'ksi.

The bar diametep, fprf.fpe*:10",3"="ang5.,",bore.'air.'cy'lirfgr.'are:

Dave mention'ed pe,,foesp,.t know, th'e:fatsgue'l i.fe .in'foriiiat)'onof the .sprig .. 'HI„said that,i;t;.,j s .very'pnusua1„.'to, hear .thatsprings fai,lied in, lej,stress, cycles .(j ersz.than JoDI;000'.cy'cl es)when designed..'to th'e gu',lisf menQioned iri„:,(1),;above.;;.„',„"„

Req'd Action By

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Signed:

Distribution:

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Company: t y ~~ p ., „QTelecon ' Conference Report

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Job No.VPPSS Eauipment .Seismic/Hydrodynatrtj.cRequal xfication .— - -— —~e ~+9i~—'—

018004, 018009,II ~ ~, II!

N. Hardy

L. Fernandez.$. ~

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Item Comments a

RBO ha oriana? veri faICari0ri ~aragaa iaIr..ahaabove referenced files which specify imcojnglete i,,status. These:sh'H 1 'be &organ%'zed 'into completepackace format 3q@ fa,l.ed ip, tpq,. RBQI QID',.binders. ',

The completed packages are <forthcoming from theArea Offices"-i n~5he -foem"'o& Reezsiorf:-R ~''theseRevision 1 requatjification packages will supersedeRevision 0 in RBO QID files.

Ig ' > aZt is noted that nond of'hese incomplete packages(Revision 0) hpve,„'bqen qubmittep- to the~ctS.

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rAlva l e~l4~tY,. Hardy. N. Be~m~

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