Text

Forwards Wppss 2 Purge & Vent Valves Seismic & Hydrodynamic Analysis, Per SER Outstanding Issue 26
	ML17277A649
Person / Time
Site:	Columbia
Issue date:	06/22/1983
From:	Bouchey G; WASHINGTON PUBLIC POWER SUPPLY SYSTEM
To:	Schwencer A; Office of Nuclear Reactor Regulation
Shared Package
ML17277A650	List: ML17277A649; ML20024C146;
References
	RTR-NUREG-0892, RTR-NUREG-892 GO2-83-550, NUDOCS 8307120309
	Download: ML17277A649 (559)
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ACCESSION NBR: 8307120309 DOC. DATE: 83/06/22 NOTARIZED: NO DOCKET FACIL:50-397 WPPSS Nuclear Proiect. Unit 2P Washington Public Powe 05000397 AUTH. NAME AUTHOR AFFILIATION, BOUCHEY.G.D. Washinaton Public Power Supply Svstem RECIP.NAMERECIPIENT AFFILIATION SCHWENCERPA Licensino Branch 2 (

SUBJECT:

Forward ds "WPPSS 2 Purae L Vent Valves Seismic 8 Hydr odvnamic Ana'Ivsiss" per SER Outstanding Issue 26 DISTRIBUTION CODE: BOOIS TITLE: Licensina COPIES RECEIVED:LTR Submittal: PSAR/FSAR Amdts L i ENCL Related 5 SIZE:

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

RECIPIENT COPIES ID CODE/NAME LTTR ENCL ID CODE/NAME LTTR ENCL NRR/DL/ADL 1 0 NRR LB2 BC 1 0 NRR LB2 LA 1 0 AULUCK R. 01 1 1 INTERNAL: ELD/HDS2 .1 IE FILE 1 IE/DEPER/EPB 36 3 IE/DEPER/IRB 35 1 IE/DEQA/QAB 21 1 NRR/DE/AEAB 1 NRR/DF/CEB 11 1 NRR/DE/EHEB 1 NRR/DE/EQB 13 2 NRR/DE/GB 28 2 NRR/DE/MEB 18 1 NRR/DE/MTEB 17 1 NRR/DE/SAB 20 1 NRR/DE/SGEB 25 1 NRR/DHFS/HFEBOO 1 'RR/DHFS/LQB 32 1 NRR/DHFS/PSRB 1 NRR/DL/SSPB 1 NRR/DSI/AE8 26 1 NRR/DSI/ASB NRR/DSI/CPB 10 1 NRR/DS I/CSB 09 NRR/DS I/ICSB 16 1 NRR/DS I/METB 12 NRR 9 22 1

NRR/DS I/PSB 19 ~

1 0 1 NRR/DSI/RSB 23 1 G FIL 00 1 1 RGN5 3 R /MI8 1 0 EXTERNAL: ACRS 01 0 BNL(AMDTS ONLY) 1 g DMB/DSS (AMDTS) g FEMA REP DI V 39 LPDR 03 1 1 NRC PDR . 02 1 1 NSIC 05 1 1 NTIS 1 1 TOTAL NUMBER OF COPIES REQUIRED: LTTR 53 ENCL 06

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Washington Public Power Supply System P.O. Box968 3000 George Washington Way Richland, Washington 99352 (509) 372-5000 June 22, 1983 G02-83-550 Director of Nuclear Reactor Regulation Attention: Mr. A. Schwencer, Chief Licensing Branch No. 2 Division of Licensing U. S. Nuclear Regulatory Commission Washington, D.C. 20555

Dear Mr. Schwencer:

Subject:

NUCLEAR PROJECT 2 QUALIFICATION OF WNP-2 CONTAINMENT VENT AND PURGE VALVES

References:

1) Letter, A. Schwencer (NRC) to R. L. Ferguson, (Supply System), "Request for Additional Information""; dated September 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 valve operability concerns cited in Reference 1) and 2). This letter transmits stress analysis work to address the remaining open issues.

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

These margins of safety were found only with the modifications described in the attached reports. These modifications will be performed prior to operation of WNP-2.

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Mr. A. Schwencer Page 2 June 22, 1983 With the modifications in place, these valves will remain functional through forty years of postulated hydrodynamic events, five operating basis earthquakes, and one,.safe shutdown earthquake.

phd G. D. Bouchey, nager Nuclear Safety and Regulatory Programs RWH/sms Attachments cc: Mr. R. Auluck - NRC Mr. W. S. Chin - BPA Mr. A. Toth - NRC Site

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Washington Public Power Supply Sys'.em P.O. Box 968 3000 George Washington Way Richland, Washington 99352 (609) 373-6000 The attached reports are the structural analysis of the purge and vent valves and operators installed at NNP-2. The loads used in th. anal'"-'i are the valve operating loads combined with the dynamic '~oads which would result from seismic and hydrodynamic events as determined by the piping analyses for the plant.

There are three reports attached. They separately address:

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

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

3) The air operators manufactured by Miller Fluid Pcwer and suppl'.ed by 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 ppli System's Equipment Qualification Group and are in heir compl-te form in the Equipment Qualification files. However, in the '.ntei"est of conserving space in the transmittal to the U.S. NRC, pages wh'.ch are duplicated in the reports have been removed from all but one of the reports. Also, documents which have previously beett submitted to ".h=

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

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...24" Cylinder Operated Butterfly Valves for:

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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 MANUPACTURKRt BIF MODKI NOI A-206765 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 plates to aualifv air operators for reauired fatiaue cvcles.

THK ABOVE SKISMIC ANO QUALIPICATION REPORTS HAVE BEEN RKKVALUATKDIN ACCORDANCK WITH THK CURRENT NRC SKI5MIC AND CRITERIA'

~ IKEK 5TANOAROS 244 (1575) 2 USNRC RKOULATORY CUIOKS 1.$ 2, 'I,144 2>> 5TANOARO REVIEW PLANS 2&Pe 2>>14eEN

~WSKkggW THK ABOVE COMPONENT HAS BEEN P'OUNO ACCEPTABLE POR PKRPORMINQ IT5 INTKNOKO SAI ETY RKLATKDPUNCTION WHEN SULIECTKD TO THE PLANT SPKCIPIC VIBRATORY LOAO5.

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REVISION Q WASHINGTOt4 PUBI IC POWER SUPPLY SYSTEM T ~'j- E S T
llllllllllllllllllllllllllllll Qualification Summary of Equipment QIDN 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 9 CEP-V-3A ET 4A I~ SCOPE: NSSS Q BOP MOOEL NU4BER. A-206765 OUANT I TY:
~. VENOOR: B~F 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 1 ation, orevent ion o f the release of radioactive material to the environment.
c. IS THE EOUIFMENT REOUIREO FOR: HOT STANOBY COLO SHUTOCMN P] BOTH NEITHER 9 PERTINENT REFERENCE OESIGN SPECIFICATION: WPP ec. 2808-I I I. IS EOUIRIENT AVAILABLE FOR INSPECTION IN THE PLANT: YES NO PAGE I OF 5
REVISION,Q 2.2 Qualification Summary of Equipment (Continued)
QID-":. 361106 l Ref. No.
IV l EQUIPMENT QUALIFICATION METHOD:
I TEST QX ANALYSIS C(NBI NATION OF TEST & ANALYSIS QUALIF(cATIQN REpcRT ~ 24" c 1inder-ooerated Butter f1 va lve* I ~
I (NQ ~ TITLE 6 DATE) OT 0 1 . F Revision 3, June, 1 98 3 I 15
'a CCMPANY TIIAT PREPARED REPCRT: e cQMPANY THAT REYIEwFQ REPORT: washin ton Public Power su olv svstems
Plus original valve analysis 3,4 V, III BRAT ION I NPUT:
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~l. LOADS CONSIOEREO: a. SEISMIC ONLY I
Q HYCRQOYNAMIC ONLY CM ) Cf'~l'2
c. Q CCMBINATON OF (a) ANO (b)
I MET)K)O OF C(MBINING RRS:
Q ABSOLUTE S(H Q SRSS OTHER (SPECIFY)
REQUIRED RESPONSE SPECTRA (ATTACH THE GRAPHS):
I
<4 ~ DAMPING CORRESPONDING. TO RSS: CBE Q SSE I5 REQUIRED ACCELERAT ION IN EACH DIRECTION:
Q ZPA Q OTHER (SPECIFY) )i/~h 15 QBE sos - Attached F/B . V ~
Attached l J, t
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6. 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>>:
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1. SINGLE FREQUENCY Q MULTI-FREQUENCY Q RANOO4 2+
Q SINGLE AXIS MULT I-AXI S SINE BEAT
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3 NO, OF QUAL IF ICATION TESTS: OBE SSE OTHER (SPECIFY)
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) v~ Q~ =~
NO 8, INPUT g-LEVEL TEST: CBE S/S ~ F/8 a SSE S/S i F/8 s
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9, LABORATORY MOUNT I NG:
BOLT (NO.
a ) C3 0 FUNCT I 0 OPE L TY ER EO: ES NO Q 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 NTAT I ON OF TEST ANO ANALYSI 5 i ALSO COI4 LETE I TEM VI"I ~
PAGE 3 OF 5
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'Qualification Summary of Equipment (Continued)
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~S w>> 'w QID~ 361106 Ref. No Vl I. IF QUAL IF ICATION BY ANALYS I S, THEN CO4PLETE:
I~ METHOO OF ANALYSIS:
STATIC ANALYSIS iC EQUI VALENT STATIC ANALYSI S Q 0YNAMIC ANALYSIS T INES I STCRY Q RESPONSE SPECTRIH 2 NATLRAL FREQUENCIES IN EACH OIRECTION (SIOE/SIOE, FRONT/BACK, VERTICAL):
s/s - 10.81 Hz 26.1 Hz v ) 100 MOOEL TYPE:
Q5O . Qa) Q IO Q FINITE ELEMENT Q BEAM Q CLOSEO FCRM SOLUTION 4.Q COMPUTER COOES:
PREQUEL Y RANGE ANO NO OF MODES CONSIOEREO HANO CAI.CULATIONS OTHER 5, METHOO OF CCHBINING DYNAMIC RESPONSES:
R' ~
ABSOOLTE SIR
[)(j SRSS Q (SFECIFY) 6, OAI>>IIIO: CBE SSE
~ F 7>> SUPPORT CONS IOERATIONS IN THE MOOEL:
8 CR I T ICAL STRlJCTtRAL ELEMENTS 6 GOVERN I NG LOAO OR RESPONSE SE I SMI C TOTAL STRESS A, IOENTIFICATION LCCAT I OR CCIBI RATICR STIIESS STRESS ALLO6ABLE
,o,Valvel Ears CPP-T)-3&4 PLPB-BR&&1 15743 19538 26880 (PS )
Ear 'Bolts CSP-V-3&4 pipe-normal 15777 18382 6600a (PS )
Drive Rod CSP-V-4 rod-normal 8543 33019 86400 (PPI) I
'hr- Bolts CSP-V-6 pipe-normal.57543 58884 66000 (PPZ)i
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MAxIMMY ALLQIABLE BE MAX>> CRITICAL OEFLECTION TO ASSURE I, OEFLECTION LCCAT I ON FUNCTIONAL OPERABI L I TY
<0. 01" Valve disk radial approx 1/8" radial deflection clearance VT>>IFA>>>>>>>>>>AA>>~'>>>> R AA WW
Final.response accelerations rom pining analysis I
Bre=uBed.
PAGE 4 OF 5
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Revision 2 2.5 Qualification Summary of Equipment (Continued) gQID 361106 Vill. REFERENCES
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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"
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2. 4'PPSS Unit 2 Drawin s:
CSP-807-81 '8 Containment Purge Air Supply
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pr CSP-809-1.2 Suppression Pool Vacuum Breaker CEP-625-3.4 From Reactor Nozzle X-67 to SGT-Fu-lA, 1B
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CEP-625-1.2 From Reactor Nozzle X-67 to SGT-Fu-lA,
'B,
>>> >g l D.220-0310 Support and Erection Isometric-IR64 (Johnson Controls)
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3. BIF Report TR-27234 and TR-27235, "Dynamic Torque Calculation of Butterfly Valve; Sizes 24 and 30 inch", dated November 1P, 1982.
4. Report //TR-74-7 by McPherson Assoc., Inc., "Design 6 Seismic Analysis 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 gP l>
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Calculation c Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII
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Date Date 5/27/83 Subtect Equipment Seismic/Hydrodynamic Requal. + .-~/=~
CSP & CEP 82044 OT.01.F Rev. No. Sheet No.
QID 361106 2 2.6
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z c SECTION 4.4
. REFERENCES (CONTINUED):
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 Walkdown Verification Forms, Revision 1, dated 1/5/83.
9. WPPSS, %3P-2, Safety Related Mechanical Equipment List Summary Sheets, dated 2/10/83.
10. "AISC Manual of Steel Construction", American Institute of Steel Construction, 8th Edition, 1980.
ll. Preliminary Transfer of Final Burns & Roe Piping Loads for CSP-V-1,2,3,4,5,6 and CEP-V-3A&4A, received 4/13/83.
12. Cygna Energy Services, "Equipment Seismic and Hydrodynamic Requalification of 30" Cylinder Operated Butterfly Valves for 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 Hydrodynamic Requalification for 8", 10" and 12" Bore Air Cylinder Operators," 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 Hydrodynamic Requalification of 24" Cylinder Operated Butterfly Valves for CSP-V-3,4,5,6, & 9 and CEP-V-3A & 4A," File No. OT.01.F, QID No. 361106, Revision 3, June, 1983.
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TABLE Or CONTENTS QXDN 361106 SECTION TITLE NO OF PAGES 1.0 Requalification Certificate 2.0 SQRT Forms 3.0 Table of Contents 4.0 Requalification Analysis 4.1 Conclusions 4.2 Summary of Results 4.3 Analysis 4.3.1 Introduction 4.3.2 Calculations 66 +Appendices 4.4 References 5.0 Appendices 5.1 Response Spectra 5.2 Nalkdown Sheets 21 5.3 Valve Local Coordinate Systems 5.4 SRM Sheets 5.5 Final Pipe-Mounted Equipment Response G-levels 6.0 Drawings Revision 3
TABLE OF CONTENTS QIDI 361106 CON'T SECTION TTTLE NO OF PAGES 7.0 Transmittals, Prior Calculations and Reports 7.1 Communication Reports & Correspondence 37 7.2 Old Regualification 6 SQRT Forms 7.3 BXF Report 98 7.4 McPherson Associates Analysis 75
SECTION 4.0 REQUALIFICATION ANALYSIS
4I 4 O4 OW Pt I
Calculation Cover IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Sheet Project Job No. 82044 E ui ment Seismic & H drod namic RequalificatioA'" 'T.01/F Client Gale. Set No. ]
No. of Sheets Washin ton Public Power Su ply System Subject Seismic Qualification of 24" Cylinder Operated Butterfly Valves QID 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 using valve and operator response g-levels transmitted by the A/E,(Final piping 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 Checkers Distribution Revision No.
Supersedes Calculation Set No.
J. Rakowski D. Searle WPPSS-2 Project File-1 Revision 2 L. Kaner Approved By: Date:
M. Scott LC Fernande Ii
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared Date By.'hecked Subject By; Date System Job No. Fite No.
Analysis No. Rev, No. Sheet No.
CONTENTS Calculation Cover Sheet 4.1 Conclusions 4.2 Summary of Results 4.3 Analysis 4.3.1 Introduction 4.3.2 Calculations 4.4 References rccs cc
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII project Prepared By: Date Subject Checked Date By.'ob System No. File No.
Analysis No. Rev. No. Sheet No, SECTION
4.1 CONCLUSION
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project .WPPSS Equipment Seismic Prepared By, Oate H drod namz.c Re ualification 6'9 83 Subject BIF Valves/Miller Operators Ã. ~ay, ~ 4, 6/9/83 System Job No. File Jlo.
CEP 6 CSP 82044 1T.01.F Analysis No, Rev. No. Sheet No, 361106 4.
1.1 CONCLUSION
S Seven 24-inch BZF,Butterfly valves with Miller Air Products cylinder operators have been analyzed for structural integrity and operability for the plant, specific seismic and hydrodynamic piping loads transmitted from Burns and Roe. ,These piping loads are in the form of air operator response G-levels (Section 5.5, dated March 31, 1983) .
The valves will be qualified after incorporating the following modifications:
1). Remove the existing operator bracket attach-ment bolts (A-307) and replace with an A-325 or A-490 bolt.
2) Reinforce the operator support ears with the addition of shear plates as shown on page 4.3-48 or 4.3-54 of 361106, Rev. 3 (this report) .
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By; Date Subject Checked By: Date System Job No. Fite No.
Analysis No, Rev. No. Sheet No.
SECTION 4.2
SUMMARY
OF RESULTS rooe oo
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Prepared By Date WPPSS MECHANICAL EQ '3z, 3 Subject Checked By; 24" Butterfly Valves 3 aolas System Job No. File No.
CSP it'r CEP 82044 OT.01.F Analysis No. Rev. No. Sheet No.
36 1 1 06 - ~Z-36110
SUMMARY
OF RESULTS Parametric data for the seven subject valves in this report, is given in Table 1.1. Results of the requalification analyses, which include a comparison of calculated stresses to the allowables are given in Table 1.2. Allowable stresses for the various material types are given in Table 1.3.
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WPPSS EQ mV3 Subject Checked By, Date II 8 55 System File No.
82044 OT.01/F Analysis No. Rev. No.
361106 3@/lb/ -4.z-Qo ~~cCZ>> c io/s>
SUMMARY
TABLE 1.3 P(>d- Q)m~r) ~/ I I/')
ALLONABLESTRESSES Since operability is required, the stresses for the faulted condition will be kept below yield. The table below is based on AISC criteria and the yield stresses at temperature (340'F) from PG. 9 of REF. 4 for conservatism.
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SECTION 4.3 ANALYSIS
Calculation z cz = s =- f = i Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Pro ect GPSS Mechanical E ui ment QualificationPrepared By: ""1 10 Subject 24" Butterflv Valves Checked B i XJ..~'.~()
2 Date System 82044 'T.01/F Artalvsis No. Rev. No. Sheet No.
361106 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 according to the parametric data given in Summary Table 1 1. ~
Since hydrodynamic loads apply in certain cases, fatigue analyses were provided for components with the highest stress ranges.
The calculated stresses are based on valve and operator G-levels calculated from the piping analysis and re-from Burns 6 Roe. Since theseloads were initial- 'eived ly too high to qualify all EPN's the response G-levels were 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 in the piping system (see Section 5.4). Each computer program (Appendix A) is compiled and hence not subject to subsequent change unless recompiled (and documented).
The method calculates stress from the north, vertical, and east component of operator response g-levels. The SRSS is taken at the stress level and operating loads due to seating torque force and dead weight are later combined by an absolute sum. Valve ear bending stress components due to any one response g-level component are combined by an absolute sum.
1000 00
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII
'CVSS Mechanical Equipment 2k'utterfl Sub e~t Valves Qualification '
Checked By
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Date 1/10/83 System Job No. File No.
CSP & CEP 82044 OT.01 F Rev, No.
361106 - g,g g The computer analysis addresses only the more highly stressed 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 operator mass/stiffness model which was incorporated in the final 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 which are directly output from the piping analysis with the valve/operator model included. This was not finally utilized, however, to qualify the subject equipment.
The equipment locations and elevations were taken from the PAID's in section 6.0. Natural frequency calcu-lations are given for the air operator assemblies in Section 4.3.2.1.
Preliminary analyses were performed which showed that, for operator response g-levels greater than ap-proximately 3 g's, the air cylinder spring preload force would be exceeded and hence some disk flutter would 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 due to upper bound g-levels which occur in the hydro-dynamic frequency range is approximately 6 degrees.
This flutter was evaluated to have no detrimental effect'n system safety function as noted in Reference 5.
Valve operability was addressed in the following manner.
For the valves with Use Code 2, operability after the event can be assured by demonstrating that faulted con-dition stresses remain below elastic limits (see Summary of Results.
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1 10 8 Subject Checked B g r Date
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24" Butterfl F v r, .: -Q,."rg SySterh Job No. File No.
Rev. No. Sheet No.
361106 For valves CSP-V-3 and 4, which must operate from open to fail closed during an event, the following additional evaluations were made:
1) Dynamic flow torques were assessed per Ref. 3 and found to be less than the seating torque which controlled the equipment ~tresses.
Furthermore these flow torques tend to move the valve disk toward the fail-closed position, as noted in the above report.
2) The details of BIF drawing 206 767> parts of which are shown in figures 1.1 and 1.2, allow the following conclusions to be made for valve operability:
A) Figure 1.1 shows that thrust bearings are part of the shaft bearing design. This design prevents lateral movement of the disk in the direction of the shaft to eli-minate interference with the valve body when closing. Further, it is noted on Page 26 of Ref. 3 that frictional torques in the shaft bearing system are negligible.
B) Figures 1.1 and 1.2 show a circular valve cross section having an internal rim within which the valve seats, in the closed posi-tion. The only mechanism remaining to af-fect valve closing which can be postulated is out-of-round distortion of the section due to DBE piping loads and dynamic loads on the valve.
These loads were accounted for in Ref. 4 in the overall valve sizing calculations, where analysis showed that the stress intensity in the 0.5 inch thick valve body remained below 1.2 Sri, or approximately 0.8 of yield.
Stress contribution from dynamic loads on the valve and operator were relatively small. Further, as shown in the figures:
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Rev. No.
An~lys~ N~.
361106 - +, g The valve seat forms a heavily reinforced section made up of the valve body, internal hub and external flanges (including the mating flange of the piping). Hence the stress levels in this section are much lower than in the valve'ody and hence no distortion of the section could occur to affect seating'f the valve. Valve flange dimensions are given below. Note the relatively large internal radial clearance of 1/8 inch.
2 Stress analysis of the valve extended structures are given in this report. Air operator operability is addressed in QID 018001.
The design data used in the analyses are given in Summary Table 1.1 (pipe-orientations and elevations are taken from the appropriate PAID's in Section 6.0).
Other pertinant data is given below.
1) Spring preload per communication report in Section 7.0 of QID 018001 are:
Fail Open Preload =
= 1850ijj 350'inal Fail Closed Preload = 15009 Final = 30008
2) Cylinder C.G.'s shown on the following sketches represent 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, 11/83 communication report - Section 7)/
Flange: width = 3.5", thickness = 1.78" Radial Clearance Disk/Seat 1/8" rccs co
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Grou I - Fail 0 en EPN's CSP-V-5 6> and 9 Case l: Valve Open Case Il: 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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CSP and CEP 82044 OT.01 F Rev. No. Sheet No.
c~ 361106 -A.5 ZZ 4.3.2.3 STRESS ANALYSIS The procedures for the analysis of the subject valves are outlined below:
Recalculate the valve appurtenance stresses addressed in Ref. 4 using response g-levels from the final piping analysis. Incorporate the 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 significantly stressed components. Determine allowable alternating stress ranges from AISC 8th Edition, Appendix B, noting commentary.
The fatigue analysis is to be performed only for those EPN's subject to;hydrodynamic loads. The number of respective .load cycles is given below,
-LOAD COMBINATIONS G,STRESS CYCLES The following table lists the load combinations and the number of expected stress cycles for each com-bination. 'From the design criteria)
Combination ~Ccles
1. SRV Alone 13500-200=13300 cycles
2. OBE+SRV 50
3. SRV+AP+CHUG 140
4. SSE+SRV+AP+CHUG 10 Note: Load combination g4 with 150 cycles can be used to conservatively bound combinations 3 and 4.
10CS CC
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: ~ Date 1 10 83 24'utterfl Sut(ject Valves Checked "" ~(ao/a~
System Job No. File No, CSP and CEP Anatvsis No. Rev. No. Sheet No, 361106 z f;I) ALg)I 5 QF /QLVE AV~ AIR Oi==r~~<~."- C'J')~~ IEtfT Q
))DT COd EkB-9 II) QIO -O(7~(
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I
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= (Lp po Lc.r ) Wpo < 1
= -'1 ",4 lB'1.(l.<c-)
LFoo L zs~~
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Z. I f.qS 4F It Fgyp = (2+1 0> I FoIZ 8 Z 13'8'ft 6= ItSb w&t" f(T(z) = Fo~ (O z~
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Calculation J i fs 3 Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII project WPP M ha preearee atr:
( jj~aate Subject Checked By. Date 24" Butterfl Valves Bd b3 Svstem Job No File No.
CSP and CEP 82044 OT.01 F Analvsis No Rev. No, 361106 341 e4 -4.S-Z4 J-I E to Tnt LOA f: 0< THE.
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rr rih ) /H7 I F i2ret Z.
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rr'i f .-Pgg~ i ayPg )bio@-i1r-r-I q P P )Z 1) < jf'ht'< df' it i=
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TCtt plp3tou 5 fiiVD IhJTL4>piL- gjcprHS fjoLt) TH." VALur Ig %if C- tLO12- i ='~'1mrr>>tl, F'~p,~gP
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Checked 8
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~ Date 10 II Job No, C8P anti CEP 82044 OT.01/F Analysis No Rev. No.
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project ,Prepared By: i Date t
Subject Checked By Date 2 " Butte Valves System CSP and CEP 82044 OT.01/F Analysis No, Rev, No. Sheet No.
361106 361106-E.V M)A'P~ i~ & STPggg - gK Qs,r f R, ~t'. t-I ~
4+ 5 IU- Lg I
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= l2~ 26'7 LG t.HtN 5 ppg = Eflux Z71 351
'k="$ It sHap- E hy z y oF KEY = (.3y I
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII project WPPSS Subject Mechanical E ui ment ualification prepared Checked B By;/
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4 A, Date 1 10 83 II System Job No, CSP and CEP 82044 OT.01/F Analysis No. Rev. No. Sheet No.
361106 ID I. I Zq'Z t.z,s" U =zr= Z.Sty Ig+
h 4.3z II I o,EI j.zS I IP$ o'5 i~ ze~ 7 cI ir~
7l 2< I'7f (, I.~s) 7Z" 7 f'sl:
CG Vt,E Fco ~5. FRom Flt" . c.P PPQI.
I
~, ~> f<>. I A I.I<<+'lr5s i = osage Ls
+advs. = 7m~ - /geo rs-,
~. 't'7 Q~ M = lv+q fa.sz..)(II Is~
l4,"I5 =(4(,)
0- = Pa "I/9 I < (i IZ4E) '7I58 PS l I.rS .l C<< ~~9.0/I 7$ 0E<'( A'"..) jQQ 5I'/ C ~t
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project h Date MPPSS Mechanical E ui~ment ualificationPrepared Byf 1 10 83 Subject Checked B:
24" Butterfl V lv s a 50/es System Job No. File No, Rev, No.
361106 -g +-pg Disc The stresses in the disc were shown on page 51 of Ref. 4 to be due almost entirely', to the pressure load. Since the stress found in Ref. 4 of 3871 PSI will not change significantly for the new ac-celerations, the disc is acceptable.
Ta er Pins The stress in these pins is due only to the seating tor q ue. The stress in Ref. 4 p a g e 53 is 10753 I pst and is therefore acceptable.I For rhe new, lower seating 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 output from the piping analysis (Summary Table 1.1) and the absolute sum of stresses.
The conservatism of SRSS summing of the component stresses cannot be assured because the independence of the six element forces (/moments) cannot be de-termined without. analysis of modal par-ticipation.
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project p Mechanical -Equipment QualificationPrepared By 1/10/83 Subject Checked Qy:
24" Butterfl Valves System Job No, File No.
P dCP 82044 OT.01 F Rev. No, Sheet No'361106 - g Q- gg Method Il: Use the north, east and vertical operator accelerations output .from the piping analysis. Absolute sum for stresses with each component then SRSS over re-sults for N,E and V.
Note t; Analysis of the distribution of stress on 4 valve ears to predict the maximum tensile stress cannot confirm a maximum value lower than the absolute sum of the elemental ten-sil stresses due to the six forces (from one 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 deadweight plus seating torque force after above SRSS combinations are performed. (ABS)
Note 3: 10" A/0 parameters are shown for use in QXD 361104.
Anal sis of Seatin Tor ue Forces
1) Seating Torque loads control the stress in the valve lever arm, keyway, shaft and taper pins. These stresses were less than allowables for the valves of seating 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 during the faulted and upset conditions (CSP-V-5,6).
3) For the Fail-Closed valves, the forces at the trunnion pins are shown below, along the cylinder axis, for +2-axis g-loading:
~2, ~ ~is cn c!evis/valve skid I
I I ~
cn sac.~AalVe CarS
~eisrr ic./i7Mre&ic F~ f'rem oPer~r irr a. - cu'/8 dlrCcdDhf
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Pro"ect GPSS Mechanical Subject E ui ment ualificationPrepared Checked By B:
h 6( '/10/83 Date Oate / /
24" Butterfl Valves B/50 /8Q 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 extent of relief depends on the relative stiffness of the bracket and valve ears relative to the valve seat.
Since the steel backets and ears are very stiff in this direction, little relief can be expected.
Hence seating torque forces will be added as an ABS sum to the valve ears. However, seating torque force will oppose operator weight when the brackets hangs downward from horizontal pipes.
0 erator Drive Rod Drive rod dynamic stress is due only to g because g and g forces are taken out by trunnion pins.
Ald seating torque stresses. 7. IZS F~ = Lcc Wg Lj,o~
T'No F'at~ t .ARE r=EtT<cqL FT 4 A I I
THt: E'iiSNt~tt" /Iyb PV'E RW Tij c
@~>Uc.G~~
"tEEC9 PI+ME.PE,F w
~O MA = r (.Lr.o ~>.s') <<CM Cp)
g. (z5 Fc.
VF~
= t t" t"-r."
2.qI I,tj
. ~
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Calculation I i j Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: .Date M
Subject Checked By: Date 24" Butterfl Valves System Job No. File No.
C c1 Ahalysis No. Rev. No. Sheet No.
36>106 361106 5t WigAt L/:
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Calculation L= = ~ I Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project PrePared By - Date 11083 24 'utterfl Subject Valves Checked B
'ob Date 3 &de System No. Fite No.
CSP and CEP Analysis No. Rev. No. Sheet No.
361106 4 611 cooRDINATE SYsTEM ( LOCAL) 1 t
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Date 8SS Mechanical E ui ment ualification Prepared Byl Subject 24 'utterfl Valves Checked: tI 1
~i c.. vf~rJ/ Date
~ I~&!6"-
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CSP and CEP 82044 OT.01 F Analysis No. Rev. No' Sheet No.
361106 361106-Pop CE g OgE. 7O TOW<t-'lE.
= 4g (to.S')
lb.
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Pro'ect Prepared By: k h A . Date g
MPt'SS Mech n 1 10 83 B;
'utterfl Subject 24 Valves Checked Date System Job No File No.
5'
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82044 v Analysis No. Rev, No. Sheet No.
361106 611 T)) gtr F SqF ES5 CeE t o brtZ -.
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IIIIIIIIIIIIIIIIIIIIIIIIIIIIII project Date WP h Prepared By:
i gp Subject Checked By: A Date 24" Butterfl Valves Add System Job No. File No.
CSP and CEP 82044 Analysis No. Rev. No Sheet No.
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OT. 01 F Analysis No. Rev. N'o. Sheet No.
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A5SPf.LlTQ SQfg (L<<ss <<o'4/o FELS<<ETo~
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Rev. No, Sheet No,
-4 5-s7 PdL. T= W>t t I ~'IS SL'gC'KB7S TO Efl t~S
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24 'utterfl Subject Valves Checked 8 Date san ka System Job No. File No.
CSP and CEP 82044 OT.01 F Analysis No. Rev. No.
361106 Ski I d5 4. 5-Nt ETtlCd 9 g TH G. Pk:SVI dU 5 E<QU 4T(GP r j=) I r tr C-~ z Q J'E -THrs 0 f 5> = Pl'PjtCPl=LE. Ha~RLr&:-",
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ot=
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~np.~i~V VCc~or~~~it> >A t r4 U JH LC(A t-ea orb jH A TK 5> PE.Xa PAt" <.~~
~~ToR bio pC 'tF.':oLrV I o"AL 0 ii5 3 ZNs tnnr. vP+ = Fipt ez + FdR,en + Fnn=<-. +t re-.e, g+ '2 ((htnb e2n vnnae )~~
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared Date WPP By,'hecked 1 10 83 Stjtject 2rt Butterfl Valves B
~~~ ~ / ""afro ss System Job No, File No.~~
~~CSP and CEP Analysis No. Rev. No. Sheet No.~~
361106 3 &lid&-4.3-FORCES 00 L)PPOZT ARS t UE To LOCAL -A<l5 itjcc "LERAT(O p) g a Fc)kc.E 5 I 9 HE MeAL coo c.foiH A r8
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~~~ I 0 ~~~
~~Q FA,~~ e,-.S.~'<= < W~~
~~= -A v(5 CovPovt=p? wgp)~~
~~N FTp ~ I Oc' A~~
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~~~~ tr-'= T IQ B. Tr R = ~ (R )t. j t> z> g >AoZ~~
~~+T rPU H/) to~~~
T
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~ ~ 5 56/3 System Job No File No CSP and CEP 82044 OT.01 F Analysis No. Rev. No. Sheet No.
~~361106 GC ]lbt' FDRCQ O~Ctg.g t/t-Iropg ON L=~ < ". pp-Fg.~~
F
~~>>sr<, Trc I + 6~~~
0
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~~+/pIaI= I 4cec Lca) IMFIel Lace Ic~~
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+o oPEq ao Ão 1'Lrgy I 4o' 7c Z I I L C(i )g or~
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: Date 24'utterfl Subject Valves Checked B(; p Date System Job No File No.
CSP and CEP 82044 OT. 1 Rev. No. Sheet No.
M ilb(o-5~ =
FA Z + I-PPP = iWit~ qN;. JQ
~2. Ftffb = I,rz ~e~oz < "~V=. +
OR OUT Ot- +>%yQ I r=h>>l.~/Q:
F~oz e~ Fr@ eq rg~e~(g. q~" e4
--u tt
(>>>>>o~ >>>sz >gz "+ >>>z~)483 >>>
fair.
4= ToP =.q'5
(~Ace Z, "R ~c><Z )~D ~~>~% ~ TErr<ao<
8gS +
2 N>z =
+4 - 4Fr>>> >'-d < Fz>'-><a -,'>>ocz r>'zs~i i t"
=
j (FT>>; O wd>tp>>>'<g)>>> <z" >>>pq~>)gg 4 "LE I
>z Fez>> t i >'>>>>>>>+~6P~d i' C b~+Pt/
T- =
+g esA~tS
=
(~i>~+'>it>z)<~ Ã>>- 'D
~Z, ~ "~Z g
~> + Cher"L57~
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Proiect WPPSS Mechanical E ui ment uglificationPrepared By:/
1 10 83 Subject II Checked B /
rye,~/ hP <&
Oate System Job No. File No.
0 Analvsis No. Rev. No. Sheet No.
361106 361106- .'5" 2 4~/ U set Condition Stresses Th'e cylinder drive rod and valve ears were separately analyzed for upset condition loads for the EPN's and associated response g-levels noted below. All other component 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 seating torque only. The allowable stress for the bracket bolts also holds for upset conditions per the AISC manual, 8th Edition. Bolt fatigue is considered as presented in Section>.3.5.
Upset g-levels (per revised B&R piping analysis, Sec. 5.5)
EPN N CSP-V-3 1.73 1.60 0.96 CSP-V-4 1.14 1.40 1.50 CSP-V-5 0.97 1.40 1.71 CSP-V-6 1.64 1.44 0 '9 Component stresses are given in Table 1.2.
scca 00
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII project WPPSS Subject System II Analysis No.
Mechani 1 o i Rev. No.
n Prepar.d By:j Checked Job No, Sheet No.
B:g g 82044
~
gP~~
File No.
Date Date 0
/
361106 - 4.3-45 Section4,>.5 Fati ue Anal sis Discussion The operator and bracket assembly are not part of the pressure boundary, therefore, the fatigue analysis will be performed in accordance with Appendix B of the AISC Manual for Steel Con-struction. The following assumptions apply to the. fatigue analysis.
~~1) Faulted stresses (based on piping-analysis accelerations) will be used. This is necessary to insure operability after a design basis event.~~
~~2) The actual stresses used will be the ones calculated in Section g.3.~~
3) If the alternating portion of the stress has been cal-culated separately only this part will be used. If the operating 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 long as no failures occur, the operating stress does not need 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 1.7 of the Commentary'on the AISC Manual).~~
~~6) The actual stress range is taken as 2 times the maxi-mum stress for components subject to alternating tension and compression.~~
Iced Cd
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII project Prepared By:
-(P Date Subject 24" Butterf1 Valves.
System Job No. Fite No.
82044 OT.01 F 5'BbF. Rev, No.
'61106- g,+- Qcf.
~~7) Bracket bolting is assumed to be properly tightened and will not be considered for fatigue per Section B3.1 of the AISC Manual.~~
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 showing the descriptions of the relevent stress categories.
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Pr t Prepared PW Date
$ 8VSS Mechanical E ui ment Qualification, By:I
')
4P( 1/10/83 Subject Checked By Date 24" Butterfly Valves 8 b System Job No. File No.
Rev. No.
z '361106-Q >-g~
Fati ue Anal sis (cont.)
STRESS STRESS STRFSS STRESS 1.5 x ALLOW ITEM TYPE (PSI) RANGE (PST) CATEGORY (FROM AISC)
TRUNNION PIN 4108 21 DRIVE ROD MAX SEE TA LE 1.2 SUPPORT EARS SEE TAB E 1.2
$ 127 19,~M+ 90000 HAIN SHAFT 8064 1 12 NOTES:
(I} Assume shear stress on nominal area of a stud type shear connection.
Note that this comparison includes all of the load combinations in one conservative comparison using the maximum stress and the total number of cycles ([3 x 4478] + 60 = 13494 cycles).
>Ocs.00
Prepared By: Date Calculation Sheet !!/l&F~~
Checked By'. Date
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S ZS 0~1; I Hc ~RIt LF 8 Ei.o~ H+S BEEN ~H DEnac'D FiZnM R PPErvbX'x 9 oF THE HZSc QAHu H v dI'- '4TEEt-COIYS'fRlA.C 7-~Or f. TH c C.RISES uSEb H iZc HRRIr'E21 4J Z' H en lfjRROM.
Stress General Cate-Condi ~ Situation Kind of gory.
tion (See Stress'or Table B3)
Plain Base metal with rolled or cleaned sur- Rev.
material faces.
Built-up Base metal and weld metal in mem- Tor Rev.
members be'rs, without attachments, built-up of plates or shapes connected by contin.
uous full. or partial. penetration groove welds or continuous filletwelds parallel to the direction of applied stress.
Calculated flexural stress, Is, in base T or Rev.
metal at toe of welds on girder webs or flanges adjacent to welded transverse stiffeners.
Base metal at end of partial length Tor Rev.
welded cover plates having square or tapered ends, with or without welds across the ends.
hlechani- Base metal at gross section of high- Tor Rev.
cally strength. bolted friction.type connec.
fastened tions, except connections subject, to connec- stress reversal and axially loaded joints tions which induce out.of-plane bending in connected material.
Base metal at net section of other me- Tor Rev. D chanically fastened joints.
~
Base metal at net section of high. Tor Rev.
strength bolted bearing connections.
httach.
ments Shear stress on nominal area of stud-type shear connectors.
S (i.= )~)
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361106 361106 - k.s.Cs SEcTtoN >.4
~~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 Containment Purge Air Supply CSP-809-1.2 Suppression Pool Vacuum Breaker .
CEP-625-3.4 From Reactor Nozzle X-67 to SGT-Fu-lA, 1B CEP-625-1.2 From Reactor Nozzle X-67 to SGT-Fu-lA, 1B D.220-0310 Support and Erection isometric-TR64 (Johnson Controls)
~~3. BIF Report TR-27234 and TR-27235, "Dynamic Torque Calculation of Butterfly Valve; Sizes 24 and 30 inch", dated November 10, 1982.~~
~~4. Report JTR-74-7 by McPherson Assoc., Tnc., "Design 6 Seismic Analysis 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
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII project Prepared By: Date Washin ton Public Power Su 1 S stem L.C. Fernandez 5/27/83 Subject Checked Date Seismic/Hydrodynamic Requal. By.'quipment
~. ~~a g~,, y/q~/o~g CSP 6 CEP 82044 OT.01.F
~tHy5%'Ne'. Rev. No. Sheet No.
QID 361106 2 4. 3. t'(o r~i L-.,;~ ~j./'Z, SECTION 4.4 /c~~~J r/q/~< y REFERENCES (CONTINUED):
~~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 Walkdown Verification Forms, Revision 1, dated 1/5/83.~~
~~9. WPPSS, WNP-2, Safety Related Mechanical Equipment List Summary Sheets, dated 2/10/83.~~
~~10. "AISC Manual of Steel Construction", American Institute of Steel Construction, 8th Edition, 1980.~~
~~11. Preliminary Transfer of Final Burns & Roe Piping Loads for CSP-V-1,2,3,4,5,6 and CEP-V-3AG4A, received 4/13/83.~~
12. Cygna Energy Services, "Equipment Seismic and Hydrodynamic Requalification of 30" Cylinder Operated Butterfly Valves for 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 Hydrodynamic Requalification for 8", 10" and 12" Bore Air Cylinder Operators," 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 ~
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sbasic csp34 tm
-BASIC Compi 1er Version 5.4b 0001:00 REM~++++ BIF VALVE AND AIR OPERATOR SEISMIC STRESS 0002:00 REM+%%% 4 ++++%+: +++% CSP-Vj'AO-3/4 0003!00 REM++SAME ORIENTATION FOR EPN 3h4, SAME PARAMTERS, VARY G'S 0004:00 REM 0005!00 var i,j,k = integer 0006:00 var lrod,lcg,x,phi,lave,abl t,li,l2,ei,e2,e3,e4,e5 = real 0007'00 var fst2, ca, ia,cb, ib,aa,ab,dl,d2,ci, ii,c2, i2=real 0008:00 var lrodo, ego, dr,d, abush, pbush=real 1 1 0009:00 var fcof, fco, ma,mb, siga, sigb, fcdr, fcdrf,maf, mbf=real 0010:00 var dear, f cear, f r, f 11, f 22, la, c 12, c i 21, st t3, semi=real i
0011:00 var sem2, se t3,sesi, ses2,sr, taui 1, tau22, tauear,aear=real 0012:00 var b'tens, taubl t, se t3f, semi f,.sem2f, f cear f, f r f, f 11 f=! eal 0013:00 var f22f,stt3f,sesif,ses2f,srf,tauif,tau2f,taurf=real 0014:00 var taubf,btf, dsr,dtaur,dtaub,dbten,dsa,dsb,dpb=r eal 0015:00 var sdraf,sdr bf,pbushf, tau11f, tau22f=real 0016:00 var wao,wbr, f tr i,watr 1, si, si f, s2, s2f,mi,mi f,m2=r eal 0017!00 var m2f,t3,t3f,tt3,tt3f,lbr,wtot=real 0018:00 var bs1,bs2,bt3,bmi,bm2,btt3=real ~
0019:00 dim r eal av(3) 0020:00 dim real wa(3) 0021!00 dim r eal wb<3) 0022:00 REM 0023:00 REM +++ BURNS 7 ROE EAR FORCES ARE bsi etc TURN ON WITH K=1+~+
0024:00 REM
.'l25:00 REM 026:00 dim real a(3,3) 0027:00 dim real b<3) 0028:00 dim real glc<3,3>
0029:00 1 data 7;5, 10, .75, 1.$ 5, 1.25, .7 0030:00 2 data 25,14.46,.531,53.,7.125, 31,1.5,2.5~
0031 $ 00 3 data 1150 , 875,.46,.648,.138,2.41,1.4 0032: 00 4 data 399,277,5.25,8.5,28.5,15.,6.875 0033:00 5 data 40.,10.96,26.5,30.5,2.075 0034!00 6 data 90.,90.,180.,0.,90.,90.
0035:00 7 data 90 s180 r90 s1'80 '90 s90
~ ~ ~ ~ ~
0036:00 REM DATA 657 FOR VALVMGLOBAL-G ORIENTATIONS AND WEIGHT VECTOR 0037:00 restore 0038!00 read di,d2,ci,i'i,c2,i2 0039!00 resto! e 2 0040'00 read l rod, cg, x, ph i, ave, 1 1 ab 1't, 11, 2 1
0041!00 restor e 3 0042:00 read fst2,ca,ia,cb,ib,aa,ab ATT~ ~f L~, 0 7 0043:00 restore 4 0044!00 read wao,wbr,el,e2,e3,e4,e5 Bi.o SZb4 0045:00 restore 5 FlLEI;Q. OWbf 0046:00 read lrodo,lcgo,ldr,d,abush 0047:00 restore 6 GHLRT"'0 BJ 0048:00 read a(1,1),a<2,1),a<3,1),a(1,2),a<2,2),a(3,2) 0049:00 r estor e 7 0050!00 read a<1 s3> ra<2,3),a(3s3) sav<1),av(2),av<3>
'51: 00 text 0,8c INPUT GLOBAL ACCELERATIONS 5 v052:00 i npu t b(1), b(2), b(3) 0053:00 pr int 0054:00 text O,h INPUT DATA h 0055:00 pr int 0056.'00 print "GLOBAL G-LEVELS "ib(i ) sb(2) tb(3)
LES = ",;a(1,1),a<2,1),a(3,1)
cs +34 I 'UT GLOBAL ACCELERAT I OhlS
? .66,2.99,3.76 INPUT DATA GLOBAl G-LEVELS " = 2,66 2. 5'5'0 3.76 NORTH UECTOR ANGLES = 5'0 180 VERTICAL VECTOR ANGLES= 0 5'0 90 EAST VECTOR ANGLES = 90 180 90 WEIGHT VECTOR ANGLES = 180 5'0 90 LOCAL G-LEVELS
-'1.01471E-5 '""
2;95' -1.43433E-5
.,1
-.2.66
'1471E;5, -1.14059E-5
-1.14059E-5 3 '6
-1.43433E-5 I
I OPERATING DP IUE 'OD STRESS AT A 5525.52 OPEPATIhlG DP, I VE ROD STRESS AT B 8542.57 OPERATING CYLINDER BRG PRESSURE -98.4646 OPcRATIhlG VALVE EAR TEl lSI LE STR 3795.21 OPERATING VALVE EAR SHEAR STRES 244.5'o2 OPERATING EAR BOLT SHEAR STRESS 25'63.25 OPERATING EAP, BOLT TENSILE STR 2ol5.8o D .,AMI C COMPONEhlTS DRIVE ROD TENSILE STRESS AT A 15094.5 DRIUE ROD TENSILE STRESS AT 8 23086.2 BUSHING PRESSURE 294.409 VALVE EAR TENSILE STRESS 14765.9 VALVE EAR SHEAR STRESS 967.76 EAR BOLT SHEAR STRESS 11706.8 EAR BOLT TENSILE STRESS 14225'.2
, FIXED PLUS DYNAMIC COMPOhlENTS DRIVE ROD TENSILE STRESS AT A 20620.1 DRIUE .ROD TENSILE STRESS AT B 31628.7 PUSHING PRESSURE 35'2.874 VALVE EAR TENSILE STRESS 18561.1 VALUE EAR SHEAP. STRESS 1212.72 EAR BOLT SHEAR STRESS 14670 EAR BOLT TENSILc STRESS 16845.1 CVGW~
A~At-HiHFMT Joe xo. bz'os FLENo.< .dl i=
SHEEV NO.4.e.
O.qI ti'~'JT GLOBAL ACCELERATIONS
? '. ~6)2.99,3.76 INPUT DATA GLOBAL G-LEVELS 2.66 2.99 3 76
~
NORTH VECTOR ANGLES = 90 90 180 VERTICAL VECTOR ANGLES= 0 90 90 EAST VECTOR ANGLES = 90 180 90 WEIGHT VECTOR ANGLES = 180 90 90 LOCAL G-LEVELS
-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, 5525.52 OPERATING DRIVE ROD STRESS AT B 8542.57 OPERATING CYLINDER BRG PRESSURE -98 '646 OPERATING E*R WELD TENSILE STR 4338.59 OPERATING EAR WELD SHEAR STRES 519.72 OPERATING E*R BOLT SHEAR STRESS 2963.24 OPERATING EAR BOLT TENSILE STR 2615.86 Db...+MI C COMPONENTS DRIVE ROD TENSILE STRESS *T A 15094.5 DRIVE ROD TENSILE STRESS AT B 23086.2 BUSHING PRESSURE 294.409 FAR WELD TENSILE STRESS EAR WELD SHEAR STRESS 16435.2 2053.24 CVGMA E*R BOLT SHEAR STRESS 11706.8 EAR BOLT TENSILE STRESS FIXED PLUS DYNAMIC COMPONENTS DRIVE DRIVE ROD ROD 14229 '
TENSILE STRESS AT A 20620.1 TENSILE STRESS AT B 31628.7 JQB NO.~
PILE MQ SHE+i NO ~
PUSHING PRESSURE 392.874 E*R WELD TENSILE STRESS 20773.8 EAR WELD SHEAR STRESS 2572.96 EAR BOLT SHEAR STRESS 14670 EAR BOLT TENSILE STRESS 16845.1
I t<+UT GLOBAL *CCELERATI ONS 56E2.99,3.76 INPUT DATA GLOBAL G-LEVELS 2.66 2. 3 76
~
= 90 95'0 NORTH VECTOR ANGLES 180 VERTICAL VECTOR ANGLES= 0 5'0 90 EAST VECTOP. ANGLES = 5'0 180 5'0 4IEIGHT UECTOR ANGLES = 180 5'0 90 LOCAL G-LEVELS
"-1".01471E-'5 2.5'9 -1.43433E-S
-1,. 0,14?1E-.5,'-1 . 140S9E-5 -3.76
-2. 66 -1 . 14059E-5 W
-1.43433E-5 OPERATING DRIVE ROD STRESS AT A 5525.52 OPERATING DRIVE ROD STRESS AT B 8542.57 OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING VALVE EAR TENSILE STR 375'5.21 OPEPATING VALVE EAR SHEAR STRES 244.962 OPERATING EAR BOLT SHEAR STRESS 25'63.25 OPERATING EAR BOLT TENSILE STR 2615 '6 si -906.782 s2f= 1150 t3f=-2.57873E-3 ml f~-7906. 1 5 m2f=-6234. 1 t t3f=-12328. 8 DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 15094. 5 DRIVE ROD TENSILE STRESS AT B 23086.2
'BUSHING'RESSURE 294 '09 VALVE EAR TENSILE STRESS 14765.9 VALVE EAR SHEAP, STRESS 967.76 EAR BOLT SHEAR STRESS 11706.8 EAR BOLT TENSILE STRESS 14229.2 sld= 2711.27 s2d= 2541.76 t3d= 175'8.16 mid= 59281.6 FE.ENQ.E+~< <
m2d= 22662MISHEAR
' EHEE7 NO. ~~
tt3d= 68555 '
F IZED PLUS DYNAMIC COMPONENTS DPIVE ROD TENSILE STRESS AT A 20620.1 DPIUE ROD TENSIl E STRESS AT B 31628.7 PUSHING PPESSURE 392.874 VALVE EAR TENSILE STRESS 18561.1 VALUE EAR STPESS 1212 '2
EAP, BOLT SHEAR STRESS 14670 16845.1 t
EAP. BOLT TENSILE STRESS s1 t= 3618. 06 s2t= 3691.76 t3t= 1798.16 ml 0= 67187 . 8 m2 28896.7 tt3t= 80884 '
cspSQ I UT GLOBAL ACCELERATIONS
? .96,3.17.4.19 INPUT DATA GLOBAL G-LEVELS 2.96 3.17 4 19
~
NORTH VECTOR ANGLES = 90 90 180 VERTICAL VECTOR ANGLES= 0 90 90 EAST VECTOR ANGLES = 90 180 90 4IEIGHT VECTOR ANGLES = 180 90 90 LOCAL G-LEVELS
-1 . 1291'5E-5
~~,,1 1 291 5E-5;.~~
~
'3. 17 '1.59836E-5
-l.; 20926E-5 -4 19 ~
2 . 96 -1 . 20926E-5 -1 . 59836E-5 OPERATING DRIVE ROD STRESS AT A 5525.52 OPERATING DRIVE POD STRESS AT B 8542.57 OPERATING CYLINDER BRG PRESSURE -98.4646 OPEPATING VALVE EAR TENSILE STR 3795.21 OPERATING VALVE EAR SHEAR STRES 244 '62 OPERATING EAR BOLT SHEAR STRESS 2963.25 OPERATING EAR BOLT TENSILE STR 2615.86 D. AMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 16003. 2 DR I VE ROD TENS I LE STRESS AT B 24476 BUSHING PRESSURE 312 133
~
VALVE EAR TENSILE STRESS 15743 VALVE EAR SHEAR STRESS 1034.29 EAR BOLT SHEAR STRESS
~
12511.6 EAR BOLT TENSILE STRESS 15776.8 FIXED PLUS DYNAMIC COMPONBWS DRIVE ROD TENSILE STRESS AT A 21528 7 ~
DPIVE ROD TENSILE STRESS AT B 33018 6 ~
PUSHING PPESSURE 410. 597 VALVE EAP. TENSI LE STRESS 19538. 2 VALVE EAR SHEAR STRESS 1279.26 EAR BOLT SHEAR STPESS 15474.9 EAP. BOLT TENSILE STRESS 18392.7
p3 3
INPUT GLOBAL *CCELERATI ONS
?; '6,3.17) 4.19 I NP UT DATA GLOBAL G-LEVELS 2.96 ,
3.17 4.19 NORTH VECTOR ANGLES = 90 90 180 VERTICAL VECTOR ANGLES= 0 90 90 EAST VECTOR ANGLES = 90 180 90 WEIGHT VECTOR ANGLES = 180 90 90 LOCAL G-LEVELS l.12915E-5 3.17 -1.59836E-5
-1.12915E-5
-2.9o -
-1.20926E-5
-1.20926E-5
-4 '9
-1.59836E-S OPERATING DRIVE ROD STRESS AT A 5525.52 OPERATING DRIVE ROD STRESS AT B 8542.57 OPERATING CYLINDER BRG'RESSURE -98.464o OPERATING EAR WELD TENSILE STR 4338.59 OPERATING OPERATING EAP. WELD SHEAR STRES EAR BOLT SHEAR STRESS 519 '2 2963.24 OPERATING EAR BOLT TENSILE STR 2615.86 D'. <MIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 16003. 2 DRIVE ROD TENSILE STRESS AT B 24476 BUSHING PRESSURE 312.133 EAR WELD TENSILE STRESS 17548.3 EAR WELD SHEAR STRESS 2194.4 EAR BOLT SHEAR STRESS 12511.6 EAR BOLT TENSILE STRESS 15776.8 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS 'AT A 21 528. 7 DRIVE ROD TENSILE STRESS AT B 33018 6 ~
PUSHING PRESSURE 410.597 EAR WELD TENSILE STRESS 21886.9 EAR WELD'HEAR STRESS 2714.12 EAR BOLT SHEAR STRESS 15474.9 EAR BOLT TENSILE STRESS 18392.7
~pg gp 82cl44 l:ILK MO DP.e(.P sv"-=-i Np.=
A-'7
esp/4 I NPOT GLOBAL ACCELERATI ONS
? 96,3.17,4.19 INPUT DATA GLOBAL G-LEVELS 2.96 3 17
~ 4 19
~
NORTH VECTOR ANGLES = 90 90 180 VERTICAL VECTOR ANGLES= 0 90 90 EAST VECTOR ANGLES = 90 180 90 4IEIGHT VECTOR ANGLES = 180 90 90 LOCAL G-LEVELS
-1 12915E-5
~ 3.17 -1.59836E-5 1, 1291 5E .'5 ~ '1 '2092oc 5 4 19
-2.. 96 ',; .::" -1 . 20926E-5 -1 . 59836E-5 OPERAT I t }G DRIVE ROD STPESS AT A 5525.52 QPERAT I } }G DR I VE 'OD STRESS AT B 8542.57 OPEPATING CYLINDEP. BRG PPESSURE -98.4646 OPERATlt'}G VALVE EAP. TENSILE STP. 3795.21 OPERATING VALVE EAR SHEAR STRES 244 '62 OPERATING EAR BOLT SHEAR" STRESS 2963.25 OPERATING EAR BOLT TENSILE STR 2615 '6 sl -906.782 s2i- 1150 t3$ =-2.57873E-3 ml$ =-7906.15 rn2$ =-6234.1 tt3$ =-12328.8 DYNAMIC COMPONENTS
'PIVE ROD TENSILE STRESS AT A 16003.2
, DRIVE ROD TENSILE STRESS AT B 24476 BUSHING PRESSURE 312.133 VALVE EAR TENSILE STRESS 15743 VALVE EAR SHEAR STRESS 1034.29 EAR BOLT SHEAR STRESS 12511,6 EAR BOLT TENSILE STPESS 15776.8 sid= 2874.49 CVQMA s2d= 2832.44 ATTACHMEN'7 t3d= 2000.96 mid= 65975.4 JOB NO 8ZdM rn2d= 24418.8 Ftt.a No. ~<>~'<
tt3d= 72951.2 SHEET MO.
F .ED PLUS DYt }AMI C COMPONENTS DRIVE POD TENSILE STRESS AT A 21528.7 DRIVE POD TENSILE STRESS AT B 33018. o PUSHING PPESSURc 410.597 VALVE EAR TEt'}SILE STRESS 19538 '
VALVE EAR SHEAR STRESS 1279.2o c*R RAI T RHFAR RTRFRR 1%4r4.o
EAR 80LT TENSILE STRESS 18392 '
s1 t= 3781 . 28 s2t= 3982.44 3t= 2000 '6 1t= 73881.5 m2" - 30652.9 tt .= 85280 CYQMA AYYACHSEM7 sos xo.2~~~
FlLKRg ~~01.F SHEET MQ.
esp GQ4 INc'UT GLOBAL ACCELEPATI QNS QQER GE-PC'/ (c,zg~~~r c lS~- 7-~~
? '. r'0 s 1 . 97, 1 ~ 71 INPUT DATA GLOBAL G-LEVELS NOPTH VECTOP, ANGLES VERTICAL VECTOR ANGLES= 0 cAST VECTOR ANGLES idEIGHT VECTOR ANGLES = 180 2.8
= 90 90 90 1.97 90 90 180
'.71 180 90 90 90 LOCAL G-LEVELS
.-'1 . 0 68 1,E-,5.,"
1, . ~, 1,. 97'" -6.52313E-6
. 0681 ' 1E-5 -7. 51495E-6',1
-1 .71
'-':". 8 -7. 51 495E-6 -6.52313E-6
" 'I 0 ll, OPERATING DRIVE ROD STRESS AT A 5525.52 QPEPATING DRIVE RQD STPESS AT B 8542.57 OPEPATING CYLINDER BRG PRESSURE -98.4646 OPERATING EAR MELD TENSILE STR 4338.59 OPERATING EAR MELD SHEAR STRES 519.72 OPERATING EAR BOLT SHEAR STRESS 2963.24 OPERATING EAR BOLT TENSILE STR 2615.86 D'. iMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 9945.23 DRIVE ROD TENSILE STRESS AT B 15210.7 BUSHING PRESSURE 193.975 EAR MELD TENSILE STRESS 10668.6 EAP. MELD SHEAR STRESS 1296.94 EAR BOLT SHEAR STRESS 7394.64 EAR BOLT TENSILE STRESS 14365 F 1 FIXED PLUS DYNANIC COMPONENTS DRIVE RQD TENSILE STRESS AT A 15470.8 DP. I VE ROD TENS I LE STRESS AT B 23753.2 PUSHING PRESSURE 292.44 R MELD TENSILE STRESS 15007 '
EAR WELD SHEAR STRESS EAR BOLT SHEAR STRESS 1816 '6 10357.9 EAR BOLT TENSILE STRESS 16980.9 s p~1,~ gg Jpa xo A~~
ss.s No.
SHEET <<1 A-Ib
sp Q4 INPUT GLOBAL ACCELERATIONS Q pS'E'7 EQ Jc-'bP~
?"1 l4,1.40,1.5
~ ~
ItlPUT DATA GLOBAL G-LEVELS 1.14 1 ~ 4 1.5 NORTH VECTOR ANGLES = 90 90 180 VERTICAL VECTOR ANGLES= 0 90 90 EAST VECTOR ANGLES = 90 180 90 WEIGHT VECTOR ANGLES = 180 90 90 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 A 5525.52 OPERATING DRIVE ROD STRESS AT B 8542.57 OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING EAR WELD TENSILE STR 4338.59 OPERATING EAR WELD SHEAP, STRES 519.72 OPERATING OPERATING EAR EAR BOLT SHEAR STRESS BOLT TENSILE STR 2963 2615
'4
'6 Y'AMIC COMPONENTS DR I VE ROD TENS I LE STRESS AT A 7067. 68 DRIVE ROD TEtlSILE STRESS AT B 10809.6 BUSHING PRESSURE EAR WELD TENSILE STRESS 137 '5 7558.92 EAR WELD SHEAR STRESS 940. 809 EAR BOLT SHEAR STRESS 5364. 13 EAR 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. 315 EAR WELD TENSILE STRESS 11897.5 EAR WELD SHEAR STRESS 1460.53 EAR BOLT SHEAR STRESS 8327.37 EAR BOLT TENSILE STRESS 8744.9 CV C~ll'fld%
A~ ~ACRE'.".R7
sbasic csp5 tm S-BASI C Comp i l er Ver s i on 5. 4b v001:00 REM+++++ BI F VALVE AND A I R OPERATOR SE I SMI C STRESS 0002:00 REM%%%%+%% i+:w%%w%% CSP-V/AO-5 0003:00 REM 0004:00 var i,J,k = integer 0005:00 var l rod, 1 cg,x,phi, ave,abl t, 1,12,ei,e2,e3,e4,e5 = real 1 1 0006:00 var f st2, ca, i a,cb, ib,aa, ab,di,d2,c 1, i,c2, 2=real i i 0007$ 00 var lrodo, ego, ldr,d, abush, pbush=real 1
0008:00 var fcof, fco, ma,mb, siga, sigb, fcdr, fcdrf,maf, mbf='real 0009:00 var dear, fcear,fr, f1 i,f22, la, ci12,ci 21,stt3,semi=real 0010 00 var sem2, se t3, sesl, ses2, sr, taui 1, tau22, tauear, aear=real 0011:00 var btens, taubl t, set3f,semi f,sem2f,fcear f, frf,filf~real 0012:00 var f22f,stt3f,sesif,ses2f,srf, tauif, tau2f, taurf=r eal
,.; .,0013$ 00. var, taubf-, bt f, dsr, dtaur, dtaub, dbten, dsa, dsb, dpb=real
,00,14: 00 var sdr af, sdrbf, pbushf, taui 1 f, tau22f~r eal 0015 $ 00 var wao,wbr, f trl,watr i,si,s1f,s2,s2f,mi,mi f,m2=real
-0016:00 var m2f,t3,t3f,tt3,tt3f,lbr,wtot=real 0017:00 var bsi,bs2,bt3,bml,bm2,btt3=$ eal 0018: 00 dim real av(3) 0019:00 dim real wa(3) 0020 00 dim real
$ wb(3) 0021: 00 REM 0022: 00 REM +w+ BURNS 7 ROE EAR FORCES ARE bsi etc TUPIK ON WITH K=1+++
0023:00 REM 0024:00 REM n025:00 dim real a(3,3) 326:00 dim r eal b(3>
0027$ 00 dim real glc<3,3>
0028:00 1 data 7.5, 10, .75, 1.95, 1.25, .7 0029$ 00 2 data 25,14.46,.531,53.,7.125,.31,'1.5,2.5 0030:00 3 data 0 i 875s 46s 648s 138~2 '1$ 4
~ ~ ~ ~ 1 ~
0031:00 4 data 399,277,5 '5,8.5,28.5,15.,6.875 0032:00 5 data 40.,10.96,26.5,30.5,2.075 0033:00 6 data 42.5,47.5,90.,90.,90.,0.
0034:00 7 data 47.5,137 ',90.,180.,90.,90.
0035:00 REM DATA 6%7 FOR VALVE/GLOBAL-G ORIENTATIONS AND WEIGHT VECTOR 0036:00 restor e 0037:00 read di,d2, cl, i 1, c2, i 2 0038!00 $ 'estore 2 0039:00 read lrod,lcg,x,phi,lave,ablt,l1,12 0040:00 restore 3 0041$ 00 read fst2,ca,ia,cb,ib,aa,ab 0042:00 r estore 4 0043:00 read wao,wbr,ei,e2,e3,e4,e5 0044:00 restor e 5 0045:00 r ead lrodo, i ego, dr,d,abush ATE " CHMENT 1
0046:00 r estore' 0047:00 read a(1,1), a(2, 1), a(3, 1), a<1,2), a<2,2), a<3,2) ~264~
0048:00 restor e 7 JOB NO 0049".00 read a(1,3),a(2,3),a(3,3),av(1) )av(2),av(3) FILE Np ~QT.O 0050:00 tex t O,h INPUT GLOBAL ACCELERATIONS 5 SHEEi i'JC. A-IZ
~51:00 input b( 1),b(2),b(3)
. a52 00 F
print 0053:00 text 0,8c INPUT DATA h
UT GLOBAL ACCELERATIONS
? .96,3.44)5 '2 INPUT DATA GLOBAL G-LEVELS NORTH VECTOR ANGLES =
2 '6 42.5 3.44 47.5 5.42 90 VERTIC*L VECTOR ANGLES= 90 90 0 EAST VECTOR ANGLES = 47.5 137. 5 90 WEIGHT VECTOR ANGLES = 180 90 90 h
LOCAL G-LEVELS 2.18234 -1.31225E-5 3.66169 1.99974 -1.31225E-S -3,.99606
-1.12915E-5 3.44 -2.06756E-5 OPERATING DP IVE ROD STRESS AT A 5048 35
~
OPERATING DRIVE ROD STRESS AT B 7721.14 OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING VALVE EAR TENSILE STR 4664.25 OPERATING VALVE EAR SHEAR STRES 297.614 OPERATING OPERATING EAR BOLT SHE*R STRESS EAR BOLT TENSILE STR 3600 1340
'7
'9 D..AMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 21519. 6 DRIVE ROD TENSILE STRESS AT B 32912 '
BUSHING PRESSURE 419.724 VALVE EAR TENSIL'E STRESS 20190.5 VALVE E*R SHEAR STRESS 1,312.91 EAR BOLT SHEAR STRESS 15882 EAR BOLT TENSILE STRESS 19507 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 26567.9 DRIVE ROD TENSILE STRESS AT B 40633.9
'USHING PPESSURE 518.189 VALVE E*R TENSILE STRESS 24854.8 VALVE EAR SHEAR STRESS 1610.53 EAR BOLT SHEAR STRESS 19482.2 EAP. BOLT TENSILE STRESS 20847.7 ATTACHMENT aoswo. ~~44 va.exa ~<W F SHEET tlO.
csp5
?
UT Gl OBAL ACCELERATIONS
>6;3.44,5.42 r >Q ~Rb ~ Jqt b; i C -';:
I NPUT DATA GLOBAL G-LEVELS NORTH VECTOR ANGLES 2 '6 42.5 3.44 47.5
5. 42 90 VERTICAL VECTOR ANGLES= 90 90 0 EAST VECTOR ANGLES 47.5 137.5 90 WEIGHT VECTOR ANGLES 180 90 90 LOCAL G-LEVELS
,,2 . 1 8234 ..; -1 . 31 225E-5 3.66169 1 ~ 99974 . -1.31225E-5 -3.99606
'-'1 .12915E-5 3 44' -2.06756E-5
'5 H~ ~
OPERATING DRIVE ROD STRESS AT A 5048 OPERATING DRIVE ROD STRESS AT B 7721.14 OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING EAR MELD TENSILE STR 5107.51 OPERATING EAR MELD SHEAR STRES 631.431 OPERATING EAR BOLT SHEAR STRESS 3600.17 OPERATING EAR BOLT TENSILE STR 1340.69 D, WMI C COMPONENTS DRiVE ROD TENSILE STRESS AT A 21519.6 DRIVE .ROD TENSILE STRESS AT B 32912.8 BUSHING PRESSURE 419.724 EAR MELD TENSILE STRESS 22736.7 EAR MELD SHEAR STRESS 2785.52 EAR BOLT SHEAR STRESS 15882 EAR BOLT TENSILE STRESS I 9507 FIXED PLUS DYNAMIC COMPONENTS PILSNER.
DRIVE POD TENSILE STRESS AT A 26567.9 DRIVE ROD TENSILE STRESS AT B 40633 '
PUSHING PRESSURE 518 '89 EAR WELD TENSILE STRESS 27844'.2 EAR MELD SHEAP. STRESS 3416 '5 boa wo.MC~Od EAR EAR BOLT SHEAP, STRESS BOLT TENSILE STRESS 19482 '
20847.7
~+I <
SHEET Ho.dl <<L.
I } r'UT GLOBAL ACCELERATI ONS
'7 96)3 44s5 42
~ ~
INPUT DATA GLOBAL G-LEVELS NORTH VECTOP. ANGLES 2 '6 42.5 3.44 47.5 5.42 90 VERTICAL VECTOR ANGLES= 90 90 0 EAST VECTOR ANGLES 47.5 137. 5 op WEIGHT VECTOR ANGLES 180 90 90 LOCAL G-LEVELS 2 18234
~ -1 31225E-5
~ 3. 66169 1 . 99974 -1 . 31225E-5 -3. 99606
-1 12915E-5
~ 3. 44 -2.06756E-5 OPERATING DRIVE ROD STRESS AT A 5048 35
~
OPERATING DRIVE ROD STRESS AT B 7721 . 14 OPERATING CYLINDEP. BRG PRESSURE -98.464o OPERATING VALVE EAR TENSILE STR 4664.25 OPERATING VALVE EAR SHEAR STRES 297 '14 OPERATING OPERATING EAR BOLT SHEAR STRESS EAR BOLT TENSILE STR 3600 '7 1340.69 si -906.782 s2$ =-2.57874E-3 t3%=-2.57873E-3 ml f= 9.89667E-2 m2$ =-6234. 1 tt3j=-22103.8 DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 21519.6 DRIVE ROD TENSILE STRESS AT B 32912.8 BUSHING PRESSURE 419.724 VALVE EAR TENSILE STRESS 20190.5 VALVE EAR SHEAR STRESS 1312.91 EAR BOLT SHEAR STPESS 15882 EAR BOLT TENSILE STRESS 19507 sld= 3865.34 s2d= 3020.7 t3d= 2325.44 mid= 76145 8ZOM m2d= 31 3o9. 7 OBHQ tt3d= 84539.5 FILE IIO.
SIIEn'II. A'<<
F ,ED PLUS DYNAMIC COMPQl }ENTS DRIVE ROD TENSILE STRESS AT A 2o567.9 DRIVE ROD TENSILE STPESS AT B 40633 '
PUSHING PRESSURE 518.189 VAI VE EAR TENSILE STPESS 24854 '
VALVE EAP. SHEAR STRESS lol0 53
~
~r I t'lPUT GLOBAL ACCELERAT I Ot'lS j3 PSEUD
'? ~ o7,1 4,1.71
~
I NPUT DATA GLOBAL G-LEVELS .97 io4 1.71
?lORTH VECTOR ANGLES 42.5 47.5 90 VERTICAL VECTOR AtlGLES= 90 90 0 EAST VECTOP, ANGLES 47.5 137.5 90 WEIGHT VECTOR *tlGLES 180 90 90 LOCAL G-LEVELS
-5 '4057E-6
. 655321':
~ 715158
'-5. 34057E-o 1 ~ 15526
-1 . 26075
-, -.3.70025E-, 6 1.4 -6.52313E-6
'OPERATING DRIVE ROD STRESS AT A 5048. 35 OPERATING DRIVE ROD STRESS AT B 7721 . 14 OPERATING CYLINDER BRG PRESSURE -98.4o46 OPERATING EAR WELD TEtlSILE STR 5107.51 OPERATING EAR WELD SHEAR STRES 631.431 OPERATING EAR BOLT SHEAR STRESS 3600.17 OPERATING EAR BOLT TENSILE STR 1340.69'~
'AM I C COMPONENTS DP.IVE ROD TENSILE STRESS AT A 6859.18 DRIVE POD TENSILE STRESS AT B 10490 7 ~
BUSHING PRESSURE 133.784 R WELD TEtlSILE STRESS 7323.31 EAR WELD SHEAR STRESS 892.936 EAR BOLT SHEAR STRESS 5091 . 16 EAR BOLT TENSILE STRESS 7599.75 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 11907.5 DRIVE ROD TENSILE STRESS AT B 18211.9 PUSHING PRESSURE 232.249 EAR WELD TEt'ISILE STRESS 12430.8
=AR WELD SHEAR STRESS 1524.37 R BOLT SHEAR STRESS 8691 . 33 EAR BOLT TENSILE STRESS 8940. 43
sbasi c csp6 tm S-BASIC Compiler Version 5 'b JOI '00 REM+>>s+++ BIF VALVE AND AIR OPERATOR SEISMIC STRESS 0002:00 REM>>s>>s~>>s>>. ~~>>. ~~~>>.>>.s. ~ CSP-VyAO-6>>s~>>s>>s~>> ~>>s~~~>>s~>>s>>'+>> + ss~ss~~~~>>s 0003:00 REM 0004:00 var 1 s J sk = integer 0005:00 var lrod, leg,x,phi, ave,abl t,11,12,el,e2,e3,e4,e5 = real 1
0006200 var fst2, ca, i a,cb, ib,aa,ab,di,d2,cl, i i,c2, i2=r eal 0007200 var rodo, 'i cgo, dr, d, abush, pbush=real 1 1 0008:00 var fcof, fco, ma,mb, si ga, s i gb, fcdr, fcdrf,maf, mbf=r eal 0009:00 var dear, f cear, fr, f 1 1, f22,1 a, c i 12, c i 21, st t3, semi=real 0010:00 var sem2,set3,sesi,ses2,sr, taul 1, tau22, tauear,aear=r eal 0011:00 var b tens, taubl t, se t3f, semi f, sem2f, f cear f, f r f, f 11 4 =real 0012:00 var f22f,stt3f,sesl f,ses2f,srf, taul f, tau2f taurf=real s 0013200 var taubf,btf, dsr, dtaur, dtaub, dbten, dsa, dsb, dpb=real 0014:00 var 'dr af,sdrbf,pbushf, taui 1 f, tau22f~r eal 0015200 var wao,wbr, f tri,watri, sl, sl f, s2, s2f,mi,ml f,m2=r eal 0016:00 var m2f, t3, t3f, t t3, t t3f, br,wtot=r eal 1 0017:00 var bsl, bs2, bt3, bml, bm2, bt t3=real 0018:00 dim real av<3) 0019200 dim real wa(3) 0020200 dim real wb<3) 0021:00 REM 0022:00 REM +>>s>>s BURNS 7. ROE EAR FORCES ARE bsl etc TURN ON WITH K=1>>s+>>s 0023:00 P.EM 0024:00 REM 0025:00 dim r eal a(3,3) 126200 dim real b<3) v 027: 00 dim real glc(3,3) 0028:00 1 data 7.5, 10, .75, 1.95, 1.25, .7 0029:00 2 data 25,14.46,.531,53.,7.125,.31,1.5,2.5 data ' 875s 46>> 648s 138>>2 '1sl 4 0030: 00 3 0031: 00 4 0032: 00 5 0 ~ ~
data 35'5',277>>5 '5>>8 '>>28 '>>15 data 40.,10.96,26.5,30.5,2.075
~ ~
'6 ~
'75 0033 00 6 data 5'O.s90 ~ st >>0 '90 '90 2
0034200 7 0035200 data 5'0 REM DATA 6h7
'0 '5'0 s180 s90 s90
~ ~ ~
~
~
FOR VALVE/'GLOBAL-G ORIENTATIONS AND WEIGHT VECTOR 0036:00 restore 0037200 read dl,d2,cl,i i,c2,i2 0038:00 restore 2 0039200 read 1rod,'icg,x,phi,lave,ablt,11,12 0040:00 restor e 3 0041:00 read fst2,ca, ia,cb, ib,aa,ab 0042200 restore 4 0043200 read wao,wbr,ei,e2,e3,e4,e5 CVGNA 0044:00 res tor e 5 ATTACH1icNT 0045200 read lrodo, ego, dr,d,abush 1 1 JOB NO. 0 0046:00 r es tore 6 0047:00 2 ead a(1 1) sa(2s 1) sa(3>>1) sa(1,2)>>a<2>>2) sa(3>>2)*
s RLENO. ~T Oi 0048:00 restore 7 sHf s No.
0049:00 r ead a< 1, 3), a(2, 3), a(3, 3), av (1), av (2), av (3) 0050:00 text 0>>h INPUT GLOBAL ACCELERATIONS 8c nn51:00 input b<1) sb<2) sb<3) 52200 print 0053:00 text 0,6 INP,UT DATA h 0054200 pr int 0055:00 pr i n t "GLOBAL G-LEUELS ">>b(1)sb(2>sb(3>
0056:00 pr int "NORTH VECTOR ANGLES ";a(1,1),a<2,1),a(3,1)
Pl I II I, 0060: 00 for i=i to 3 0061: 01 for j=l to 3; 0062: 02 a<j,i)=a<j',i)+2.+3.1416/360.
'0063: 02 glc(j,i)=b<i)icos(a(j,i))
0064:02 next 0065:01 next i
)66:00 for j=l to 3 367:Oi av ( j ) =av j
( ) +2. +3. 1416/360 .
0068:01 next J 0065':00 print 0070:00 text 0,& LOCAL G-LEVELS 4 0071: 00 pr int 0072: 00 print gl c(1,1),gl c(1,2),gl c(1,3) 0073:00 print glc(2,1),glc(2,2),glc(2,3) 0074:00 pr in t gl c(3,1), gl c(3,2), gl c(3,3) 0075:00 REM WE I GHT COMPONENTS 0076:00 for j=i to 3 0077:01 wa(j)=wao+cos(av(j))
0078:01 wb(j)~broncos(av(j))
0079:01 next 0080:00 'ph'i=phi+2.+3.1416/360.
0081". 00 0082: 00 la='lave/2'c112=c1/i 2 0083: 00 c i 2l=c2/i 1 0084: 00 aear=l 1 +12 0085:00 REM CALCULATE EAR FORCES USE BhR LOADS AS OPTION LATER 0086:00 REM FIXED COMPONENTS ARE ALWAYS THERE 0087:00 br= r od+1 cg 1 1 0088:00 watr 1=1 br+wa(1)/1 rod 0089".00 slf=wb<1)+watr 1 0090:00 w t o t~wao+wbr 0091:00 s2f=wb(2)+wa(2)+f st2 5'2: 00 t3f=wa(3)+wb<3) v093:00 mi f=-<wa(2)+wb(2)+f st2) +e5-wa(3) +(e3+ cg)-wb(3) +e4 1 0094:00 m2f=(watr 1+wb(1) ) +e5-wa(3) +e2-wb(3> +el 0095:00 t t3f =watr 1+e3+ <wa(2)+ f st2) +e2+wb< 1 > we4+wb(2> we 1 005'6:00 f cdrf~l cg+wa(1)/1 r od 005'7:00 maf~fcdr f+(lrod-13.5) 005'8:00 mbf~fcdr f+7.125 0095':00 sdraf=f st2/aa+abs(maf +ca/1 a) 0100:00 sdrbf=f st2/ab+abs(mbf +cb/lb) 0101:00 fcof=l cgoxwa(1)/1 r odo 0102:00 pbush f=fcof +< dr+d)/(d+abu sh) 1 0103!00 REM STRESSES FROM FIXED COMPONENTS 0104:00 deat =(dl+dl+d2+d2) ++.5 0105:00 se t3f=abs( t3f/(4+aear ) )
0106:00 semi f=abs(ml f/(2+d2+ae ar > )
0107'00 sem2f =abs<m2f/(2wdl +ae ar ) )
0108:00 f cearf=t t3f/(2+dear) 0105'.00 frf=x+fcearf CY 0110:00 f i if=-<fcearf+sin(phi )-frf+cos(phi) ) ATTACHVi=MT 0111:00 f 22f=f cearf icos(phi )+fr f +sin< ph 1 ) sos NO.~MA 0112:00 st t3f=abs< f 11 f+1 a+c i 12)+abs( f22f +1 a+c i 21 crier )
0113:00 se s1 f=abs( sl f +c i 12+1 a/4. ) FiLE NQ.QX 4~i 0114:00 ses2f=abs(s2f+ci 21+la/4 '
0115:00 srf=se t3f+seml f+sem2f+sesl f+ses2f+st t3f SHEETRO. 4 ~
0116:00 REM EAR SHEAR
'7:00 taul f=abs(si f/<4+aear) )+abs< f f/aear )
1 1 1 18:00 tau22f=abs(s2f/(4~aear) )+abs( f 22f/aear) 0115':00 taurf=( tau1 f +taul f+ tau22f +tau22f ) ++ 5 1 1 ~
0120:00 taubf=taur f+aear/abl t 01 21: 00 REM E*RBOLT TENSION 0122: 00 btf=(se t3f+seml f+sem2f ) +aear/abl t 0123:00 print 0124:00 pr int" OPERATING DRIVE ROD STRESS AT A ";sdraf ni oR.nn nr i n & ~~
AocpbTTMf'ptlJc Inn QTpccc 6T R " h4
V 4 V ~ VV P ~ ~ ~ ~ s vo 0 4
~ ~ ~ 4 ~ 1V 8 l4
~ V I ~ 'I'VV V I ~ % ~ VV ~ I ~ %J ~ ht I 01 26: 00 print"OPERATING CYLINDER BRG PRESSURE ";pbushf 0127: 00 print"OPERATING VALVE EAR TENSILE STR "Isrf 0128!00 print"OPERATING VALVE EAR SHEAR STRES "; taurf
'0129!00 print"OPERATING EAR BOLT SHEAR STRESS "; taubf 0130:00 print"OPERATING EAR BOLT TENSILE STR ";btf 0131! 00 pr int "132: 00 REM i33:00 REM CALCULATE VARIABLE COMPONENTS 0134 00 REM 01 35: 00 dsr~O. f 0136! 00 dtaur =0.
01 37: 00 dtaub=0.
0138! 00 dbten=O.
0139! 00 dsa=0.
0140! 00 dsb=0.
0141:00 dpb=O.
0142: 00 for j=i to 3 0143: Oi f c o= c go+wao+g c ( 1, j ) 11 r odo 1 1 0144! 01 pbush=f co+< l dr +d)/(d+abush) 0145: 01 f tr1=1br+waowgl c<1, j)/1 rod 01.46! 01 si=f tr 1+wbr +gl c(1, j) 0147: 01 s2=wtot+glc(2,j) 0148! 0 1 t3=wtot+glc(3,J) 01 49: Oi mi=-wtot+glc(2,j)+e5-wao+glc(3,J>+(e3+ lcg)-wbr+glc(3,J)+e4 0150: 0 1 m2=(f tr.i+wbr+gl c(1, j ) >+e5-(wao+e2+wbr+ ei)+glc(3,j) 0151: 01 tt3=ftriwe3+wbr+glc(i,j)+e4+glc(2,J)+( waowe2+wbr+el) 0152! 0 1 fcdr=lcg+wao+glc( l,j)r'irod 0 1 53: 01 ma= f c dr+( l r od-1 3. 5) 0154! 01 mb=f cdr+7. 125 0155! Oi si ga=ma%cM i a 0156: 01 s i gb=mb+cbl i b 0157!01 REM CALCULATE EAR TENSION 58: 01 se t3=abs( t3r'(4+ac ar > )
!59:Oi semi=abs(mit'(2wd2+aear) )
0160:01 sem2=abs(m2/(2+di +aear > )
0161! 01 f cear =t t3/(2%dear) 0162! 01 5 r=x+fcear 0163: 01 f 1 1=-(fcear+sin(phi )-fr icos(phi ) )
0164! 0 1 f 22~% cear+cos<phi )+fr+sin(phi )
0165:01 st t3=abs( f 11+1 a+c i 12)+abs( f 22+1 a+c i 21) 0166!01 sesi=abs( si +c i 12+1 M4. )
0167!01 ses2=abs(s2+c i 21+1 al4. )
0168!01 sr ~se t3+semi+sem2+sesi+ses2+s t t3 0169:01 REM EAR SHEAR 0170! 01 taui i~abs( si/(4. +aear > >+abs( f 11aear )
0171! 01 tau22=abs< s2/< 4. +aear ) )+abs( f 22/aear )
0172'01 tauear=( tau11+tau11+ tau22+tau22) w+. 5 0173:01 taublt=tauear+aear/'ablt 0174:01 REM EARBOLT TENSION 0175:01 btens=(se t3+semi+sem2) +aear/abl t 0176:01 dsa=dsa+ s i ga+s i ga 0177:Oi dsb=dsb+si gb+s i gb gyGRA 0178:01 dp b=dp b+ p bu sh +p bush ATTACHE!BI".!
0179:Oi dsr=dsr+s! +sr 0180! 01 dtaur=dtaur+ tauear+tauear 0181:01 dtavb=dtaub+ taubl t+ taubl t 0182: 01 dbten=dbten+btens+btens
~'3: 01 next j 84:00 REM CQMBINE STRESSES 01 85: 00 dsa=dsa++.5 0186: 00 dsb=dsb++.5 0187: 00 dpb=dpb++ 5 ~
0188: 00 dsr=dsr++.5 0189! 00 dtaur=dtaur++:.5 0190: 00 dtaub=dtaub++.5
'n! 01 ~ nn rlh 0 on .rib or 4 WS
0192: 00 print 0173!00 text 0,& DYNANIC CONPONENTS &
0194: 00 print
'01 5'5: 00 print "DRIVE ROD TENSILE STRESS AT A";dsa 0196! 00 print "DRIVE ROD TENSILE STRESS AT B";dsb 015'7:00 print "BUSHING PRESSURE acids "VALVE ";dpb 198:00 print EAR TENSILE STRESS 'dsr E 5'5': 00 print "VALVE EAR SHEAR STRESS ";dtaur 0200:00 print "EAR BOLT SHEAR STRESS ";dtaub 0201:00 print "EAR BOLT TENSILE STRESS ";dbten 0202! 00 ds a+ abs ( sdr a f )
0203:00 dsb=dsb+abs(sdt bf )
0204:00 dpb=dpb+abs( pbush f )
0205:00 dsr~dsr+abs(srf )
0206!00 dtaur=dtaur+abs( taur f )
0207:00 dtaub=dtaub+'abs( taubf )
0208!00 dbten=dbten+abs(btf )
0209:00 print 0210:00 text 0,& FIXED PLUS DYNANIC CONP ONENTS &
"' 0211 200 print
'0212!'00 pr i'nt "DRIUE ROD TENSILE STRESS AT A";dsa 0213:00 .pr.int "DRIVE ROD TENSILE STRESS AT B";dsb 0214'00 print
"' 0215!00 "PUSHING PRESSURE "
ldpb pt.i'nt "UALVE EAR TENSILE STRESS "Edsr
-0216:00 pr int "VALUE EAR SHEAR STRESS ";dtaur 0217'00 print "EAR BOLT SHEAR STRESS ";dtaub 0218:00 print "EAR BOLT TENSILE STRESS ";dbten 021 5'! 00 end 0220: 00 0221 $ 00 0222!00 0223:00
'.24! 00 225$ 00 ++ww+w End of program +++++w ATTACHE'ENT gpss No 5'Zbd FllENO. 0 .bl EHEEi NO.~
csp6 INPUT GLOBAL ACCELERATIONS 11.39.3.33,5.85
~ ~ ~
Il~rUT DATA GLOBAL G-LEVELS 3.33 5.85 VECTOR ANGLES = 90 11.39'ORTH 90 0 VERTICAL VECTOR ANGLES= 0 90 90 EAST VECTOR ANGLES = 90 0 90 LOCAL G-LEVELS
-4.34494E-5 3.33 -2.23loE-5
-4.34494E-5 -1.27029E-5 5.85 11.39 -1.27029E-S -2.2316E-5 OPERATING DRIVE ROD STRESS AT A 5048.35 OPERATING DRIVE ROD STRESS AT B 7721.14 OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING VALVE EAR TENSILE STR 4664.25 OPERATIIIG VALVE E*R SHEAR STRES 297.614 OPERATING EAR BOLT SHEAP, STRESS 3600.17 OPERATING E*R BOLT TENSILE STR 1340.69 DYNAMIC COMPONENTS R " ROD E TENSILE STRESS AT A 16811 DRxv'E ROD TENSILE STRESS AT 8 25711.4 BUSHING PRESSURE 327.887 VALVE EAR TENSILE STRESS 17822.1 VALVE EAR SHEAR STRESS EAR BOLT SHEAR STRESS 1154 '2 13963.o EAR BOLT TENSILE STRESS 57543 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT
21859. 4 DRIVE ROD TENSILE STRESS AT B 33432.5 PUSHING PRESSURE 426.352 VALVE EAR TENSILE STRESS 22486.4 VALVE 'EAR SHEAR STRESS 1451.93 EAR BOLT SHEAR STRESS 17563.7 E*R BOLT TENS I LE STRESS 58883.7
~TTACHQgg<y JQBNo. Bzo4cf,
<ALE NO. ~dd~ll SHEET MO. A Z5
csp6 T GLOBAL ACCELERATIONS
,39.3.33,5.85 ~ ~
INPUT DATA GLOBAL G-LEVELS 11.39 3. 33 5.85 NORTH VECTOR ANGLES = 90 90 0 VERTI CAL VECTOR ANGLES= 0 90 90 EAST VECTOR ANGLES = 90 0 90 LOCAL G-LEVELS
-4.34494E-5 3.33 -2.2316E-5
-4 . 34494E-,5,,1 . 27029E-5 5. 85 p
1'1 39
~
~
- ~
~
II
-1 . 27029E-5 -2. 231 6E-5
~
OPERATING DRIVE ROD STPESS AT A
~
5048. 35 OPERATING DRIVE ROD STRESS AT B 7721.14 OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING EAR WELD TENSILE STR 5107.51 OPERATING EAR WELD SHEAR STRES 631.431 OPERATING EAR BOLT SHEAR STRESS 3600.17 OPERATItlG EAR BOLT TEhlSILE STR 1340.69 D><AMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 16811 DRIVE ROD TENSILE STRESS AT B 2571'1 4 ~
BUSHING PRESSURE 327.887 EAR WELD TENSILE STRESS 21586.2 EAR EAR WELD BOLT SHEAR STRESS SHEAR STRESS 2449 '5 13963 '
EAR BOLT TENSILE STRESS 57543 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 21859.4 DRIVE ROD, TENSILE STRESS AT B 33432.5 PUSHING PRESSURE 426.352 EAR WELD TEhlSILE STRESS 26693.7 EAR EAR WELD BOLT SHEAR STRESS SHEAR STRESS 3080 '8 17563.7 EAR BOLT TENSILE STRESS 58883.7 JOB RO.~~4 Fn.e WC.~
SHEETXO.~<- <
spaI t"~UT GLOBAL ACCELERAT I ONS
.35',3.33,5.85 INPUT DATA GLOBAL G-LEVELS NORTH VECTOR ANGLES 11.39
= 90 3
90
'3 0
~~5. 85 VERTICAL VECTOR ANGLES= 0 90 5'0 EAST VECTOR ANGLES = 90 0 5'0 LOCAL G-LEVELS~~
-4.34494E-5 3.33 -2.2316E-5
-4.3445'4E-5 -1.27025'E-5 5.85 11.35'1.27029E-5 -2.2316E-5 OPERATING DRIVE ROD STRESS AT A 5048.35 OPEPATING DRIVE ROD STRESS AT 8 7721 . 14 OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING VALVE EAR TENSILE STR 4664.25 OPERATING OPERATING VALVE EAR SHEAR STRES 25'7 '14 EAR BOLT SHEAR STRESS 3600 . 17 OPERATING EAR BOLT TENS! LE STR 1340. 65' i"'--906. 782
2. -2.57874E-3 t3f=-2. 57873E-3 ml f= 9.89667E-2 m2f =-6234. 1 t t 3f =-221 03. 8 DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 16811 DRIVE ROD TENSILE STRESS AT B 25711.4 BUSHING PRESSURE 327.887 VALVE EAR TENSILE STRESS 17822 VALVE EAR SHEAR STRESS EAR BOLT SHEAP. STRESS 1154 '2 13963.6 F 1 EAR BOLT TENSILE STRESS 57543 sld= 3019.58 a2d= 3954.6 t3d= 7699.63 mid= 2.44083E+5 m2d= 58968.3 tt3d= 78875.3
=D PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 21859.4 DRIUE ROD TEt'lSILE STRESS AT B 33432.5 PUSHING PRESSURE 426.352 VALUE EAR TENSILE STRESS 22486.4 VALVE EAR SHEAR STRESS 1451.93 EAR BOLT SHEAP. STRESS 17563.7
EAR BOLT TENSiLE STRESS 58883.7 sit= 3926
=-Zt= 3954.6
'6 t3t= 7699.64 mlt= 2.44083E+5 m2>= 65202 '
tt = l.00979E+5
II JT GLOBAL ACCELERATIONS EQgQ g f-gQy
? 11.37,3.18,5.83 INPUT DATA GLOBAL G-LEVELS 11.37 3. 18 5.83 NOPTH VECTOP. ANGLES = 90 90 0 VERTICAL VECTOR AIIGLES= 0 90 90 EAST VECTOR ANGLES = 90 0 90 LOCAL G-LEVELS
-4 '3731E-5 3.18 -2.22397E-5
-4 '3731E-5 -1 21307E-5
~ 5.83 11.37 -1 21307E-5
~ -2.22397E-5 OPERATING DRIVE ROD STRESS AT A 5048.35 OPERATING DRIVE ROD STRESS AT B 7721 . 14 D'AMI OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING EAR MELD TENSILE STR 5107.51 OPERATING EAR MELD SHEAR STRES 631 .431 OPERATING EAR BOLT SHEAR STRESS 3600 17
~
OPERATING EAR BOLT TENSILE STR 1340.69 C COMPONEIWS DRIVE ROD TENSILE STRESS *T A 16053.7 DRIVE ROD TENSILE STRESS AT B 24553.2 BUSHING PRESSURE 313. 117 E*R MELD TENSILE STRESS 20967 EAR WELD SHE*R STRESS 2365.96 EAR BOLT SHEAR STRESS 13489.8 EAR BOLT TENSILE STRESS 57426.5 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 21102.1 DRIVE ROD TENSILE STRESS *T B 32274.4 PUSHING PRESSURE 411.582 EAR MELD TENSILE STRESS 26074.5 EAR MELD SHEAR STRESS 2997.39 EAR BOLT SHEAR STRESS 17090 c R BOLT TENSILE STRESS 58767.2
c&p6 I hlPUT GLOBAL ACCELERAT I ONS Q Pg Q
'P 2.69,3.09,1.48 (
Its> JT DATA GLOBAL G-LEVELS 2.69 3 09
~ 1.48 NORTH VECTOR ANGLES = 90 90 0 VERTIC*L VECTOR ANGLES= 0 90 90 EAST VECTOR ANGLES = 90 0 90 LOCAL G-LEVELS
-1.02615E-5 3.09 -5.64575E-6
-1.02615E-5 -1 17874E-5
~ 1.48 2.69, ,. -1 '7874E-5 -5.64575E-6 OPERATING DRIVE'OD" STRESS AT A 5048.35 OPER*TING DRIVE, ROD,;,STRESS AT B 7721.14 OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING EAR WELD TEl'lS I LE STR 5107. 51 ~
OPERATING EAR WELD SHEAR STRES 631 . 431 EAR BOLT SHEAR STRESS 3600 . 1 7 'PERATING OPEPAT ING EAR BOLT TENS I LE STR 1 340 .
69'YNAM I C COMPONENTS DP.;: ROD TENSI LE STRESS AT A 15599 '
DR I VE ROD TENS I LE STRESS AT B 23858.3 BUSHING PRESSURE 304.256 EAR WELD TENSILE STRESS 16110.8 EAR WELD SHE*R STRESS 1976.81 EAR BOLT SHEAR STRESS 11271 EAR BOLT TENSILE STRESS 14173.8 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 20647 '
DRIVE ROD TENSILE STRESS AT B 31579.4 PUSHING PRESSURE 402. 72 EAR WELD TENSILE STRESS 21218.3 EAR WELD SHE*R STRESS 2608.24
=AR BOLT SHEAR STRESS 14871.2 J08 NG.ZtFc4C~
EAR BOLT TENSILE STPESS .15514. 5 FlLE NQ ~~d. t=
SHE TRQ.MWW
Pl I II i Wl 1 VIII V4VI Vli PIIWVI I 4 yOVi I t )4ViC I gOVi4) sba ic cep3a tm S-BASIC Compi er Versi on 5.4b 1
701:00 REM+++++ BIF VALVE AND AIR OPERATOR SEISMIC STRESS v002:00 REM~+~w++w++w+++++ CEp-V/AO-3A +wwww++++++++w+ww+w++++++
0003:00 REM 0004:00 var i, j,k = integer 0005:00 var lrod,lcg,x,phi,lave,abl t,l1,12,el,e2,e3,e4,e5 = real 0006:00 var f s t2, ca, a cb i b, aa, ab, di, d2, c 1, i 1, c2, i 2=real i y >
0007!00 var ir odo, l cgo, l dr,d, abush, pbush=r eal 0008:00 var f cof, f co, ma,mb, si ga, si gb, f cdr, f cdrf,maf, mbf=real 0009:00 var dear, fcear, fr, f11, f22, l a, c i 12,c i 21,st t3,seml=r eal 0010:00 var sem2, se t3, sesi, ses2, sr, taui 1, tau22, tauear, aear=r eal 0011!00 var btens, taub) t, se t3f,semi f,sem2f, f cearf, frf,fl if=real 0012:00 var f 22f, st t3f, sesi f, ses2f, sr f, taui f, tau2f, taur f=real 0013:00 var taubf,btf, dsr,dtaur,dtaub,dbten,dsa,dsb,dpb=t eal 0014!00 var sdraf,sdr bf,pbushf, taui if, tau22f=real 0015!00 var wao,wbr, f tr i,watri,si,sif,s2, s2f,mi,mi f,m2=r eal 0016:00 var m2f t3s t3f tt3s tt3f ib!'swtot=real s s s 0017!00 var bsi,bs2,bt3,bmi,bm2,btt3=real 0018:00 dim real av(3) 0019!00 dim real wa(3) 0020:00 dim real wb(3) 0021:00 REM 0022:00 REM +++ BURNS 7 ROE EAR FORCES ARE bs1 etc TURN ON WITH K=1+++
0023:00 REM 0024:00 REM 0025:00 dim real a(3,3)
"026:00 dim r eal b(3)
J27! 00 dim real glc(3,3>
0028: 00 1 data 7.5s 10s ~ 75s 1 '5< 1 ~ 25< ~ 7 0029:00 2 data 25,14.46,.531,53.,7.125,.31,1.5,2.5 0030:00 3 data 1150.~.875s.46s 648s 138s2 41si 4
~ ~ ~ ~
0031:00 data 399,277,5.25,8.5,28.5,15.,6.875 40.,10.96,26.5,30.5,2.075 0032:00 0033:00 0034:00 5
6 data data data 90 '90 A >0 '90 '0 180.,90.,90.,90.,180.,90.
A >90 '
0035!00 REM DATA 6&7 FOR VALVE/'GLOBAL-G ORIENTATIONS AND WEIGHT VECTOR 0036:00 restore 0037!00 r ead di, d2, c 1, i 1, c2, i 2 0038!00 restore 2 0039:00 read lrod,lcg,x,phi,lave,ablt,l i,l2 0040:00 restor e 3 0041!00 0042:00 read fst2,ca,ia,cb,ib,aa,ab'estore 4
CYGRA 0043:00 read wao,wbr,ei,e2,e3,e4,e5 ATTACHMENT 0044:00 r estore 5 ~os wo.
0045:00 read lrodo, ego, l dr,d,abush 1 FiiE XO. < ~
0046!00 restore 6 0047:00 read a(1,1), a(2, >, a<3,1), a(1, 2), a(2, 2), a< 3, 2) 1 SHEET NO. WM~
0048:00 r estore 7 0049!00 read a(1,3), a<2,3), a<3,3>, av (1 ), av(2), av(3) 0050:00 text 0,& INPUT GLOBAL ACCELERATIONS &
0051!00 i npu t b(1), b< 2), b< 3) i52t00 pr in
..a53!00 t'ext 0,& IliPUT DATA &
0054 00 print 0055:00 print "GLOBAL G-LEVELS "; b< 1), b(2), b(3) 0056:00 print "NORTH VECTOP. AliGLES ia(1)1>,a(2,1),a<3,1) 0057:00 print "VERTICAL VECTOR ANGLES= "la(1 t2) sa(2~2) sa(3<2>
0058!00 print "EAST VECTOR ANGLES ")a(1,3),a<2,3),a(3,3)
Compilation comp) ete ce a
? 4 INPUT BLOB*L *CCELERATIONB
'7,1.2o,.S6 PER-4-B4 ( .
RI ~)
INPUT DATA GLOBAL G-LEVELS 4.57 1 ~ 26 .86 NORTH VECTOR ANGLES 90 90 0 VERTICAL UECTOR ANGLES= 90 0 90 EAST UECTOP. ANGLES 180 90 5'0 WEIGHT VECTOR ANGLES 90 180 90
,, LOCAL., G-,LEVELS,"
-1.74332E-5
., 1;,,1 .
4.57 74332E-,5, OPEPATING 1 .
~
-4.80652E-6 26
~
-4 '0652E-6
'3.~
DRIVE POD STRESS AT A
-.S6 28064E-6
-3.28064E-6 477.15'8 OPEPATING DRIUE ROD STRESS AT B 821.458 OPERATING CYLINDER BRG PRESSURE -3 '5613E-4 OPERATING VALVE EAR TENSILE STR VALVE EAR SHEAR STRES 89.1706 1136.52'PERATING OPERATING EAR BOLT SHEAR STRESS 1078.68 OP~~ATING EAR BOLT TENSILE STR 525.595 sl f=-3. 4591E-3 s2f= 474 t3f=-2.57873E-3 ml f=-3258. 67 m2f=-5.29623E-3 tt3f= 4929.17 DYNAM!C COMPONENTS DRIVE ROD TENSILE STRESS AT A 4341 '7 DRIVE ROD TENSILE STRESS AT B 6640.18 BUSHING PRESSURE 84.6795 JQB No.~~
VALUE EAR TENSILE STRESS 4711.31 FILE NO.~CT'
~
VALVE EAR SHEAR STRESS 285.5'35 SHEET VO.M~~
EAR BOLT SHEAR STRESS 3458.89 EAP. BOLT TENSILE STRESS 22999.3 sl d= 779. 831 s2d= 851 . 76 t3d= 3089.31 mid= 5'7498.o m2d= 22785 tt = 19965.7 FIXED PLUS DYI'iAMIC COMPONENTS DP.IVE ROD TENSILE STRESS AT A 4818.7o DRIVE ROD TENSILE STRESS AT B 74o1.64 PUSHING PRESSURE 84.6799
VALVE EAR TEtISILE STRESS 5847.84 VALUE EAR SHEAR STRESS 375.106 EAR BOLT SHEAR STRESS 4537.57 EAR BOLT TENSILE STRESS 23524.9 1 t= 7?9.835
~ 3 s2t= 1325.76 ~
3089.32 mls= 1.0075?E+5 m2t= 22785 tt3t= 24894 '
JoaMo ~8Z 4 pgpgp STOIC svsevwo.8->~
Ccnpilatian cceplete cep3 SLOBAL ACCELERATICNS
? 4.5711.26)0.86 INPUT DATA GLOBAL G"LEVELS = 4.57 1.26 ,86 NORTH VECTOR ANGLES = 90 90 0 VERTICAL VECTOR ANGLES= 90 0 90 EAST VECTOR NGLES = 180 90 90 MiiGHT ViCTOR ANGLES = 90 180 90 LOCAL G-LEVELS ql I~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 477.198 OPERATING DRIVE ROD STRESS AT 8 821.458 OPERATING CYLINDER BRG PRESSURE
-3,75613'PERATING EAR MELD TENSILE STR 1326.01 OPERATING EAR MELD SHEAR STRES 189.188 OPERATING EAR BOLT SHEAR STRESS 1078.68 OPERATING EAR BOLT TENSILE STR 525.595 DYNANIC CONPNENTS DRIVE ROD TENSILE STRESS AT A 4341.57,'RIVE ROD TENSILE STRESS AT B 6640.18 ',
BUSHING PRESSURE 84.6795 EAR MiLD TENSILE STRESS 6247.02 EAR MELD SHEAR STRESS 606.65 EAR BOLT SHEAR STRESS 3458.89 EAR BOLT TENSILE STRESS 22999.3 FIXED PLUS DYNANIC CNPlNBffS DRIVE ROD TENSILE STRESS AT A 4818.76 DRIVE ROD TENSILE STRESS AT B 7461.64 PUSHING PRESSURE 84.6799 EAR MELD TENSILE STRESS 7573.03 EAR MELD SHEAR STRESS 795.838 EAR BOLT SHEAR STRESS 4537.57 ,
EAR BOLT TENSILE STRESS 23524.9
sbasic cep4a tm
-BASIC Compi 1er Version 5.4b 0001:00 REM++++~ BIF VALVE AND AIR OPERATOR SEISMIC STRESS OOO2:0O REM%%%%%%%%%%%%%%% CEP-V/AO-4A %%%%%%%%%+%%%%%%%%%%+i:%%OF+
0003:00 REM 0004:00 var i,J,k = integer 0005:00 var lrod,lcg,x,phi,lave,abl t,l1,12,ei,e2,e3,e4,e5 = real 0006:00 var fst2, ca, ia,cb, ib,aa,ab,di,d2,ci, i1,c2, i2=real 0007'00 var 1 rodo, ego, l dr, d, abush, pbush=real 1
0008:00 var f cof, f co, ma,mb, si ga, si gb, f cdr, f cdrf,maf, mbf=r eal 0009:00 var dear, fcear, fr, f11, f 22, a, c i 12,c i 21, st t3,semi=real 1
0010:00 var sem2, se t3, ses1, ses2, sr, tau11, tau22, tauear, aear=r eal 0011200 var btens, taubl t, set3f,semlf,sem2f,fcearf, fr f,f11f=real 0012:00 var f22f,stt3f,sesi f,ses2f,srf, tauif, tau2f, taurf=real 0013:00 var taubf, btf,, dsr,dtaur, dtaub, dbten, dsa, dsb, dpb=r eal 0014:00 var sdraf,sdrbf,pbushf, taui f, tau22f=real 1
0015:00 var wao,wbr, f tri,watr1,si,si f,s2,s2f,mi,mlf,m2=real 0016:00 var m2f, t3, t3f, t t3, t t3f, br,wtot=real 1
0017'00 v ar bs 1, bs2, b t 3, bm 1, bm2, b t.t 3=r e a l 0018:00 dim real av(3) 0019:00 dim real wa(3) 0020:00 dim real wb(3) 0021: 00 REM 0022: 00 REM ++< BURNS 7 ROE EAP. FORCES ARE bsi etc TURN ON WITH K=1+++
0023: 00 REM 0024: 00 REM l25'00 dim real a(3,3) u026'00 dim real b(3) 0027:00 dim real glc(3,3) 0028:00 1 data 7.5, 10, .75, 1.95, 1.25, .7 0029:00 2 data 25,14.46,.531,53.,7.125,.31,1.5,2.5 0030:00 3 data 1150.s.875'.46< 648s 138>2 '1si 4
~ ~
0031:00 4 data 399,277,5.25,8.5,28 ',15.,6.875 0032:00 5 data 40.,10.96,26.5,30.5,2.075 0033:00 6 data 90.,-38.,52.,90.,52.,142.
0034:00 7 data 180 ~ s90 ~ s90 s90
~ ~ s 128 ' 38 0035:00 DATA 657 FOR VALVMGLOBAL-G ORIENTATIONS AND WEIGHT VECTOR
'EM 0036:00 restore 0037500 read di,d2,ci,ii,c2,i2 0038:00 restore 2 0039:00 read l rod, leg, x, ph i, ave, ab1 t, 1, l 2 1 1 0040:00 restore 3 0041:00 read fst2,ca,ia,cb,ib,aa,ab 0042:00 restore 4 ATTACHMENT 0043:00 read wao,wbr,ei,e2,e3,e4,e5 0044'00 re tore 5 408 NO.
0045'00 read lrodo,lcgo,ldr,d,abush 0 0046:00 nestor e 6 FILE NO. OT 0047:00 read a< 1, 1), a(2, 1), a(3, 1), a(1,2), a(2,2), a<3,2) SHEET',:.O.~~
0048:00 restore 7 0049:00 read a(1,3),a<2,3),a<3,3),av<1),av(2),av(3) nO5O:OO text o,h INPUT GLOBAL ACCELERATIONS h f51:00 input b,b(2>,b< -)
u052:00 print 0053,:00 text o,h INPUT DATA 6 0054:00 pr int 0055:00 print "GLOBAL G-LEVELS lb< 1 ) )b(2) fb(3) 0056:00 pr int "NORTH VECTOR ANGLES = ";a(1,1>,a(2,1>,a(3,1) 0057:00 pr i nt "VERTICAL VECTOR ANGLES= " la(1 >2) a(2 s2> a(3s2>
0058:00 print "EAST VECTOR ANGLES
~ ~
= ":a(1.3) .a(2.3) .a(3.3)
0059:00 pr int "WEIGHT VECTOR ANGLES = ";av(l),av(2),av(3)
OC'60:00 print 0061'00 for i=i to 3 0062:Oi for j=i to 3 0063:02 0064:02 a< j, i )=a(j,, i >+2.+3.1416/360.
gl c(j, )~b( ) +cos<a(j, i ) )
1 1 0065:02 next J 066:Oi next i U067r00 for j=l to 3 0068:01 j j av ( ) =av ( ) +2. w3. 1416/360 ~
0069:Oi next 0070: 00 pr int 0071: 00 tex t O,h LOCAL G-LEVELS h 0072: 00 print 0073:00 pr int glc(l, l),glc(1,2),glc(1,3>
0074:00 pr int gl c(2,1),gl c(2,2>,gl c(2,3) 0075:00 print gl c(3,1),gl c<3,2),gl c(3,3) 0076:00 REM WE I GHT COMPONENTS 0077'00 for j=i to 3 0078:01 wa(j)=wao+cos(av(j>)
0079:01 j
,wb( ) =wbr +co's< av ( J > )
0080:01 next J 0081:00 phi=phi+2.+3 1416/360. ~
~
0082:00 la=lave/2 0083!00 cii2=ci/i2 0084:00 c i 21=c2/i 1 0085:00 aear=ll+12 0086:00 REM CALCULATE EAR FORCES USE BhR LOADS AS OPTION LATER 0087:00 REM FIXED COMPONENTS ARE ALWAYS THERE 0088:00 1 br =1 rod+ cg 1 0089:00 wa tr 1 = br ~a(1 1 )/1 rod 0090:00 si fm=wb< 1 ) +watr 1 "091:00 wtot=wao+wbr 392r00 s2f=wb(2>+wa(2>+ f st2 0093:00 t3f~a(3)+wb(3) 0094:00 ml f~>><wa<2)+wb<2)+f st2) +e5-wa(3) +< e3+ cg) -wb(3) +e4 1 0095:00 m2f=(watrl+wb(1) ) +e5-wa(3) +e2~b(3) +el 0096:00 t t3f~atr I +e3+(wa(2>+f st2>+e2+wb( 1 ) +e4+wb(2) +el 0097:00 fcdr f=l cg+wa(1)/1 rod 0098:00 maf=fcdrf+(lr od-13.5) 0099:00 mbf=fcdr f+7.125 0100r00 sdr af=f st2/aa+abs<maf ~ca/1 a) 0101!00 sdrbf~f st2/ab+abs(mbf +cb/lb) 0102:00 f cof=l cgo+wa(1)/1 rodo 0103:00 p bush f=f cof +< dr+ d)/( d+abush) 1 0104:00 REM STRESSES FROM FIXED COMPONENTS 0105:00 dear=(dl+dl+d2+d2>++.5 0106:00 se t3f=abs< t3f/(4+aear ) )
0107:00 semi f=abs (ml f/( 2+d2+ae ar ) >
0108:00 sem2f=abs(m2f/(2+di+aear))
0109:00 f cearf=t t3f/(2%dear) A~P{ HiNEMT 0110:00 f rf~x+fcearf 0111:00 f f=-< fcearf +sin(ph i >-frficos(phi ) )
1 1 0112:00 f 22f~f cear f icos(ph )+f r f+s n ph i )
1 1 <
0113:00 st t3f=abs(f f+1 a+c i 12)+abs(f22f+1 a~re i 21) 1 1 0114:00 sesl f=abs< si f +c i 12' a/4. )
0115:00 ses2f =abs( s2f +c i 21 +1 a/4. )
0116:00 sr f=se t3f+semi f+sem2f+sesl f+ses2f+ st t3f 17:00 REM EAR SHEAR vl 18r00 t au f=abs( si f/< 4+ac ar ) ) + abs( f f/ae ar )
1 1 1 1 0119:00 tau22f=abs(s2f/(4+aear) )+abs(f 22f/aear >
0120: 00 taur f=( taul f ~taui if+ tau22f +tau22f ) ++.5 1
0121:00 taubf=taur f +aear/abl t 0122:00 PEM E*PBOLT TENSI Oil 0123:00 btf=(se t3f+seml f+sem2f ) +aear/abl t 01 24:00 pr int
01 25: 00 pr int" OPERATING DRIVE'OD STRESS AT A ";sdraf 0126: 00 pr int" OPERATING DRIVE ROD STRESS AT B ";sdrbf 0127: 00 print" OPERATING CYLINDER BRG PRESSURE "; pbushf 0128:00 print" OPEPATING VALVE EAR TENSILE STR ";srf 0129:00 print" OPERATING VALVE EAR SHEAR STRES "; taurf 0130:00 pr i n t" OPERATING EAR BOLT SHEAR STRESS "; taubf nl31:00 print" OPERATING EAR BOLT TENSILE STR ";btf 132:00 print 0133:00 REM Oi 34: 00 REM CALCULATE VARIABLE COMPONENTS 0135! 00 REM 0136:00 dsr=0.
0137:00 dtaur=0.
0138:00 dtaub=0.
0139:00 dbten=0.
0140:00 dsa=0.
0141:00 dsb=0.
0142:00 dpb=o ~
0143:00 for j=l to 3 0144:Oi fco=lcgoxwao+glc<i,j)/irodo 0145'01 pbush=fco+<ldr+d>/<d+abush)
Oi 46: 01 ftri=lbr+wao+glc(l,j)/lrod 0147:01 s1=f tr 1+wbr +g l c (1, j )
0148:01 s2=wtot+glc(2,j) 0149:01 t3=wtot+glc(3,j>
0150: 01 ml=-wtot+glc(2,J>we5-wao+glc(3,j>+<e3+ cg) -wbr +ql c ( 3, j ) +e4 m2=( f tr 1+wbr+gl c(1, j > ) +e5-<wao+e2+wbr+ e ) +ql c(3, j )
1 0151: 01 1 0152:Oi t t3=f tr +e3+wbrwql c 1, j ) +e4+gl c(2, j >+( wa owe 2+ wbr we )
1 <
0153: 01 fc dr= i cg~ao+gl c (1, J )/l rod 1
0154:01 ma=fcdr+(lrod-13.5) 0155:01 mb=fcdr+7.125 01 56:01 siga=mawca/ia 157:01 sigb=mb+cb/ib
~158: 01 REM CALCULATE EAR TENSIOi'i 0159: 01 set3=abs(t3/(4+aear))
0160:Oi semi~abs(mi/(2+d2+aear))
0161:01 sem2=abs(m2/(2+dl+aear))
0162:Oi fcear=tt3/<2+dear) 0163:01 fr=x+fcear 0164:01 f 11=-< f cear+s in(ph i )-fr+cos(ph i ) >
0165:01 f22=fcear icos(phi )+fr+sin(phi )
0166:01 st t3=abs(f +1 a+c i 12)+abs(f 22+1 a+c i 21) 1 1 0167:01 ses 1 =abs < sl +c i 12+1 a/4. )
0168:01 ses2~abs( s2+c i 21+1 a/4. )
0169:01 sr ~se t3+seml+sem2+sesi+ses2+st t3 0170:01 REM EAR SHEAR 0171:01 tau1 i=abs( si/(4. +aear) )+abs< f 11/aear )
0172:01 tau22=abs(s2/<4. waear) )+abs(f 22/aear )
0173:01 tauear=( taui 1 +taul 1+ tau22+tau22) ++. 5 0174: 01 taubl t=tauear+aear/abl t 0175: 0 1 REM EARBOLT TENSION 0176:01 btens~< se t3+seml+sem2) +aear/abl t 0177'01 dsa=dsa+si ga+si ga 0178:01 dsb=dsb+sigb+sigb ATTACHMENT 0179:Oi dpb=dpb+pbush+pbush 8.
JOB NO.
0180:01 dsr=dsr+srwsr .6 0181: 01 dtaur=dtaur+tauear +tauear FILENO. Q nl 82:01 d t aub=d t aub+ t aub t + t aub t 1 1 EHEET HQ
!83:01 dbten=dbten+btens+btens 01 84:01 next J 0185!00 REM COMBINE STRESSES 0186:00 dsa=dsa++.5 0187:00 dsb=dsb++.5 01 88:00 dpb=dpbw+.5 0189:00 dsr=dsr++.5 0190:00 dtaur=dtaur ++ .5
0191: 00 d t aub=d t aub++. 5 01<2! 00 dbten=dbten~+.5 0193: 00 print 0194 '0 text Q,h DYNAMIC COMPONENTS h 0195:00 pr int 0196:00 print "DRIVE ROD TENSILE STRESS AT A";dsa n197:00 print "DRIVE ROD TENSILE STRESS AT 8";dsb i98!00 print "BUSHING PRESSURE ";dpb 0199:00 print "VALVE EAR TENSILE STRESS dsr print S
0200:00 "VALVE EAR SHEAR STRESS ";dtaur 0201r00 print "EAR BOLT SHEAR STRESS ";dtaub 0202:00 print "EAR BOLT TENSILE STRESS ";dbten 0203:00 dsa=dsa+ abs( sdr af )
0204:00 dsb=dsb+ abs( sdr b f )
0205:00 dpb=dpb+abs(pbushf )
0206:00 dsr=dsr+abs(sr f )
0207:00 dtaur =dtaur+abs( taur f )
0208:00 d t aub=d t aub+ abs ( t aub f )
0209:00 dbten=dbten+abs(btf )
0210:00 pr int
-0211-: 00 tex,t -Q,h'IXED PLUS DYNAMIC COMP ONENTS h 0212: 00 print 0213:00 print "DRIVE ROD TENSILE STRESS AT A";dsa
'214:00 print "DRIVE ROD TENSILE STRESS AT B";dsb 0215: 00 print "PUSHING PRESSURE "; dpb 0216:00 print "VALVE EAR TENSILE STRESS I dsl 0217:00 print "VALVE EAR SHEAR STRESS ";dtaur 0218:00 print "EAR BOLT SHEAR STRESS ";dtaub 0219:00 print "EAR BOLT TENSILE STRESS ";dbten 0220:00 end 0221:00 0222:00 223:00 224:00 0225:00 0226:00 End of progr am w+++++
CYGNA ATTACHMENT JOB NO. ZO 4 RLEXO OT.bl SHaEv No.k
ep4a INPUT GLOBAL ACCELERATIONS
'? '5,1.34,.86
~ ~
INPUT DATA GLOBAL G-LEVELS NORTH VECTOR ANGLES '
3 90
'5 1.34
-38
.86 52 VERTICAL VECTOP ANGt ES= 90 52 14 2 EAST VECTOR ANGLES = 180 90 90 4IEIGHT VECTOR ANGLES ~ 90 -128 -38 LOCAL G-LEVELS
-1.27792E-5 -5.11169E-6 .86 2.63983 .824984 -3.28064E-6 2.06246 -1.05594 -3.28064E-6 OPERATING DRIVE ROD STRESS AT A 477.198 OPERATING DRIVE ROD STRESS AT B 821.458 OPERATING CYLINDER BRG PRESSURE -3.75613E-4 OPERATING VALVE EAR TENSILE STR 1946.57 OPERATING VALVE EAR SHEAR STRES 128.033 OPERATING EAR BOLT SHEAR STRESS EAR BOLT TENSILE STR 4771.17 1548.79'PERATING D.'MIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 4341.57 DRIVE ROD TENSILE STRESS AT B 6640. 18 BUSHING PRESSURE 84.6795 VALVE EAR TENSILE STRESS 5948.81 VALVE EAR SHEAR STRESS 379 '11 EAR BOLT SHEAR STRESS 4587.24 EAR BOLT TENSILE STRESS 13246.5 F IXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 4818.76 DRIVE ROD TENSILE STRESS AT 8 7461.64 PUSHING PRESSURE 84.6799 VALVE EAP. TENSILE STRESS 7895.38 VALVE EAR SHEAR STRESS EAR BOLT SHEAR STRESS 507 '44 6136 03 ~
EAR BOLT TENSILE STRESS 18017. 7 ATTACRh3ENY JpBNp. ~i~+4 FILENP ~dt 0/
SHEET Np F.
~A> ~
B>cep4a INP GLOBAL ACCELERATI ONS 35sl 34s 86
~ ~
INPUT DATA
.GLOBAL G-LEVELS 3 ~5
~ 1 ~ 34 .86 NORTH VECTOR ANGLES 90 -38 52 VERTICAL VECTOR ANGLES= 90 52 142 EAST VECTOR ANGLES 180 90 90 WEIGHT VECTOR ANGLES 90 -128 -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 477.198 OPERATING DRIVE ROD STRESS AT B 821.458 OPERATING CYLINDER BRG PRESSURE -3.75613E-4 OPERATING EAR MELD TENSILE STR 2592.98 OPERATING EAR MELD SHEAR STRES 271.64 OPERATING EAR BOLT SHEAR STRESS EAR BOLT TENSILE STR 4771.17 1548.79'PERATING D~ 'ANI C CONPONENTS DRIVE ROD TENSILE STRESS AT A 4341 . 57 DRIVE ROD TENSILE STRESS AT B 6640. 18 BUSHING PRESSURE 84 . 6795 EAR WELD TENSILE STRESS EAR WELD SHEAR STRESS 7493 804.547
'2 EAR BOLT SHEAR STPESS 4587 '2 EAR BOLT TENSILE STRESS 13246.5 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 4818.76 DRIVE ROD TENSI LE STRESS AT B 7461 PUSHING PRESSURE 84.6799
'4 EAR WELD TENSILE STPESS 10086.1 EAR MELD SHEAR STRESS 1076 '9 BOLT SHEAR STRESS
'AR 6136.01 EAR BOLT TENSILE STRESS 18017.7
EFFT B) cep4a INPUT GLOBAL ACCELEPATIONS
>s 3 '5si ~ 34s 86
~
INPUT DATA GLOBAL G-LEVELS 3.35 1.34 .86 NORTH VECTOR ANGLES = 90 -38 52 VERTICAL VECTOR ANGLES= 90 52 142 EAST VECTOR ANGLES = 180 90 90 MEIGHT VECTOR ANGLES = 90 -128 -38 LOCAL G-LEVELS
-1.27792E-5 -5.11169E-6 .86 2.63983 .824984 -3.28064E-6 2.06246 -1 05594
~ -3 '8064E-6 O PERATING DRIVE ROD STRESS AT A 477.198 OPERATING DRIVE ROD STRESS AT B 821 .458 OPERATING CYLINDER BRG PRESSURE -3 '5613E-4 OPERATING VALVE EAR TENSILE STR 1946.57 OPERATING VALVE EAR SHEAR STRES 128.033 PER*TING EAR BOLT SHEAR STRESS P,'TING EAR BOLT TENSILE STR 1548 '9 4771 .17 slf=-3.4591E-3 s2f = 733. 811 t3f= 532. 695 mi f=-21 826. 4 m2f=-3818.52 t t3f = 6791 . 56 DYNAMI C COMPONENTS DRIVE ROD TENSILE STRESS AT A 4341.57 DRIVE ROD TENSILE STRESS AT B 6640.18 BUSHING PRESSURE 84.6795 VALVE EAR TENSILE STRESS 5948.81 VALVE EAR SHEAR STRESS 379E211 EAR BOLT SHEAR STRESS 4587.24 ATTACHMENT EAR BOLT TENSILE STRESS 13246.5 qOE NO.LZOet J
s 1 d= 779. 831 FE.ENO. STS~ F s2d= 1869.64 SHEET NO.~2 t3d= 1566.33 mid= 59205.9 m2+- 12442.3 23258.6 FIXED PLUS DYNAMIC COMPOIIENTS DPIVE ROD TENSILE STPESS AT A 4818.76 DRIVE ROD TENSILE STRESS AT B 7461.64 Rl IRHT Nfi PRFRRI IRF Ad.4799
~ ~
VALVE EAR TENSI LE STRESS 7895.38 VALVE EAR SHEAR STRESS 507.244 EAR BOLT SHEAR STRESS EAR BOLT TENS I LE STRESS 6136 '3 18017.7 Gi t= 779. 835 s2" 2603.45 t3 2099.02 mit= 81032.3 m2t= 16260.8 tt3t= 30050.1
APPENDIX B VALVE/AIR OPERATOR MODEL FOR FINAL PIPING RESPONSE G-LEVEL CALCULATION.
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Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Protect Prepared By: Date Suotect Checked By, Date System Job No. Frte No.
Analysis No Rev, No. Sheet No.
SECTION 4.2
~~SUMMARY~~
OF RESULTS
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII WPPSS Mechanical Equipment Requalif ication "'.C. Fernandez, 6/13/83 Subject 30" linder ated Butterfl Valves Checked By:
M.A. Scott
~~/Date 6/13/83 System Job No. File No.
CAC 6 CEP 82044 OS.01.F
'tttttat~ Rev. No. Sheet No.
4.1 Conclusions Four 30" BXF butterfly valves with Miller Fluid Power cylinder operators have been analyzed for structural integrity to the seismic and hydrodynamic piping analysis and'perability loads. These Burns and Roe piping analysis loads are in the form 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-2A qualify with the following modifications:
1.. Manufacturer supplied A-307 bolts must be replaced with A-325 bolts.
~~2. Shear plates must be added to reduce the ear weld stress (see sheets..4.3.30 through 4-3.48 ).~~
Valve operability was also demonstrated (see p. 4.3.20) while cylinder operability is addressed in QXD No. 018001.
100e 00
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII WPPSS Mechanical Equipment J.E. Rakowski 3/25/83 Subject Checked By: Date 30" Butterfly Valves ~~Pc-c~ C /~/ ~m File No.
CSP 6 CEP 82044 OS.01.F Analysis No. Rev. No. Sheet No.
361104 4.2.1
~~SUMMARY~~
OF RESULTS Parametric data for the four subject'alves in this report is given in Table 1.1. Results of the regualification analyses, which include a comparison of calculated stresses to the allowables are given in Table 1.2. Allowable stresses for the various material types are given in Table 1.3.
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Calculation i 6= ~ifai Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared WPPSS Mechanical E ui ment Qualification By:
J.E. Rakowski.Date
" "'50" Butterfly Valves Checked By:
t .C'. I-~" ~Wc, Date
~/~ /c"-
System CSP and CEP 82044 OS.01/F AnalYsis No. 36] lp4 Rev. No. Sheet No.
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'e a Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII NPPSS '.E.Rakowski 3/25/83 Subject EQ checked By:
C g F
'ace System 82044 OS. 01/F Analysis No, Rev. No, Sheet No.
36110 4 ~ ~
~~SUMMARY~~
TABLE 1.3 ALLOWABLESTRESSES Since operability is required, the stresses for the faulted condition will be kept below yield+. The table below is based on AESC criteria and the yield stresses at temperature (340'F) from PG. 9 of REF. 4 for conservatism.
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'SECTION '4.3 ANALYSIS,
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII
" L.C. Fernandez NPPSS Mechanical Equipment Requalification 6/13/83 Subject Checked By: Date 301I ated Butter f1 Valves M.A. Scott 6/13/83 System C Sr CEP Job No, 82044 'S.01.F File No.
Rev. No. Sheet'No.
QID 361104 1 4.3.1 EQUIPMENT REQUALIFICATION FOR QID NO. 361104 BIF 30"CYLINDER OPERATED BUTTERFLY VALVES 4.3.1 Introduction The four valves in this file are classified according to the parametric data given in Summary Table 1.1.
Since hydrodynamic loads apply (Ref. 7) fatigue analyses were provided for components with the highest stress range.
The analysis method calculates 'stress from north, vertical and east components of operator response g-levels. These g-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 each value assembly in its specific orientation. The SRSS is taken', at the maximum stress level due to seismic g-loading.
Operating loads due to seating torque force and dead weight are combined with the seismic stress by absolute sum. 'alve ear bending stress components due to any one response g-level component are combined by absolute sum.
100s tO
Calculatlon Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Date
'QNSS Mechanical Equipment QualificationPrepared By.
J.E.Rakowski 1/10/83 Subject 30" Butterfl Valves Checked By t L. ( .
i t ~i~ tie'A.ti'/-7Ir3
~ Date System Job No. File ttro.
CSP & CEP 82044 OS~01 F Rev. No. Sheet No.
"N'VP84 1 4 3 The computer analysis addresses only the more highly stressed 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 operator mass/stiffness model which was incorporated in the final 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 which are directly output from the piping analysis with the valve/operator model included. This was not finally however, to qualify the subject equipment. 'tilized, The equipment locations and elevations were taken from the P&ID's in section 6.0. Natural frequency calcu-lations are given for the air operator assemblies in Section 4.3.2.1.
Preliminary analyses were performed which showed that, for operator response g-levels greater than ap-proximately 3 g's, the air cylinder spring preload force would be exceeded and hence some disk flutter would 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 due to upper bound g-levels which occur in the hydro-dynamic frequency range is approximately 6 degrees.
This flutter was evaluated to have no detrimental effect'n system safety function as noted in Reference 5.
Valve All valves operability was addressed have a Use Code of 1-3. 't in the following manner.
the g-levels pertaining to CSP-V-2 envelope CEP-V-1A and CEP-V-2A.
is noted that
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII O. Prospect Prepared By; Date VPPSS Mechanical E ui ment ualification J.E.Rakowski 1 10 Subject Checked By: Date Butterf L 0a 4 JAl&ILGe ~ l '76 ~
System Job No. Fite Qd.
Sf@4'ev. No Sheet No, 4 3 3 RJ3~'or valves CSP-V-3. and 2, which must operate from open to fail closed during an event, the following additional evaluations were made:
~~1) Dynamic flow torques were assessed per Ref. 3 and found to be less than the seating torque which controlled the equipment ~tresses.~~
~~Furthermore these flow torques tend to move the valve disk toward the fail-closed position, as noted in the above report.~~
~~2) The details of BTF drawing 206 767> parts of which are shown in figures 1.1 and 1.2, allow the following conclusions to be made for valve operability:~~
A) Figure 1.1 shows that thrust bearings are part of the shaft bearing design. This design prevents lateral movement of the disk in the direction of the shaft to eli-minate interference with the valve body when closing. Further, it is noted on Page 26 of Ref. 3 that frictional'torques in the shaft bearing system are negligible.
B) Figures 1.1 and 1.2 show a circul'ar valve
'cross section having an internal rim within which the valve seats in the closed posi-tion. The only mechanism remaining to af-fect valve closing which can be postulated is out-of-round distortion of the section due to DBE piping loads and dynamic loads on the valve.
These loads were accounted for in Ref. 4 in the overall valve sizing calculations, where analysis showed that the stress intensity in the 0.5 inch thick valve body remained below 1.2 Sm, or approximately 0.8 of yield.
Stress contribution from dynamic loads on the valve and operator were relatively small. Further, as shown in the figures:
Calculation j~Jkjs 'tP Sheet Illlllllllllllllllllllllllllll Qualification " '" "'J.E.Rakowski 8'LES Mechanical Equipment Subjec!
30 'utterfly Valves Checked By.'ate l.e. F 1/10/S3 System Job No, File 5o.
CEP and CSP 82044 OS.01.F Analysis No, Rev. No. Sheet No.
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WPPSS S5 Butterfly Valves
@4'hecked J.E.Rakowski By: ~ Date 1/10/83
~/ "/IF~
S stem Job No. File N6.
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~.E.Rakowski 5/25/83 u
System Job No, File No'.
CSP and CEP 82044 OS.01 F Analysis No. Rev. No Sheet No.
361104 4 3 The valve seat forms a heavily reinforced section made up of the valve body, internal hub and external flanges (including the mating flange of the piping) . Hence the stress levels in this section are much lower than in the valve body and hence no distortion of the section could occur to affect seating of the valve. Valve flange dimensions are given below. Note the relatively large internal radial clearance of 1/8 inch.
~~2. Stress analysis of the valve extended structures are given in this report. Air operator operability is addressed in QZD 018001.~~
The design data used in the analyses are given in Summary Table 1.1 (pipe-orientations and elevations are taken from the appropriate P&ZD's in Section 6.0) .
Other pertinant data is given below.
1), Spring preload per communication report in Section 7.0 of QZD 018001 are:
Fail Closed Preload = 2800 Final = 4800
~~2) Cylinder C.G.'s shown on the following sketches represent 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, 11/83 communication report Section 7)~~
Flange: width = 3.88nr thickness - 2.625" Radial Clearance Disk/Seat 1/8" tccs tO
Calculation I Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Pr'oject WPPSS Mechanical E ui ment Prepared Qualification By.'ate J.E. Rakowski 3/25/83 Subject lE Checked By~ Date 30" Butterfl Valves "
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'0n Butterfly Valves Checked By /} 1 / 4, >D.,iQ ESP and CEP '82044 OS.01/P Analysis No. Rev, No. Sheet No.
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P cI P 82044 OS.01 F Analysis No. Rev. No. Sheet No. 4 3, 12 361104 chLC fZI Aatog oF 4PJ I'AtQ~ To Ttt G. PPOIE goP giles RLt VN IO 9 AI P. 6 gRrlCi ET 5'TIFFPESE l5: ( CAPTIIE PER aEAM OF EFF~TTvE 2~)
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: Date WPPSS Mechanical Equi ment Qualification J.E. Rakowski 3/25/83 Checked By Date Subiect 30" Butterfl Valves I- .0. 4~t ~kr "I&tr'rS System Job No, Fite No.
CSP and CEP Analysis No, Rev..No, Sheet No. 4 361104 l 4,'3.z. 2 P koX wAw WZF I= WA Q5 Ig 0, P IWEg~lo Qp Fgo~ FtGULE I.3
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~, Oate System Job No, File No CSP and CEP 82044 O.S.01 F Analysis No Re .No, Sheet No.
36110 4 4 3 14
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C'!3$ /6 3 4.3.2.3 STRESS ANALYSIS The procedures for the analysis of the subject valves are outlined below:
Recalculate the valve appurtenance stresses addressed in Ref. 4 using response g-levels from the Burns a Roe piping analysis. Incorporate the current seating torque given in Ref. 3.
Compare stresses to the lower yield strengths in Summary Table 1.3.
If faulted condition stresses exceed the upset 2.
condition allowable stresses, repeat the analy-sis for the affected components using upset
~ tj accelerations from the piping analysis.
~~3. Perform a fatigue analysis on significantly stressed components. Determine allowable alternating stress ranges from AISC 8th Edition, Appendix B, noting commentary.~~
The fatigue analysis is to be performed only for those EPN's subject to hydrodynamic loads ~ The number of respective 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 lee
~~l. SRV Alone 3 (4500) =13500~~
~~2. OBE+SRV 50~~
~~3. OBE+SRV+Chugging 2000~~
~~4. SSE+SRV+Chugging/~~
SSE+AP 10 Note: Load combination N4 with 15560 cycles can be used to conservatively bound all combinations.
3COS OC
Calculation c rciI t Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII l'repared Project Sublect System WPPSS 30" Butte
-Mechanical Equi ment fl V v
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Date Date 3 25 4I2..
I 83 CSP and CEP 2 Analysis No. Re,No Sheet No.
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Calculation I ~s'i ==, a e a Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Subject WPPSS Mechanical Equi ment Qualification Prepared checked By. By.'ate J.E. Rakowski Date 3/25/83 30" Butterfl Valves t ~ F <</Lr~sS System Job No. File No.u CSP and CEP 82 Analysis No. Rev. No, Sheet No. 4 3 j ioRAt Log r; OiJ ~F Ct Evig Ig 7VE VEt~og 5U~ CF Fcm AN C F~Q . 1 l2oi /f47
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s='z) r z F f S z Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: Date WPPSS Mechanical Equipment Qualification J.E. Rakowski 3/25/33 Subject 30" Butterfly Valves c. .i~w~lwc( r/2rir5 System Job No. File No.
CSP and CEP 82044 St)ee(No. Analysis No. 361104 Re . No. 4 3 ]9 IO I. jz,g'(j l.z 5" G -zI- c.,S(q I(j'( Z.Vp >u4 Qg L.eaS ('..3z 4 Qg Io,bl II. ($ Z 't.zs "I l 9((
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=
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Prorect WPPSS Mechanical Eoui~ment ualificationPrepared By.'ate J.E. Rakowski Date 1 10 83 Suhiect Checked By: 30." Butt rf1 Valves j .( . I'~neer g(rr l//2q/ca System Jot'o. File Nor. Rev. No. Sheet No.
~
4 3 20 Disc The stresses in the disc were shown on page 51 of Ref. 4 to be due almost entirely to the pressure load. Since the stress 'found in Ref. 4 of 4540 PSI will not change significantly for the new ac-celerations, the disc is acceptable. The stress in these pins is due only to the seating torque. The stress in Ref. 4, page 53, is 11265 PSI and is therefore acceptable. For the new, lower seating torque, the stress becomes 8985 PSI. Analysis for:'rive Rod, valve ears cylinder bushing pressure, and valve ear bolts. Method It Use element forces and moments output from the piping analysis (Summary Table 1.1) and the absolute sum of stresses. The conservatism of SRSS summing of the component stresses cannot be assured because the independence of the six element forces (/moments) cannot be de-termined without analysis of modal par-ticipation. rccs cc
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project 'repared Mechanical .Equipment Qualification
~~~ By:~~
J.E. Rakowskz Qate 1/10/83 Subject 30'utterfl Valves L.C. F~~~ q/tqj+ System Job No. File No) d P 82044 OS.01 F Rev, No Sheet No. Method IIt Use the north, east and vertical operator accelerations output from the piping analysis. Absolute sum for stresses with each component then SRSS over re-sults for N,E and V. Note!: Analysis of the distribution of stress on 4 valve ears to predict the maximum tensile stress cannot confirm a maximum value lower than the absolute. sum of the elemental ten-sil stresses due to the six forces (from one 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 deadweight plus seating torque force after above SRSS combinations are perfoimed. (ABS) Note 3: 10" A/0 parameters are shown for use in QID 361104. Anal sis of Seatin Tor ue Forces
1) Seating Torque loads control the stress in the valve lever arm, keyway, shaft and taper pins. These stresses were less than allowables for the valves of seating 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 during the faulted and upset conditions (CSP-V-5,6).

3) For the Fail-Closed valves, the forces at the trunnion pins are shown below, along the cylinder axis, for +2-axis g-loading:
~~t2 LaQld Mta an clevis/va.lvc s4& I aaC~kolve~~
~~~ets~tc.lgllnprnlc. ~F~ <ram oper~r Ih a. - CLk'/2 dlfCLODh/~~
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Calculation c sa Sheet llllllllllllllllllllllllllllll Proiect By. WPPSS Hechanical E ui ment ualificationPreparea J.E. Rakowski Dare
~~] /10/83 Subject " Bu terf v Valve l . C. F~)t,ut 'I jrz+j/~>~~
System Job No. File No. Rev. No, Sheet No. 4 3 OS'NY78'4 As the bracket deflects in +2, under dynamic loads, the seating torque force is releived. The extent of relief depends on the relative stiffness of the bracket and valve ears relative to the valve seat. Since the -steel backets'and ears are very stiff in this'direction, little relief can be expected. Hence seating torque forces will be added as an ABS sum to the valve ears. However, seating torque force will oppose operator weight when the brackets hangs downward from horizontal pipes. 0 erator Drive Rod Drive rod dyanmic stress is due only to g because g and g forces are taken out by trunnion pins. A3d seating torque stresses. 7.I25 F~ - Lc.c L~ ~ T~o FD<<75 HE g~
+A = Fc. (.Lt,p 6.K QA C'A .W2s (4 "l. (ZS Fc. l3$ 3tH I Hp, Cg f.cIObid 2.QI IH 2.'H IH
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Protect Subject System WPPSS 30" Mechanical Butterfl Valves E ui m Prepared By; tion Checked Job No, By;, J.E. Rakowski Date Date 3/25/d3 v '~ Il'6 File No. CSP Analysis No Rev. No. Shee!No. 361104 ) 4 3 23 ftuAt LV: tm Z. g')ggytgr Ap, 1A p4
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Calculation Sheet llllllllllllllllllllllllljllll Project Sublect WPPSS Prepared Mechanical Equi ment Qualification Checked By'ate By: J.E. Rakowski
' Da'e 3/25/83 30" Butterfly Valves / ~ F g/~ltd< g System Job No File N CSP and CEP 82044 Analysis No. Rev. No. sheet No, 361104 ~
4 3 24 cooRDINATE SYSTEM ( LOCAL) li !3 r l~ (1 100S 00
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: Date WPPSS Mechanical E ui ment J.E. Rakowski 3/25/83 Svtstect checzed By: - Daie 30" Butterfl Valves ~ System Job No, File No. CPad F Analysis No, Rev. No, Sheet No. 361104 4 3 25 l
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Subject System WPPSS 30" Mechanical Butterfl Valves E ui ment uglification Prepared Checked Job No. By'ate By." J.E. Rakowski
~~'.c. F File No.~~
Date 3/25/83 CSP and CEP OS.01 Analysis No. Rev, No. Sheet No 361104 I
~~~ ~~~
p QTHO p + TH c PRBV(dU 0 E@U ATroI" 5 Fo I 9 pM~S I3g ME 'THo c 3. AR & ~t.tcAgLE. Homt uE.R, i') $ ,')C'PRES> jOAt S Fo TZ W9E. GtM FoF~ qR'S P&iINRP BSLow i4 ~ZEUS . OF j +a&auTS Co M pci>t- P T9 IN tH 6 Lc C 41 AWI 5 '5p> >E M ( 565SE RUE~'T L. Y Qt'EC~RC hl C'O Sl ASE5, Wt~ t36. tJ oE -Tct Erlb 7IoV 'IIEET'ok& coMlJFQ-'T N
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Calculation e &K t Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Ptepared By: Date WPPSS Mechanical Equipment, Qualification J.E. Rakowski 3/25/83
~~'J,~~
~~Subject, 30" Butterfl Valves L. t.'=e.~<<~~
System Job No. File No. d CSP and CEP 2 Analysis No. Re.No. Sheet No, 4 3 27 361104 ~ FOI'<CES Od uFPOVT ARS DUE To LOCAL -AA> Act'LEBATtOP5 R'& 5 6 LocAL coo IAI A tt= F25'tI.S'z IN H I-t = QE/Q( Fcskt- E5 AC T le TH.E e LOCA t- I>2> 5 A/0 A'XIS S vS~ 0 i8 y FAo>iz - ~. gal~ 8~=28',S IS=eg W FTp g
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII project Prepared By'. Date WPPSS Mechanical E ui ment Qualification J.E. Rakowski 3/25/83 Subject 30" Butterfl Valves Checked By:,(.,
~~~ r.i '~~
I . - ~ rt x t (( r l ~ Date 6ISeZ System Job No, File No, CSP and CEP Analysis'o Rev. No. Sheet No, 4 3 28 3 11 FDLCQ OE".IEQ T/t t tages QiiJ f.+k9 IP + TP F
~~>et SI= Frirr i. Fsr<,~~
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Calculation t j Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By-WPPSS Mechanical E ui ment Qualification J.E 3/25/83 Subject 30" Butterfl Valves Checked By: L ~ F
~~'a<<@~I ~t~~~
System Job No. File No. CSP and CEP 82044 Analysis No. Rev. No. StteetNo. 4 3 29 361104 I 5z -- Fg~z + F pzz = L. wpa + rUgrz J) z.
~~+SrZ ~+~csX t ~SV'Z OllT Ot= PL/) yE ~h >~I =~~
~~8 = F~o-z <s Frizz es- (x. Fary-'<4 Fws~eq tl I v, =-(w..w)gz e~-m),ge's-. w q),e~ 4= ToP ~by~~
~~=(<Aoz t wszg+ Fgyz)e~ -Wpszk~z gps~+ IW YEAIQO<~~
Mz ress cc
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII WPPSS ~hanical Ecpxiprent ~lification ~ M.A. Scott By.'~gW
~ 6/15/83 Butter fl Valves Subject Checked Oate 30" linder rated 6 .d. Fernandez 6/15/83 System Job No. File No.
P d 82044 OS.Ol.F gagl-'ysii eat Rev. No. Sheet No. QID 361104 4.3.30 Section 4.3.4 Ear Support Weld Stress Comparison of a similar file (QZD No. 361106) to this file noted the unconservative assumption of considering the bracket support ears to be a guided cantilever (fixed-fixed) . The resulting ear weld stresses exceeded the allowable stresses. The ear weld stresses can be lowered by the addition of- shear plates to stiffen the whole assembly. The resulting weld stresses (both existing and modified) are to be kept within the fatigue allowable stress, i.e., Q stress range. The allowable fatigue stress range from AISC for fillet welds in shear with less than 20000 cycles of loading is: SR = (1.5)(15000)=22500 PSI This includes the 50% increase due to fewer than 20000 cycles. The weld stresses are calculated using faulted loads. These loads produce less than one percent of the total 15560 cycles of faulted/hydrodynami~ loading. Since the upset and emergency conditions are considerably lower in magnitude, small margins of overstress in fatigue will be tolerated for faulted stress levels. The following allowables will be 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. This is 4 the allowable stress range of AISC Appendix B:
~~=1. 25 (1. 5) (15) = 14 KSI fat 2 1.25 = 25% increase due to previous comments 1.5 = 50% increase due to AXSC commentary~~
'lees.00
Calculation r s t Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII
~~~Ac Project NPPSS Mechanical ification Prepared By:~~
M.A. Scott Date 6/15/83 Subject Checked By: Q(p Date 30" linder ated Butter f1 Valves L.C. Fernandez 6 15 83 System Job No. File No CSP. and CEP 82044 OS.01.F Rev. No. Sheet No. QID 361104 4;3.31 W/~x4 x I o/p
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~~Calculation Sheet . IIIIIIIIIIIIIIIIIIIIIIIIIIIIII~~
~~~~+6ate NPPSS jvjechanical t Reaualification Prepared By:~~
M.A. Scott . 6 15 83 Subject 30" Butterfl Val Checked By: /P Oate es System Job No. File No. Rev. No. Sheet No. 361104 4.3.32 C~ V'-1 T, iS Mt Ps
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Calculation f Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project ' Prepared By: ~a+~r bate WPPSS Mechanical ' lification M.A. Scott 6 15 83 Subject Checked By: Date 30" linder rated tte f V System Job No. File No. CSP and CEP 82044 OS. 01.F Rev. No. Sheet No. 2
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project WPPSS Mechanical Equi@rent Bequalification Prepared By.'GVOate M.A. Scott '/15/83 Subject 30" linder ated Butter fl Valves Checked By: L.C. Fernandez prQ Date System Job No. File No. CSP and CEP Rev, No. Sheet No. QID 361104 ~ ~ 3 7& ~c3t rldc SacW o4 ><orat-d5 I///. FM M rg+4yQ~ e:zS~/ S).
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII NPPSS Mechanical Bpiipnent Requalification M.A. Scott ~ 6/15/83 Subject 30" Cylinder Operated Butterfly Valves Checked By: ~ate L.C. Fernandez 6 15 83 System Job No. File No. CSP and CEP 82044 Acne~~. Rev. No. Sheet No. 4 3 35 QID 361104 HO &~7 Q ccJ~~M~7
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project WPPSS Mechanical t alification Prepared By. M.A. Scott
~t~w+~'tDate 15 83 Subject '0" linder rated Butt f V v Checked By: ~~. Date System Job No. File No.
CSP and CEP 82044, GS.01.F Rev. No. Sheet No. QQD 361104 ~ ~
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII
'" "'.A. Scott ~'/15/83 Subject NPPSS Mechanical Equignent Requa1ification 30" Cylinder Operated Butterfly Valves Checked By.'ate . L.C. Fernandez 6/15/83 System Job No. Fite No.
CSP and CEP 82044 OS. 01.F AR~CP, Rev, No. S eetNo. ID 361104 4 3 37 4 I%8 C l38(K) C +g/
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII WPPSS Mechanical Bpipnent Requalification "'.A. Scott+~+ 6/15/83 Subject 30"e Cylinder Operated Butterfly Valves Checked By: ~~ L.C. Fernandei Oate 6/15/83 System Job No. File No. CSP and CEP 82044 OS.01.F Rev. No. Sheet No.
~~~ ~~~
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII WPPSS Mechanical Equipment ~lif ication '.A. Scott '/15/83 D Subject 30" Cylinder Operated Butter fl Valves Checked By'. L.C. Fernan8ez Oate 6/15/83 System Job No. File No. CSP and CEP 82044 OS.01.F Rev. No. Sheet No. ID 361104 4 3 40
~~~o~r Co mm.i tJ no ( o~m ~%5> cs/i J~~
~~Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII~~
'"'PPSS Mechanical Fquipnent Reqmli.fication "'.A. Scott '~ 6/15/83 Subject Checked By: Date 30" Cylinder Operated Butterfly Valves L.C. Fernandez 6/15/83 System Job No. File No.
CSP and CEP 82044 OS. 01.F Rev. No. Sheet No. QID 361104 1 4 ~ 3.41 I ~ ~~acled-~~~~ ~~ P6v t ~+a
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII WPPSS Mechanical Equiprent Requalification '.A. Scott"" '~, 6/15/83 Subject System 30" linder ated Butterf1 Valves, Checked By: Job No.
~~+C~Date L.C. Fernandez File No, 6 15 83 CSP and CEP 82044 Rev. No. Sheet o.~~
~~QID 361104 1 4 3 42 HS 4 ~IAt>> L GA=Co corJ ~M ~t "~ IS~~
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2" ri\ IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Sheet Project Prepared By: ~'i,Date WPPSS Mechanical Equipnent Hequalification M.A. Scott ""4 6/15/83 Subject Checked By; Date 30 II linder ated Butterfl Valves L.C. Fernanddz 6 15 8 System Job No. File No. CSP and CEP ~n5~M%H Rev. No. Sheet No. QID 361104 ~ ~ Tdr o)s'L2O WWS rf c 4 WD o ( PR ~/4C QP Q- 10. + -Dl Pc~77Cr J /~ C~dcA-755. A-S Mat om. MSm~~~i tA~-r COW.~l r-io CMa ~~~ I LE M Zo
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~~Calculation Jar=i Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII project Mechanical Equi t lification Prepared By; .. M.A. Scott "'tt,~~
~ Date WPPSS 6/15/83 Subject Checked By: ~Date 30" linder rated Butter f1 Valves L.C. Fernandez System Job No. File No.
~~CSP and CEP Rev. No. Sheet No. QID 361104 4.3.44~~
~~~H~, M~z~&~oM ~cd~ ~Zo e~ u~r~~~
~~Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII~~
'" WPPSS Mechanical Byu.pnent Requalification ' M.A. Scott~~4'/15/83 Subject 30" Cylinder Operated Butterfly Valves Checked By: ~ate L.C. Fernandez 6/15/83 System Job No. File No.
~~CSP and CEP 82044 OS.01.F hasted~ Rev. No. Sheet No. 4 3 45 QID 361104~~
/ Ra ~s/~w Lc>w7o ~~ ~nJw ~ rs , BP I ~/iw 4-D~ ~Zo bee"-M oQ h
~~Calculation~~
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Jkist Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII NPPSS Mechanical i t ification Prepared'y: ~ /,Qate M.A. Scott i~6>> 6/15/83 Subject Sy'tem 30u linder ated Butter fl Valves Checked By: Job No. L..Fdz File No. Oate OS.01.F Rev. No. Sheet No.
~~55) 361104 ~ ~~~
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~~Calculation~~
~
~~Sheet Illllllllllllllllllljlllllllll~~
~~'" WPPSS Mechanical Ecpiipttent Requalification " " "'.A. Scott ~5 6/15/83 Subject 30" Cylinder Operated Butterfly Valves Checked By:~~
~~L.C. Fernandez~~
~ Date 6/15/83 System Job No. Fiie No, CSP and CEP 82044 OS.01.F Rev. No. Sheet No QID 361104 4.3.47 ~V"roc) Pr- P a+oat. ps77 4/g z.( 7 CM/ /dr@
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Calculation i~ f J Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII NPPSS Mechanical t, lification Prepared By: M.A. Scott ~WtItOate 6 15 83 Subject Checked By: linder Operated Butter fl Valves ate 30" L. System Job No. Fite No. P %6iaijsm+a=. Rev. No. Sheet No/ ID 361104 4 3 48
~~.@ps i (s. sent+( l.s</~J) =Q+UgcA $ f =z /os (o)~~
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~~++ 4 /6 = /~C g ~0~ MW ~~ uJ ~ /z5'57 w~
~~no7(W~S)~~
+ ~if(s ~A~ Is <~~w~c'.~ 4(h,.' ~M ~PS ~kc- C) ~A=rp&( ~i+77C~ UF '/rZF jNi)cr ( ~
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Calculation i xit Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Date Pro'tect WPPSS Subject Mechanica c i Prepared By. Z.E. Rakowski rr Z]'-le" System Job No: File No 82044 0 Analysis No Rev, No. Sheet No 361104 1
~~~ ~~~
Section 4.3.5 Fati ue Anal sis Discussion The operator and bracket assembly are not part of the pressure boundary, therefore, the fatigue analysis will be performed in accordance with Appendix B of the AISC Manual for Steel Con-struction. The following assumptions apply to the fatigue analysis.
1) Faulted stresses (based on piping-analysis accelerations) will be used. This is necessary to insure operability after a design basis event.

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

3) If the alternating portion of the stress has been cal-culated separately only this part will be used. If the operating 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 long as no failures occur, the operating stress does not need 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 1.7 of the Commentary on the AISC Manual).

6) The actual stress range is taken as 2 times the maxi-mum stress for components subject to alternating tension and-compression.
icos 00
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Protect Prepared By.'ate J.E.Rakowski Subtect Butterfl Valves g. c ~ F~~~ ~ j~Q jg~Q System Job f4o. File No. 82044 0 .01 F Rev. No Sheet No. SBb 4 3 50
~~7) Bracket bolting is assumed to be properly tightened and will not be considered for fatigue per Section B3.1 of the AISC Manual.~~
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 showing the descriptions of the relevent stress 'categories.
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII WPPSS Mechanical E ui ment ualificationPrepar'ed By: J.E. Rakowski Oate 1/10/83 Sobject 3'0" Butterflv Valves L., C. F~m~i~', p jL~ (E3 System Job No. File No. Rev, No. Sheet No
~~'5L'l'Mp4 4 3 51 Fati ue Anal sis (cont.)~~
STRESS STRESS STRESS STRESS 1.5 x.ALLOW ITEM TYPE (PSI) RANGE (PSI) CATEGORY (FROM AISt") TRUNNION PIN 410 DRIVE ROD MAX SEE TA LE 1.2 SUPPORT FARS SEE TAB E 1.2 9127 18254 90000 MAIN SHAFT 7158 14316 NOTES: (/) Assume shear stress on nominal area of a stud type shear connection.
/
Note that this comparison includes all of the load combinations in one conservative comparison using the maximum stress and the total number of cycles ( 3. x 4500 + 2000 + 60 = 15560). 1006 00
Prepared By Date Calculation Sheet Date Project ' ly / SZ. File No zs a. J k. ik~ r Job No o'rT -'p r + VC el IIIIIIIIIIIIIIIIIIIIIIIIIIIIII 50 I azQR4- Qs Sysrem Sneet No. Analysis No. +4'll + + . Rev, No 4.3.52 DENT; I HE j t9$ LE 8 Ei o ~ 9 +5 BEEN ~H DEADER 'F 2 n& I PPG'Pfb~x 5 oF 7 H e Hx'sc Qt4Hex t. aP ZTEFc C onsrauc rx on. TH E c.pjsEZ uS Eg g as H pj's aC> Ld z'v H <e RRRouJ. Stress General Cate-Condi- Situation Kind of gory Stress' (See tion Table B3l Plain material Base metal faces. with rolled or cleaned sur- or Rev. ~~ (g0 QQb) Built-up Base metal and weld metal in mem. T or Rev. members hers, without attachments, built-up of plates or shapes connected by contin-uous full. or partial. penetration groove welds or continuous filletwelds parallel to the direction of applied stress. Calculated flexural stress, fs, in base T or Rev. metal at toe of welds on girder webs or ilanges adjacent to welded transverse stiffeners. Base metal at end of partial.length Tor Rev. welded cover plates having square or tapered ends, with or without <<aids across the ends. hiechani ~ Base metal at gross section of high- Tor Rev. B cally strength. bolted friction.type connec-fastened tions, except connections subject to connec- stress reversal and axially loaded joints tions . which induce outwf-plane bending in connected material. Base metal at net section of other me. Tor Rev. D chanically fastened joints.
~
Base metal at net section of high- Tor Rev. B strength bolted bearing connections. httach. ments Shear stress on nominal area of stud. type shear connectors. (~~,s 5
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: ui ualification Subject System WPPSS 30" Mechanical Butterfl E Valve ment Checked By: Job No.
~~'. C. Fe ~~~~
File No. Date 3/25/83 q/qI'it~ CSP and CEP 82 Analysis No Rev. No. Sheet No. 361104 4 3 53 4 ' REFERENCES
1) BXF Drawings Drawing I Revo Description A-206763 General Arrangement CEP-625-10 From Reactor Nozzle X-3 to SGT-FU-1A, 1B CEP-625-11.12 H From Reactor Nozzle X-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 General Arrangment lan mis level CSP-807-3.4 Containment purge air su 1 s stem tcos.00
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII WPPSS Mechanical Equipment Qualifica~tVon J.E. Rakowski 3/25/83 Subject Checked By: Date 30" Butterfl Valves I-.c'. Fe.~~~~, +/:~'~ ". System Job No, File No. CSP and CEP OS.01/F Anatysis No. Rev, No. Sheet No. 36] 104 1 4 3 54 Reference cont'n Formulas for Natural Frequency and Mode Shapes, Robert D. Blevins Van Nostrand Reinhold Company 1979 Edition
~~3) BIF Report TR-27234 and TR-27235, "Dynamic Torque Calculation 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) WPPSS, WNP-2 SRM Equipment List Summary Sheets dated 2/10/83.

7) Cygna Energy Services, Equipment Qualification Walkdown Verification Form dated 7/14/82 and 7/19/82.

8) Cygna Energy Services, "Project Manual Design Criteria,"
~~DC-1, Rev. 1, 10/82.~~
9) Burns and Roe Revised Piping Analysis Loads for CSP-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. Rakowski of CES, nB1F Valve Dimensions", 2/ll/83
'l000 Oo
APPENDIX A COMPILED PROGRAMS AND RESULTS FOR CSP-V-1 CSP-V-2 CVGNA ATTAC>!iAC,ViT V OS IIO.~<<< FILE No ~0~. oI. F SHEE7IIO.~4'
sbasi c csp12 tm S-BASIC Comp i 1 er Version 5.4b uooi:00 REtlJJ++++ BIF VALVE AtiD AIR OPERATOR SEISI"iIC STRESS 0002:00 CSP-V/'AO-1/2 0003:00 REt"t+++++++++++++++ 10 IhiCH AO PARAMETERS OOO4:OO REt'1 0005:00 var i,j,k = inteoer 0006:00 var rod, cg,x,phi, ave,abl t,11,12,el,e2,e3,e4,e5 = r eal 1 1 1 0007:00 var fst2, ca, ia,cbs ib,aa,ab,dl,d2,cl, ii,c2, i 2=real 0008:00 var lrodo, ego, dr,d, abush, pbush=r eal 1 1 0009:00 var fcof, fco, ma,mb, siga, sigb, fcdr, fcdrf,maf, mbf=real 0010ioo var dear, f cear, fr, f 1, f 22,1a, c i 12,c i 21,st t3, seml=r eal 1 0011:00 var sem2,set3,sesl,ses2,sr, taul 1, tau22, tauear,aear=real 0012:00 var btens, taubl t, se t3f, semi f, sem2f, f cear f, f r f, f 11 f=r eal 0013:00 var f22f,stt3f,sesl f,ses2f,srf, tauif, tau2f, taur f=r eal 0014:00 var taubf, btf, dsr, dtaur, dtaub, dbten,dsa, dsb, dpb=real 0015:00 var sdraf,sdrbf,pbushf, taui if, tau22f=r eal 0016:00 var wao,wbr, f tr 1,watr1,si, si f, s2, s2f,mi,mi f,m2=real 0017:00 var m2f, t3, t3f, t t3, t t3f, br,wtot=real 1 0018:00 var bsisbs2sbt3sbmlsbm2sbtt3=r eal 0019:00 dim real av(3) 0020:00 dim real wa<3) 0021: 00 dim real wb(3) 0022:00 REN 0023:00 REM ss+ss BURNS 7 ROE EAR FORCES ARE bsi etc TURN Ohi WITH K=is'++ 0024:00 REM = "025:00 REI"1 326'00 dim real a(3,3) 0027:00 dim r eal b(3) 0028:00 dim real glc(3,3) 0029:00 1 data 9.5,,10.5, .88, 3.94r 1.50,1.34 0031:00 3 0032:00 4 0033:00 5 data 1847 't 0030:00 2 . data 25,21.50,.488,48.,4.8S,.627,1.75,3.0 875s i6s 648s 138s2 41si 4 data 593.,321.,S.25,8.5,28.5,15.,7.75 data 40 s16 2Ss26 5s43 s2 075
~ ~ ~ ~ ~ ~ ~ ~
~~0034:00 6 data 135 s90 r135 s90 r180 r90~~
~~~ ~ ~ ~ ~ ~~~
~~0035:00 7 data 45 s90 r135 r90 s0 s90~~
~~~ ~ ~ ~ ~ ~~~
0036:00 REM DAT* 657 FOR VALVMGLOBAL-G ORIENTATIONS AND WEIGHT VECTOR 0037:00 restor e 0038:00 r ead dl,d2,cl, i l,c2s i 2 0039ioo restore 2 0040ioo read lrod,lcg,x,phi,lave,ablt,11,12 0041:00 r estore 3 0042:00 r ead fst2,ca, i a,cb, ib,aa,ab 0043:00 res tor e 4 0044'00 read wao,wbr,ei,e2,e3,e4,e5 Aii.~~.CH~'. 0045'00 restore 5 "r'QB 0046:00 read lr odo,lcgo,ldr sd,abush NQ.9~~ 0047:00 r estore 6 t'-ILE hs0 os. 0 t. F 0048:00 0049:00 read a< 1, 1), a(2, >, a(3, 1), a(1, 2), a(2,2), a< 3, 2) restore 7 1 SH=.KV JQ. < '<< 0050:00 r ead a< 1,3), a(2,3), a(3,3), av(1 >, av(2), av 3) <
'151'00 text 0 rh INPUT GLOBAL ACCELERATIOt iS 8c vu52:00 i npu t 6< 1), b(2), b(3) 0053:00 print 0054:00 tex t 0 s8c INPUT DATA 8c 0055:00 print 0056:00 print "GLOBAL G-LEVELS ";b(1> sb(2) sb<3) 0057'00 print "tiORTH VECTOR AhiGLES = ";a(i, l),a(2,1),a(3,1) 0058:00 pr i n t "VEPTI CAL VECTOR ANGLES= "; a< 1 2) a< 2 2) a< 3 2) s s s s s
oo592ao p rint " EAST VECTOR ANGLES ";a<1,3),a(2,3),a<3,3) 0060:00 pr int "WEIGHT VECTOR AiiGLES ";av(i),av(2>,av(3) 0061:00 print 0062:00 for i=1 to 3 0063:01 for j=l to 3 0064:02 ~065:O2 j, a( i ) =a( j, i ) +2. glc(j,i)=b(i)icos(a<j,i)>
~~~3. 141 &'360 .~~
~~~')66:02 next j~~
~~~067201 next i 0068:00 for j=i to 3 0069:Oi j j av < ) =av ( ) +2. +3. 1416/360 .~~
0070:01 next 0071: 00 print 0072: 00 t e x t 0, h LOCAL G-LEVELS 8c 0073: 00 print 0074: 00 pr int ql c<1,1),gl c(1,2),gl c<1,3) 0075:00 print gl c(2,1),gl c(2,2),ql c(2,3) 0076:00 pr i n t gl c (3, >, gl c (3,2), gl c(3,3) 1 0077200 REM WE I GHT COMPONENTS 0078:00 for j=i to 3 OQ79:01 wa( j )~ao+cos(av( j) ) 0080:01 wb( j )=wbr icos(av( j) ) 0081:Oi n.ex t j 0082:00 ph i =ph i +2. +3. 141 &'360 . 0083:00 a= av e/2 1 0084200 c i 12=c 1 0085:00 c i 21=cd'i 1 ll i 2 0086:00 aear=l 1 +12 0087:00 REM CALCULATE EAR FORCES USE BhR LOADS AS OPTION LATER 0088200 REM FIXED COMPONENTS ARE ALWAYS THERE 0089:00 lbr=lrod+lcg 0090200 wa tr 1 = l br ea( 1) 11 rod 091:00 si f=wb( 1 )+watr 1 392:00 wtot=wao+wbr 0093:00 s2f=wb(2)+wa(2)+ f st2 0094 00 t3f=wa(3)+wb(3> 0095:00 mi f=-(wa<2)+wb<2)+f st2) +e5-wa(3) +< e3+ l cg>-wb(3) +e4 0096200 m2f=(wa tr 1+wb< 1) ) +e5~a(3) +e2-wb(3) +e 1 0097:00 t t3f=watr 1 +e3+ (wa< 2)+ f st2) +e2+wb< 1) +e4+wb(2) +e 1 0098:00 f cdr f=l cg+wa( l )t'1 rod 0099:00 maf=f cdrf +< l rod-13.5) 0100:00 mbf =f cdr f+7. 125 0101:00 sdraf=f st2/aa+abs(maf +cali a) 0102200 sdrbf=f st2r'ab+abs<mbf+cbJ'ib) 0103:00 f cof=l cgo+wa<1)/ir odo 0104:00 pbushf=f cof +( dr+d)f'(d+abush) 1 0105:00 REM STRESSES FROM FIXED COMPONENTS 0106:00 dear=< di wdi+d2+d2) ++. 5 0107:00 se t3f=abs( t3f/(4+aear) ) 0108:00 semif=abs(mif/(2+d2+aear>) 0109:00 sem2f =abs(m2f 1( 2+di +ae ar ) ) 0110:00 f cear f=t t3f/'(2+dear) CVGiNA Oili:00 f r f=x+fc ear f ATTACH>>'AT 0112200 f 1 if=-(fcearf +sin(phi )-frfwcos(phi ) ) 0113:00 f22f=fcear f+cos(phi )+frf+sin(phi ) J08 ~'10. ~So~ 0114:00 s t t3f=abs( f 11 f +I a+c i 12>+abs( f 22f +1 a+c i 21) Fli.E NO. O~ 0115:00 sesi f=abs(sl f +c i 12+1 a/4. ) SHEET N0,M4~ 0116:00 ses2f=abs(s2f +c i 21+lax'4. >
~~~ 17:00 sr f=se t3f+semi f+sem2f+sesi f+ses2f+st t3f 2~~
218200 REM EAR SHEAR 119:00 tau f=abs(sl f/(4+aear > )+abs( f fi'aear) 1 1 1 1 0120:00 tau22f=abs(s2f/(4~aear ) )+abs< f 22f/aear) 0121:00 taur f=( taui f +taui f+ tau22f +tau22f ) ++ 5 1 1 ~ 0122:00 taubf=taurf+aear/abl t 0123:00 REM EARBOLT TENSION o124:ao b t f= ( se t 3f + semi f + sem2f ) +ae ar J'ab t 1
0125:VU pr i n t "Ul hKA I lNU UYL INDE,K BKG f Kh.SbUKh lpousnf 0127:00 print"OPERATING VALVE EAR TENSILE STR " 'srf 0128:00 print"OPERATING VALVE EAR SHEAR STRES "; taurf '0129! 00 print"OPERATING EAR BOLT SHEAR STRESS "; taubf Oi 30: 00 print"OPERATING EAR BOLT TENSILE STR "; btf 0131: 00 print "132:00 REM
~~'33: 00 REM CALCULATE VARIABLE COMPONENTS I .84!00 REM 0135:00 dsr~O.~~
0136! 00 dtaur=O. 01 37: 00 dtaub=0. 0138! 00 dbten=0. 01 39: 00 dsa=O . 0140!00 dsb=O . 0141: 00 cip b=o ~ 0142: 00 for J=l to 3 Oi 43: 01 fco=lcgo+wao+glc(l,j)/lrodo 0144:01 pbush=fco+(ldr+d>/<d+abush) 0145!01 ftrl=lbr+wao+glc<l,j)/irod 0146!01 sl=f trl+wbr +gl c(l,j) 0147:01 s2=wtot+alc(2,J) 0148:01 t3=wtot+glc(3,J) 0149! 01 mi=-wtot+glc(2,J)+e5-wao+glc(3,J)+<e3+ lcg)-wbr +glc(3,J)+e4 0150! 01 m2=( f tr 1+wbr +g1 c 1, J ) ) we 5-(waowe 2+wbr + el ) +gl c<3,J l,j Oi 51: 01 t t3=f tri we3+wbr+gl c( ) +e4+gl c(2,J >+( )'ao+e2+wbr+el> 0152: 01 f c dr= cg+wao+gl c (1, J )/1 rod 1 0153! 01 ma=fcdr+<lr od-13.5) 0154: 01 mb=f cdr +7. 125 0155: 01 s i ga=ma+ca/i a 0156! 01 s i gb=mb+cb/ b 1 0157!01 REM CALCULATE EAR TENSION
~~~8!01 se t3=abs( t3/(4+aear > )~~
9:01 seml=abs(ml/(2+d2+aear) ) 0160!01 s em2=abs(m2/( 2+0 1 + ae ar ) ) 0161:Oi fcear =t t3/(2+dear ) 0162! 01 4 r=x+fcear 0163: 01 f 1=-( f cear+s in(ph i ) -fr+cos(ph ) ) 1 1 0164: 01 f22=fcear icos(phi )+fr+sin(phi ) 0165:Oi st t3=abs( f +1 a+c i 12)+abs( f 22%1 a+c 1 1 1 21 ) 0166!01 ses1 =abs( si +c i 12+1 a/4. >
~~.0,1 67! 0 1 ses2=abs( s2+c i 21+1 a/4. )~~
0168! 01 sr=se t3+semi+sem2+sesl+ses2+st t3 0165'! 0 1 REM EAR SHEAR 0170 201 tau 1 1=abs( sl/(4. +aear ) )+abs( f 1 1/aear ) 0171! 01 tau22=abs(s2/(4.+aear > )+abs< f 22/aea! ) 0172: 01 tauear ~( taul 1 +tau11+ tau22+tau22) ++.5 0173! 01 taubl t=tauear+aear/abl t 0174: 01 REM E*RBOLT TENSION 0175: 01 btens=(se t3+semi+sem2) waear/abl t 0176! 01 dsa=dsa+s i ga+s i ga 0177: 01 dsb=dsb+sigb+sigb 0178!01 dpb=dpb+pbush+pbush 0179:01 dsr~dsr+sr +sr 0180:01 dtaur=dtaur+ tauearwtauear 0181! 01 dtaub=dtaub+taublt+taublt JO 8 gO.~~~ 0182! 01 dbten=dbten+btenswbtens fllKgO. A1 Q3 ~ Of next J TNO 4!00 REM COMBINE STRESSES 0185:00 dsa=dsa++.5 0186:00 dsb=dsb++.5 01 87: 00 dpb=dpb++ 5 ~ 0188! 00 dsr=dsr++.5 0189! 00 dtaur=dtaur++.g 0190! 00 dtaub=dtaub++.5
0192: 00 print 01'F3: 00 text 0, h DYNAMIC COMPONENTS 5 0194: 00 pr int "01 95: 00 pr i n t "DR I VE ROD TENSILE STRESS AT A" I dsa 0196:00 pr i n t "DR I VE ROD TENS I LE STRESS AT B" Idsb 197:00 print "BUSHING PRESSURE I dpb 98:00 print "VALVE EAR TENSILE STRESS I dsl 99:00 print "VALVE EAR SHEAR STRESS ;dtaur v~00:00 print "EAR BOLT SHEAR STRESS ;dtaub 0201:00 print "EAR BOLT TENSILE STRESS ;dbten 0202:00 dsa=dsa+ abs ( sdr a )f 0203:00 dsb=dsb+abs(sdt bf) 0204:00 dpb=dpb+abs(pbushf) 0205:00 dsr =dsr+abs(sr f ) 0206:00 dtaur=dtaur+abs( taur f ) 0207:00 d t aub=d t aub+ abs( t aub f ) 0208:00 dbten=dbten+abs(btf ) 0209:00 print 0210:00 text O,h FIXED PLUS DYNAMIC COMP ONENTS h 021 1: 00 print 0212:00 print "DRIVE ROD TENSILE STRESS AT A"tdsa 0213:00 print "DRIVE ROD TENSILE STRESS AT BNidsb 0214:00 print "PUSHING PRESSURE "ldpb 0215:00 print "VALVE EAR TENSILE STRESS r dsl 0216:00 print "VALVE EAR SHEAR STRESS ";dtaur 0217:00 print "EAR BOLT SHEAR STRESS ";dtaub 0218:00 print "EAR BOLT TENSII E STRESS ";dbten 0219:00 end 0220:00 0221: 00 0222:00 223:00
~~~4:00 5:00 End of program CYGNA A i rwcvr@Env JOB NO.~<'~<~~
FlLE NO. SHEET NO.~>.AE
cspi INPUT GLOBAL ACCEI ERATIONS 'P 2.26,3 '2,2.8 INPUT DATA GLOBAL G-LEVELS NOPTH VECTOR ANGLES 2 '6 135
3. 62 90 2.8 135 VERTICAL VECTOR ANGLES= 90 180 90 EAST VECTOR ANGLES 45 90 135 WEIGHT VECTOR Al'lGLES 90 0 90 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 '66.432 OPERATING DRIVE ROD STRESS *T B 1319.35 OPERATING CYLINDER BRG PRESSURE -7.15824E-4 OPERATING VALVE EAR TENSILE STR 2111.01 OPERATING VALVE'EAR SHEAR STRES 293.896 OPERATING EAR BOLT SHEAR STRESS 2460.85 OPERATING EAR BOLT TENSILE STR 1625.1 DYNAMIC COMPONEllTS DRIVE ROD TENSILE STRESS AT A 28384.4 DRIVE ROD TEI'lSILE STRESS AT B 43412 2 ~ ~'~'>'4(g'-'"c'~ C6g ."i lr<wA .'.~ BUSHING PRESSURE 477.447 SCC SfRCTQ 1,3 3o - 4:E.<'a EAR BOLT SHEAR STRESS 7039 EAR BOLT TENSILE STRESS 10524.9 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 29150.9 DRIVE ROD TENSILE STRESS AT B 44731.6 PUSHING PRESSURE 477 '48 CVG~~~A
~~>me-.sa EAR BOLT SHEAR STRESS 9499.86 EAR BOLT TENSILE STRESS 121 50 Jos zo.~~~~
FiLs No svaa'o. ~s4'
cs@2 UT GLOBAL ACCELERATIQtlS E
~~'26,3.62,2.8 ~ ~~~
~~INPUT DATA GLOBAL G-LEVELS NORTH VECTOR ANGLES 2.2o 135 3 90~~
~~'2 2 8 ~~~
135 'ERTICAL VECTOR ANGLES= 90 180 90 EAST VECTOR ANGLES 45 90 135 WEIGHT VECTOR ANGLES 90 0 90 LOCAL G-LEVELS
-1 .59807 -1.38092E-5 1.97989 -8 '2121E-6 -3.62 -1.06811E-5 -1 .59807 -1.38092E-5 -1.97991 OPERATIflG DRIVE ROD STRESS AT A 766.432 OPERATIf'lG QPERATIflG DRI'VE ROD STRESS AT B CYLINDER BRG PRESSURE 1319 '5 -7.15824E-4 OPERATING EAR WELD TENSILE STR 3090.43 OPERATIt'IG EAR WELD SHEAR STRES 735.124 OPERATING EAR BOLT SHEAR STRESS 2460.86 OPERATING EAR BOLT TENSILE STR 1625.1 WI C CQMPOt lENTS DRIVE ROD TENSILE STRESS AT B 43412.2 BUSHING PRESSURE maua -e zan a=Ed ~R-WEf=& SHEAR .rrR EAR BOLT SHEAR STRESS EAR BOLT TEf'lSILE STRESS smcss DRIVE ROD TEt ISILE STRESS AT A 28384 4 477.447 vis~~ +
~~7039 10524.9~~
~ <Cc~ g,'i '875 FIXED PLUS DYNAMIC COMPONENTS CVQ<4A DRIVE ROD TENSILE STRESS AT A 29150. 9 DRIVE ROD TENSILE STRESS AT B 44731.6 JOB &!0.~ ~EAR'WEL~~
~~PUSHItlG PRESSURE R-MEt.-D 7 Eh 477.448 28~&6-(~~ ~~ ~05.6(. gfaacT QQ. g.s,A7 EAR BOLT SHEAR STRESS 9499 86~~
~
EAR BOLT TENSILE STRESS 12150
c=p Q INPUT GLOBAL ACCELERAT I Ot'lS
'? 1 '4s3 54fl ~ 9 I t lPUT DATA GLOBAL G-LEVELS 1.44 3.54 1.9 NORTH VECTOR At'lGLES = 135 '90 135 VERTICAL VECTOR ANGLES= 90 180 90 EAST VECTOR ANGLES = 45 90 135 WEIGHT VECTOR ANGLES = 90 0 90 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 OPERATING DRIVE ROD STRESS AT A 766.432 OPERATIt'lG DRIVE ROD STPESS AT B 1319.35 OPERATING CYLINDER BRG PRESSURE -7.15824E-4 OPERAT I t lG VAL'VE EAP. TEtitSI LE STR 2111.01 OPERATING VALVE EAR SHEAR STRES 293.896 OPERATING EAR BOLT SHEAR STRESS 2460.85 OPERATING EAR BOLT TENSILE STR 1625.1 DYNAMIC CONPONENTS DRIVE ROD TENSILE STRESS AT A 18806 DRIVE ROD TEt'lSILE STRESS *T B 28762.8 BUSHIt'lG PRESSURE 316.332 P Cm SWe,VS %.3.~~ -II"%.~
EAR BOLT SHEAR STRESS 5077.94 EAR BOLT TENS I LE STPESS 7164.63 FIXED PLUS DYNANIC CONPONENTS DRIVE ROD TEt'lSILE STRESS AT A 19572.5 DRIVE ROD TENSILE STRESS AT B 30082.1 PUSHING PRESSURE 316
~~"'868. '33 CVQblA MA~EAR-TSttS.FQ~7RESS 59~~
~tNE-EA~HEA~7RES8 - 900~48- ATTACH)BEiil, BOLT SHEAR STRESS 7538.79 'AR EAR BOLT TENSILE STRESS 8789.72 JOB NO. f~'pp+ FILf NO. OS.PI ~ P SHffTNO. "~.~f
c IQ2 UT GLOBAL ACCELERATIONS 54)1 9 '4s3 INPUT DATA GLOBAL G-LEVELS 1.44 3.54 1.9 NORTH VECTOR ANGLES = 135 90 135 VERTICAL VECTOR ANGLES= 90 180 90 EAST VECTOR AllGLES = 45 90 135 WEIGHT VECTOR Al'lGLES = 90 0 90 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 A 766.432 OPERATING DRIVE ROD STRESS AT B 1319.35 OPERATING CYLINDER BRG PRESSURE -7.15824E-4 OPERATIl'lG EAR WELD TENSILE STR 3090.43 OPERATING EAR WELD SHEAR STRES 735.124 OPERATING EAR BOLT SHEAR STRESS 2460.86 OPERATING EAR BOLT TENSILE STR 1625.1 'INIC CONPONENTS DRIVE ROD TENSILE STRESS AT A 18806 DRIVE ROD TENSILE STRESS AT B 28762.8 BUSHING PRESSURE
~~~R-IdELD SHEAR-SFRESS EAR BOLT SHEAR STRESS 316 '32~~
~~+SM.;R2.~~
5077 96~ EAR BOLT TENSILE STRESS 7164.63 F I XED PLUS DYt lAN I C COMPONENTS DRIVE ROD TENSILE STRESS AT A 19572.5 DPIVE ROD TENSILE STRESS AT B 30082.1 PUSHING PRESSURE ~-WELD. TENSI-l-E-STRESS = 316. 333 1-1 506-..3-EAR BOLT SHEAR STRESS 7538.81 EAR 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. ~ F SaENG. OSSA SHEET NG
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SECTION 5.0 APPENDTCES CONTENTS g~ Q+&E'
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5.2 Walkdown Sheets 5;3 Valve Local Coordinate Systems g~ (QPwz&i SE++Tf >c) 5.5 Revised 'burns and Roe Piscina Analysis Accelerations 5.6 Load Comparative Sheets
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MODEL( 6&5 SERIALS / I "7Z+g- ( MAT'L 5l < Q -'75 4~ PSI 8 84D LBS SIZE~@ YOKE ORIENTATION MOUNTING CONDITION I TO AXIS OF PIPE ( ) NO OF BOLTS
~g ~//s // TO AXIS OF PIPE ( ),/V[n I/'i BOLT TYPE WELD TYPE 8 BOLT 0 //4-(uY SIZE ~cA~)c ~ Ci:~ z'3Z7 'JC YOKE LENGTH (FLANGE TO FLANGE) PIPE MOUNTED YES (vi) N (
PERYiANENT OBSTRUCTION (WITHIN 2 ")................ YES ( ) NO ( Q IS 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 GLOBAL CO-ORDINATE OPERATOR EPN MODEL NO SYSTEM 4- '/ VALVE STEM ORIENTATION MANUFACTURER SERIAL NO r'zz<~ TYPE SIZE ORDER NO MOTOR EPN MANUFACTURER MODEL NO SERIAL NO ID NO INS CLASS 1-PHASE ( ) 3-PHASE ( ) AC DC TYPE OF CONDUIT CONNECTION: RIGID ( ) FLEX (Q) NOTES: 1. Definition (N/F = Not. Found)
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MiFR COMPONENT EL~50 DSCRP i - ~m L(/ MODELS SERIAL% /- 2 Z -Z HAT'L 5 Cf-5'S I 8 Sdt) 'F ASME CLASS I LBS~/SI SE 3Q YOKE ORIENTATION MOUNTING CONDITION TO AXIS OF PIPE ( ) NO OF BOLTS BOLT TYPE //c V(' c
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J/p WELD TYPE & SIZE Le~c >z YOKE LENGTH (FLANGE TO FLANGE) PIPE MOUNTED YES (4) NO ( ) PERYIANENT OBSTRUCTION (WITHIN 2")................YES ( ) NO (Y) IS COMIP BETWEEN CONT & 1ST ANC (FULL 6 WAY ANC) YES Q() NO ( ) DO MULTIPLE SUPPORTS EXIST BETWEEN CONT & COMP , YES ( ) NO X Z GLOBAL CO-ORDINATE VALVE STEM ORIENTATION SYSTEMi OPERATOR EPN HANUFACTURER //< C. -g +/ MODEL NO SERIAL NO TYPE SIZE ORDER NO MOTOR EPN MANUFACTURER MODEL NO SERIAL NO ID NO INS CLASS I-PHASE ( ) 3-PHASE ( ) AC DC TYPE OF CONDUIT CONNECTION:'IGID ( ) ...FLEX (P) NOTES: 1. Definition (N/F = Not Found) Alkf~jCd C.~+//7 "iJ/-,E~ (- gg~,r g Q/g 74gpg /(gg
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lllllllllll!lllllllllllllllll; QI DT", Ud I/O BLDG FLOOR EL ~ I/ COORDS '7, $ /gv j. MFR COMPONENT EL~~ ~ii;-', -
/;
MODELTL C>l: i SERIALT,'SYiE MAT L Vj -6,<@~a CLASS Z LBS /5O SIZE Zg YOF'E ORI KTATIOh MOUNTING CONDITION TO A).'IS OF PIPE ( ) NO OF BOLTS 2Q
~~/j TO A>:IS OP PIPE ( ) /jj'.~~
~~BOLT TYPE WELD TYPE & SI ZE BOLT (2 'U ql~~
~~~, ~r/i YOFFE LENGTH (FLANGE TO FLE NGE) PIPE MOUNTED YES (P ) NO ( )~~
PERt~iAhIENT OBSTRUCTIO1 {i'ITHIK 2 ") YES ( ) NP (2 ) I S COMP BETv',EEL CONT & 1ST ANC (FULL 6 NAY ANC) YES (Y~) NO ( ) DO MULTIPLE SUPPORTS E>:IST BETNEEK CONT 6 COMiP YES (p,=) NO ( ) GLOBA CO-ORDINATE VALVE STEM ORIEL TATION SYSTEM
'OP:JU;TOR EPI2~C~P- 'Pi-1:ODEL NO SERIAL NO TYPE S1 c.E ORDER NO MOTOR EPh MANUFACTURER MODEL NO SERIAL HO ID tIn IHS CLASS 3 -PHASE ( ) 3-PHASE { ) AC DC TYPE OF CONDUIT COIlNECTIObl: RIGID ( ) FLE>: ( )
NOTES: 3. Dc.in'ion (ti/F = Not Found) 2'V'h/'"~ C2 <2/'/'7 2 rJ/ QrlC q S~C/i /& C. Q/~j j @Qadi 0 IQD I .AC.C VJC ' rg<,ll~ ./'-lC " '. ~ -< i, 6 P(>bCL, DC J:,"i<47 f~'J TAt=" i=a pJq. PREPARED BY DAT~~REVIEilED B'l,C,+~iiiii/i DATE ~//2o /" (SIGNATURE) ( S I GNATURE )~> D Jell/.e. L P FF tJi'NOF.~~
~~'/<:v " ~'/.;-'. Qcw:'!Cr ~ Cc 0~ I Cnec<ec Ep'('< g D&tt I~~
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Ca IC Ulation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Pioiecl Prepared By Date 4tPPSS Hechanical Eaui ment ualifi o I Srrbiect 24" Butterfl Valves grt M/ "2 Z'(bs Svslern Joo No File No P (j Analvsrs No Rev, No. Stteet No 361106 g Or-3 gl"Ill'l.il:J, r'l- 4 vaAAilo'< ~ (Alk DP&rlr I ok Ac uc:g') gSPAO
E),)UI,P:" t.'i ()U):iL1.' v'.s.'i ) Uli WALKDOWIi VERI'CAT10!'. FOP)'. PAGE 1 OF IIIIIIIIIIIIIIIIIIIIIIIIIIIIII EPN CSP-Y-d QID". 8C Id BLDG FLOOR EL ~7/ COORDS 7, 5/g8.C~ MFR c- COMPONENT EL~s~ DSCRP AVE, ~i MODELS,' . 7 SERIALS",' 3( - Z ~w ASME CLASS Z LBS i S) SIZE C4 YOKE ORIENTATION MOUNTING CONDITION I TO AXIS OF PIPE ( ) NO OF BOLTS ZQ BOLT TYPE BOLT g
~~// TO AXIS OF PIPE ( )~~
yj/A WELD TYPE & SIZE ('C4-, ().~~ YOKE LENGTH (FLANGE TO FLANGE) PIPE MOUNTED YES (X) NO () PERMANENT OBSTRUCTION (WITHIN 2").... ~ - - . ~ - -
~~~ .. ~ ~ YES ( ) NO (A )~~
IS COMP BETWEEN CONT & 1ST ANC (FULL 6 WAY ANC) YES W) NO ( ) DO MULTIPLE SUPPORTS EXIST BETWEEN CONT & COMP YES (y) NO ( ) pg GLOBAL CO-ORDINATE VALVE STEM ORI ENTATION SYSTEM OPERATOR EPN MANUFACTURER . Is MODEL NO 'Q~ SERIAL NO TYPE SIZE ORDER NO MOTOR EPN MANUFACTURER MODEL NO SERIAL NO ID NO IWS CLASS I-PHASE ( ) 3-PHASE ( ) AC DC TYPE OF CONDUIT CONNECTION: RIGID ( ) FLEX ( ) NOTES: 1. Definition (N/F = Not Found) (~) s'4///1 ~0 <~WI7 gpJI Qt/C Z(W P('g 7+QQ Q /QL) 7>/~AC sJcae. sos) s)ssz sss~~slrssa ssitc, zsDsscL/~ccJ-,ss-sccirsssv 7A65 pgggg I PREPARED BY (~'.lr/ ~tJ", DATECcllbll:~REVIEWED BY + i ci,i, r, DATE (SIGNATURE) (SIGNATURE) LI DMw~c4QL.E, C..C. Fppdrr.lopez
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EQUIP! iE?i T Qi.!Al 1I 1 CATI 0?i WALKDOWN VERIFY'ATIOI! FORM PAGE I, DP~ t" -V'- S IIIIIIIIIIIIIIIIIIIIIIIIIIIIII FLOOR EL 4-7I EPN
~
COORDS I ~/I 4,7 8.5 BLDG Q. MFR COMPONENT EL 475 DSCRP Qgr7. MODEL( SERIALS <7'Z 5C -I MAT'LGALS/4 6&id tS~ PSI 8 'Z'?4 F ASME CLASS Z LBS /5(3 SIZE Zg YOKE ORIENTATION MOUNTING CONDITION l TO AXIS OF PIPE ( ) NO OF BOLTS ZD BOLT TYPE BOLT 0 l~
~~// TO AXIS OF PIPE ( )~~
WELD TYPE & SI ZE (SO dsz YOKE LENGTH (FLANGE TO FLANGE) PIPE MOUNTED YES (X3 NO () PERY&NENT OBSTRUCTION (WITHIN 2" ) .'............... YES YES ( (K)
~~) NO NO~~
(+ IS COMP BETWEEN CONT & 1ST ANC (FULL 6 WAY ANC) ( ) DO MULTIPLE SUPPORTS EXIST BETWEEN CONT & COMP YES (K) NO ( ) C~ gyle X Z GLOBAL CO-ORDINATE VALVE STEM ORIENTATION SYSTEM OPERATOR EPN+$ MODEL NO
~
~~3 MANUFACTURER SERIAL NO TYPE SIZE ORDER NO~~
~O~OR EPN~g MANUFACTURER MODEL NO SERIAL NO ID NO INS CLASS I-PHASE ( ) 3-PHASE ( ) AC DC TYPE OF CONDUIT CONNECTION: RIGID ( ) FLEX Oc,)
~~NOTES: 1. Definition (N/F = Not Found)~~
~~2. (8) ~JAaC.o <i~>(i <>Jii C~<~ 4CQrp~ 'C4 74QQC)/g~~~
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EAUX PMENT QUALIF1 CE<. 1 0!i WALKDOWlx VFRXF1CATION FOR!'I PAGL' OF 2 IIIIIIIIIIIIIIIIIIIIIIIIIIIIII EPN C.SP-V'- b
~~&En I { 0&~~
~~BLD M(FR G~ $P FLOOR EL COMPONENT EL 47 l~~
~~~Q QI DC COORDS DSCRP Pl.+ /5.~~
MODEL,", 04 S7 SERIALS MAT'L BA { a b (SC< PSI S~ZS 'F ASME CLASS LBS~QO SIZE ZC~ YOKE ORIENTATION MOUNTING CONDITION TO AXIS'F PIPE ( ) NO OF BOLTS Zb BOLT 0
~~// TO AXIS OF PIPE ( )~~
Qp BOLT TYPE WELD 'TYPE 6 SIZE {1 Earns YOKE LENGTH (FLANGE TO FLANGE) PIPE MOUNTED YES (g) NO ( ) PERMANENT OBSTRUCTION (WITHIN 2")..... YES ( ) NO (+ XS COMP BETWEEN CONT 6 1ST ANC (FULL 6 WAY ANC) YES (X,) NO ( ) DO MULTIPLE SUPPORTS EXIST BETWEEN CONT 6 COMP YES ()C) NO ( )
-. ~X GLOBAL CO-ORDINATE VALVE STEM ORIENTATION SY STEPi OP ERATOR EPN 55/- MANUFACTURER g( ~ c.
MODEL NO SERXAL NO TYPE SIZE ORDER NO MOTOR EPN MANUFACTURER SERIAL NO
~j'ODEL NO ID NO XNS CLASS 1-PHASE ( ) 3-PHASE ( ) AC DC TYPE OF CONDUIT CONNECTION: RIGID ( ) FLEX (+
~~NOTES: 1. Definition (N/F = Not Found) z., (zJ/J4wu ~<<r 5'<<i<ro<Ee~ ze<iiwc.~ i@4 So /oo~~
~~+~ %6$ ((-duub.~~
IVSEC Qo AtA! aPH4aa. An<- 5 Z(O DSc./ZD<BJfzpi CAVIES J PREPARED BY DATEP Z$ REVIEWED BY .~-~(.F s~-<~<~. DATE (SIGNATURE) (SIGNATURE)y QosJ ~EA~ ( .6< F Q<C(~h(l jf j~
~~',.'~aies llllllllllllllllllllllllllllll Sheet e "ei i ~ ~~~
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EQUIP?~iENT QUAL11 1 CATIOli WALKDOWN VERI FlCATION FORl I P) GE I OP~ llllllllllllllllllllllllllllll EPN Q9~ V'- 9 OID:; Z //Qb BLDG FLOOR EL 47 COORDS MiFR COMPONENT EL~ DSCRP &CtTTE&- MODELN 66 0 SERIALS' MAT 'L (50 ISI 8 275' ASME CLASS Z LBS SIZE ZC1 YOKE ORIENTATION MOUNTING CONDITION TO AXIS OF PIPE ( ) NO OF BOLTS BOLT TYPE BOLT q) TO AXIS OF PIPE ) )J/ WELD .TYPE 6 SI ZE Fc.~cb COLS YOKE LENGTH (FLANGE TO FLANGE) PIPE MOUNTED YES (~ NO ( ) PERl)(IANENT OBSTRUCTION (WITHIN 2")................YES ( ) NO (<) IS COMiP BETWEEN CONT S 1ST ANC (FULL 6 WAY ANC) YES (K) NO ( ) DO MULTIPLE SUPPORTS EXIST BETWEEN CONT & COMiP YES ( ) NO (g) X GLOBAL CO-ORDINATE VALVE STEMi ORIENTATION SY STEIN OPERATOR EPN Qg~ MANUFACTURER k.c ur MiODEL NO 3 SERIAL NO TYPE SIZE . ORDER NO MOTOR EPM~ MANUFACTURER MODEL NO SERIAL NO ID NO INS CLASS I-PHASE ( ) 3-PHASE ( ) AC DC TYPE OF CONDUIT CONNECTION: RIGID ( ) FLEX (g)
~
~~NOTES: 1. Defipition (N/F = h'ot Found)~~
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'rotect / ~z Prepared By.' Date Checked By: > g > Date Egulk. OA<,
System JobNo, ~ ~l FiteNo. Analysis Ns. Rsv. Na. Sheet No. g~Q a~ .r~g '20 l4 I ~IA
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PAGE 1 OF EQUIPMENT QUALIFICATION VALKDOWN VERI F I CATI ON FORK& L C R ~ 6 llllllllllllllllllllllllllllll ZPN< Ce, V- l 8 OID~ '3 (.ll O BLDG R- FLOOR EL 5 I cooRDs ~.( S 'I
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MiFR COMPONENT EL oscar 3o 8 rloDf, 0 "20(& ~3 SERIAL( 2 7 2. 3g - 3 AT'LSh- S I(-- t'< ( 5 PSI 6 3'IO 'F LBS Nl( SI EE QrD ASl"E CLASS YOKE ORI ENTATION MOUNTING CONDZTZON To AXIS OF PIPE ( ) No OF BOLTS ~%i TO A>'ZS OF PIPE BQLT TYPE r /9 BQLT q) t fh ( ) WELD TYPE 6 SIZE YOKE LENGTH (FLANGE To FLANGE)
~~+~P MOUNTED YES (~ No +IA'IPE~~
~~( ) LQ(4 Q~ PERr'&ANENT OBSTRUCTION (WITHIN 2") YES ( ) NO ( IS COMP BETWEEN CONT & IST ANC. (FULL 6 WAY ANC) YES~~
~~~ (g &(0 ( )~~
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Fll.E NO. 0S.ol. F SHEc~ NO.~ ~ X 'rr'LOBAL CO-ORDINATE VALVE .STEM ORI SYSTEM Eb'TATZor)'IANUFACTURER PERATOR EPri oDEL r"o S ERIAL No YPE SIZE ORDER No ioTOR EPN Y~UFACTURER iODEL No SERIAL No D No INS CLASS I PHASE ( ) I PHASE ( ) AC DC COMMENTS: g L>~it 5 mskgQg Q~g CPfd's'- af g (4 8J: 4>salon ma~ la~4rai .. Ha ~ Co 3.mls
~~~ ER~ ok')oo )~~
P PREPARED BY D TER/lg//LREYI,WED BY DATE ~/ ~ (S GNATURE) T~ eW ( SI G &%A'ZU A!i6 L/A~ E) /
PAGE 3 OF E UZPMJ. l'".'UALZFiCA71ON NJ)J kiDO43'ER1 k I CATION FOr" Illllllllllfllflllillilllillll EPNt CE' > A l QZD> 34, t f'0 ELD,G , .,,FLOOR EL ~ jP COORDS S 'i xF COMPONENT EL SSF DSCRP 3O' 8~('l MODE QG5 + SERIALS ZWQ i I MAT'L SA -Sl~- MM PSI 6 3SO LBS ~ f= SI ZE AShiE CLASS YOYE ORIENTATION MOUNTING CONDITION TO AXIS OF PIPE ( ) NO OF BOLTS v/p BOZ,T TYPE V A BOLT e TO AXZS OF PZPE ( ) Vi'ELD TYPE & SIZE YOk:E LENGTH P'/ 6 (FLANGE TO FLANGE) PZPE MOUNTED YES ( +) NO ( ) LL)X (I Tg S PERlJiANENT OBSTRUCTION (WITHIN 2" ) YES ( ) NO ( ) IS COl'.P B:"TWEEN CONT 6 1ST ANC. (FULL 6 WAY ANC) YES ( (6 NO ( ) DO MULTIPLE SUPPORTS EXIST BETWEEN CONT & COMP YES NO ( g CYQ)",4A A77ACHMENT JOS NO. FILE NO. r6' SltrrT NO. GLOBAL CO-ORDI NATE VALVE . S TEM ORI EUTATION SYSTEM PERATOR EPN Y~UFACTURER ODEL NO SERIAL NO YPE SIZE ORDER NO JOTOP, EPN hJANUFACTURER
.ODEL NO SERIAL NO D NO INS CIASS 1-PHASE ( ) 3-PHASE ( ) AC DC OMMENTS: Z L(~5 5( (Xc.L5 g o.~~ C 4-ls 5~i.l 4: l rc Stoa Gfw: C( f-L~s-2* 'EA >SOrO>~O PREPARED BY & 9~fr 14 [ DATER/tM/grHEVIEWED BY DATE (S I GNATURE ( GNAT ~r.)
5.3 Valve Local Coordinate Systems CSP-V-1 CSP-V-2
4R QpE&i QR ATiACH~,ENJT SCRAP-T 0 05 4~~ = . ~ 707..., s 50S j~~ - Q
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~~5. 5 REVISED BURNS 6 ROE PIPING ANALYSIS ACCELERATIONS~~
~~QJ!,'> fear<<> i ~~~
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r,' MAY 11 f983,. I' ~ P Sub5ectx W. 0. 3900/4 000 R f CEIQrFD
~~%lashing ton Public Power Su ppl y S ye ter"..~~
~~N4P-2 Qualification of Ncchan ical Pipe I!l/Al '! J )f83 t.'ounted Equipnent; Forv arding of f Zn oxma t ion CYGNA-RICHLggo '--:"-~~
~ I April 29, 1983 DNPP-83-07 6 I /i !fr. L. T. Harrold Assistant Director Washington Public Powe r Supply System 3000 George Vaohington May r Richland, Vashington 9 9352 %laic>
~~Attention: hlr. B. A. lfolmbc:rgr sos wo.~ F!!.a!40.~ 8p.c +0 os.o{. F g,~~
~
~~g.5, I~~
~~References:~~
~~(a) >7PBR-03-17, Bated 3/16/93. SHeET No. {b) WPBP;S3-20, Gated 4/12/83. (c) MPHR-83-29, datod 4/12/83.~~
'MQ+.o,i. '. ~ ~ '(d) Te3.ecopy, B. A. Holmherg to J. J. Vere>crber, dated 4/4/83 Gentlemen: ~ I .,C. W.rn, ~ 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 valves represent the second iterati.on of the refincraent task.. Valve .', i"..tg.! sheets for the other four {4) valves represent the first iteration of the refinement task. Please inform the Noodbury:.",.-
~~'h Office further.~~
~~if efforts should bc r.-ade to rer1uce accelerations ~ I~~
~~~ I ;, \~~
~~Ve ry truly your s, QR )caps twL ctCi.'I ED BY J. J. Vr2',DERSEP~~
~~~ ~~~
~~+ei<~A;~:':>'-" O'JV/BPM/es John J. Verderber I~~
" i~i;;;j~:g,<-',! Att Pro5ect Engineering Manager Hr. >1. S. Chin - DPA 3 ~r/1 QHr. J. Z. Rhodes - VPPSS - 1 xr/l P. Buck - E,"Pp"S - l ~./1 .'lail Drop ."'75
~~~ I 0:"'C:~~
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A k ATTACHE1ENT Data forwarded with BRNP-83-078, dated April 29, 1983 Valve Kale. No. SP-V- 125 8. 14 .129 (~SP V-2 .~ 125 8.14 .129 CSP-V-3 125 8.14 .129 CSP-V-4 125 8.14 .129 CSP-V-5 125 8.14 .129 RCIC-V-31 107 8.14 .112A RHR-V-17B 31 8.14 ..121 RHR-V-53A 29 8.14 ~ 62C REER-,V-53B 31 8. 14 . 121B CVGMA ATTAChV~Eii-'7 JGB NG. FILE NO. SHEET IIG.
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII BIO'- E.G y<<, - I Prepared By: <<P~~ j Date Subject 4/l- <<i 1Lt t r<<-,.bi,"Qg C)hd<<5 fuI..<< '.Checked By g J Date System~gp 'zd<4 " 'o-.oil~ Analysis No. Rev, No. Sheet No. I lO( 0%@ i PV ERA ~t= l=L&<t--lT'7 l.77 (tc<<) ~/ 3.b-ChLCVI.P f'- EI-F"-C.WIVQ Mc<<t <<-= '~ 7" Ot= t: Au gt(. E<<) E2 JERE Qc pD 7'o p6 I."gF "-E)l T TYING /+Cga T, Q<l= 7H5 Fat t.bwtd& DIM,<<=U- lO<<V 5 D <<< 1000 00 Calculation Sheet Prepared By: Date 3 Date h'h (* r'" /4 aaedd 0 dl/.(= '"""'I.>>ab-~.-I=)Q )Otta 00 /, Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII P oiect Prepared By: Date PP,~~ Subject /) ~ Kdr' + l' /'70' i i D p Checked By t=t'rll./l,'-'.c' J ~d,e.>Jr. Da e System Job No. Fite No. ~~@ + 3ai(~4 ".-3C link + '~(I<Q4>>9.+ -815 rot: Tp! c j (Jcgg.~ gL,<,u Ev T tt (MAICF- Q = o f F'iJT 277~ l5 reulV ) ~5.G'(IS ~I..S ) QgAc=~~ ).r = WE.tt'g = 'Q7 )f3 A,l 4K+ - 4g = 0.'S9- Ill (( io r. ) ( t.~ ,~ C- = .2 < Itl .n(a .) 1~ ( gsve ) I~~ htaS- W7I~') (( I~N)zss >~') '2.N IAI i.PPC F ~7' ( 'tt2. ) IN Zu kA<I= l:FQ & ted& IM t."~i 0 oF jf9" t.<I= ~ pggt 3 J-xx = (o.~)((. =- ) t 2. I - .L~S- .'005 00 Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII ~ jPP~% ~A Prepared By: tk g fzf ) 5 Date Subject 8,'ZF VA.ku=/P.ct-u6 tnP. Mn F'. 3l Checked By:Q r~e~'!< ~ el Ji g C r" M~A"A'.=,<~f5". j Date System (\ q 88644 Ot.at I= Analysis No. '! Iln~ a)OIo Rev. No. 34l l04- 9.5- 8',! PEIVC. Po p ~~ L~i> p sL '. PlgyaaCc ARE ~ Qo+I-L '. 5 c +A/ .n fQtb gq x "l4 cA) Qgg ~ n ( Q'. Pr.we Wt: L = zJ~.5 = Z.+ A - TI/~ 9 Z,klIP ~ Y'l S I~y = X p-- (5 'Iz P.ta ) (to) (r~~") Qz '5 c yL'. PGV s19 /t7 CS ~ 0> Zyy = '1 0 ut ~ (!!9>) +z. = l~~~ i.~~ = s- z iN i )~~+jr~) . 14.o ((0) A = p<g = so,3 iN (1g) =':,[z. i~ c = u."(s) 10" s 00 Calculation Sheet Prepared 8y.' Ii ~t ~ t )( '.,') 4kvAi" ' Date . / Jabwo. FleNo. oa+~4 i/ Sheet No. Df<IYZ I!ol0 =TI P) hi~ CaaC& 5 VL~>>iD 'I w i z! 1e06 CO Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Prepared By: PPR ) Stjb't System 'e T iA v / I ~ra.,sj /n O~L Checked By. upr;P'.Ls'! Date 8,!Zd'h5 Job No. No., File No. ~ 2.Od.cf. Gt ~ col ~ Analysis Rev. No. 44I/O", 8 ting@ >.Io I IC>4-',.3- l~ I 3, ~AR s: ~j = VA~~~ ~tz. IV o~~M~ j'a'r* ea r, Z,l 2.S ps - I,5 %2.5 g 4 = I- (J.J X I. S" (i.v <) e .X(J~;-~IA S: It~ y('-~~ (' Tst' Ty. )10 (i.SrSt>>)8 l.1Z.(.(oI ~~ - T i~a 4 P X gg= ,q z((0)~ ) gers'QO) g I S.~St.to> ej rsyce c Ixv I o4 %lO I 04 i(J 4.'RS C5g IV lc( + i.VZ q. IZS tees 00 Calculation t~ ~j~J Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By:,' ' Date 'tJ~l) q~ Sub ect I hacked By: '/' Date '.~ 6 VAD/2 1 6 t 'gf~i I 'gp tv(rgb~ t ~U>pt'r f pled ~ Z4 a3 System n 52odh 0T,d I /~ 3LllaR 8 )04 0 ~ " '4/134-~.>- $ 13 g Cggrg~g4e r C y -- S.de 1/i (i7Q Qs.~ E, = Z I 0 IQ F~L ~EC.AUSE ot= Bfv~IPII" oF- >~<6 P o>e. CELOcu IH / jy '6 lg 70 /IctoilA T. ( Illl5 vJIl9 Do th) /Nest QS/K I=~ l~ I(+g) " +err@'m ~is,c= Q.z-~5 Y~~ = f'o L IZ~Z'z. ~') Q.1 ~(h,c~ 7w ~ ~J T. 7.9 = ( )r'ac) r.s~) 10cs cc Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project tel t.NS Prepared By: jt p it ~ . Date /r, Subject System 'I 0} VE l Cl 4A <C'I 0 r Checked By. L ~<<trttrAQ.'l . Jr'4';-ct- / Date ."Irg .s!"" bZD44 d t. 01 /t-Analysis hto. .5( I la I d I 4 Rev. No. 6 '.;t >lgj - -! ='-(Big I=tgt td!=7 7,1~5 ~7 g8 I rg !I (g g f..'-.5 Vcr=- LF"==,,%~I~ ~lWs (<I.l>3 +g.o)) ~sHAF PIll = '2.2-5 Ir:~ !eIeFtlel.son l -'4 In~ ! !zs .(I 2<) I .zr. rn l>r(!'Iz)= Vj - Il< Z= ..s~ I.o 88+) Qe gZ, A=mt, ="=.qS N + Sll JI.Ft ( gpss) (s )=(z.sr ri ) i,q" 'II.S', - 7,(z5 ! Q,)i'<) -- Iq '-Ite 5g!!I Fq ~o ~C. =.at=7 7.1 H~ ~ P- f;=Fu=e~ 0tj q STIFF pJ g g C. = r =.Pr c- D V (C .u.~ (":0 " Cjt q,O (pg =-,cr: -') f.,)H'l jl! IC /J J Italo(I:gCQ P P ~ I: 6, tgp Q p.~gQr'lr Lc,lJ ~~it !!+=',78 ill (2'I ) 5'rY = 3+'E-'3 = g lI ~.g<) .2( g.t1+.et> I00S 00 APPENDIX C SAMPLE HAND CALCULATIONS TO CHECK PROGRAM CEP-V-3A ~ y I 4 V \ ~ ~ v 'I ~ N t ~: ~ nbi f Cc P V'- Calculation INPUT GLOBAL ACCELEPATI Ct l$ ? 13.89,1.66,1.04 Sheet It'lPUT ANGLES OF NORTH VECTOR ? 90,90,0 INPUT ANGLES OF VERTICAL VECTOR 90 0 r90 Prepared By Oate INPUT ANGl ES OF EAST VECTOR ? 0,90,90 Checked B 5 Rl I t lPUT DATA "" 'e.os@ OT:0 i(~= GLOBAL G-LEVELS NORTH VECTOR ANGLES = 90 13.89 1 90 '6 0 1.04 5C I I o(.-C -i VERTICAL VECTOR Al'lGLES= 90 0 90 EAST VECTOR ANGLES = 0 90 90 INPUT AtlGLES OF MEIGHT VECTOR %Pl MPCE. CHECl< CALC 5 ? 90,180,90 <A R TL.VSl<E H~ZE>5 LOCAL G-LEVELS TPF - (F T-e~)~V.~ -m> ~~.~ -5.29861E-5 -6.33239E-6 (tlS'o -age)+ bS: 27)~S Z> 1.04 -5.29861E-5 1.66 -3.96728E-6 9031. ) tc --~~~~ I<~% 13 '9 -6.33239E-6 -3.96728E-6 'TgF OPERATING DRIVE ROD STRESS AT A 477.198 F= -.~>~T)F = -~+ OPERATING DRIVE ROD STRESS AT B 821.458 OPERATING CYLINDER BRG PRESSURE -3.75613E-4 Fez. = l-i 4'3+T-F = Zdg OPERATING VALVE EAR TENSILE STR 1136.52 SNlr=f-"5'A t I~Sy .7> I+J~o>~7 (~5y t -'5 OPERATIl'lG VALVE EAR SHEAR STRES 89.1706 OPERATItlG EAR BOLT SHEAR STRESS '078.68 OPERATING EAR BOLT TEllSILE STR 525.595 = $ ZC PiT glc(i,j)= J=-S.29861E-5 ~ 1 Ml, due dc'uad tl>>>>dl~g= l~llakwr+-FST )pep fcdr = -1.22282E-2 Q(/~d ~g259 - d.>>. I r siga= -.267492 ~ r Zw (0 g lD':l Z.S si gb= .409114 Fc due to T3=-5.71181E rd'l>> du 8 (~A<>+Jl r 7')y+'1.!,(4l fii= 2.73638E-2 $ ~ (tJ>flit = f 22=-5. 85968E-2 4 ds a= . 071 5S2 dsr= 3.3257E+7 +gee ~ ~~~ 4>~ ~i.tg ~7.iz.~ c7i P5 dbten= 4.86604E+9 glc(i,j)= j=-6.33239E-6 2 TC TqL t)NP EAR E.~5tt.r- ~ASS= f cdr= -1.4614E-3 f2I. t++fZ'll=.II%I vS~II37 '.Qg siga= -3.19681E-2 sigb= -4.88934E-2 Fc due to T3= 321.752 f1 1 0' 43 (p)gg~ pAr E) Ctl Pc<@ p~ f 22= 33 . 082 'zri (u+ wvs) r, n>> la-~=as dsa= .072574 t5 dsr= 3.7607E+7 Ir dbten= 4.86759E+9 '(( 55: zs.z+ zn>> I oqw<r)/~='7I9 glc(i,j)= j= 1.04 3 fcdl = 240. 013 s i ga= 5250 . 28 s i qb=, 8029. 99 Fc due to T3= 919 516 ~ f11=-440.516 f22= 943.322 Ac.a= 2 PSr'REF+7 10CO 00 Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII '"'"'PP ss- E< c.- v Prepared By; / . Date 3w Subject -c Checked By: Date 'V.gI-( System gyp'~p 5 ZC44 Analysis No. Rev. No. Sheet No. M I lob - -Z CR KCK -X Q TEASDALE. O'T12$ )5 CALC 5: ~ ~ ~ 154 -,4-It, y~>o 4103 4c 3ZX 322 ~~it VS~at t" = ZO Fc 12 8 + ~>2 = /OHIO lr ~ gN Ec(<: Ftr., A2S.- lwgp ~o WIG ~ Nb~ ~cj2 ~q~~ +~ay ~~a+~ -. ~ I3 (I<<c tII 2.@03 g4 I 99+ I 4 + 3.5 + "12 << I '6 -5 ttQ o 4-0 vs O'Dz-o a t ChQCLg rove 5f t Sj:-Cg C.RSE P(gh.0 ~gTD 5$ h$ Qtt E:Is L$ Cij '- c(Q 9 & g VANE F~l t [ifdptji1 6 Sr@.=.&5 (cHtpa A)i"-!iTS ~l't i CM. BF, W 4i N t PI'4~7 Q j2$ +HhC.QQ L JVO~ ~gt~~I~tI ) fik,top I~I) sic--ss Q.f c.(9 (.Ho t ": topi l ) Sot- T w&H uiog C.H-C'<~ (Vd T >! A) ) I CC0.00 SECTlON 5.0 QZDI 361106 APPENDICES CONTENTS 5.1 Response Spectra 5.2 Walkdown Sheets 5.3 Valve Local Coordinate Systems 5-.4 aces IP~ (go~ruisrRAri Jw) 5.5 Final Pipe Mounted Equipment Response G-Levels Revision 3 Response Spectra C) C) D.. ~ ~ I C) I C3 l l ~ CD l I I I l I I I l C~ ~ I I tM ~ I I n rD I I ~ ~ LU I I j ~ ~ 'I ~. ~ la) ~ I~ (3~ l I l ( ) ~ ~~ I CL I Qj ll >'3 ' l I ~ I ~ ~ ~ I m prn 0N I ~ ~ I ftl I C l I I ~OP a I ~ r ~ 1 1 r I ~ o.oo. 2o.oo uo.oo eo.no 8o.oo ioo.oo . i2o.oo ><to.oo , 160.00 FREQUENCY (}IZ) IJf'f'SS BERCTCfR BLOG. SRSS CfF SRV SSE Rf'/CHUG..'f]SS. i'IO. 182 EL. 500 FT. HI3RIZ. TRANSt FITIQN . C5flfTflINf)EAT VESSEL OAHP ING= . 005, . 01, . 02.. 04 v ~ 5.2 Walkdown Sheets k ~ ~ ravw a VI r; )UIPMENT QUA3 3FI CA TIO" hAL1:DO')iN VERI' CATI Ol: 1'OR". '<Illllllilltllllllllllllllllll C)IDI I.,'.. l l '(- FLOOR EL )/;I ~>l.. / Q,f-L CONPOh'= N"T EL~it DSCRP . + ~ c ) U'/.Lv /. >:ODf 9-&-A SERIALS + i 3.~. PgrTsL > ~g ( f /'> PSI S 2r~ LBS (/r" SIZE CLASS A/r >='S)'.E r YOKE ORIENTATION NOUNTINC CONDITION TO AXIS OF PIPE ( ~ NO OF BOLTS ~V~ /fA // TO AXIS OF PIPE I ( g Q I( BOLT TYPE VELD TYPE 6 X,/J. SI ZE BOLT r/ YOKE LENGTHEN - 2 (FLANGE TO FLANGE) 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 )/ SECS c-" pp~ <'-- Ii,'Sp t. f. Co<< r'>Z),~ t GLOBAI, CO-ORDINATE VALVE STEM ORIENTATIOI): SYSTEM ERATOR ZP1 &~am~>> 1"D3'UFACTURER ~~Dr.L NO SEPIA NO SIZE ORDER NO ATTICH"";i ~)!: S= JOB NO.BcLQ-FILE NO.CKC~~ OP. EPN + $ /6 /7d//0 RA ~& Y~ UFACTURER SHEEVWO.iM I DEZ NO SERI',1 NO NO INS CLASS I-PHASE ( ) 3-PHASE ( } AC DC '"~NTS: Def inition (N/F = Not Founa) c'sP- ~ 4~-3 op pip~ jr~ +y+ &~~~'y~g~~ ~ow y4 L&K 7u ~h~pp/AJPf~A'T, .:P~ D BY/z 'ATE%/r'-, : (SIGNATURE) RIEYVED .BY W K (SI N .TUFE) DATE~~b'I /4 &au Yl'I)C .'f(, ) (b Calculation a.=='io, ta Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII "'""'k/t'ai+ Z Subtect Prepared By. ' -Jg<. 'i~J-., Date < Z7'i>". ~ yy i, +UALyCy 4 oo 'Ft. ~ter," .

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Systeth pp Re.No. 'Zddd AoelyseNog Q, ~i i y Sheet No. I,) Q <g Pe,~ ~f!iPh ~ teeo P gist'rgb~ te JQB HO.~~" gLE NO.>~V.Ol sHEEv No M~ Or ~I e I cJ e VC(tr PAL En/6(.8 ZEKrlo'J/.-A / tELb DKEy o~ (ioR ryrE Pv&osE of bEAc-<<.Jc, ooQsroyL ooyE'Jri'ryo y o g$ 1005 cc Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Prospect WPPSS Subiect Mechanica1 E uiomen a P~ o Prepared Bv'ate 1 zjrfiV~'-'-. Checked By. l I Date 24" Butter+1v Valves g System Job No File No, Anatvsrs No, Rev. No. Sheet No. 361106 I ~,, v 'A / Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Rroreer Pg~g)~rr Z J-llI;. ')y4'J- r:4ZrI < Subtect Checked By: Date F-Aij: b. Mc/A<( ) 'I """P Job ND. ~~ Flic No. Sheet No, Aoelye e No, Qyl+~ i@ Rer. No. C+gjP Ptp 4774CV. ftt'->'T gas r]O.ERMA r' FILSNO.~T'<<~ / ( sHEav xo.~>M ey I ~ i I/ ~ ',:>'0 di~IJ) 04 r I . I VCCriuC. Ci<6C.E. i 6<7/Kl A-/-. t leo& ZKr r EAI (iform r lIE iylrlfroE " I4R 4yErr Jro OIAEErfyyAyr oyfrE jyAA4 4 oo JAyy) 1C06 Oc "(.3U: Pl':ti . I ~va J V!' C)US.3.I F I CATI ON X E.;i i I CATI 01'OFJ l I"') o!',III)I!(",(I!Illlli ERNE (c j-'( QI D 3 ( l l 04. BLDG /(, FLOOR EL I (l COORDS R3 l ~.3 Cpl".PONENT EL ( 75 DSCRP 2'(" 6fLV KOD$ gab f} >D3C 5 SERIAL: 2R L 36- l MAT 'L PSI g oF LBS SiZE ASME CLASS }'OVE ORI ENTATI MOUNTING CONDI Tp pN Ol'P AXIS OF PIPE ( ) NP PF BOLTS // TO AXIS OF PIPE ( ) BOLT TY'PE HELD TYPE & SIZE BOLT ql 5'Ol:E L NGTH PIPZ (FLANGE Tp FLANGE) 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-ORDINATE VALVE STEM ORIENTATIpl)', SYSTEM PZRATOR ZPN iODEL Np MANUFACTURER SERIAL Np QW~~ ~ 3q p~ YPZ SIZE ORDER Np A77AC;- <<1" t>"g+) 1 JOB,'(O. ~O( 9 iOTOR EPN F)L= "NO.QTop /~ MANUFACTURER ~>-( SHE=-Y HO. ~ODZL NP SERIAL Np ID NO IWS CIASc I-PHASE ( ) 3-PHASE ( ) AC DC 6~ IiS~a~l~SWCT(O~ gSDS,HIE.ZIS7)<<. T.)<<c COMMENTS: Dcrinx~ioh'i/F = Bio~ FouTiP) ~ ~~ 'J4<'(J< ~4Th~ 5& gp<~~<Z 4 <<(vc. lrt4 5'4 0 i <<5 <<5 VI+(/ / I ,~i PREPARED BY .~///zp . 4 DATE -.~Ã REVIEWED BY 25 c)<< DATE 9/I< ( S I GNATURE ) (SI NYATURE) i/s/6 Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Pre~eee / Suolec: Checked By; J 6:Cubi'~ C~~iX'F~e8r o.. Systelll Job No. File No. Analysis No (.jl/'~ A zygo: +, //+BI Rev No. Sheet No. Z bg'2 l~ e 'h e eeeemereee CVGÃA e ge ATTACHi'~RF i'i!7 JOB NO.MQ~ RLE NO. QT.pic (.v~-) ., SHEET NO.S~+ Qcp ti' 0 circ. Oi:c@370/2 4,~Q(~L &cd~~ 'e zc "esp), i ,'.AIJ "~/ -,(,I I fE'L5 5KEe CEJ (rdE 'eiE&elSPd E de= e'd Je .JG ~~<V~'<OR d 6(e 4T4 i i Cd t OJr y EQ'lzi ..:.!'I QUALZ FZ CAYZ Oti 1; p~>>:Pi)'<;g'i V !,Z. j CA. I 9.'OP>'. ~ /<' F ll.".:l)l.".'i):".l;.:!!l.'l:!!ill( B D("- FLOOR EL COOM) S KFR COMPOENT EL 9 (IO oscar 2'(- Qk~~ h11OD Ti > -gab>GS SERI AL4 hUL rsz LBS SIKE AS1:E CLASS YOk: E'RZ Et A TATZ Oti hiOUb'TING CONDZ TI ON J TO FD:ZS OF PZPF ( ) NO OF BOLTS // TD A>:IS O. PIPE ( ) BOLT TYPE TYPE 6 SZ ZE BOLT q'ELD YOE;: LEti'GTH (FLAt"GL TO FLANGE) PIPE hiOUNTED YES ( } 1:O ( } PER! LRNEtilT OBSTRUCTION (hI THIN 2 ") YES ( ) NO ( ) IS COtiP BET4'EEN CONT & 1ST ANC (FULL 6 WAY ANC) YES ( ) NO ( ) DO 1/!ULTIPLE SUPPORTS EXIST BETWEEN CONT & COYiP YES ( ) NO ( ) GLOBAL CO-ORDZ t~!ATE VALVE STEY1 ORI ENTATZOt); SY STEYi PERATOF. EPN h~UFACTUREP CVG:; l~X! ':ODEL t'0 SERI AL NO ATTACHMENT SIZE 'g YPF ORDER NO 510.<~O FILE NO.~C)I. I/F COTOR EP ti Y~UFACTURER SHEET hlO. &Uk iODEL NO SERIAL NO D NO INS CLASS I-PHASE ( ) 3-PHASE ( ) AC DC COKA&tiTS: Defini tion '(tA'/F = Not Found) ('. 5p- L r~ - (. l, ~.4 PREPARED BY,'/~'w fgg~7 DP (/)g~"~z/zz(gA< (S /i~ I Gi'AT ~ D RE ) .. DATk IT sl4I 4irDD P - d4~ REVIEifED BY ZQ~T4 ( S a Gh i Gt'ATUP, ~<(- ) Wci'Zaa DATE 9('t fz g/s/b3 9o~ l<uz.. Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII l;'iJ ' Prolec:, x Prepared By J'/lA ~ ".. /i~ Dare r'2- ZR r"Z-Sub!eel Checked By -(ill-: &'uf> i ir eiof Job No, File No. EE'0/c LS r Analysis No A 1"r,~+ Rev. No. Shee! No. wVc Il0(o ~ g A7TACH "~"',:Yr7 JOB NO. ~chO~I FILE NO.~OWO F sHE~w No..h >M "--~/ -<<~ ~*~~~ <<~O ~ l'j ~.p f lKLd /ger Q,g r % if PClg+C)5C Dr DCPidrigg dP'ZdATbQ. OgrggrA rra,g Or Jr') 'IOQ6 0c I EQU1 PMENT OUhl F1 CAT1 VERI F1 CAT1 Ol'OR.'l Ol'ALKDO'v'K S.=-, 'j,.; c a,:i c', EPNf <lllllllllllllllllllllllllllll PI Di 3Q 'l I 0(,. BLDG FLOOR EL f+ I COORDS Me l 5'. I liFR Q ff- CONPONENP EL~o DSCRP L "I " FL-'( NOD$ Q ~ +45 SERIAL, YiAT'L PSI 6 SIZE ASl"iE CLASS YOKE ORIENTATION YiOUNTIN G COND I T1 ON J TO AXIS OF PIPE ( ) NO OF BOLTS // TO AXIS OF PIPE ( ) BOLT TYPE VELD TYPE a SIZE BOLT P YOKE LENGTH (FLANGE TO FLANGE) PI PZ r >lOUNTED YES ( ) NO ( ) PERMANENT OBSTRUCTION (WITHIN 2 " ) YES ( ) NO ( ) IS COMP BETWEEN CONT & 1ST ANC (FULL 6 NAY ANC) YES ( ) NO ( ) DO MULTIPLE SUPPORTS EXI ST BETWEEN CONT 6 COMP YES ( ) l'0 ( ) GLOBAL CO-ORDINATE VALVE STEYi ORI ENTATIOK SYSTEM PE PATOR EPN YiANUFACTURER ATTAC~I:83KNT ~ODYL ho SERIAL NO aOa WO.MQ~9 YPE SIZE ORDER NO PiL-NO.~iDl. i t SsaSY Wo.~ iOTOR EPN MANUFACTURER lODEL NO SERIAL NO D NO INS CLASS I-PHASE ( ) 3-PHASE ( ) AC DC C0~1YiENTS: Definition '(N jF = Not Founc) .< -/~ /s-- I PPEPARED By ir.jul, . 8 r p, DAIEPI~P RE'KrIFN-ED BY DATE ~lU~2. (SI GNATURE) (SIGKATURE) Q,.q W.~ i i u uii i;i t5 a t.luaal t t '/5'2'J t.th V5ALk;DO';) VERI F 3 CATI 0)'OR"'. )w' g t', " / illlf)llli!llllltll)llllllll)l -;.lit 5, 1 l FLOOi; EL COORDS 4 ~ /:Q'i~

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'.',,:.,-'7 or cl i ., g,-5 A'SCRP POD' SERIAL; )J T'1 -/t -~ ' =/' >i PSI g 77> 'F LBS 4 /F-" SI ZE I ASME CLASS 'r'./-. YOk'E ORI ENTATIOK MOUNTING CONDI TI ON J TO JD IS OF PIPE ( Q NO OF BOLTS TO AXIS OF PIPE ( 9 BOLT TYPE / '~'OLT g. / ~g/ KELD TYPE cZZE 'n c g YOk;E LENGTH c.- - ',.' (FLANGE TO FLANGE) PIPE MOUNTED YES (~ ( ) PERMi(iNENT OBSTRUCTION (WITHIN 2 ") YES ( ) NO ( Q IS COMiP BETi>EEN CONT 6 1ST ANC (FULL 6 NAY ANC) YES Q NO DO MULTIPLE SUPPORTS EXIST BETWEEN CONT 6 COMP YES ( ( ) NO ( ( ~ ) GLOBAL CO-ORDINATE VALVE .STEMi ORIENTATION( SYSTEM PERRTOR EPll +/A ~~'F ~ C T URER ODEL NO SERIF'. NO ATTACi c L9.- tdT YPE SI ZE ORDER NO JOB NO. GRQ~~ PiLERO.O~>>> ~ .')OTOR EPN h// kiANUFACTURER SHEET NO. ~+ 'iODEL NO SERIAL NO D 4'O INS CLASS 3-PHASk ( ) 3-PHASE ( ) AC DC CO! "<iENTS: Def ini tion '()i/F = Not Founa ) C EP- iuS-3A g Q~ zdeez zo< z FoE o~g~g~g ag,t<JTQT'Igg PREPARED BY g . r~ (SIGNATURE) 7/~/' ATE'r, ZRZVIEl; ED BY (ci+G,.< TDR-.) D%TE ~l 'I4 'L),'7rv- Calculation Sheet II!>tIII!IIIII!l!IIIIIII!llll! Ptlta' Date p5, pr g. gp Z C(gpskp v Ao Ct>ec>'ec Bt, ' I ~P'A< / Date i '<'/8c c. Svs'e". Joo No F>le No, t sP E)Z t>a,;s s t!o Rev No St>eet No ~~'V '~ M:5 tJJALI'; OWP 97,!. tJ ". g 0<'f.t.'A~.) f; O'- I> PZ/ "ted'. CEP V" 3A Voa I >O.3QWM ~~ 4R eILE No. ~O ~ NO.~ ~t'HEET c~f -u- ~A-rn 0 P 4 M I i ~ ~ ~ ~ lllllllillilllilillliiiii! 3! l: C'2 a': 'I'..5 IS.5 MFR $T t-1 LOUR COh.'PONE!i"" EL i'l5 COORDS DSCRP 2 'zg -"li NOD j u R5>SERik'- tJ PP h~hT'L SA - 5 l( SIC ssz g Lss~d F szzs 2 'I ASME CLASS 5 ORE ORI EN ~ ' Ol 2'.OUNTihG COND'i Oh TO FDli S O. PIPE ( hO OF BOLTS Pr j/ro x>:z o.- ':rs (~) BO' TYPE V;ELD TYPE 6 SIZE BOLT - 9 g A VA YORE I EN.C- ".:: 0 PIPE MOUNTED YES(~)'NO ( ) (FLANGE Ti l L2 NGE) PEE~~iANENT OBS: i"'~TION (WITHIN 2" ) YES ( ) NO ( IS COMiP BETNE'ONT 6 1ST ANC (FULL 6 NAY ANC) YES ( ) HO ( ) DO MULTIPLE Si." ORTS EXIST BE&a'iEEN CONT & C MP YES ( ) NO ( '9s v GLOBAL CO-OJ.:?:ATE VALVE STEMi SYSTEh! ORIENTATIOY'ANUFACTURER PERATOR EPN 'iODEL NO SERiAL pTTa m 'll, gl~ NO YPE Si ZE ORDER NO OTOR EPN Y~ UFACTURER Jps sp.BR099 PlLE gO SHRIFT ~ RO.QW&l I iODEL NO SERIAL NO D NO s ( ~ z-~ssss ~ ~ t DC COl&KNTS: Deg i ~i tiori (N/F = Not Founa) ~ 4 ~<8 jb 5gp<7.Zo+ Z. CC 8 GDG24TDR, 0<(MV Al ibd / PREPARED BY r'... (S GNATUFZ ) '- >>T-, I GNATUR: ) DATE ' >iltz (S ~l ge i C'VC Calculation I ~ Sheet lllllllllllllllllilllll! Illlll Protect SobleCt System N 4t'5 Ec i<. Preoa ec By Ctrectiec By Joe No ~ h /'i ~l"'A< File No 5ate 5ate r 8 ZC'/Sic 2 csP 52 Aitatysrs No Rev No Stree! No. C 'f o 't r i ill%>> ATTACH'"'s't=N7 JOB HO. WRGdM FILE NC.~~ cE( -J - ='.A . SHE TNO ~l I 5.3 Valve Local Coordinate Systems CSP-V-3 CSP-V-4 CSP-V-5 CSP-V-6 'I prig-e~~ c~ p~ p>~> p ~r> y ~p~~+v '~lit /Y~ ~SR-i-s 4:-:~~., li N 'I r AI4 Cy'6/~IGNI? I&"l9PC)5= i g C.dez,'c ~~ Od rc c-r~lr~ / -'- CyS i ~/4 I . 4K=v ~ @gz( Ms@,<<=.,O ecs @gal-,-. -l 0 gg 4,-,: ISo'5tg~g -/ . I 8sE5gz= D 8 fE Bi~= 9d.'rse..= a'g~ / = ~< >vs= < 0~5vs= Q g:-. ><a.8~ t [gQ piQ M 0~7gL'$7;0.$ Csf-- /- > f-Qi b ~zP C,r'~/ ~: RF')(E~> < ~ ~d, /li(4 l. Dp~w i dg f+kdSPOSC Td C.dCA 4YS( <,v/ SAA~7 oP 8~ = 4Z~/z.',= Q~s 8<, - d.731 4>i." Gas <z= Q.( 7g e,= 5c'"3 ebs 8<q= ., = 4'l/z.'= dos 4~i-(Bl< ~~z= c)~~7 Cosd~= 5 QOSqg = Q <~S&vz= Q l eas4g, = I r'$ oslo ~S .-I~=.~o.CKc~~~ S~~" hO.M ~ kv I c <4- ~/-5 . -rFgcb Ig/, ~,.'.'. >

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I ~ I April 29, 1983 1 I DRifP-83-07 0 ~ N I !ir. L. T. Harrold ~ ., '@~i" Assistant Director ""'r'-.p'~'~'.~i.."Washington Public Po~<er Supp ly System A~@,OH<Dr.i'd% , ~ iI~ I .."-s=.",.;.:",9'r -" 3000 George Washington May Pichland, Washington 99352 JO B HO. ~~ I Ir. B. A. kfolmberg FILE I40.~ gp. oi, r-EHEET IIO.

~~"i'-", . ".~~
~~References:~~
(a) WPBR-03-17, dated 3/16/8 3 . (b) WPBR-83-20, dated 4/12/83. vP cq~ ~ (c) f&HR-83-29, dated 4/12/83. Ih (d) Telecopy, B. A. Holmberg to 0
~ F,,'E r$ N'r J. J. Verderber, dated 4/4/03; Gentlemens 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 furth r if efforts should be r."+de to rec1uce accelerations .'.",.'ffice Very truly yours, ORIG,~L SIC~rICO GY 3 3 ~r~DEASEP John J. Verderber Project Fngineering Manager CC: Hr. W. S. Chin BPA 1 r/1 QHr. J. 7.'. Rhodes - WPPSS 1 ~;/1
~~p. Buck 5"Ep~~rop ~r75 i Ebi~~~~
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ATTACHMENT Data forwarded with BRWP-83-078, dated April 29, 1983 Valve I Kale. No. CSP-V-1 125 8. 14 . 129 CSP-V-2 '25
8. 14 .129 CSP-V-3 125 8.14 .129 CSP-V-4 125 8. 14 .129 CSP-V-5 125 8.14 .129 RCXC-V-31 107 8.14 .112A RHR-V-17B 31 8.14 ..121 RHR-V-53A 29 8.14 .62C RHR-V-53B 31 8.14 .121B
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QZDg 361106 7.0 TRANSMITTAL, PREOR CALCULATlONS AND REPORTS CONTENTS 7.1 Communication Reports 7.2 Old Requalification and SQRT Forms 7.3 BIF Report: Dynamic Torque Calculations of Butterfly Valve (Excerpt)
~~~~7.4 McPherson Associates Report:~~~~
Design and Sei'smic Analysis of 24" Cylinder-Operated Butterfly Valve. (Excerpt) *
NOTE 1 See Cygna Energy Services Project File; "Equipment Seismic and Hydrodynamic for 24" Cylinder Operated Butterfly 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 BIF D-207110-H Rev B D-207110-G Rev A A-206767 Rev C Bovee 6 Crail CSP-807-8.10 Rev 4 CSP-809-1.2 Rev 4 CEP-625-3.4 Rev 6 CEP-625-1.2 Rev 3
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QIDN 361106 7.1 Communication Reports a Correspondence
it 1 Communications Report llllllllllllllllllllllllllllll Company: C BS'elecon 0 Conference Report Project: Job No. Date: f3
~~~~Subject:~~~~
~~~~Time: jl- tUK I AC. StOQ5 Place: g g~~~~~
~~~~Participants:~~~~
of C 4-gb-CP p-Item Comments Req'd Action 8y z./ tot F+ j 5iF .VA4V E FL AQ &6 Pie&,N sion s 4 'gtc,~~ Z.iz.S
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ATTACHMENT JO8 HO.SI ilLE NO. ~+. SH"=Bi NO.~7' I Signed: Page of Distribution:
Washington Public Power Supply System P.Q. Boy.968 3030Georae Washington Way Richland, SVashtnoton 99352 (509) 372-5000 December 17, 1982 GE-02-RWH-82-018 Cygna Energy Services 141 Battery Street Suite 400 San Francisco, CA 94111 Attention: Hr. T. Wittig, Project thanager
~~~~Subject:~~~~
~~~~NUCLEAR PROJECT 2 CONTRACT C-0892~~~~
'l Investigation of the CSB and CEB systems shows that during a dynamic event the systems are not degraded in any way by the butterfly valves fluttering. Therefore, all work on Work Release Nos. 14 and 17 which address valve stability should be terminated.
R. W. Hickman - 575 Senior Engineer, Equipment qualification RWH/sms cc: F. Khanachet, Cygna Richland R ECElVED Joe ~O.~' L'=Can j982 FILE NO.~ slRET No' CYG<<'A-RICHLAND
Communications Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII CR-030 company: CES X3 Teiecon O Conierence Report Project: 82044 WPPSS 7 29 82
~~~~Subject:~~~~
~~~~Time: 9:40 A.M.~~~~
~~~~Participants:~~~~
/ID 361110 - 18" BUTTERFLY VALVE R 'DAO Dick Hickman I Supply System Hal Reeser oi CES, SDAO ot Comments Req'd Action By I called Dick re. dynamic instability of BIF valve while in open 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 analysis of the valves and flag the dynamic instability issue as a separate subject that will require Supply System action for resolution. o Supply System has granted a contract to BIF for operability studies on their valves. The contract admistrator at BIF is John McDonald (401/885-1000). Our action should be to determine the scope of the BIF study and to make certain H. Abolhoda that we do not overlap our efforts with theirs. Also we shouId attempt to assure~hat our work does not conflict with the BIF effort. o Dick said we may contact GE direct. Our contact at GE for MD Rajan* the decision on faulted or upset allowables is: Arian DeVault (408/925-2208).
*ACTION: Rajan, this resolution should be documented via revised criteria in our Project Manual.
~~~~pTT qCI;MEINT IO'0 DT.rst F FILE HO. 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)~~
Communications Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII CR-027 Company: XI Telecon 0 Conference Report Project: sob wo 92OQ6 WPPSS Date: 7/20/82 sttbject: Time: P.M ~ APPLICABILITY OF HYDRODYNAMIC LOADS Piece: SDAO
~~~~Participants:~~~~
W. Schlafer of CES, SDAO H. Reeser CES, RBO of of Item Comments Req'd Action By The Hydrodynamic Load Column in the WPPSS SRM list is known to have errors. A "non listing is not to be trusted.
2. For packages in analysis Cygna will trace down the P 8 ID to determine the applicability of hydrodynamic loads to line mounted equipment.

3. To accomplish this, Cygna will: GNA Al AC HM:-H

a. Check the line routing to.see if it penetrates the fuff rI.
~~~~"I'.~~~~
~~~~primary containment. If not, hydrodynamic loads do op.o i. I-not apply. Rt.E O.~~~~
~~~~b. If the line penetrates the primary. containment, hydro-SHE NO.Z.I~~~~~
~~~~dynamic loads will apply unless:~~~~
1. An anchor point appears first in that line, or

2. The line first connects with floor mounted equipment outside the, primary containment and it is sufficiently sturdy to eliminate the propagation of pipe line hydrodynamic loads beyond it.
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 final piping analysis and examine actual pipe accelerations. WS/sak W. Schlafer Page of L. Kammerzell, J. Read, P. Guglielmino, J. Minichiello, P. Patel, M. Rajan, 1020.00 H. Abolhoda,~RE~ P. Curry, H. Reeser, T. Wittig, F. Khanachet
Communications l j s j Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII CR-027 Company: CES Telecon 0 Conference Report project: Job No. WPPSS Date:
~~~~Subject:~~~~
~~~~Time: APPLICABILITY OF HYDRODYNAMIC LOADS Place:~~~~
~~~~Participants:~~~~
~~~~of of of Item Comments Req'd Action By~~~~
5. For packages whose analysis is complete and where hydrodynamic loads 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 a memo 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 is required.
~~~~p "t'gP CH iOB<<.~ Fas<<~~~~
~~~~~gFP~ ~~~~~
~~~~V'r.~I ho.~~~~~
~~~~~ f signed: W. Schl a fer Page of Distribution:~~~~
1020 00
Communications Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII CR-023 Company: g) Telecon 0 Conference Report project: 82046 WPPSS Jul 20 1982
~~~~Subject:~~~~
~~~~Time: Hydrodynamic Loads g A~ San Dieao~~~~
~~~~Participants:~~~~
J. Minnachiello of F of of Item . Comments Req'd Action By 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.
2. One should use 1.5X peak acceleration unless the system frequency (line plus equipment) indicates otherwise.

3. If the equipment satisfies the allowable stress limits, then one should perform fatigue analysis using the fatigue design curves given for Class components. To calculate the 1
fatigue damage for normal operation (excluding all dynamic events) one might take a conservative approach by assuming the calculated stresses are equal to the allowable stress limits. f f(>> r 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. Curry 1020 00
~~~~-'IF July 7, 1982 CYGAA Sygna Energy Service .IOB XO. ~~<<~~~~
~~~~225 Stevens Street 0 o( C Solana Beach, CA 92075 "Bill" Schlafer PILE VQ SHEET HO. ~~ ~ I I V Attention: Mr.~~~~
~~~~Subject:~~~~
~~~~Butterfly Valves for Nuclear Applications with IEEE Qualification Requirements~~~~
~~~~Dear Sir:~~~~
~~~~This information is provided in response to your recent phone call.~~~~
l. Enclosed please find some catalog information describing BIF's line of butterfly valves, including our current models as well as our new Model 0668 design (which will shortly 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 (which did not require IEEE qualifications) with valves and oper-ators that are fully qualified to IEEE-382-1972, IEEE-323-1971 and IEEE-344-1975 is almost impossible to obtain prices from IEEE quali ied 't actuator vendors without a detailed specification showing exactly what is required; therefore, these are our best guestimates of what the replacements would cost. They could be high or low by 10 to 20$ , depending upon the wording used in the engineer's resultant specification.
Replacements for Valves Furnished Ori inall on N-27232 14 18" BV's with electric oper- $ 40,000 ea. if qty. ators (See NODS ll/1/79) or $ 25,000 ea. if qty. Re lacements for Valves Furnished'Ori inall on N-27233 2 18" BV's with spring to cylinder operators
~~~~~o en $ 60,000 or q45,000 ea.~~~~
~~~~ea. if if qty. qty.~~~~
", 600 OI VISION ROAD ~ WEST WARWICK,RI 02893 BOX 21 7 ~ ~ ~01.885.1000 CABLE: BIFWRWKRI TWX 710.382 0402 ~ ~ ELFX 827 631
Sygna Energy Service July 7, 1982 Page 2 Replacements for Valves Furnished Ori inall on N-27234 4 30" BV's with spring cylinder operators to close $ 75,000 or 660,000 ea. ea. if sty. if qty. Replacements for Valves Furnished Ori inall on N-27235 4 24" BV' with spring to close cylinder operators
~~~~$ 60,000 or 550,000 ea.~~~~
~~~~ea. if sty. if qty. Re lacements for Valves Furnished Ori inall on N-27236 3 24" BV's with spring to ~o en cylinder operators~~~~
~~~~$ 60,000 or $ 50,000 ea.~~~~
ea. if sty. if sty. Ne trust that this information will be of some help to you, and are sorry that our prices cannot be more precise. Sincerely, eorge E. Sayer BV Sales Applications Engineer
~~~~Enclosures:~~~~
650.20-4 BPD-668-45-1 BPD-668-1 NODS-1 1 /1 /7 9 ATTACH[.hler"MY JOB BO. or f2oqg'ILE FIG. sI p BHB:T FIG. I 5
BUTTERFI Q, VALVES. MODEL '6C8 l2 .'2+ THRU SHAFT PARTS . A ottt: or cattaaat. stcam coaaoaaztott a I2 7 II
+ IS ITEM 22 IIEET 2 3 WECHANCZLLV RrraIHED ADJuSTABLE SHRUNK f. SEALED SEAl ~ IIELD IRREPLACEABLE WITHCUT . 8 WITII LOCKTITE REHovWG VALVE mom PIPE LWE.
~~~~3 ~ tT EM 5 SECURED WITH 5 wvLott IHsetar~~~~
..SECT ION A-A ALTERNATE AOJUSTABLE VEE PACKING 'ATERIAL MATER I AL VALVE BODY CAST IRON ASTM AI26 CL B RUBBER SEAT BUNA-N ASTM 02000 CLAMP I NG R I NG TYPE 304 ST. ST'L CLAMP ING R ING LOCK TYPE 304 ST. ST'L HALF DOG POINT SET SCREW TYPE 304 ST. ST'L SHAFT BEARING REINFORCED TEFLON BRZ OR PHENOLIC BACKED STUFFING BOX PACKING VEE P ACKING BUNA-N STUFFING BOX GLAND CAST BRONZE ASTM B62 HFX HEAD CAP SCREW TYPE 304 ST. ST' IO OPERATOR SHAFT TYPE 304 ST. ST'L HAt F DOG POIhll SET SCREW TYPE 304 ST.- ST'L I2 YALYE DISC CAST IRON ASTM A48 CL40 OR DUCTILE I RON ASTM A536 GR. 65-45-12 WASHER TYPE I8-8 ST.ST'L l4 DISC P IN TYPE 304 ST.ST'L l5 KEY ST'L l6 HEX NUT TYPE 304 ST. ST'L l7 THRUST COLLAR TYPE 303 ST. ST'L I8 THRUST BEAR ING COVER CAST IRON AS Tidal AI26 CL B HEX HEAD CAP SCREW TYPE 304 ST. ST'L 20 0-R ING BUNA-N THRUST BEAR ING RE I NFOR CED TEFLON 22 DISC SEATING RING TYPE 3IG ST ST'L Al TA CHMEI~T 7-r-82 METERS-FEEOERS~ONTROI S BPD 668 rS-l
AWWA BUTTERFLY VALVES MODEL' 0668 30" THRU l20 A UNIT OF GENERAL SIGNAL ~ ~ PARTS ITEM 5 SECURED 5 WITH NYLOK 7 INSERT 19 2 l2 05 a I 15 XKZXlL THRUST ADJUST-MENT PARTS" l3 6 II MECHANICALLY RETAINED ADJUSTABLE SEAT F I ELD R EP LACEABLE Wl TH OUT R EMO V I N G VALVE FR OM P I P E LINE '(FOR 30'HRU TEM 2 I VALVE BODY RUBBER SEAT 48'.V) MATER I AL
~~~~'FOR ITEM 27 HEAT SHRUNK AND SEALED WITH LOCKTITE CAS T I MATERIAL czuuLJLa 54'HRU l20'.V;)'~~~~
~~~~RON AS Tidal Al 26 CL B BUNA-iV AS TiVI 02000 ~ 3 CLAMP ING R ING TYPE 304 ST. ST'L~~~~
.4 CLAMP I NG R ING LOCK TYPE 304 ST. ST'L 5 HALF DOG POINT SET SCREW TYPE 304 .ST. ST'L 6 SHAFT BEARING REIN ORCED TEFLON BRZ OR PHENOLIC BACKED 7 STUFF IN G BOX P ACKI NG VEE P ACK I NG BUiVA-N 8 STUFFING BOX GLAND CAST BRONZE ASTi'A B62 9 HEX HEAD CAP SCREW TYPE 304 ST: ST'L IO OPERATOR SH P,.=T TYPE 304 ST. ST'L II STU HA T TYPE 304 ST. ST'L l2 VALVE DISC GAST IRON ASTM A48 CL40 OR DUCTILE IROI'I ASTiil A536 GR. 65-45-12 '3 WASHER TYPE l8-8 ST.ST'L I4 DISC P IN TYPE 304 ST.ST'L I5 KEY ST'L l6 HEX. NUT TYPE 304 ST. ST'L l7 THRUST COLLAR TYPE 303 ST. ST'L I8 THRUST BEARING'OVER CAST IRON ASTM AI26 CL B I9 HEX HEAD CAP SC EW TYPE 304 ST. ST'L 20 0-R I NG BUNA-N 2I THRUST BEAR ING P. E I NFOR CED TEFLON P HENOL I C B ACKED 22 THRUST ADJUSTING SCREW TYPE 304 ST. ST'L 23 JAM NUT TYPE 304 ST. ST'L 24 THRUST BEAR ING PLATE STEEL ASTM A36 25 SEAL S ILICOI'IE RUBBER 26 HEX HEAD CAP SCREW T'(PE 304 ST. ST'L Ml %1>>
~~~~27 SEATING EDGF '(PE 3I6 ST.ST'L I-I5-82 JO Fll.gag ~o7. SiiE~,'i0.7'I:~~~~
~~~~~lo.~~~~
~~~~MEYERS-FEEDERS~ONTROLS SPD-668-I~~~~
~~~~/ .>~~~~
~~~~y LIMtrpttpuz~~~~
~~~~,i j,,:~>' 1. /~~~~
k~<. (~i ~~,:., ',":;, sMaPL %ha~ LIMITORQUE CORPORATION ~ P. O. BOX 11318 ~ LYNCHBURG, VIRGINIA 24506 IEEE 323 (1974) and IEEE 382 (1972) NUCLEAR QUAUFICATION DATA FOR SAFETY RELATED SERVICE THREE PHASE ONLY D.C. Nuclear Containment Outside Containment Containment-Inside or Outside (See Option 8 Price Adders) (Standard Prices) tt (See Option 8 Price Adders) Design Life 40 years (2000 cycles) 40 years (2000 40 years (2000 cycles)'20'F cycles)'20'F Ambient Temperature 140'F (Continuous) Ambient Humidity 60.100% 30 100% 30.100% Aging Motor Stator only Entire Unit Motor Armature, Field 180'C tor 100 hours 165'F for 200 hours at 'oils, 8, Brush Box only 100% relative humidity 180'C for 100 hours Total Radiation 2.04x10'ads 2x10'ads 1.0x10'ads (40 yrs, Integrated) Seismic Rof: IEEE344 " "6.0 g's
~~~~""6.0 3.0 g's (SMB/SB)~~~~
~~~~(SMB/HBC) ~~~~~~~
~~~~~~~~~~~~
~~~~6.0 g's (SMB/SB) 3.0 g's (SMB/HBC) ""'3.0 t6.0 g's (SMB/SB) g's (SMB/HBC) g's (SMB/HBC) 6.0 g's (SMB/HBC) 6.0 g's (SMB/HBC)~~~~
~~~~'mber of transients I'ransient Temperature 340'F (BWR) 250'F 340'F 300'F (PWR)~~~~
Test Humidity 100% (saturated) 100% (saturated) 100% (saturat Profile PWR/IEEE382 73, ANSI (yot to be published) Special Page 12, Table 1 BWR/IEEE382.73, )~77ACHK~E~t 7 Page 12, Table 2 Length ot Test 30 Days 15 Days 25 Hours Completed Test Date PWR-September 1974 February 1975 October 31, 19 (600456) (600461) (80009) BWR-September 1972 (6000376)
~~~~'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 were added 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's hOrizontal. Since no cross coupling was noted between axes, the test qualities the SMB/SB to 6.0 g's In both vertical and horizontal axis. Maximum g level dwells ln each of the three axes qualify the units tor any mounting position. (Seismic Qualification 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 their similarity to the SMB actuator. NODS ~ 11/'I/79
Communications Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Company: CES M Telecon 0 Conference Report Project: WPPSS 82046/CR-019 Date: 7/] /8 Hydrodynamic Loads for Line Time: Subject.'articipants: Mounted Equipment SDAO Harkness of Bechtel Norwalk CA W. Schlafer CESi SDAO of Item Comments Req'd Action By Callid the Seismic Qualification Working Group to determine their current criteria for line mounted equipment subjected to hydrodynamic loads.
~~~~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 Octave Intervals from 1 to .200 Hertz >each for 15 seconds at 6.0 g. b) Two OBE + SRV Events: Required Input Motion (RIM) of two sine sweeps at 1 Octave/Minute from 2 to 200 to 2 Hertz at 2/3*6.0 g = 4.0 g. c) In-Plant Vibration: Required Input Motion of sine sweep testing at 2 Octaves/Minute from 5 to 200 to 5Hertz for 90 minutes at .75 g.
3. This type of environment is distinctly more severe and more correct than that proposed in the NPPSS interim dynamics criteria memo 5 856. Eventually WPPSS will need to be informed of curren practice such as this.
~~~~'ry ACHMENT JOB NO.~~~~
~~~~FiLS NO. Df.o(.F SHE"-T NO.~I'~ WS:lgn W. Schlafer Page 1 of 1~~~~
~~~~'"" "" "Messrs. Eammerzell, Read, Reeser, Nittig, Minichiello, Guglz.elms.no, Bosch, ~~eh Patel, Ra jan, Abol oaa r urry~~~~
Communications Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Company: CES i5 Telecon 0 Conference Report Project: Job No 82046/CR-018 WPPSS Date: 6/29/82
~~~~Subject:~~~~
~~~~EQ of BIF Butterfly Valves 12205 QID 361104, 361106 Place: SDAO~~~~
~~~~Participants:~~~~
of John Henry of John Henry Associates of Item Comments Req'd Action By Called John Henry because he was the engineer who approved the original seismic calculations for BIF Butterfly Valves.
~~2. His recollection of these analyses was vague but did mention they, as consulting engineers, never tried to assure operability. Operability was the manufacturer's responsibility.~~
\
~~~~3. He recommended testing a similar valve.~~~~
g, I, ACHI~.EElA~ ! JQS NO. SS.=- HO.~>." SHEET NO. BS:lgn Signed Bill Schlafer Page 1 of L. Eammerzell, J. Read, H. Abolhoda, 222~gsj~~ P. Patel, P. Curry 1020.00
Communications 2 r Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Company: CES tK Telecon 0 Conference Report Project: 82046 CR017 NPPSS 6/29/82
~~~~Subject:~~~~
~~~~Time: EQ of BIF Butterfly Valves a.m. QID 361104, 361106 Place: SDAO~~~~
~~~~Participants:~~~~
Bill Schlafer of CES S George Sayer BIF, 401-885-1000 of of Item Comments Req'd Action By Called George Sayer, the BIF sales agent to get a budget price for BIF 18", 24nr 30" air-operated butterfly valves and an 18" motor actuated butterfly valve. These valves are similar to ones in WPPSS QID files but do not use the same air-actu ators. The original BIF valve serial numbers (for reference) are N-27234-F, N-27235-F, N-27236-F and N-27232-1.
~~~~2. He required a few days to work out also send descriptive brochures.~~~~
~~~~a price and will C v G ~g 'Q~~~~
~~~~.q"pAr HMb MT JOB HO )go~~~~~
FlLs NO. Oyo(.F SH=aV NO.~I BS:lgn Bill Schlafer Page 1 of P. Patel, P. Curry 1020 00
Communications Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Company: CES H Teiecon o Conference Report Project: 82046/CR016 WPPSS Date: 6/29/82 EQ of BXF Butterfly Valves QID 761104, 361106 Piace: SDAO
'Bill Schlafer of CES, SDAO Allan Berger BIF 401-885-1000 of of'tem Comments Req'd Action By Called Allan Berger, a BIF engineer, to get technical drawings for the 18", 24" and 30" air-operated butterfly valve actuators.
2. Requested drawings of Miller air cylinders showing details of a) Cylinder dimensions b) Piston dimensions c) Rod/piston connections

3. Conversation indicated a) There is a bearing and seal around the piston rod where it exits the cylinder b) The piston rod fits through a clearance hole in the, piston and is bolted on.
c) No seismic functional tests have been done on fargo~ the Miller air cylinder d) For dimensional data to verify functional operability of the motor actuated valve, con-tact Limitorque in Lynchburg, Vir Q~/GNA
~~~~,.~T-,;gHMENT BS:lgn JOB NO.~r pf'.ol.F rlLP. FIO.~~~~
GHEKT NO. ZL Bill Schlafer Page 1 of 1 Distribution; L. Kammerzell, J. Read, H. Abolhoda~"H+Xe , P. Patel, P. Curr 10t0 00
Memorandum PROJECT MEMO: ~P IIIIIIIIIIIIIIIIIIIIIIIIIIIIII
~~~~~.Oc (~~~~
~~~~To: gg/ C Oate: From: Job No: 82046 NPPSS~~~~
~~~~Subject:~~~~
~~~~MISSING DATA REQUEST 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'/,r C~ 8 - > t'/ ~ - ~- (Cl Pp/5 tI,,I . JOB tqp FIl.E tqO. 0T',o(.F: SHEc=.T gO ~~~( NOTE: Please sign and return the attached copy of as acknowledgement of receipt of this memo. this memora~ THANK YOU. ~ Received by: Date Received:
Memorandum IIIIIIIIIIIIIIIIIIIIIIIIIIIIII P . Gugl i elmi no To: June 17 , 19 8 2 J . Ni n i ch i ell o>, W. Schlafer, PZ.'atel 82046/SDM-003
~~~~Subject:~~~~
opies: Analysis for Operabil tyT+>t HgEpT L. Kammerzell J. Read JOB NO.~~ H. Reeser FiLK RO.~ or~I I: G. Shipway T. Wittig (Wyle) gHEEY NQ. Project File ln order to assess operability by analysis of mechanical equipment which can be modelled to correctly predict its stress 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 the seismic in Group II is expected to perform during and/or hydrodynamic event then the following requirements shall be met: I (1) Elastic displacement calculations shall be performed to assure non-interference between mating parts, and (2) The calculated stresses shall be within the allowable stress limits. If the calculated stresses for any service loading are such that permanent deformations might have occurred due to high allowable stress limits, a displacement analysis as in (3) shall be performed. (3) A comprehensive elastic-plastic analysis should be conducted in these cases to assure non-interference between between mating parts. For an equipment in Group I which is expected to operate after the seismic and/or hydrodynamic event then the following requirements shall be met: (4) Total stresses in the part must be limited to a yield strength of the material, OR
~~~~'(5) Satisfy the requirements of Group II equipment.~~~~
WS:lgn
Communications s =si r Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Company: 8 Telecon 0 Conference Report Project: 82046/CR-014 WPPSS Date 6/16/82
~~~~Subject:~~~~
Wyle Data Bank Time: a.m. Place: ParticiPants: W. Schla fer CES, SDAO of G. Shipway Wyle, Norco of'f Item Comments Req'd Action By Asked George to initiate a search in their testing data bank for seismic or seismic/hydrodynamic tests 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 those butterfly valves experiencing the extended fre-quency range of the hydrodynamic event.
~~~~P.TT A C'r'hi=I"~~~~
~~~~'S:lgn Signed:~~~~
~~~~W.Schlafer Page of Distribution: L. Eammerzell, J. Read, H. A o o a, . see, roy ect: 3.J.e~~~~
~~~~;:-"; EC '.- I V",= D Communications Report 4 4 C J I c llllllllj!I!ill!!!!Illllllll gfJI'1 fy d~~~~
~~~~(~~~ e~'~~~~~
~~~~',ttr-( -"~~~~
is~ P I"tI'~l f Company Telecon 0 Conference Report I r nw Itiv1 > Profe ! kauipfttent Seismic/Hydrodynamic ~ Requalifi- ~ ~
~~~~'2044 Job No.~~~~
r gati 6./1 5/8 2 Subject Interim Dynamic Loads C 1 1 00 Participants' Pwticit o r Jim Foreman ri ro man JoBNo FiLE
~
No.~~'ime Nylen 4 of of of Richland Office Laboratories Item Comments Rep'd Action By Joe Braverman of Burns and Roe was contacted by telephone on June '15, 1982 to get a clarification on the subject criteria for use in the Requalifi-cation of Equipment for Seismic and Hydrodynamic effects. Joe concurred that the accel eration va1 ues shown in the table of the attachment to the conference note were intended to be used for rigid line mounted components only and not for flexible components. i.e., those having natural frequencies below the cutoff frequency. To be consistent with B6R re-commendation for qualification of line mounted components by test would indicate that for the ana ysis of flexible line mounted components a static load would be applied at the C.G. of the extended structure equal to theamplification factor for sin susoida1 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 = 16-7 This loading may be in some cases present a very conservative loading on the line mounted component A somewhat more realistic input motion would be Signed: Page 1
~~~~" 3 Distribtition'tandard Di ~tri hut i on rfg ol @~et ~ . <<tc~ . <Et r~f~~~~
Communications llfillllllllllllllllllllllllll Report Company: Cy<na/Qlyl e Telecon D Conference Report Project Job No. Equipment Seismic/Hydrodynamic 82044 Reaualification 6/15/82 Subject'nterim Dynamic Loads Criteria and 11:00 Fatiaue Criteria Place: Richland Of j ce Participants." Joe Braverman O'Y of Burns and Roe Jim F A~ACHig~<~tj7 of ta VT dOB No, r'loge C .~OI. of 8H FT Xr .f. Item Req'd Action By continuous sine beats of 12-15 ocsillations per beat as recommended by the IEEE-382 draft "Ameri-can Standard of Safety Related Valve Actuators". The amplif'ication for a 15 oscillation sine beat at resonance for 3K damping is approximately 11.5. If the static loadings given above show an over-stressed condition or deflections which would cause operational malfunction, the alternative to develop a more realistic approach would be to per-form in. situ testing from which the data could be used to develop response spectra at valve location The in-situ tests would allow the determination of the natural frequencies and mode shapes of a sufficient part of the piping system along with the valve and extended structure to validate the mathematical models used to generate response spectra'at the valve location and/or component locations on the extended structure. The response spectra at component locations allow direct com-parisons with component test data. It is felt that a combined test and analysis would be a feas-ible and cost effective approach. Signed.' xi' Page of
~~~~'tandard Distribution 1020 00~~~~
~~~~&Ull I I I I Uj j jf 'ct L(uj jS c~~~~~
c
~~~~c. s tt.~~~~
s F i c Report llllllllllllllllllllllllllllll ComPanyCyqna/Ny1 e Telecon D Conference Report Profect Job No. 82Q44 Eouipment Seismic/Hydrodynamic Reauali- Date; 6/15/82 c Ff, Subject Time.. 11 - PP Interim Dynamic Loads Criteria and Pfttce'i ch1 and Of f i ce Fatigue Criteria Panicipants: 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. Distribution: Signed: +~~ Pege ol
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Communications Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Company: Teiecon D Conference Report CES Project: 82046/CR-008 WPPSS Date: 6/11/82
~~~~Subject:~~~~
Time: Qualif ication of Line Mounted Equip. Piece: SDAO Participants': H. Reeser CES, Richland of W. Schlafer CES, SDAO of of Item Comments Req'd Action By The new work authorization had not yet been re-leased. Use the Initial Analysis EQ-12-3000 number for the week-ending Friday 6/11/82.
2. Hal recommends that as a result of using our best engineering judgment in the qualification of line mounted equipment, it is more prudent to fail a few items first before presenting WPPSS with our con cern for a more well defined position on line mounted equipment qualification. At that time, w can present a'lanned approach for additional YOND analytical and/or in-situ testing to be conducted < TACHMEHT which. will yield data needed for a more accurate 8 iXO.~+~
~~~~definition of the dynamic input to line mounted equipment. LE NO. z TN0.~7'."~~~~
3. An examination of the preliminary horizontal OBE and SSE response spectra outside the containment building for a frequency of 8Hz, indicate that the' levels from Attachment 1 (of the Interim Dynamic Loads Criteria) to be used in the static analysis of line mounted equipment not affected by hydro-dynamic loads, may already have a multiplicative factor incorporated in them. This factor may not yet still address the issue of a possible resonance condition of the line mounted equipment which would result in even higher g levels for use in analysis.
Signed: W. Schlafer Page 1 Distribution: L. Kammerzell, J. Read, H. Reeser, J. Minichiello, P. Guglielmino 1020.00 P.K. Pate3
Communications Report Illllljlllllllljllll IIIIIIIIII company: CES R "Telecon Ci Conference Report Project: "o '82046/CR-005 WPPSS Equipment gualification June 8 . 1982
~~~~Subject:~~~~
~~~~Time: Response Spectra Il WPPSS E.g. Documents Place: SDAO~~~~
~~~~Participants:~~~~
H. Reeser CES, Richland of J. Forman Hyle (CES, Richland) W. Schlafer CES, SDAO Item Comments Req'd Action 8y Hal has asked Jim Forman to help Cygna obtain. the following information form WPPSS or from similar data available within 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 stress cycles 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) associated with the LOCA event.
~~~~2. The large compilation of Response Spectra for OBE, SSE and combined hydrodynamic events recently received. by the BAO, SDAO and the SFAO are to be considered preliminary.~~~~
~~~~spectra to'be used for analysis/testing.~~~~
~~~~3. Hal is also sending the WPPSS a) FSAR Section 3.10 and Appendices b) The 2/12/82 submittal to the HRC concerning Equipment qualification.~~~~
~~~~w qg C~& e G Qg's, fii gy-f .CHi.fjt-it F~~~~
~~~~'l,ot NO.~~~~~
~~~~SiiEF., i'iO. ~ t'iLi:~~~~
7. (,$ o Signed: Page of Kammerzell, Read, Patel, Rsleh Rajan, Abolhoda, Curry, tlinichiello, Guglielmino imo.oo Reeser, PROJECT FILE
~~~~Communications Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Company: Telecon 0 Conference Report Project:~~~~
~~~~'2046/CR-004 WPPSS Equipment qualification June 8, ]g82~~~~
~~~~Subject:~~~~
~~~~Time: (}ID File Review am Pface: SDAO~~~~
~~~~Participants:~~~~
P. Gu lielmino of BAO W. Schlafer of SDAO of Item Comments Req'd Action 8y In the revietf of a AID file, if errors in other than seismic analysis are discovered which adversly affect the equipment's qualification, these too must be noted and corrected or justified. If the error that the equipment can still be ifi ed, noteis thesucherror 2. qual and the fact i t does not advers ly affect qualification, but avoid the expense of altering that portion of the analysis.
~~~~3. Both Peter and myself feel that a better defensible position needs to be investigated for the loads used in the analysis of line mounted equipment.~~~~
~~~~p, vT>QC+ti.,z" fil t JOB HO.~~ Fll.E NO.~~~~
~~~~7. I.3I SHEET NO.~~~~
~~~~Signed: W. Schlafer Page of'""~~~~
"ammerzell. Read. patel. Hsie@ Raian. Abolhoda. Curr . Minichiello. Reeser PROJECT FILE
~~~~Communications Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII company: CES Telecon 0 Conference Report Project:~~~~
~~~~'8204 R-00 WPPSS Equipment qualification June 3, 1982~~~~
~~~~Subject:~~~~
~~~~Time: Place:~~~~
~~~~Participants:~~~~
H R of W. Schlafer CES, San Diego of Item Comments Rett'd Action By Hal questioned his immediate contact at WPPSS, Dennis Armstrong, about the number of SRV events and number of cycles. Their reply was "we don't know".
~~~~2. Hal has suggested that Cygna investigate these issues, formulate a position, and then get WPPSS concurrence.~~~~
WPPSS has generated combined response spectra for 'ince seismic and SRV events, I suggested to Hal he obtain separate SRV response spectra and time histories from HGR which they were derived. This will help in determining the length an SRV event and the number of significant cycles. The number of SRV events is more difficult to determine and possibly needs a more thorough'nderstanding of the BWR's systems.
~~~~3. Hal will be our contact in Richland to submit our Action Plan and cost estimates for approval.~~~~
~~~~Q'tf'QUA~~~~
~~~~~ r. AcHME~~T .>0- >>0.~~~~
p>LE NO EHEET >>0. 1 I 12 1 Signed: ol W. Schlafer ."f.w Page Distribution: I'ammerzell, Read, Patel,~Brreh, Rajan, Abolhoda, Curry, Guglielmino, 1020 00 Ilinichiello, Reeser, PROJECT FILE WS:ib
COf f ft IUiRICatlOf1~ I llllllllllillllllllllllllllll.
~~~~¹pot'otnpan~~~~~
X Tetecon o Con'.etence Re por. CES Ftofec! Joo No, 82044 4NP-2 Eouioment "Ouali ication 4 / '7 P. / A 0 Subfec!, Tint size at %'alve Flange/Ear interface eeld Richland F arnot pants Don Searle ol CES/RBO R1 Ck Ri C29'D1 to of ElF /t0l-885-1000 of Iten. Contfnents Rea'o Action By Reouested ano received information concerning tne attachment of the rectangular shaoed "ears" to the valve body flanges. Pick info med mc tha- all of these items- vere af-
~~~~xed to the valve fl-tge by means o we" ding.~~~~
~~~~a) 0. 3l') llet weld three si oes 0.3T" 3 '/Groove welc on ~ 1"sn %v~sn~~~~
~~~~la..ge face.~~~~
~~~~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.~~~~
~~~~"ILKNO. oi. ~(,F 't <.35 3HMT NO.~~~~
~~~~S cnec > ~~.~,Jg Race 0~~~~
"-rc-'ect .. = e,t-'-:D.
~~~~v,,an a c -,e - SearLe~~~~
~~~~~ . fr,.:s G== ice t ong ..'.. ScG t; R ~ f'.1cK:ian,~~~~
July 16, 1974 Confere nce Notes No. 258 Sub)ect ' 2808 Washington Public Power Supply System ,Jgg g 7~yndrickson WPPSS Nuclear Project No. 2 Contract No. 68
!a" a ~~ ~~>A-RlP%'g'jg Date: -Jii:lych.",-';<1.,974~ -"-'-<, PPerry MHroncich Place: B ~ X.F ~ DMurphy Providence, Rhode Xs land HReh
~~~~Purpose:~~~~
~~~~Rem, nnan~~~~
~~~~'...::, nmmenee~n Bm'aa1hanMa1 'meeBCO"iT"tde V'in ~ t fee a an B nn'. ann CVesy (PT&O)~~~~
RLuken RECamp JHagan Pres nt: B.I.F HDoon RWoodward J.P. Cunningham - Product Engr-Butterfly Valves JBlas (2)
*T. Masse Engr. Product Mgr. Butterfly Valves HSybi1 *G-F- MacDonald -- Director Nuclear Q .A. JO'Donnell '*T. Wolfe Marketing anager - Butterfly Valves AWChamos MGooaman Burns and Roe SFox JVZalavadia D, Sheikh DSheikh J. V. Zalavadia BBedros'an O
~~~~RBa ldwin.~~~~
Part Time cca CO C EFerrari (6) l MKahn Ci ..CO CP pf Notes: 1. Documents to BIF db Burns and Poe Comments on Q.A. Manual- BVGFa)A Burns and Roe letter BRBIF-68-74-011, da ted March 19, 1974. ATTACHMENT
~~~~2. Seismic Calculations B&R Comments JOB NO.~~+~~~~
~~~~na.B No. Burns and .Ro~~e 'ES'" BBePT NO.~~~~
~~~~a. C~ha ~e~mar,~~~~
" '~~eB xa ~ ." TM~~,"=:!'>6;-'" ~~~w~hicb='acrm~g~g~;- .Xro'n pter ontract Specif ication.
b. ubmit the ~g4 Ohab+~~pgre,mriW~TZ.:P~~r~"'~>

c. Submi" the calculations for the detail of seating torque value, used in design calculations
~~~~Page 2~~~~
f. Submit;.'p cjo~~ti'-there.~wohu:1d:;:be> no'W'oss o f" fuacWon-.,du~ing.'xa'n'd .ref t'ei:thee jr'esecsr'ibemd-'seismic d't~banc~a'll:eritrhone>d in'pacrag'rar'h"~3'" of'he pecific.-xtion. The seismic calculations include stress an lysis only. The analysis for strain/deformation
~~~~~ I is also'required as a proof that there will be no loss 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" valves considering normal. load with the combination of >> SSE stresses shall be maintained within the normal allowable working stress limit as mentioned in paragraph 3.3.1.1 of specification. 'h
~~~~3. Mandatory Testincr for Seismic Qualif ications~~~~
~~~~~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 accelerationo than Burns and Roe specified and that they will sub the test: data for Burns and Roe review and approval 4 ~ Stardvne tlodel used in Seismic Calculations P TTACHMEh I>Rlmmx, ., Lh,ln mcco1XX!rnernnsmn~oe:".command's the<"SZMM~~535"d~Yi's5~oP,."84aRB+3Y'.
',QQB NO.~~ <VETves. ~~~~!1&0> 4' FILE NO ~>~~
~~~~sosh . '3 n 1 T"Xm SHEET NO. 7.' (.3<~~~~
~~~~':",oe~dgas 'o .,r-,~~~~
C'V'L LIggjg~peo &Le~a-i:"'- <>>cia>eeI'xmenL ..,.. ha.t~-halva hv,.s~w-i@=...QP. A CX>>Ied~>i>i~i>In>Ceje'C Xr~m>>~pr . r 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 Scpecifi'ca t ion'--'requ'irem'enl ts'. t '>hem ".COn gaia>C t>-
~~~~6. W5U e.--'Ec'.centi&'&'bC-&Can'd<.r~~~~~
~~~~@~ p Mme> 1AM AIFeKdFd~oxcce orL h'ehh:ebould'-cones. 'e -double eccen~~~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"~~~~
~~~~7. M~maa1 Breauermxe'~6f<WS'~4-.7;:and:;.30 "~ Valves ",'~~~~
~~~~Bu ns and Roe asked B1F to submit the natural fundamental frecuency of 18", 24", and 30" valves. B re;~~~~
. 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 '<T:.~at~>Lt'..~~
~~~~1 an:.i Roe state; th;:t a;L'. 'L.vl:.:wl:;~ the).r 1 ql!ctat cn nd after !'PPSS's approv.-l Br>ms ..nd:.',re '~> 51 h;Ot-'. fy B>F i ~ a(Mlt AhDna WOX><..l S Ou Cn>>r)ZC(is~~~~
~~~~!.; F c-I ~, ll-h o l 'rh! le <'>~~~~
I
~~~~<37.: l>v t- '>~~~~
~~~~(B lr()o!l<n that tho co:>t <'L~~~~
~~~~slrOr!I'>'~~~~
see r, ~ ~ ~ se h/ 'ppaeehh ae
Page 3 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, thc rubber seal should be on valve disc, correctly specified by Burns and Roe, instead of valve body. Rubber seal if on valve body, is fixed by glue, which cannot resist high temperature. Rubber seal on valve disc is fixed in-between metal pieces.

b. If water or any other fluid is supposed to flow in the pipe, the shaft in the valve should be vertical. The vertical shaft would mean C.G. of pressure due to fluid will'be on the axis and hence much less driving force is -remi ed to operate the valve . But in case of air or steam it makes no difference.

9. ualitv Assurance Hanual-Burns and Roe stated that Burns and Roe comments on BIF Quality Assurance Hanual was mailed to BIF on Harch 19, 1974 (BRBIF-68-74-011) and was classified "Not Approved". The response 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 w updating QA Hanual on July 15 and he e..pects to complete by ill s tar t July 19, 1974. BIF will revise their Q.A. Hanual and/or provide necessary supplements to the manual as per Burns and Roe comments. Bu ns and Roe comments were discussed. Hr. HacDonald will call Hr. Sheldon Paige of Burns and Roe on July 15, for the clarification of the following Burns and Roe comments:
a. Corrective action

b. Audit of Purchase Regs./P.O.'s/change orders

c. Complian'ce to supplier Quality Control Progr

d. Compliance to Lower Tier Procurement

e. Welding Process Sheet Form N-152 (BIF) and t fQPPS~2oC4 of Contract Specification 17A-30 and 17A-31

10. Inservice Insaection Recuirements PILH NO.~
ggKET NO: Burns and Roe auestioned regarding the requirements of "calibration blocks" in accordance w'th the draft of the 1974 Edition of ASHE Section XI, Article I-3000 "Prep ration for Calibrat'on" for Inservice Inspection. BZF stated that the special calibration blocks are not required. They will submit detailed method of Inservice Inspection with Standard Cal.ibration blocks. Zt~- 0:"i~~3 t~ '~:- L-.;- '3'.R Decisic;n on B, guoLatiol')n ca ':: Lat .ons on nc tu
page 4 tern 12 e Owed to B&R bv-.',-8 P. a.; -"3Suzvxssz.on o~ev'C"M'sexsr;.~E'XeaMMons Mo'."e-"'2'".!3~aadePabove".' ",." as'-per: tern
~~~~b. Suhmissi.on of revised Q;A. Manual (Item Ho. 9)~~~~
~~~~Inservice Inspection Recuirements (Item hTo." 10)~~~~
~~~~~~dÃe<"~~~~
~~~~J JV/JV 2/dc~i prepared by).~ Submitted by Q6~0e~ cc: Mr. J. E. Noolsey WPPSS -3 Mr. P. C. Otness BPA -1 CPG($ :~$ PTTP,{'H'MEN~~~~~
~~~~)OG <tLO. -Fl g,NO ~.yl. F HP"-7 NO.~~~~
e
~~~~~ e e ue ~ ~ I 9~~~~~
QIDg 361106 7.3 BIF Report
B IF A UNIT OF GENERAL SIGNAL 1600 DIVISION ROAD WEST WARWICK, R.I. 02893 QUALIFICATION OF PRIMARY CONTAINMENT BUTTERFLY ISOLATION VALVES UNDER LOCA CONDITION. DYNAMIC TORQUE CALCULATION OF BUTTERFLY VALVE PREPARED FOR: WASHINGTON PUBLIC POWER SUPPLY SYSTEM VALVE SIZES 30", and 24" WPPSS CONTRACT NO. 68 BIF ORDER NO.: PN27234 & PN27235 WPPSS IDENTIFZCATZON NO. CSP-V-1 & 2, and CSP V 3 & 4 Prepared by.- Debeadra K. Dae Date: Qov. 10 19 62 Checked by: Dezso Szila i Date: REPORT NO. TR-27234 And TR-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 40

d. 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 67

h. Computer results and comparision with hand computation 69

7. Appendix 80

a. WPPSS Calc.No. M-02-83-08-0, Sheets 1 thru 9

b. LOCA Temp. Curve

c. LOCA Pressure Curve

d. WPPSS Letter dated 10/22/82

e. BIF Flow Loss Coefficient K plot

f. BIF dynamic torque Coefficient CT plot
'SUMfMRY This report contains the dynamic toraue analysis of two butterfly valves of sizes 30, and 24 inch. The analysis is performed for LOCA (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 of these valves. The results of the analysis tabulated on page two through five of the report indicate that the dynamic torcrues developed under the specified flow conditions are less than the design toraues used in the. 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'GNA AT i ACHMKST
~~~~~~ ~Po F...~~~~
RLE NO ~oT o SHEET 40. 2
SUK LORY OF RESULTS Table 1 30 Inch Valve, airflow degas T3.me Angle W Dynamic s Torque in-lb 1.0 90(Full open) 11020 1.5 78.75 23098 2.0 67.50 18138 2.5 56.25 14747 3.0 45. 00 12428 3.5 33.75 10780 4.0 22.50 8014 4.5 11.25 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 is 27800 in-lb. Therefore the design is safe.~~~~
~~~~SUMMARY~~~~
OF RESULTS Table - 2, 30 1rch Valve Steam- flow degas Time Angle W Dynamic S Torque in-lb 1.0 90(Pull open) 11032 1.5 78.75 23175 2.0 67.50 18142 2.5 56.25 14668 3.0 45. 00 12424 3.5 33.75 10580 4.0 22.50 7809 4.5 11.25 3867 5.0 9. 0 (Pull closed) 00* TNet= 22174 in-lb
~~~~At full closed position the dynamic torque is zero and the net torque is due to seating and bearinc friction.~~~~
SU?&fARY OF RESULTS Table 3E inch Valve; Air flow Time Angle W Dynamic s deg. Torque in-lb 1.0 90(Full open) 5525 1.5 78.75 11692 2.0 67.50- 9095 2.5 56.25 7428 3.0 45. 00 6239 3.5 33.75 5430 4.0 22.50 4043 4.5 11.25 2020
~~~~9. 0 (Full closed) 0.0~~~~
TNet= 13808 in-lb

At full closed position the dynamic torque is zero and the net torque is due to seating and bearing friction.
~~~~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<~q FtLE HO ~ot o F..~~~~
~~~~SHEET HO. S~~~~
~~~~SUMMARY~~~~
OF RESULTS Table 4 Inch Ualve, Steam flow e Time S Angle W deg 24 Dynamic Torque in-lb 1.0 90 (Full open) 5425 78.75 11394 2.0 67.50 8921 2.5 56. 25 7213 3.0 45.00 6109 3 5 33.75 5202 4.0 22.50 3842 4.5 11.25 1902 5.0 9. 0 (Full closed) 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, Sheets 1 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 Butterfly Valves. American Water Works ASsociation, Colo. Beard,C., Final Control Elements, Valves and Actuators, First Edition, Rxmbach Publications, 1969. Hutchison J. W. ISA Handbook of Control Valves 2nd Edition Torque 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 Cast Iron Streamline Disc versus Fabricated Flat Plate Disc dated May 13, 1974. B I F Test Report iTR-0650-43, Hydrocynamic and Headloss Test of 12" - 150 Lb. Butterfly Valve with directly connected short radius elbow upstream, dated 2/24/82. B I F Drawings: 30 inch Valve General Arrangement Drawing A-206763 24 inch Valve General Arrangement Drawing A-206764
QID4~361106 7.4 McPherson Associates Analysis
0
~~~~~ ~~~~~
~~~~I 0 BXF A UNIT OF GcCKRAL SIGNAL 1600 DIVISION ROAD NEST NARNXCK, R.X. 02893~~~~
~~~~~ ~~~~~
~~~~DESIGN A'K) SEZSiMC ANALYSZS OF 24 CYLINDER OPERATED BUTTERFLY VALVE FOR WASHINGTON PUBLIC PO~ SUPPLY SY~ AND BURNS AND ROE 0 CUSTOMER P.O NT 68~~~~
~~~~'BZP 5EO . "R~hO'MS-U-0708,'236-U-0808.~~~~
0 I~ B r S PN27235-1 th~ '4 PN27236-1 theo '3 REPORT NO. TR-74-7 PREPARED BY McPHERSQN ASSOCIATES, ZNC. APPRO~~ BY 3 7 7(f' I/5I7+ ~I@~ 1~
DESIGN AND SEISMIC ANALYSIS OF 24" CYLINDER OPERATED BUTTERFLY VALVE A-206765 22 February 1974 Prepared For: BIF 1 A Unit of General Signal Corporation 408 No. RP~) 9
'PILE NO. ..ol. F Prepared By: OHEKT N Thomas M. Riley John R. Henry A Unit of Generai Gisnp Co'rpfration Purchase,Orf er Nq 8+468-68 M he sonAssociates, Inc. ~ . ~
aport No. TR 74 7-- -<eLta>>J>> les McPherson Associates, Inc. 400 Totten Pond Road Naltham, Massachusetts 02154 4C MS <<~5 ~~tel 400 TOTTER PONO ROAO ~ WALTHAM.MASSACHUSETTS 02154
DESIGN AND SEISbll C ANALYSIS OF 24" CYLINDER OPERATED BUTTERFLY VALVE A-206765 BIF A Unit of General Signal'orporation: 40E HO. E~~>"'I Purchase Order No. 84908-63 PLE Ho. ~O. o i. P'HEET ND. ~~ (~X() Associates, ~7-Inc. l V'cPherson Report Ho. T R74- RSV- i'd/~)/vs FOR 24" VALVES BIF Contract No. BIF S.O. No. Valve Tax No's 68 N 27235-F CSP-V-3 N 27236-F CSP-V-4 CEP-V-3A CEP-V-4A CSP-V-5 CSP-V-6
REVl S lOH RECORD NUS REPORT TR-74-7 REVfSlON 1 12/31/75 Page 3 a) Hat'1 was ASTM A-126 s A-48 b) Allowable Stress Yalue corrected Page 5 a) 'rive Lever was.8-184005"6 b) Clevis was D"146578 JOB NO.~B~'~ Page 9 a) Hat'1 was ASTM A-126, Class C 0 PLE NO O&.ol V b) Corrected yield stress allowab e ONE ET NO. + c) Deleted ASTM A-48 Page 32 a) Ref. drawings were " 840054 pD-t 578 >agas 33, 33, 36 < 37 a) b)
~~~~~ 4 X ('x Hat'1 wa~M A-32& '~~~~
~~~~Corre Cad'Stress AQcwab le~~~~
~
Section 1.0 QlTRODUCTlON The purpose of th's report is to determine the structural adequacy o fa 24" . Butter fly Valve Ass emb 3y when s ub j ected to seismic accelerations as described. in Reference '1 and to insure the valve design is in accordance with Reference o this report. CVGNA ATTACHMENT 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 ~~~~~
t ST~(WW~ETET t'l 74 SuaJEET <cg~ V.V'v. SHEET NS. S S -Sl CHKD, SY.A .. QATAR..Z d~ c' rt ~ h R'$ dd8 Nd. C4fWP&CLl7 +VCC C'menSeu (r i') a hhT<CS SL
~ A3 0 ~ .R<QQi4Q P<QL 7SI'ffg C.C ay =flfoo (5g L-7T'St,I I ~"< ' et TX 0 0"J~ gQ zz flz( Sy flfodo C Ilsl-010 0 Cgt.S 5Q~ S AhtI C 5~= 3bSSO fPPIA-3G )
Cu. IJ) sf w . c~ = zg ~ C4sssf a ef iS Pie P= ff3G C .S 5y -- ff'00 (B-Z ONA bccvC l-v~ II = 4S< <a C ~~ = 4S~ (Z . A EST 401 fIO.~<><~ YHAz po+ "EhPd 16~$ 1 K 'Ey ~ z8~, (5) . O~ SI.V,'Hs No.Q-> Bhfiolup p.~ ~ sy, c~~z.~~
~~~~~ ~~~~~
t z,7 (><- SlkhS- S, a.7=.1axa7 <,I.a- z7,<<> (<<,, ~ s.z. - K a'nfl' s Issso I tt sE -. j 78M Px)5, S3 1+~tt IO Ss +~HIf S lES 0 (SS E7' Vhhue'my r,' '-f."~>> 1> <>c.~ a ~
~~~~IoE=T ( s ~Hits)~~~~
~~~~~ ~ ~~~~~
~~~~GLAIR t=M~~ mWK&HC%N C Q~)Z ~py~~~~
~~~~~ ~~~~~
~~~~M~V KEaa~~c Cevcg +ICRLl+5$ C +~M~ QL3f~~~~
/
~~~~tee pars To ST'P- -s5 )g~wq<l~ C ~ SH~~~~
~~~~~ ~~~~~
3
~~~~~ I Section 3.0 I ~ ~~~~~
CONCLUSIONS HcPhers on Ass ocia es, Inc. concludes that all components for thi 24" Butterfly Valve, as analyzed in this report, meet the requirements'of all governing specifications for seismic and operating considerations as de ined in References 1, and 3 of this report. mSHa~E> HD.~O. o I. F
~~~~'ILE SHEET HO. ~~~~~
~~~~TABLE OF CONTENTS Section No. ~Pa e~~~~
~~~~Table of Contents Certification 1.0 Introduction CYGMA A'rTACHMENi 2.0 Summary of Results es wo. '~>'>~<~~~~
Pgg gQ,~O'0 I'F 3.0 Conclusions ND.Q-~ 'aav 4.0 References 0 S Dc'eeeer gee cree See 6.0 Analysis 10 6.l. Cylinder Operator;Ns emb 14 6.2 c(X Cylinder Support Eracke~ 23 6.3 Clevis Assembly an Drive Lever 6.4 Valve Body Support "Ears" and Associated 38. Hardware ~ ~ 6.5 Shaft and Disc Assembly and 'Associated . 46 Hardware 6.6 Valve Si "ing and Stress Analysis Considering Combined Operat'ng and Seismic Conditions
Certification McPherson Associa es, Inc. certifies tha the 24" Butterfly Valve, A-206765, as shown on the customer drawings was analyzed in accordance with Nashington Public Power Supply System 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 of Section 4.0 of this report. meso. '>>"<< p~~ gg ~O ol ~ F. oHEav no. C+ Xr/h. v John: R.(Fenzy~~) F Regis t'er ed'Qr of ess 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~~~~
. M-206765 B 24" Butterfly Valve-General Arrangements A-900523 Body, Fabricated A-900524 Body,.hfachining A-900339 A-900340 Dis c, Fabricated Disc, Machined, ~~ ~E gC EPOS SLEWED. <~oi S
~~~~A-208293 . Cylinder Support Bracket OHEET NO.G~~~~
~
B-&00521,B-900522 Operator Shafts. S. Z'I >8~b Drive Lever CD pe Ql'LQ)'2+ I Clevis ..',>' ~) D-206661 Miller C Tinder<> 3~ Section XXI, Nuclear Power Plant Components, AShfE Boiler and Pressure Vessel Code, 1971 w'th,Addenda.
+)
~~~~Moring Faires, Design of hfachine Elements, 4th~~~~
~~~~'v'Virgil Ed" tion, The MacNillan Co., N.Y.', 1965.~~~~
5. Raymond J'. Roark,. Formulas;.So Stress'nd Strain, 4th Edition, McGraw Hill Book Co., 1955.

6. Laddish Catalog No. 5S.
~~~~7~ Grinnel, Piping and Engineering, 3rd Edition, 1971.~~~~
8. 1963 Supplement to Sc=ew Thread Standards for Federal Services s 9 ~ Baumeister ff Marks, Standard Handbook for Mechanical Engineers, 7th Edition, hfcGraw Hill Book 'Company.
~~~~h ~ical Engineers Handbook. T M. Standards~~~~
~~~~- Part 2.~~~~
~~~~S 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 zcHznery Edition, The Industrial Press, yI gg R209V 364. SCX WO. <~ of ~ Q4EET NO. ~~
~~~~-tion yrZT, Pressure Vessels, Division 2 alternative les, 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 B16.5 tied "Steel Pipe Planges and P3.anged Pittings."~~~~
~~~~.. 'y'q( V: ~ ~ ~ ~ ~~~~~
~~~~J ~ ~~~~~
~~~~~ ~ ~ ~o t ~ ~ ~ ~ &~~~~~
~~~~p ~ g ~~ '~~~~
~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 4 ~ ~ 0 ~ ~ ~ ~ ~ HIKQMRu. ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0 ~ ~ ~
~~~~gg ~ ~ ' ~ ' ~ ~ I~~~~
~~~~~ I ~ ~ ~ ~~~~~
~~~~~ ~ ~ ~ ~ ~ M M M M~~~~
~~~~~ ~~~~~
~~~~Final Qualification~~~~
~
IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Report PROZZCT: Equipment Seismic and Hydrodynamic Requalification O'OB NO: 82044 CALC NO- OS.01.F CLIEVl: Washington Public Power Supply System QID NO- 361104 TITLE: Equipment Seismic and Hydrodynamic Requalification of 30" Cylinder Operated Butterfly Valves: CSP-V-1 and 2 CEP-V-lA and 2A PREPARED BY: M.A. Scott 6/15/83 DATE
/
REVIEWED BY: L.C. Fernandez PC+~w >a&. 6/15/83 J DATE APPROVED BY: F. Khanachet 6/15/83 DATE REVISION:
QID=:. 361104 REVISION STATUS LOG Prepared Approved
~
by by Cygna Approved 'ev. Reviewed Energy by No. Date .by Services M'PSS Descrzptxon 0 2/16/83 R. Hsieh H. Abolhoda Original. Issue J. Rakowski L. Fernandez Scott evised to 6/15/8 corporate 1 Pi 8 ddition of shear L. Fernanctez, tl lates
Revision+1 1.1 WASHINGTON PUBLIC POWER SUPPLY SYSTEM REQUALIFICATIONCERTIFICATE WNP-QZD 361104 COMPONKNT NO1 -V- gp -V-2 P-V-2A CDMPDNKNTDKscRIPTIDNs
" vlinder Ooerated But ter f1 Valves MANUPACTURKR1 A-206763 KQUIPMCNT CLASSIPICATIONi gJ ACTIVE Q PASSIVE 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.
~~~~ik RE UIRED ACTION: 1) Re lace A-307 Ear Bolts with A-325 bolts.~~~~
~~~~2) Addition of shear plates, see sheets 4.3.30 to4.3.48 for additional details.~~~~
THK ABOVE SEISMIC QUALIPICATIONRCPORT5 HAVC BKKN RKKVALUATEOIN ACCORDANCE WITH THC CURRENT NRC SC15MIC CRITERIA! I ICEE STANOARO5 244 {197$ ) This equipment is qualified as 2 U5NRC RKQULATORYCUIOKS 1.92, I 144 a assembly when the air cylinders are completely qualified addressed 2a 5TANDARD RKVICW PLANS ~Ma 5 14a ISED in QID f018001. 4, NURCC&$ $ 4 THC ABOVC COMPONENT HAS BCKN POUND ACCEPTABLE POR PCRPORMINQ ITS INTENOCD SAPETY RKLATED PUNCTION WHEN SUSPECTED TO THC PLANT SPCCIPIC VIBRATORY LOAO5 PREPARED BV R EV I KW CD 6 Y J.E. Rakowski 8 ~~4~ Da iA./D5 DATE OATK 3 25 83 APPROVED BV
~
~~~~p/r i ~~HM.~~~~
~
OATK 941 12574
Revision 1 2.1 WASHlNGTON PUBL1C POWER SUPPLY SYSTEM B S J c f llllllllllllllllllllllllllllll Qualification Summary of Equipment QIDN 361104 Ref. Mo. I PLANT NAME: WNP-2 TYPE NSSS: GE Burns & Roe BwR 5, Mark II CSP-V-1 & 2 I I~ COMPONENT NAME: y V.COMPONENT Np CEP-V-1A & 2A I~ SCOPE: Q NSSS 2 MOPEL NLf4BER. A-206763 PUANTI TY: 5G VENDCR: BIF . 4 IF THE CCMPONENT IS A CABINET OR PANELS NAME AND MODEL NOG OF THE OEV ICES I NCLUOEO N/A PHYs IOAL pfscR IPT I pN + APPf ARANcf Butter f1 Valve with 10 " C 1 0 erat
b. DIMENSIONS: 30" Nominal D' tr 1208 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 (CEP FUNcTIpNAL pfscRIPTION; Primar Containment isolation revention of of 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. No IV EQUIPMENT QUAL IF ICATION METHOD: TEST X ANALYSIS Q C(NBINATION OF TEST Equipment Seismic and Hydrodynamic Requalifica Ij ANALYSIS QUALIFICATION REPORT: tion 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 the AISC 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. VI 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 QUAL IF 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 F/B R R SSE S/S F/B R 9>> LABORATORY MOUNTING: BOLT (NO., SIZE I IIELO (LENGTH ) Q 10>> 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) QiD~< 361104 Ref. No Vl I ~ IF QUALIFICATION BY ANAI.YSIS, THEN COMPLETE: I~ METHOD OF ANALYSIS: STATIC ANALYSIS EQUIVALENT STATIC ANALYSIS Q DYNAMIC ANALYSIS T IN' STORY RESPONSE SPECTRLH 2G NATIRAL FREQUENCIES IN EACH DIRECTION (SIDE/SIDEP FRONT/BACK, VERTICAL): 13' Hz F/B 11 45 Hz v ) 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 OTHER
~~~~5. 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~~~~
8. CRITICAL STRU TIRAL ELEMENTS: GOVERN I NG LOAD OR RESPONSE SEISMIC TOTAL STRESS A, IOEHTIFI GATI OH LOCATIDH COIBI IIATIOH STRESS STRESS ALLOIABLE Operator Drive Cylinder on Fatigue Rod CSP-V-1 Stress 86,826 90,000 CSP-V-2 Range 57,526 90,000 Ear Weld Support Ear Fatigue CSP-V-1 Stress Range 26 F 554 28 F 000 MAXIM'LLOWABLE B MAX, CRITICAL DEFLECTION TO ASSlHE DEFLECTION LOCATIOH FUNCTIONAL OPERABILITY Q 0.01" Valve disk radial approx 1/8" radial deflection clearance NOTE: Calculations based on accelerations for CSP-V-1 and 2 will provide an envelope for CEP-V-1A and 2A. See Table 1.1 of Section 4.3 for relative required accelerations for CSP and CEP valve operators.
~~~~~sed on calculation using Revised Burns and Roe Piping Analysis Accelerations, April, 1983; PAGE 4 OF 5~~~~
~~~~Revision 1 2.5 Qualification Summary oi Equipment (Continued) QIDN 361104 VIII. REFERENCES~~~~
1) BIF Drawings Drawing I Revl Description A-206763 F General Arrangement CEP-625-10 From Reactor Nozzle X-3 to SGT-FU-lA, 1B c CEP-625-11.12 From Reactor Nozzle X-3 to SGT-FU-1A, 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 General Arrangment lan mis level CSP-807-3.4 Containment purge air su 1 s stem References continued on page 2.6
~~~~~ c w~~ ~ i D ~N .~ ~/~/~~~~~~
~~~~Date~~~~
~~~~~/~~~~~~
Pago 5 of 5
THXS PAGE NOT USED. Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII project Prepared By. Date WPPSS Mechanical Equipment Qualification J.E. Rakowski 3/25/83 Subtect Checked By; 30" Butterfl Valves ')-.C. I=~ +/~ lzz System Job No. File No. CSP and CEP Os.ol/F Anatysis No'61104 Rev, No. Sheet No. 2.6, Reference cont'n
2) Formulas for Natural Frequency and Ytode Shapes, Robert D. Blevins Van Nostrand Reinhold Company 1979 Edition

3) BIF Report TR-27234 and TR-27235, "Dynamic Torque Calculation 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) WPPSS, WNP-2 SRM Equipment List Summary Sheets dated 2/10/83.

7) Cygna Energy Services, Equipment Qualification Walkdown Verification Form dated 7/14/82 and 7/19/82.

8) Cygna Energy Services, "Project Manual Design Criteria,"
~~~~DC-l, Rev. 1, 10/82.~~~~
9) Burns & Roe Revised Piping Analysis Loads for CSP-V-1 and 2 (received 4/13/83) and CEP-V-lA and 1B (dated 11/15/82) .

10) Communications Report, R. Ricappito o f BIF and J. Rakowski of CES, "BIF Valve Dimensions", 2/ll/83 ll) Cygna Energy Services, "Equipment Seismic and Hydrodynamic Requalification Calculation No. OS.01.F", QID No. 361104, Revision 1, May, 1983.
rccs Oc
r Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII 7 F,o,ec, WPPSS, tvNP-2 Seismic/Hydrodynamic Freoa e" By Daie L.C.Fernandez 4/29/83 Svo~ec: Systpcc II Ghee<<ea By Joo No Foie No Daie
~~~~'l,.~~~~
82044 OS. 01 Analya a No Fle ~ Nc Shee: Nc 361104 UPSET COND1T10N G-LEVELS EPICS CSP- V -1 0.76 1.36 0.88 Cep- V-2 0.66 1.33 0.79 -e FAULTED CONDI T1ON G-LEVELS ( RWuIREb) 6 AND 10 1NCH AIR CYLINDER OPERATORS HYDR EPN LDS ELEV 'R' CSP-V -1 50B. 00 2.26 3.62 2.80 CSP- V -2 Y 508.00 1.44 3.54 1.90 CEP- V -lb Y 586.00 1.93 2.23 1.85 CEP- / -2A Y 588.00 0.96 2.11 1.16 From Revised Burns and Roe Piping Accelerations, see Section 5.5. le~A cc
Og 0
TABLE OF CONTENTS QlDg 361104 SECTION TITLE NO OF PAGES 1.0 Requalification Certificate 2.0 SQRT Forms 3.0 Table of Contents 4.0 Requalification Analysis 4.1 Conclusions 4.2 Summary of Results 4.. Analysis Pg. 4.3.1 Introduction Pg. 4.3.8 Calculations Pg. 4.3.53 References 5.0 Appendices 5.1 Response Spectra 5.2 Walkdown Sheets 5.3 Valve Local Coordinate Systems 5.4 SRM Sheets 5.5 Revised Burns & Roe Piping Analysis Accelerations 6.0 Drawings Revision 1
TABLE OF CONTENTS QIDN 361104 CON'T SECTiON TITLE NO OF PAGES 7.0 Transmittals, Prior Calculations and Reports
~~~~'7. 1 Communication Reports 7.2 Original Requalification and SQRT Forms 7.3 BIF Report~~~~
7.4 McPherson Associates Analysis*
*Note: Excerpts from report included in specified section. For complete report see Cygna Energy Services File No. OS.01.F, QID 361104, "Equipment Seismic and Hydrodynamic Requalification of 30" Cylinder Operated Butterfly Valves," Revision 1, June, 1983.
Revision 1
Calculation Cover Sheet Equipment Seismic and Hydrodynamic Job No. 82044 Requalification File No. 0S 0 1 F Client Gale. Set No. Washington Public Power Supply System 1 No. of Sheets 83 Subject BIF 30 " Cylinder Operated But terfly Valves , QZDN 3 6 1 1 0 4 EPNS : 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 calculations using Revised Burns and Roe Piping Analysis Accelerations, April, 1983. (See Section 5.5)~~~~
Originators Checkers Distribution Revision No. 1 Fernandez SuPersedes Calculation Set No. JE Rakowski LC Supply System 2 H. Abolhoda MA Scott Project File-1 Revision 0, 7/23/82 R. Hsieh DE Searle Approved By:
~~~~~ p, ~ P, Date:~~~~
i~ 100$ .00
Calculation t t C5 B T Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Prepared By Date Protect Subtect Checked By Date System Job No, File No, Anatysis No. Rev No. Sheet No CONTENTS Calculation Cover. Sheet 4.1 Conclusions 4.2 Summary of Results 4.3 Analysis 4.3.1 Introauction 4.3.2 Calculations 4.4 References 1006 00
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By; Date Subject Checked By, Date System Job No, File No. Analysis No Rev, No, Sheet No SECTION
~~~~4.1 CONCLUSION~~~~
S rctjs cc V
WASHINGTON PUBLIC POWER SUPPLY SYSTEM SUPP l.1LJR Tl<ANSIlllTTALFORI'Il AREA WITHIN HEAVY BORDER TO BE COMPLETED BY SUPPLIER) To THK ATTENTIDN oF 3 p p p G PP i Denn s Arms on tr NIZJgiT PfJRCH PFOPGQNQ UYfg CON RAC$ AD I ~
)
PAGE ~~ OF l sU JKcT Eouio . Seismic H drodvnamic Re u 1 C na Ener Services 2 NEW 0 RK SUBMITTAL ADDREss. 1200 Jadwin Suite 565 Richland HA RKQUKSTKD DATE THE FOLLOWING PUBI ICATIONS/DRAWINGS ARE SUBMITTED FOR: OF RETURN:
~~~~@APPROVAL Q OF EACH REVIEW "~~~~
Q INFORMATION OP REPROOOCIEL Q DISTRIBUTION OF E CH CONTRACT NO: PO NO) NO.OF PRINTS NO SUBMITTKD BY: t WORK ORDER NO: TITLE: SPEC. NOg SUBVENDOR: CONT.JP.O, NO,: SPEC, SECT NO> WPPSS ITEM PUBLICATION 0 R RKV. DRAWING NO. NO, PUBLICATION OR DRAWING TITLE MANUFACTURER ACTION NO, T-6 1 4 3 COMMENTS< (USE ADDITIONALSHEET, IF REQUIRED) TO BE REVIEWED BY R EIVKO BY: IPURCHASING ONLY) TRANSMITTED BY: IPURCHASING ONLY) I I HAM ROVED E4Y: TITLE ACTION LEGENOc A ~ APPROVED FOR PUBI.ICATION I ~ INFORMATION ONLY AN m APPROVKO AS NOTEO FOR FABRICATION NA ~ NOT APPROVED P ~ I P PT SSS
FINAL
'- ~k> QUALIFICATION llllllllllllllllllllllllllllll REPORT 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 Requalification 8", 10" and 12" Bore Air Cylinder Operator EPN 8CEP-AO-lA, 2A REA-AO-1', 2 CEP-A0-3A, 4A ROA-A0-,1, 2 CSP-A0-1, 2 CSP-AO-37 4, 5, 6, 9 PREPARED BY:
REVIEWED BY: APPROVED BY: REVISION: 1001.00
REVISION STATUS LOG Prepared Approved by by Cygna Approved Revi Reviewed Energy by No. Date by Services NPPSS Description
1 0 REQUALIFICATION CERTIFICATION 1.1 WASHINGTON PUBLIC POWER SUPPLY SYSTEM REQUALIFICATIONCERTIFICATE WNP- QID 018001 cOMPDNENTNO, CSP-,A0-3 4 8" Bore Air Cylinder Operators MANUPAcTURKR Miller Fluid Power Cor MOOKI NOt A83 KQUIPMKNTCLASSIFICATIONt gg ACTIVE Q PASSIVE SEISMIC QUALIFICATIONREPORT REFERENCKt C a Re ort 1P.Ol/F, QID 018001 WPPSS Seismic Qualification of 8" and 10" Bore Miller Air 0 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. THK ABOVE SKI5MIC AND QUAIJPICATION REPORT5 HAVE BREN RKKVAL,UATKDIN ACCOROANCK WITH THK CURRENT NRC SKI5MIC ANO CRITKRIAt I ~ IKKKSTANOARO5 244 (l57$ I, This certificate applies only to the U5NRC REGULATORY OUIOK5 I%2, I ~ ISO operator which was evaluated as part 2 of the valve assembly. Following Se 5TANDARO REVIEW PLANS-2&~i 2 IOo~ completion of the valve requalifica-tion (QID 361106), the certification 4~~%I will be revised to address the entire assembly. THK ABOVE COMPONENT HAS BEEN FOUND ACCEPTABLE FOR FERFORMINQ IT5 INTENDED 5APKTY RELATED FUNCTION WHEN 5UBIECTKD TO THK PLANT SPECIFIC VIBRATORY .LDAos subj ect to the above remarks. PRKPARKO BY
~~~~3. E . RA&o~S&I ki4d~ la +S~~ln, ~ I ~4~ A ~vdS APPROVED BY OATS DATE~~~~
~~~~+ peggy t$ 2 l2$ 7$ / ')~~~~
1.2 WASKNGTQN PUBLIC POWER SUPPLY SYSTEMIC REQUALIFICATIONCERTIFICATE WNe- QID 018001 coMPDNKNT Noi CSP-AO-1 2 cDMPDNKNTDKscRIFTIDN3 10 Bore Air C linder 0 erators MANUFAOTURER, Miller Fluid Power Cor MODEL NO( KQUIPMKNTCLASSIFICATIONs QX ACTIVE Q PASSIVE SKI5MIC QUALIFICATIONREPORT
~~~~REFERENCE:~~~~
or 1P.01 F ID 018001 WPPSS Seismic ualification of 8" and 10" Bore Miller Air 0 erator. KNVIRONMENTALQUALIFICATIONRKPOR'T RKFKRKNCKl Remarks 1: Parts of the air operators such as the drive rod, trunnion ins, 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 ABOVE SKI5MIC QUALIFICATIONRKPORT5 HAVE BEEN RKKVALUATEDIN ACCORDANCE WITH AND'HK CURRENT NRC SEISMIC ANO CRITERIAc
'I IEEK STANOARD5 244 (I$ 75) This certificate applies only to the U5NRC REGULATORY QUIOK5 Io$ 2, I ~ IOO operator which was evaluated as part 2e of the valve assembly. Following com-Se 5TANOARD REVIEW PLAN5 SAW 2 I0+410t pletion of the valve requalification (QID 361104)., the certification will 4 fCctlRKISNNEE be revised to address the entire as-sembly.
THK ABOVE COMPONENT HAS BEEN FOUND ACCEPTABLE POR PKRFORMINQ IT5-INTENDED 5AFETY RELATED FUNCTION WHEN SUBJECTED TO THK PLANT SPKCII IC VIBRATORY, remarks. LDAD5) j sub ect to the above PREPARED BY REVIEWED BY J. 2 RAtc~OSIc I N (4. ~ IAA>5c~A DATE a4'PPROVED BY OATK ( ~v PCi/>,i~r~,,v w V ) $ 44 I2574
1.3 WASHINGTON PUBLIC POWER SUPPLY SYSTEM REQUALIFICATIONCERTIFICATE WNP QID 018001 COMPONENT NOs coMPDNKNT DKscRIPTIDN( 8" Bore Air C linder 0 erators Miller Fluid Power Corp. MODKLNOs A83 EdIUIPMKNT CLASSIPICATIONs g] ACTIVE Q PASSIVE SEISMIC CIUALIPICATIONREPORT RKPERENCKj C na Re ort 1P.01/F, QID 018001 WBP6S Seismic ualification of 8" and 10" Bore Miller Air 0 erator. ENVIRONMENTAL.QUAUPICATION REPORT REPERKNCEt Remarks 1: Parts of the air operators such as the drive rod, trunnion ins, brackets and clevis were evaluated as part of the respective valve QID packages. THK ABOVE 5KISMIC AND dIUALIPICATIONRKPORT5 HAVE BEEN REEVALUATED IN ACCORDANCE WITH THK CURRENT NRC 5KI5MIC AND. CRITERIA> I ~ IKKKSTANDARD5 544 (1 $ 75), This certificate applies
+pwcaonly 2e U5NRC REGULATORY OUIDE5 le$ 5, to the operator which was evalu-1 ~ IDO ated as part of the valve as-st STANDARD REVIEW PLANS SA>e 5 10' sembly. Following completion 1~~ of the valve requalification (QID 361106), the certification 4 NCOR$
will be revised to address the entire assembly. THK ABOVE COMPONENT HA5 BEEN POUND ACCKPl'ABLE POR PERPORMINO IT5 INTENDED 5APETY RELATED PUNCTION WHKN 5UBJECTKD TO THK PLANT SPECI PIC VIBRATORY, ~ ~ LOADS PREPARED BY REVIEWED BY Q E ~p, wan (~~g~ DATK DATE APPROVED BY I DATE
~~~~<+ IVr 1' -'ides') i~~~~
$ $ $ ~1$ $ 15
1.4 WASHINGTON PUBLIC POWER SUPPLY SYSTEM REQUALIFICATIONCERTIFICATE WNP- QID 018001 coMPDNENT Not CEP -AO- lA 2A coMPDNKNT DKscRIFTIDNt 1 0" Bore Air C 1 inder 0 erators Miller Fluid Power Corp. MODEL NO( A83 (2A), A83B (1A) KCIUIPMKNTCLA5SII ICATIONt gg ACTIVE Q I ASSIVK SKI5MIC dUAIJFICATION REPORT REFKRKNCKt C na Re ort 1P.01/F, QID 018001 WPPSS Seismic Qaulification of 8" and 10" Bore Miller Air 0 erator. ENVIRONMENTALQUALIFICATIONREPORT REFERKNCEt Remarks: Parts of the air operators such as the drive rod, trunnion ins, brackets and clevis were evaluated as part of the re-spective valve QID packages. THK ASOVK SEISMIC AND 0IUAIJFICATION RKPORT5 HAVE SEEN REEVALUATED IN ACCORDANCE WITH THK CURRENT NRC SEISMIC ANO ITKRIAt I ~ IKKKSTANOARD5 544 II%75), This certificate applies only to the USNRC REGULATORY OUIOKS I%Sr I operator which was evaluated as part
~ IOO of the valve assembly. Following corn Sr 5TANDARO REVIEW PLANS 5AAr 5 IOr~ pletion of the valve requalification OWN~ (QID 361104), the certification will 4
be revised to address the entire as-sembly. THE ASOVK COMPONENT HA5 SEEN FOUND ACCKFTASLE fOR PKRFORMINO IT5 INTENDED 5AFETY RELATED FUNCTION WHEN 5USIKCTKD TO THK PLANT 5PKCIFIC VIBRATORY '- LOAO5 PREPARED SY REVIEWED SY Rtl <C k.l (4 c3~ /A/ APPROVED SY OATS
~~~~+ti'tif ilt.rt r~~~~
$ 4$ r I 251$
1.5 WASHINGTON PUBLIC POWER SUPPLY SYSTEM CEP -AO- 3A 4A WOP ~ REQUALIFICATIONCERTIFICATE QXD 018001 coMPDNENT Not 8" Bore Air C linder 0 erators Miller Fluid Power Corp. MDDKL,ND A83 ( IA), A83B (3A) KCLUIPMENTCLA55IF ICATI ON s KjACTIVE Q PASSIVE SEISMIC GUAuPICATION REPORT RKFERENCKt 1P.01 F ID 018001 Seismic uglification of 8" and 10" Bore Hiller or. ENVIRONMENTALGUAIJFICATION REPORT REFKRENCKt Remarks: Parts of the air o erators such as the drive, rod, trunnion ins brackets and clevis were evaluated as part of the res ective valve QID ackages. THE ABOVE SEISMIC AND GUAIJPICATION REPORT5 HAVE BEEN REEVALUATED IN ACCORDANCE WITH THK CURRKNT NRC SEISMIC AND CRITERIA s I ~ IKKKSTANOARD5 344 1197$ ) certificate applies only to the USNRC REGULATORY GUIDES 1A2e 1+100 operator which was evaluated as part of the valve assembly. Following 4 S~ lfUlCKIDBRS'his STANDARD REVIEW PLANS SA&e 5 IOe~ completion of the valve requalifi-cation (QXD 361106), the certificatio will be revised to address the entire assembly. THE ABOVE COMPONKNT HAS BEEN I OUND ACCEPTABLE FOR PERFORMING IT5 INTENDED SAF'KTY RELATED FUNCTION c91&I257 WHEN SUBIKCTKD TO THE PLANT SPECIFIC VIBRATORY ~ ~ LOAO5, PREPARED BY REVIEWED BY
%.&l ~id U~ i'WS~7VW QzY 83 DATE APPROVED BY >7 &Z OATK ...1 4 ~r I'-/dzc .--. /~7/.- i
1. 6 WASHINGTON PUBLIC POWER SUPPLY SYSTEM REQUALIFICATIONCERTIFICATE 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 .
MOOKt. NOt A83 EQUIPMENT CLA$5IFICATIONt Q ACTIVE Q PA55IVK SEISMIC QUALIPICATIONREPORT RKFKRKNCKt C na Re ort 1P.01/F, QID 018001 WPPSS Seismic Qualification of 8" and 10" Bore Miller Air 0 erator. ENVIRONMENTALQUALIFICATIONRKPORT REFERENCE QUALIFICATIONRKPORT5 HAVE BKKN RKKVALUATEDIN ACCORDANCE WITH THK CURRENT NRC SKI5MIC ANO CRITERIA'
~~~~~ IKKE STANOARO5 244 (I97$ )~~~~
~~~~2 U5NRC REQULATORY QUIDK5 IA2o I I 00~~~~
~~~~~ ~~~~~
2~ 5TANDARO RKVIKWPLANS'$5&v 2 I Oe 4 THK ABOVE COMPONKNT HA5 BEEN POUND ACCEPTABLE FOR PERFORMINQ IT5 INTENDED 5AFETY RELATED FUNCTION WHKN SUBJKCTKD TO THK PLANT SPECIFIC VIBRATORY LOAO5 PREPARED BY DATE RKVIKWKDBY Widen> DATK W zan APPROVED BY z7 DATE 0-, 'iJ '<, 'i v 944 12970
2.0 SQRT FORM(S) AND REFERENCES WASHlNGTON,PUBLlC POWER SUPPLY SYSTEM GOBKJE,I Qualification Summary of Equipment IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Ref. No. I PLANT NAME.
~P- 2 TYPE I NSSS: GE z AiE. Burns & Roe 5-Mark CEP-A0-3A, 4A II coINoowENT NAME 8 Bore Air C 1 inder C~NENT NO. CSP-AO-3 4 5 6 9 I~ SCOPE: NSSS 2'DDEL NU4BER.
4 VENDOR 'T.F A83B IF THE CQ4%WENT IS A CABINET OR PANEL, NAME ANO MODEL NO QUANT I TY: OF THE DEVICES INCLUDED: N/A 5 PHYS ICAL OESCR I PT ION: a, APPEARQCE: 13. b DIMENSIONS: 8" Dia. x 1. 13 WE I GHT: 3 lb s ~ 13 Reactor ' LocATIow BUILDING Bu 475 ' 4 ELEVATION. 7 FIELD MOUNTING CONDITIONS: BOLT (NO S(ZE P NELS (LENGTH )
~~~~8. a. sYsTEM IN wHIcH LocATED: CEP ~~~~~
Containmen h CSP; Containment Supply ' Purge System b FUNOTIDNAL DEscRIPTIDN.Primar Con tainmen Io of the release of radioactive materi@ po @I CO IS THE EQUIFMENT REQUIRED FOR: HOT STANCBY COLO SHUTDOWN BOTH Q NEITHER
~~~~9. PERTINENT REFERENCE DESIGN SPECIFICATION:~~~~
I I I. IS EOUIFMENT AVAILABLE FOR INSPECTION IN THE PLANT: X YES Q NO see w PAGE 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 AXI S MULT I-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 ~ F/8 ~ SSE S/S EE 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~~~~
'k FAULTED COND I T I ON G-LEVELS 8 AND 10 INCH AIR CYLINDER OPERATORS EPN HYDR LDS ELEV G'S V E CSP-AO-1 V 5OB.OO 4.4O 6.51 4 '9 ++
~~~~CSP-AO-2 CSP-AO-3 CSP-AO-4 Y Y Y 508.00 481.00 478.00 4.95 5.72 4.65 6.45 3.82 4.06 3.72 7 '5 6.57~~~~
~~~~'A':~~~~
~~~~3.s4 p.j7 > . goy B.7&~~~~
~~~~4. (g~~~~
<<Qg'z,0t CSP-AO-5 Y 475.00 9.35 5.75 CSP~O-6 Y 480.00 9.35 5.57 1.46 3 33 i CSP-AO-9 Y 490.00 2.57 1.73 2.67 'EP~O-1 588.00 1.27 1.77 1.23 rVQ I I
EP-AO-2 Y 588.00 0.78 1.77 1.02 /JQ CEPQO-3A 495.00 13.89 1.66 1.04 4.g7 i Z( co~ CEP-Ail-4A 495.00 10.95 1.50 1.10 3.35 i +Transmi t ted from the f inal p ping anal vs is, see Sect i on 5.5. ++These va) ves are required to fai l-closed dur 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~ 4kdld ~~~< 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/
~~~~2.5 WASHINGTON PUBLIC POWER SUPPLY SYSTEM AlL ai IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Qualification Summary of Equipment~~~~
~~~~/ID 018001 WNP-2 RoI. No.~~~~
I~ PLANT HAKEE lo. HSSSI 2o A/E! Burns g Roe BNR 5 - Mark II CEP-A0-1A, 2A I I~ cosFPoNENT NAKE. 0" Bore Air linder CyerwENT NO. CSP-AO-1 2
~~~~'I SCOPE: NSSS BOP ~~~~~
2o ICDEL HLNBER: A83B OUANTITY: YEN'! BIF 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 APPf ARjgcf li drical 13 b D IKENS I OHS: 10EE dia. x, 64" ion (excludes the drive rod 13 c lC I GHT! 593 lbs. - c linder, 321 lb. - bracket 13 LocATI oH QJ I LD IHG Reactor Bui1 ding ELfyh'TI DH. 7 508 'o 560 7 FIEIO OIUIITINO COfOITIOMSF QX BOLT (IIO SIZE ) HELD (LEHGTII ) Bo Oo SYSTEK IN WICK LOCATED: CEP Containment Exhaust Pur e S stem CSP; Containment Supply Purge System bo FVICTIONAL OESCRLPTIOH: the release of radioactive material to the environm nt. Co IS THE EOUIPKEHT REOUIRED FOR: Q HOT STAHCBY Q COLD SHUTDCNH Q BOTII Q NEITHER 9o PERTLHENT REFEREM K DESIGN SPECIF ICATIOH: 68 I I I~ LS E UIFKENT AVAllhBLE FOR INSPECTION IN THE PLANT: Q YES (See Walkdown) Q HO PAGE I OF S
2.6 Qualification Summary of Equipment (Continued) QID 018001 Ref. No. EOUI PMENT DUAL IF ICATION METHOD: TEST ANALYSIS CO4BINATION OF TEST 4 ANALYSIS pty L IF IGATI0N REPDRT ~ Re ualification Anal s is of ID 0 1 800 1 tern (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 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 Rj SRSS OTHER ( SPECIFY)
~~~~3. REOUIRED RESPONSE SPECTRA (ATTACH THE GRAPHS):~~~~
Section 5.1 4 DAMPING CORRESPONDING TO RSS: OBE sss ~2 Sec. 5~4 5 REQUIRED ACCELERATION IN EACH DIRECTION: Q ZPA Q 0THER (sPEGIFY) At tached F/B . ss SSE S/s Attached F/B 6 WERE FATIGUE EFFECTS OR OTHER VIBRATION LOADS CONSIDEREDT Q YES NO 13 IF YES, DESCRIBE LOADS CONSIDERED ANO HOW THEY. WERE TREATED IN OVERALL DUAL IF ICATION FROOIAM: For those EPN's which are sub'ected to h drod amic loadin s 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 Ref. No. 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 3 NO OF QUAL IF 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 % F/B % Y % SSE S/S % F/B % 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 Qualification Summary of Equipment (Continued) QID 018001 Ref. No. IF QUAL IF ICATION BY ANALYSIS, THEN C(HPLETE: I METHOD OF ANALYSIS: STATIC ANALYSIS QX EQUI VALENT STATIC ANALYSI5 13 DYNAMIC ANALYSI S Q TIME-HISTORY I RESPONSE SPECTRLH 2 NATURAL FREQUENCIES IN EACH DIRECTION (SIDE/5 IDEE FRONT/BACK, VERTICAL): 13.0 Hz 11.45 Hz v 100 Hz 10 F/B Bs 3P MODEL TYPE: Q
~~~~/ Q Q FINITE ELEMENT BEAM CLOSED FORM SOLUTION 4 C~UTER CODES:~~~~
FREQUEICY RANGE AND NO OF MODES CONSIDERED: N/A MAND CALCULATI ONS 13 OTHER 5 NETNOO OF COIBININO OYNANIC RESPOIISES: Q ABSOULTE SIN Q SASS Q ISPECIFY) 6o 7 SB OAH ING: OBE SSE SUPPORT CONSIDERATIONS IN THE MODEL CR I T ICAL STRLCTlRAL ELEMENTS: BASIS FOR THE ROPING USED: GOVERN I NG LOAD I d*
~
OR RESPONSE SEI SHIC TOTAL STRESS A IDENTIFICATION I SCAT ION COIBI NATION STRESS STRESS ALL(%ABLE (Range) Drive Rod Operator Fatigue/Fault+ 86824 90,000 PSX CSP-V-1 HAXIHLH ALLQfABLE B HAX CRITICAL DEFLECTION TO ASSURE DEFLECTION I.CCA T I ON FUST I ONAL OPERA B I L I TY Operability to be demonstrated by test for CSP-AO-1 & 2.
**Air Operator bushing stress ) 200psi
~~~~Final Response accelerations from piping analysis were used.~~~~
A PAGE 4 OF 5
FAULTED CONDITION G-LEUELS 8 AND 10'INCH AIR CYLINDER OPERATORS EPN HYDR LDS ELEU G'S V E CSP-AO-1 Y 508. 00 4. 40 6. 51 4.89 3 Cc)Z CSPMO-2 Y 508.00 4.95 6.45 3 '2 3.s4 CSP-AO-3 Y 481 .00 5.72 3.82 7 '5 Z,4& 3.7& Z,6'.l7 CSP-AO-4 Y 478,00 4.65 4.06 6 '7 4.fQ CSP-AO-5 Y 475.00 9 '5 5.75 7.72 344, s4Z CSP-AO-6 Y 480 .00 9.35 5.57 1 .46 5.Q3 5 I 490.00 2.57 1.73 2.67
~~~~'SP-AO-9 Y >@<~~~~
CEP-AO-1 Y 588.00 1.27 1.77 1.23 EP-AO-2 Y 588.00 0.78 1.77 1.02 CEPS-3A Y 495.00 13.89 1.66 1.04 4.57 CEP-A0-4A Y 495 00 F 10 '5 1.50 1 ~ 10 3. 35 (.34 +Transmi t ted from the f inal pip in9 anal ysi s, see Sec t i on 5. 5. ++These val ves are r equir ed to fai l-closed dur ing a DBE, chanpe Use Code to '1,3" .
~ +~ + A ~~<"" ~4 7(c'4~~ 4 rvpiNg g~lgc.veil ~~~<=~~~< l4"-, 4yorbduiky ~Maoris8J/g~g724'-rrt/T QNAPczc "37 ~~ oo<<(~>><<J. roe tea. s s/are oieoo i rgL. pqgpgg~
~~~~y/gg/p~~~~
2. 10 VfASHlNGTON PUBLlt POV/ER SUPPLY SYSTEM Ak IIIIIIIIIIIIIIIIIIIIIIIIIIIN Qualification Summary of, Equipment QID 018001 ts5P-.2 RI5. llo.
~~~~~LANT NANER PNR lo. NSSS5 2 VE Buxns g Roe IIIR 5 - Mark II REA-AO-l, 2 I I. c~ENT NANE:~~~~
12EE Bore Air linder CCHQHENT NO, ROA-AO-1 2 SCOPE: NSSS g OOF 2, FIDEL NLHBER: A83B OLIANTI TY. BIF 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 13 QJ I LD I NQ Reactor Bui1 ding ELEYATIDNH f 578 'o 597 Exhaust T FIELD IOIIIITIHO COIOITI(RHI QX COLT (IHL SITE ) Q IIELO (LEHCIH I C3 I SYSTEM I N NH I cH LocATED REA Reactor Bui1 ding Air (HVAC) System ROA; Reactor Building Outside Air (HVAC) System FIIIcTIDNAL DEscRIPTIDN Reactor Buildin Containment Atmosphere Control and prevention 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 Qualification Summary of Equipment (Continued)~~~~
QID 018001 Ref. No. EOU I FMENT QUAL IF I CAT I ON METHOD: TEST Q ANALYSIS C(HBINATION OF TEST 4, ANALYSIS QUAL IF ICATION REPORT: 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 SSE 5 REQUIRED ACCELERATION IN EACH DIRECTION: Q ZPA Q] DTHER (sPEGIFY) Sect. 5. CBE S/S ~ 1.0 6, HERE FATIGUE EFFECTS OR OTHER VIBRATION LOADS CONSIOEREDT YES NO 13 IF YES, DESCRIBE LOADS CONSIDEREO ANO HON THEY. MERE TREATED IN OVERALL QUALIFICATION FROGRAM: 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 Ref. V I~ IF UAL IF ICATION BY TEST THEN CO@'LETE+: N/A I Q 5 NGLE EQUEICY Q MULTI-F ECY Q ANKH EQ 2 Q SINGLE AXIS Q MULTI AXIS Q SINE BEAT NQ, OF QUALIF ICATION TESTS: OBE SSE OTHER (SPECIFYI 4~ FREQUENCY RANGE', NATIRAL FREQUENCIES IN EACH DIRECTION (SIDE/SIDE, FRONT/BACKS VERTICAL)! S/5 ys F/B ~ V RS 6 METHOD OF DETERMINING NATINAL FREQUENCIES'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 ~ F/B ys V RS SSE 5/5 ~ F/B ~ 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 Qualification Summary of Equipment (Continued)~~~~
QID 018001 Ref. No. (', IF DUAL IF ICATION BY ANALYSIS, THEN CCHPLETE: I~ MFTHOD OF ANALYSIS: Q STATIC ANALYSIS Qg EOUI VALENT STATIC ANALYSIS 13 Q DYNAMIC ANALYSIS T IME-H I STORY Q RESPONSE SPECTRIN 2 NATlRAL FREPUENCI ES IN EACH DIRECTION (SIDE/SIDEB FRONT/BACK, VERTICAL): s/s 10. 81 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: N/A HAND CALCUlATIONS OTHER 5H METHOD OF CCHBI NING DYNAMIC RESPONSES: Q ABSOULTE SIP4 Q SRSS Q l SPECIFY) 13 6H DAIL ING: OBE SSE BASIS FOR THE OhH ING USED: 7H SUPPORT CONSIDERATIONS IN THE MODEL e-Mounted BH CRI 7 ICAL STRlCTlBAL ELEMENTS- GOVERN I NG LOAD OR RESPONSE SE I SMI C TOTAL STRESS A IDENTIF ICATION LCCATIOH COIBI HATI CH BTHBBB STRESS ALLIABLE Tie Rods Operating 13683psi 20000 psi Drive Rods threaded end faulted 31',172 psi 86,400 ps'3 MAXI MLM ALLIABLE 8 MAX CR I T I GAL DEFLECTION TO ASSLRE DEFLECTION LCCATI OH 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 Engineers 1974 Edition with Winter 1974,Addenda. Section III, Division 1, Subsections NC 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 Forms for 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", 8th Edition, 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 J.E. Rakowski Rovlowotl By Date Pape 5 ol 5
3.0 TABLE OF CONTENTS TABLE OF CONTENTS QID 018001 SECTION TITLE 1.0 Requalification Certificate 2.0 SQRT Form(s) and References 16 3.0 Table of Contents 4.0 Calculations - Cygna Requalification Analysis 4.1 Conclusions 4.2 Summary of Results 6 4.3 Analysis 43 4.4 References 5.0 Appendixes to Requalification Analyses 5.1 Response Spectra 6 5.2 Walkdown Sheets 23 5.3 Summary Sheets 16 5.4 Load Comparative sheets for REA and ROA Air Cylinders 5.5 Burns 6 Roe telex final piping G-levels 6.0 Drawings used for Requalification 7.0 Prior Calculations and Transmittals used for Requalification
SECTION 4.0 REQUALIFICATION ANALYSIS
Calculation R ~ J a 1 Cover IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Sheet ID 018001 Project '20 E ui ment Seismic H d 'P.01 F Client Gale. Set No. No. of Sheets Washin ton Publi S stem 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 using the air operator response g-levels transmitted by the A/E, current to 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 Checkers Distribution Revision No. Supersedes Calculation Set No. R. Casassa J. Foie Approved By: ate: Rakow
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII QID 018001 Project Prepared By: Date Subject Checked By: 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 Introduction 4.3.2 Cylinder Operability 4.3.3 Analysis 4.4 References APPA>tx A,IC 'lees 00
Calculation Sheet IIIIIjjjjjjjjIIIjjjjjjjjjjjjjj project Prepared By: Date Subject Checked By Date System Job No. Fite No. Analysis No, Rev. No. Sheet No. SECTION
~~~~4.1 CONCLUSION~~~~
S
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII project Prepared By: Date WP Subject Checked Date Re ualification By.'ob 2 83 System No. File No. BIF Air 0 erators Analysis No. Rev. No. Sheet No. CONCLUSIONS This QID demonstrates seismic and hydrodynamic qualification of the 8, 10 and 12 inch bore diameter cylinder operators identified in Section 4.2. Summary Table 4.2.2 presents these comparisons and shows requirements for the bolting material in the 8 and 10 inch cylinders.
~~~~1. Cylinders CSP-A0-1,2,3 R 4 must be qualified for an active function and require a representitive opera-bility demonstration as described in Section 4.3.2 of this report.~~~~
This should be performed using the, values of air operator loads in QTD 361104 and 361106. QID packages 361101 and 361102 document qualification of the valves associated with the 12 inch air cylinder in this report for the seis-mic loads which they experience. No fatigue analysis is required for these cylinders because no hydrodynamic vibration is experienced. These cylinders were shown to quali'fy with A307 bracket bolting for the actual response g-levels calculated in the piping analysis. This qualification package will be complete when a satisfactory operability test is performed and documented herein. Tt has been concluded in this report that the standard A307 "earbolts" should be replaced with A325 material type bolts on the'" and 10" air cylinders only. 1005 00
Calculation Sheet HHHIHHHHHHHHHHHI Project WPPS Subiect E i Prepared By: Checked By. Date Date Re ualification System Job No. Fi(e No. BIF Air 0 er Anatvsts No, Rev. No, Sheet No, 018001 0 SECTION 4.2
~~~~SUMMARY~~~~
OF RESULTS
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII project Prepared By: Date Subject Checked By:, R 4 rs85 System Job No File No. 82044 1P. 01 F Analysis No. Rev. No. 018001 018001 - 4..Z../. 4.2
~~~~SUMMARY~~~~
OF RESULTS Summary tables in'this section present calculated stresses in 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 taken from QID 361106 and 361104, respectively. These calculations were performed on the valve/operator assembly using the SRSS method and the actual piping response g-levels to eliminate unnecessary conservatism in the higher-stressed components. The air operator components addressed in this'eport are not highly stressed and were analyzed using simpler techniques with generally higher envelope loads having greater margin. See Section 4.3.1 for more information. The following summarv tables note corresponding g-levels and 'ooerator components. r 008 to
Calculation i-~Ia'tPPig Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII cheeaeahe:gg Subject Re ualification n~ Date p Z~ QS System Job No. File No. BIF Air 0 erators 82044 1P. 1 Analysis No. Rev. No. Sheet No. 4.2. 2 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 CSP-AO-3 481 2.66 2. 99 3.76 8 CSP-AO'-4 478 2.96 3e17 4.19 8 CSP-AO-5 475 2.96 3. '44 5. 712 8 CSP-AO-6 480 11.39 3.33 5. 85 8 CSP-AO-9 490 2.57 1.73 2.67 8 CEP-AO-3A 497 4.57 1.26 0.86 8 CEP-AO-4A 497 3. 35 1.34 0.86 10 CSP-AO-1 500 2. 26 3.62 2.80 10 CSP-AO-2 500 1.44 3.54 1.90 10 CEP-AO-1A 500 1.93 2 '3 1.85 10 CEP-AO-2A 500 0.96 2.11 1.16 12 REA-AO-1 597 1.00 0.60 1.00 12 REA-AO-2 597 1.00 0.60 1.00 12 ROA-AO-1 578 1.00 0.60 1.00 12 .ROA-AO-2 578 1.00 0.60 1.00 Refer to final piping G-levels in Section 5.5 and QTD 361104 and 36110b. 1000 00
4Cj~<SSCS C /ST~ 8u~t ~~gI r'A8<C 4 Z, Z, Co D C 0 QC /ling QCCPgfI ICQ, 0 ~gCC ICIQPQ PCP/ J6rPCCAC,gr4D CDS CF CD 0 CD CA 4 lb VA cJK K~A/S M- 9 Cl
~~~~~4 C~~~~
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~~~~/L-sZg 7e VSiCe /C'<S r 8S98 zosgg s 8 b$ 5 z5sz5' Z95ZS izi50 8,796 +~~~~
~~~~Cl zgAg. r4ro7o rS 4'/5 t4M. (7sr'4 4mb +Scab 95dC) /54d J'0'Ã4 <~outs tAg/ 4~Ak Au.ocr'kz&S clM$ r1c1 add~~~~
~~~~'l Co n '0 0~~~~
~~~~0' FPVCC,u su>.rc Cl~~~~
~~'0 DI DC' z 0 0 a CD Gl ZA-~7(. zc/Mz bZ, Ii Cll C~~
A-4/g9 A'ok'>4c. 4rgz. 4&SZ &6M r4'2 bb lg ZS b MbZ4 s782b ~ ~8rllhdg 4LLdccCAdC $0ddd 'll CD z 0
+ ~Ac)-g 6<d<c.obch dy'gp 4Q-4 ay wJ Dc ~AgGim 4 8~P-Ad-I3 C~Z4 oui) C,XZgC L dy 0Eg Ag CQ, Pg J'C-.C li)dC,G g.Z,/
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project WPPSS E i eismic H drod namic Re ual. Prepared By: J.E. Rakow Date Date Subject Re ualification Checked By: f2'g System Job No. File No. Aoalvsis No. 018001 Rev. No. Sheet No 018001 - d..Z TABLE 4.2.2 (continued) Remainin 8" Bore Air 0 erator Com onente 'h~14 =6: Cylinder: SI max = 12,056 psi c 18,000 psi O.K. Tie Rods: ft = 6099 psi < 20,000 psi O.K. Support Bracket (Bearing): F P
~~~~= 2299 psi ( 32400 psi O.K.~~~~
~~~~Total Stress:~~~~
~~~~= 7492 psi e 21,600 psi O.K.~~~~
Shear Stress: 691 psi ~ 14,400 psi O.K. Weld: f = 789 psi < 21,000 psi O.K. Fatigue: f = 1579 psi ( 45,000 psi O.K. Remainin Cylinder: 10" Bore Air 0 erator Com onents h~6 v
~~~~=5:~~~~
max 18,000 O.K. Tie Rods: ft = 6614 psi 10,000 psi O.K. Support Bracket (Bearing): f =2287 psi 32,400 psi O.K. 1008 00
Calculation 6 J ra t Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: Date r 83 Subject Re ualification System Job No. File No. BIF Air 0 erators 8204 1P. Sheet No. Analvsis No. 018001 Rev. No. 018001 - cf..2. S TABLE 4.2.2 (continued) Total Stress:
~~~~= 4830 psi 21,600 psi O.K.~~~~
~~~~SUMMARY~~~~
OF RESULTS Shear Stress: "T = 346 psi w 14,400 psi O.K. , Weld: f 832 psi ~ 21,000 psi O.K. Fatigue: N/A (Allowable stress range
~~~~= 45 ksi for welds).~~~~
12" Bore Air 0 erators Com onents Cylinder: SI max 3439 psi ( 18,000 psi O.K. Tie Rods: f 13681 psi ( 20,000 psi O.K. Support Bracket;(Bearing): fp 1775 psi ( 32,400 psi O.K. Total Stress: 4267 psi ~ 21,600 psi O.K. Shear Stress: 283 psi ( 14,400 psi 0.K. Weld: f 3445 psi < 21,000 psi O.K. Drive Rod (Tensile): 31,172 psi ~ 86,400 psi O.K. Trunnion Pins (Shear): 2,515 psi ~ 11,840 psi O.K. Support Bracket Bolts (A307): gh=g h v 1.54:
=
(I.r S~ Tensile: 12,598 psi w 30,000 psi O.K. Shear: 6,339 psi ( 1$ ',000 psi O.K. 1000 00
Calculation L aB i~ Fa 4 B aa 1 1 Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Prepared By: Date WPPSS EQ J.E..Rakowski 4 22 8 Subject II Checked By. J gg J File No. Dale
+(
~~~~System 82044 OT.01/F Analysis No,~~~~
~~~~'0'1 v001= Rev. No. '18001 - c$ .2. &~~~~
~~~~SUMMARY~~~~
TABLE 1. 3 ALLOWABLE STRESSES Since operability is required, the stresses for the faulted condition will be kept in the elastic range. The table below is based on AISC criteria and the yield stresses at temperature (340'F) from PG. 9 of REF. 4 for conservatism. Levei 8 E 8 L E VEt. tes <ek Fy t S keBt'Fy yx~t.b Sms, 4 I'y . V Fy 0.toFy o.eq F Nw ATE@.r W i (P~x 0 Sartthxrrc. SHe'HR. g frtOPf Ck 5 H t.'HR. A t.~. )t Lao&. A t.aoM. H>SZ -'II'IO Hattr IPEytmr> Ro~ ooo 8 oooo 36ooo Fkloo 57,t'oc SA-rills ) t'at~ ZD it / Ij',5 <ct Jlql oo 7,"too I7 7QQ // FVC) BsTH 1- Sf'- 4a-v$ - 1$ qs;oo~ g7>ooo / p'00m /S>koD g g,'ZoO SH- ZO7 43~S ++ / Q)Q $ 0 )~3'20 Q 2~370 / Q)) oo HrS-- /OIZ (~ V~.o) 3S OOO 2 I~ooO ) P>ooo 33, Coo 8 4,Moo 6~-193~ ts,lt. 83> ZOYSS 8tooO /P,coo /a,woo g ) >~c /0 J'yV S~ l79) 3oVJJ 0 4)(.zo /3,5 fo 9,okg 2 I,7 Yt)t /Q,~o
~H-S'lL 't a. t',o 900 4 oo //~oo 00 ZFp 8IUKRE 1 BotT At.t.oWa 5&S t'4Kt:)) Fko~ Attic., 8lt) ED., >Er . I.S.Z.2
Calculation r ~s'f== Sheet-IIIIIIIIIIIIIIIIIIIIIIIIIIIIII project Prepared By: Date Subject Checked By: Date Reaualification Job No. File No. System BIF ir 0 Analysis No, Rev. No. Sheet No. 8204 1P. 1 Section 4.3 REQUALIFICATION ANALYSIS
~~~~>cce 00~~~~
~~~~Calculation J~J =~~~~
't p,'9 r.'> Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII project Prepared By: Date Subject System checked 8y:
~~~~Job No.~~~~
~~~~/ g~ +File No.~~~~
~~~~Date~~~~
+/
~~~~Analysis No. Rev. No. 018001 018001 4.~. l tI 4.~~~~
~~~~3.1 INTRODUCTION~~~~
The analyses herein address specific parts of the 8, 10 and 12 inch diameter Miller Air Products air cylinder operators identified 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 to Table 4.3.1. The analyses in this QID were performed with enveloping g-levels. Table 4.2.1 summarizes the required g-levels from the piping analysis. The air operator mass-stiffness model incorporated in the piping analysis to calculate response g-levels on the more Beverly loade d 8 and 10 inch operators is riven in Appendix A of th is calculation. 4.3.2 CYLINDER OPERABILITY The cylinders designated as EPN CSP-A0-1.2,3,4 must operate during an DBE from open to fail-closed.. While seating the valve disk during a DBE, the air cylinders must have sufficient capacity to overcome the seating torque of the valve plus the frictional forces in the bushing and cylin-der. The following table compares the required seating torque forces and minimum cylinder spring preloads given in QID 361106 and 361104 for the 8 and 10 inch cylinders. equzre
~~~~Sprang Residual Capacity siz Seatin Fore Preload To Overcome Frictio 8ff 1150 lb. lb 350 lb.~~~~
~~~~10" 1847.lb.'500 2900 lb 1053 lb.~~~~
~~~~+ QID's 361106, 361104 and (361101 R 361102) for the 8, 10 and 12 which operators respectively.~~~~
100s Co
Prepared By Date Calculation Sheet Project P ss
~~~~o. 3g fes"s Job No File No aa~~~~
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Prepared By: Date Calcu!ation Sheet Ie I 0'83 Ghee ed y: Oate uPPz s <zz SZ A'~8~ r~~ Job No. File No IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject PQ o1/ 1P 01 F System Sheet No. 0 I Bd.dl- 4.>.Z. Analysis No. 0 Tp /LE + 3. ) C'd97INuFO X'TE Q LOa hckx'9TZ o5 QREA5 HH H I- YWG'b
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Calculation e L e d d 'I Sheet Illlljllllllllljllllllllllllll Project WPP S i . eismic H drod amic Re ual. Prepared By: J..E'. Rakowski Date 4 22 83 Subject Checked By: g ~ i / Date J / System Job No. File No. 82044 1P. 01 F Analysis No. Rev'. No. 018001 4. 3,2. 5 018001
~~~~4. 3. 2 CYLINDER OPERABILITY (CON ')~~~~
Ability of the spring to fully close the valve depends on the coefficient of friction. between the sliding surfaces of the cylinder, namely the drive rod and bushing, and the piston and cylinder. Although upper limit bushing pressures due to load reaction were given by Miller Air Products for consideration of shaft wear, (Section 7.0, Ref. 5a and 5b) this alone is not a sufficient criterion because piston friction in the cylinder is not accounted for. Therefoxe, it is recommended that one 8" air operator (CSP-AO-3 or 4) be fieldtested'to verify operability since this size has approximately only 25 percent the residual capacity of a 10 inch. operator. Dynamic plus static bush-ing pressures for these operators are calculated in QID's 361106 and 361104 and these may be used as a guide to speci-fy the simulated test g-level on the end of the air cylinder by consideration of the bushing. reaction equation in Ap-pendix B of this calculation. The test load should be applied in the direction which tends to rotate the cylinder about the trunnion pin axis. Bushing pressures for both the 8 and 10 .inch operators must be considered in compari-son to the'elative residual capacity, of the 8 and 10 inch cylinders so that both sizes axe covered by. this test.
~~~~4. 3. 3 ANALYSIS 4.3.3.1 12 inch operator assembly frequency*.~~~~
Similar calculation for the 8 and 10 inch assemblies are given in QID 361106 and 361104. 100s 00,
Date Calculation Sheet ill:~f ~ Checked 8y: Date t= 4Qa Fmject Job No File No
~~~~+WCirgr) r 0/<.9 err rt BED~~ 4l ~~~~~
~~~~IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject Analysis No. ~+- <> Aev, No. d'l8 c z i-Sheet No. YF~~~~
~~~~.9.3, / ~~~~~
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~~~~'p QAtO TO MKg.COM~ p t-tE. ' &E,ATl N Q ~O~Q =~~~~
Qppy,~ g 17000 )<gg 'e (PER Ft F ~ 4 f 18 awe,cy t
Prepared By Date Calculation Sheet At 82. Checked By: Protect t Jt J Crit C~ r'C Ja./~/s z. J File No Job No. 4Zo~
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~~~~05 B 4 s f S 5 IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject~~~~
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JJ' ~W XdA System t' 8 dot"A7er r Sheet No. ot'D Analysis No. ~~~ t Rev. No. ~ t' . 5, 5 .Z. soo+ QN I T C.A.~M LAT 0 M l COP LOAM P3+ I0oo+ ( lI? I?l 3 .ool7'ox5" A z("-to )(~>>.~) ROTAT l 0 H AT 6 Il DOE, TO 1~tO OP Jt~ ~~IA~~RA 5OO5 27? o >n.= moo( lo.ol) 5005 tw 4 rl tt 24.to> to.de 5005 7.77 0 2770
~2,c?. i . 2.l ~ S+ 7.Z7,7 . = . I2 <'9 O73 35or .3 I 1>.b y p5os> (, z. )= ZSgyy 3+t. 8 AaaA I ARFA A~n, 2 CC A00A, = 5 (I<.55) .4 5<-,>> 'l2.09 A ~%A 2.
4,gg RKc.TA s gt t= ~ II Cc - Y.( ii )=;s.z 4~=(iI 3(I2.n) = ISS Vm,t 4 Na, L-E. CC= a( II g- >,>> l '7.I.S5-I7,0$ ) = 55.f 3;. Cc= (c-~ T
)(w~) -Ccg )(A = ~i~ *l33 +'>>'-: 9 > + 55,r 3 .( 6> '.
ti r:O3 =-<.y7:
Prepared 8y: Date Calculation Sheet 63o 8~ Checked 8y: Dfte ia.lV/S 8.
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Date Calculation Sheet Ir Ps Checked 8y: Date project ~F I S&- Wc Job No File Subject Rm~u A t= C A. tL(3 No.'P. OL System Op~ Sheet No, Analysis No. < daoi-,4.3,3.4
~~~~~C AX A </~/~~~~~
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~~~~~ (S.~S'- 7 ~7")~~~~
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Prepared 8y Date Calculation Sheet Date Project la a/gQ Job No File No. IIIIIIIIIIIIIIIIIIIIIIIIIIIIII ubj eel R '1 'I Nza44 1I .O I System YO Sheet No Analysis No. Rev. No. F'z/a 8 Ir AkJAt Y&is MMT Sa.wo<ve sm.a. ~as (x,') AXiAL. smsssss (.y) W'(Q) 3~ r ('7') Cl l3
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A, t'o- I ~~ lOZ, p>> < 1006 00
Prepared By: Date Calculation Sheet z/c Ir /7~ d~ t Protect Q PP56 Lt&tC Avr O
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~~~~Job No~~~~
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~ IIIIIIIIIIIIIIIIIIIIIIIIIIIIII eZO44 t O I System 4t Sheet No, Analysis No. Rev. No. or9oar - 4.9.3.& g,~/p~/~ 4/zz/a8 ANALYStg (<>~ i) DRT~Rpn r u a OQ CYF PRr Q nr GTR OP&a. g-(,) 45$ 8 483.B 02S7 J/g '7+8 -6 VGG I Iti) .ROZ, lo2 .l27S. Iz75, l275 PRI At- I PAt @maes i s: DPE.P ~~So = II,'ill pst ~ = <>+> p~i
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~~~~'lE. S(.s) ~ (.tS.S- i rw)(.<)~~~~
4 ( cr t ~ so~ 597. Co ter"
Prepared By: Date Calculation Sheet 0 te Checked By: Project ra/~ Sz-Job No File No s t IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject At 1P'1T10 SZ.044 >P . o> System Analysis No.
~~~~///oor- 4,3 3.iZ~Y Sheet No. ~A. AAP8 A 4/Z ~JBs 8 An't-Yeti C<c'~>)~~~~
e~01M G TRES 9: N =[2.27 (2,8 s) +? 9") (os-s)] /4 0=.,2'gr %so i Zlt'is~(l~- s.sg q = 3'.> r>> 597. g XI AL s Ta.~os (I B. s - i.t,~)(, g) = FA~mt i o~~aw ~c. I ver.n~ ~ sr ot =2 1006 00
Prepared 8: Oate Calculation Sheet r 7~ Sz. Checked By: Dae Project Subject System R VA,LtF 1C.A TtOW 1 t- Qp~tt'i'(3 Job No.
~~~~'~o44 Sheet No File No. ~ ~. C) 4 jP ~~~~~
~~~~Aoalysis No. 0/c5 OO/ g. 3.3. l'Q (~~~~
~~~~~ ~/zz/ss 9 PCM L. 51 8 C.o~y~~~~
Prepared By: Date Calculation Sheet 5'2 Date Project P S5 F- tSHl r~/a s~ Job No File No. Subject ip. oi /t= System Sheet No Q ~ +goo r' g g 3 jg UK Wco~K< A.~g~ ~lazes fit>At 'l~ t o~ L~ oQ ~E.~ - (o 0 f4 AREA OF WKLY = +( 7>7) ( 'h[) = ~ W4 L~C ~ Ot= (Vt=Lg l 7. 5 rl (AJEGLec~~g t'c>+ ~o sr4rec pr~)
~~~~. ma~ az> = Cg,s-(.<w) = 7.((~~~~
( o44 7%m) / $r + + j ++0/~fr ~,' /C 7 ~ lob (9'rH BD.) FromSVC a~ ~c-. c S, (.PM AtSgA Sacmo~ ~Pc~oi m Q) ASSvrne t o~t~g ac~a tm ~ 1 C.get.~ = ? O Goo too ~Q (8t IZ, cd )pr7q p)t C Q 5 G>OQ ps r 7.( 4.
~~~~/I Prepared By Calculation Sheet A.K II IK)chal Date Project ~Z/~ g~~~~~
Job No File No Subject ~ GALt LCA T iO W '&ZO+4 l P. al 8 ~ At z I COt a,~go a Sheet No. Analysis No. +\ +G& I Rev. No. ~rigour- 4 3.3./S ttrj'( J ( ~~Sac,l
~~~~.~~)~ 4/ZZ/at ~C O~I~C M~ic Hr ANn C-W. t-aW CVLlmma~~~~~
~~~~Ama ~&Co ~~c H C2.iM Wc <<Och, C C ct= C YLt>C t=z. T=ZQP %HA.c7 = 5~~~~
~~~~~t Q,HrW B9~~~~~
C>:D = 'lO 4ZB R. 7&0 Q. a~~ 7I <0.42 or-Q. iO.4Z.S I.e(. r I4 ) 7 A4 9C .73 tn 1 MoME.wT'RM= 'DNT. FPObl T RUHNIOA TO r--Cj ~ EAG~MY CPM = cern (1+. &2+ 2 Iz&)= 'zl.& Mgy~ n = (Mom~ruy AZ~n,(MmirHi l(g) (Z I,~)( tooI~)(4') = 'T&4rt7.4 in-(b B~~~i~c Gyrz~~~=~ 6'~= ~ =
~~~~.7&4'R"1 (=(>c ANc a) )~~~~
4(22.. Zd g~'~
Prepared By Oat Calculation Sheet ii ia'Lax project
~~~~~a9/gz.~~~~
Job No. File No IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject ~WQ44 iP. H > System Sheet No. erg~.~r- <.s.s.iC wRa w P aa,~mum= ~Q g <jzz j>> AXi RL ~A~>s i -PZ~ IBO (9.q@$
~~~~'Z<z>z) BZQCo PS~~~~~
~~~~l4 co412. ~st. 4kmF: 6 goop = q = ~+~~~~~~
~~~~~AD> AI 'P ADtAl <ao 5 ~lW A. R. STRUM ~esa 6) =~~~~
~~~~47&.Z5 ~~L STza++ X O>t~~~~
~~~~+SRS R wpSR Q+~~~~
s54R 6czs E(vs i) 475 475 P<t NC tPAL ST'R'EKSmM
Prepared By: Calculation Sheet fA I Il 17 QZ Checked By: Date eh J~"Jara> Protect QP P 6 KtG C K c lZm S2-Job No. File No. IllllI IIIIIIIIIIII IIIIIIIIIIII Subject YtON 23,Z.C)44 >v .ot w Syaterrt 6 \ P At 6 fZ.l4 Sheet No.
,~ooal ... 0 O/8 ODi- d-.S.3./7 SZmc v '2'33 I 4 -3('m>I at'Sutta Cat tW CSP Ha~stat 3S ~ At t o&AB~ = ~ 4 +tJ- = Z\ GOO pat.
~~~~RZ 75. < 2> (o OQ ps<~~~~
~
~~~~C~at~m~m lm Ace ~r w~a.~ TIE Pcp>-~~~~
~~~~'Eoar = (~~~i~~ Av ap)>> (w~cawoaa) = TT (e.'llo )'l&8b'1 IZED~~~~
~~~~(~< ) Low~ >~~ Bo z = "~>~ aeZZ. II Roc DtAAK Yt t=t, A,w~ a = ~ = ~ (~i~)q.~~~~
~~~~= 182.~~~~
K G/roc = l44L C & I4 psi < 20 k'sI. (Assume. ALO7 i<waoz s >os) 1
Prepared By Date zl t-71~ 2.
'I Calculation Sheet I 1 Oate Project rz/~ ZZ r File No B J Job No a
~~~~IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject SzD44t iw. oi System Sheet No Analysis No. + ~~+ I Rev. No.~~~~
? 7.12& LcL 7 IZ5 (lI,~~ C>AA~ NO c 2< ocr' j.375 DOD TO CI XVI'8 E.'SI RAIN (E DIR) +la = MKtGH'T Of- CMI 1~~~% S 1 54 a~L~
F~= t 93 2.I.2-~3 (xs. >me) F~=( ss,c ~ 598) $ 28. 8 .. ~~DI ov t I~ Hogc 'oQ To o.l <<vI RKKTIAAINT (+ DIR 1
~~~~~F Fc 1.3"IQ )\ b I~~~~
~~~~Prepared By Date Calculation Sheet Checked By: Date p;, RP'PS&- S'- t~~~~
~~~~~~/~Ps~~~~~
Ia fa% Job No File No IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject lP.O1F System Sheet No Analysis No. ~ ~ Rev. No. C7Zdc~~- 4 3.a.i9'oc~>~
'4JJ Qt zaAvoP S4>wot=t~ ~L-RA< K.~ 7 ~o~~~o~ Pin g I.'lS FO C K A,T 7R.M )O~ Wt r4 R VAR.Ht& = = (ia..a.o. z.s. w~))
g MAL (g.c)(w93')(c M 4 75407.5 tg.-l6 O( ~a) d = >s.e a ~ ~ = A.&l i~ (ms~. D~< + A 2corrIq-g Lr~+. C) F, =~75k .C GZff VaFt.>> W t
Prepared By Oat Calculation Sheet r>>~le,z Checked By: Project Job No File No IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject aZ.a44 i~,OI I=
~~~~~** ~~/wc r - 4.8.9. ZD System Sheet No gz /~=~~~~
F~ = SKAV<14+ Worc&VK, '9 64 ~ (BI% RKPORT p is) (re+ ~3 To~At os>= F~> F~>l=~ ~Kg +~c Z. Z 2 l 964+ 5~ii ++7~ s2.> 5S5I: +>>'(4+
~~~~~49. e PKAgtN os SQPV oRY TR.a N >la sw ~i ~~~~~
~~~~BMAmN+ A,AHA, = Aa ~D L= TH tc.K.m&MM D = Dt&MM~t- ~W TW l = < ~Q D= < 7B '(Rr~. W>m@. 42 SKI IB Ap =( 'I~~~~
~~~~~5$ i.1S ) =2.'h4iN~ Du@ C-ZGOlb)~~~~
~~~~Gain mtwc = F g4g Q gp$ 7 .. p~t p, ~ 2..$ % w ATt= ~t 0.L~~~~
~~~~= . ISu.= B2 4 '~owAe,~a. 'icosi 6 RaAa)HQ =~~~~
Prepared By Date Calculation Sheet MI-'4~M \ lI 'I'7 I >Z-2/5//6 t ~Fsc )=ra Project Job No File No IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject ~ z.+ 4P ~ +. 04 H System Sheet No. Analysis No. ~ O (-l I Rev. No. c9/gooi- 4.3.3.Z/
~~~~~~f~~~~
~~~~( ua.c.~ Bvc.<a~ 7oz B=wctw~ 3..v~~~ ch!a"- 9.2% 4= 312 + ~I~~~~
~
Q=S f'3~ Sot Q Ctni Suorot y (6, CYI-la Dg Q Ctact a SRAVCS Y AHD zs,a" SECT'1 0H sacwIoIs PgoraIzvIaa (zar (o /p~cao~ac ~~ ac~+ p >v) t II 2 (. t4) = l. &8 Qn ~ ot a, = . Q4 It L+<> 25.h5 4= I5:a,e rr (osII ('Ncaa, Doaw ttuv E sm'r (Q MIN SKc'Y>o>)
~~~~~ 3I (I3.3 CoZ3) + I3 g I-SS .4 ZK,G,Za+ 'I'3 8'3 < ~ '5)I ~ C Z & I3 3) ~ ('I3 & I .'K'5 l ( Cc Z &)~~~~
( Q . ~ Z. + LCD 7 W8 7.02. rl a .4-4+ 7 ~ Z.C Z,= >3,W .4 ZQ Z. t8,+- L,8S (,( 2.+) 4 hS,Q( ~ ('K)(7,0Z) I Z. tz ( I3.% I.&3)(. I,ZK)(.3 I+ (I3.33 7O2)) = 7BO.O IN
< = (l ll (3s.a -+.za)(3s3) ~(z3.a 3.za)(~Iz)J= zaescr,al I~ / tS.M, i ~g= 23454(- z ) 205 p~~
a &Co ~ 4
Prepared By Oat Calculation Sheet I18 SZ Checked By: Date Project Job No. File No. IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject .oL F System ~ Sheet No Analysis No.
&T'tZ&~M A= (i3.w-i. tea) (.c z~)= 7 z.r. i~~ ~~t-T<t'Atda'UN.'Tt CA, t <RAT'15'1IR II ~ = I'lac L cb.'6'6 I@165 7g5 ps't P,~ Cg= 27. ZQ. + 2055 = '46( 5, . P~l.
~~~~GHEAFt &TR,EWM 6 o C clcwc. ~M ace,cmmw) Cc.a ( >+3+ ~ iZ.) = 543 O gp~p, = a, t.co w ia a ( c~~~~
~
~~~~z.B) = ia 7 5430 54.('o p>~ i5 7 AL.t ovDA.BL 6& P~mWtM+ ' C S~ QL l( O~ PW.t 5HaA,R. ~~~~~
~~~~~ 4 S~ 14 l4OO Pa<~~~~
l 000 00 pmv tovs t-q Ca,t cu Wzm
Prepared 8y Date Calculation Sheet Il i~ i+Z. Checked Date Project rzi~ Job No File No. IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject IP Q1 F System Sheet No Artatysis No 0 TWO 0 i Rey. No, or9eor- 4.B.3. E 3
~~, w~v' A,~~ ~o/zz/zz Oi o" o StNCS 6 ~o~~L=. 4$ IS <. ~ 4 Su. Z),(oOQ p>i 94co~.4-S = l4,4ao, THE, 8 Z.AC-MT iS ACE- PTA,EbL @gal C ~wc.w A m~rom ~ ~ G a~~~w LOAZO CV 'd~L> = ( +~~~ = z(.var)(.ai p= .44 LE-AQUA H ot- QELH = F7 i 7 Qt (HMG,LE-c'TIN+ Pt~) Tora< gas< (<a,76)(g<) = q.el,~
6 = 0494 ~si < 2i 4 OO ~>i k)HL~ i~ A~~wT ~Eh I c= r b PATtr'6 4<C>C.ySI5 SI&jt AQ To VA6 S'rg C)Peag ,ag, 7 WE'r=-4b STRCS'5 r5 r d W SUCH WiA~ nfG STRESS +r446'< rS r Ak 9CC,O~ y4e ZAr45e 41VGA 8y'ISC,, D~~ C&r7-roN, SGQv rortJ 8 r4PP<rJ+rg tooe oo
Prepared By: Date
~~'alculation Sheet Ghee ed By: ///Z~/92 project Job No. File No.~~
IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject ezo44 >V.CI ~t= Sy t. Sheet No Analysis No. ~4 ~ Rev. No. 4. 5 3.z.4 'renow-
~~~~+~pelt y~+(ct ,.~r~ 4/sz/3 4.~.3.4 QALYSIS aF ~a IW 'PS~I C.YL I &DE'SSUME:~~~~
~~~~(,Croe m vcc,zcOD or-~~~~
~~~~= l2. O'25 rNpo<nwne .gD = l2.o~~~~
~~~~(.I2 t 25 j2.o ) )2 op~~~~
+
~~p . 'Tl (r'L.V?.S -12< O ) pZ p Z r~ 4 4 o c.Y~i ~a (Ler. 5) C.YLI%DE.R ~ I~.cg (.~S>)HT Se) = i( 3.S Bt Or XS: Q,5 (I'2.75) ( 28)( ) ~~~
~~~~= 22-7 BA aS:~~~~
Z(a)(I.2.S)(4~.SS)(.ZS) = IOO.SS Pl STOM: (Qg.gay $ ,5+ 4.375)( M'5) &9 ~ 6 itE, RODS (q)(+s.ss)(.ass)= +i.7 iCTAL, ~Et'
Date Calculation Sheet Fz jr~ -o~ 8: Project Checke ill~ a> Date k Kit RQ&UA.Lt%'A'TtO'N Job No. File No. IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Q,z.o44 >p. Q1 F
+
System Analysis No. +I C ~ I Rev. No. Sheet No Oygoo i- cf.3.E.ZS Q ~Q~~LC. < A.&~/~~f~h; l2. AJALY+iS, (Cc ~) CYLI AVOCA. (C re~&-rT~m = DtS~t-= Wi8c~r mO~ta~ ~ C..C. rnom~~~~~r <4 SS- (Zi.~s ~(i~ 5-4.~) = lW s".
~~~~= ( ~4 5) (>+3)(5) = 422,C a ot S~E.~~F& ( X ~~~~~
~~~~E) MY - Xa~~e . ( I '@<- ]. psi T 229~~~~
~~~~~W( ) ss~(<)~~~~
I Z.~~ ESSES FRo& PREssURE. AXIS,L t j~~(~) o c' A<ini Zg g(.~~ I) I i-IoOP: < so 'a) l. Z)ob F'=i
Calculation Sheet Zg Checked 8: Date
~~~~!rf~ le=~~~~
~~~~Project Job No File No r t r IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject IF Op~i M Op~~~~
~~~~~z~44 1 ~- 0) /F 6 ydgc or- 4 3.7.2Co system Sheet No.~~~~
~~~~Analysis No. ~OD . Q l2.'WWLVSt~ (C l)g~gfntwA ftOA Of- R2I QC, I f rM STOIC.5~ F5~~~~
~~~~+p5I PR,tWC (le 8 2+1 t ~~.p PAL t'~~~~~
~~~~I l.bs 2+ SlMSS~Q:~~~~
~~~~'/ v)p OPGtp I+os 3,~~~~
g
~~~~+Re =-7S r) /~~~~
Ot
<<SR,>> '3 3e ///
j 54l 2 G~ = zdsD p OPCa. a mP==." 5 r-') . 7i'+
Prepared By: Date Calculation Sheet I//go/43% Checked 8: Oate
, ~ PP&~-<~i~uic Job No. File No, IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject ~ . OWL.EF' I Q e ~~44 lt~.OI e ystem t-~~ .T R Sheet No ,... Q Wi~aor- cf.S.Z.Z.7 +e. tZ~~~~
~~~~D.~~A- 4/z2/b3~~~~
~~
12 @+At YS I 5 C o SZ'~ = 9439 pst o~ Q~O~A<~t E. - I 8 OO~ pSt
Z g~ Oate Calculation Sheet yg/- gsz. Checked By: Oate project S SKEW \C IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject
~~~~>>4 r Job No e 2op4 File No.~~~~
~~~~1F .~> System tW Atm Ot Zt. A t Qp Sheet No Analysis No.~~~~
~~~~r. 4.3,3.zS F'//ac I2. Ruhr sly c~w t5. 5 '2 I XF 5 rRuuto Q s Ptm GScs wmoac,~~~~
~~~~)l(yea~) M.: &IS Hb. S BRACKEi WT'~~~~
~~~~Date Calculation Sheet (( ~./e~ Checked y'. p t i >>RS - +NtcWie i Job No. File No. Subject System~~~~
~~~~&ZB+ t It .ol F Sheet No. ~rumor- 4. 3, Z.Z9 ~~~~~
Rev. No. J e ~~~M+lc.l A ~~4 zz/sz lt A~ALYS t 5 Co ORcES 8 %AH<<a PlQ H= @ger 5 depth, = lb"
Prepared Py: Date Calculation Sheet rr/- /e Chec~kd y; Date project 8 ): F & ~ 'Kl-II C 1 Job No File No IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject Awt OM ZCig4 I P C)1 F System 4 tW 0~%4&Q Sheet No Analysis No. Dr<~~r - 4'.3.9. >c
~ A,<95 i - 24,r025 iO.OI ce. ~RCE.- DvE TO ~v t5 Rk&VRA.t~ Z-C iREcA) 2@= F~ 9-~c c~=P (oad af cvu~caa = G8s 'Jt1) =<5'311+= 1332 4 F~= F~t I c F, - l=~ Lc ZSzz.~e,) .94 8 e Wir >S r
p;.(zs~z 94'= )(.40 O Ot"- Pi~ Fc-P-t c. C,'Vk ~ C t "W1S ..=-V,~~i (,.'/ "~tk"- i "~) F~ = F( ' = 948~ si)= 2.99 Fc/ - fzf7 1000 00
Prepared By Date Calculation Sheet I/ ~~ a/ pn Checked By: Date Proiect ~l ) P M K. t~~l ~
~~~~~"3 k Fk Job No File No IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject 1~~~~
~~~~SZ.co44 tP. a I System spt OP ~AT 4 Sheet No Analysis No. Rev. No. 0/gcor- 4S.3,3I~~~~
~~~~~~ p&J~ 4/z 2/s 3 AM,Pt +5t'5 ce Fo = s&>gG 'ToRQ vE, = 75 Q l~~~~
Fy~= FP ~ F,~I= +F~+FD F~= <ZAN+ ~gay + ~<gg '+ (gO >, lyI SEAR t 4G ov SvPPoR., 8 ikQhJ IOhJ P le BC~ t wc ~c,~i =
~~~~~ = LD ltd H &66 L = +t'Kc. Xr4 c~~ r QF P~~~~~
Dt~Vv,<~X, Ot= Ir f = j~ ~ l. rS F;B, = l. - (j 7Z) = 2. C ~~ Br~Atting 4f c.g 1776 /sr Ikey~ Vr'6R A ~G r A! 24'> '+.Q~Ow(>> p t - . t "ay ~Z.,+ I C(~g<r ~ t '45L ~ ~ 1008 00
Prepared 8y: Oate Calculation Sheet //fr~ SZ. Project 4 t P' 0 4= E lt C
~~~~'ii~"~~~~
Job No File No Z j l I t GAMIC)N 0 I /I= IIIIIIIIIIIIIIIIIIIIIIIIIIIIII I 7 &44 I I - Sya<<~ I- tW Q~(2 A r QQ Sheet No Artatyala No 0 (QcQQ ) Re> No r Zr8ool- 4. 8.Z BZ tX" AWOL. SIS CI-I&.C V. SkaC.ICa i FC~ B~C tMG A I I SHAFT ~~i C-1 QJCl ~ I Cga CYc<~vCrt, CC cvrroat I % v pr oft C(b c, (L,lu0&L N/i 58lo' W= 58(n %=683 Zo.vS i 7.73, i7.73 zo.78 IH> wow~
~~~~~11AM (p~ q) 'Ecwou PRoraamas".~~~~
~~~~L= 22. W=LC TH I C.K.hlGS'5 mt= 4- 5~~~~
/g
~~~~(~M ~S mot 6w>st' Mtmsmv~ 'SCCA~)~~~~
~~~~'z<(.s)(,zs) (,>z- z. s)(.s)(jr-.7s) 7g s) + (z,~- z.~ s. ) (, r) Q5'2.(~~~~
~~~~(.S') '2g 2., 75 } (,$ ') )g t2 IK ( )(~~~~
~~~~+ (22. -1. 5') (, 5) (,~,~~~~
7 7 q P)- p = l441 t~4 t => t- Pr GE
Prepared gy: Date Calculation Sheet i /:~/s~ Check d Date 9 SS SWL ) MLC rd e 8z-f~ zw 'F L ~== Dalkon Project Q138 x~ tC Job No File No t >tQN i~-ot IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject SZQW F System Sheet No. Analysis No..
~ggcol- + g p gg ~Y '3~ giz(g A-tuAt YS I 5 (.~~
~~~~4 OI= BRACKF t St(~~)(s.) (~) ~ +I4(.<<)( <>(>>-t~) + 91 ( E<) (, 5') (. K) y 4 ( t 4) ( S) + 2 ( s) (.7 $ ) (>>) 1~~~~
~~~~+ 7)(i)(>$ ) ~ >>~~~~~~
I'?. 75" 7 (a')(,7 p) S~Dtma Srkca
Preparedgy: Date Calculation Sheet g P ~MS~ ~.l:- Jew Checked y: Oate project ~ PAW- W~x~W t rz,/> aa Job No File No t= M l ~iC~rtO>
~~~~'& OP S7 44-1 IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject 1P. Q I F=~~~~
~~~~System I t Z AWn< Sheet No Analysis No. I ~~& l Rey DP woe- 4,3.3.34~~~~
~~~~12. ~D tg tS Ccrr >)~~~~
~~~~Ax tat A~,= 4~+ ~'> 5') (,~) =~~~~
~~~~+X IAI ~2.84 i + l ( gb, ~ 7gq = Zl 2+3. $~~~~
~~~~gA . 2~l2 Z> ~ gg P t B~oi ~ 2.~4. t 205'Q' PPg 7 0 (~cg~ ~ lAJP~<~~~~
~~~~= s. o (>a~ >> ss>) = s.e, es'(5)+ ~ ~. = ~5S 4~~
Date Calculation Sheet rz .=.~/e-Checked By: Date P K- Swiss tc 8Z Job No File No IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject 6zo44 1P.'( At Sheet No Analysis No.+ I ++ ~ Rev. No. c>Y/oor- <.3z z< l2 ~At YSts
~~~~~ ~ Stet E,~~~~
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: Date WPPSS E ui ment Seismic H drod amic Re ual. J.E. Rakowski 4 22 83 Subject Checked By: Date
~~~~~ ~~~~~
g+ Job No. File No. System'nalysis 82044 1P.01 F No Rev. No. ol~ t B.B.s,36 lz AMALvsls (coNT ro) DIt! IIIE. ot) IO.OI Zl.57 LcC 0 11 L7.11E 2- A.>os tf 13SE, gg lO C1OIPOEf-C pglug racO CECSS SECWOlOAL PP E.A Fog. CO 9 9P'R.IIII;l t SPh Fc = LcOo O. NA +oi, = /O~l r. E9r3(3+1)= 'Bsl LgQP ZS Mg= '7.I~+ F = tHS ~-q NATL: 4r% -4I Q g@= Hg Q~ (-(ss ~ .4%~F 3l,ivz. Az
>g . I 3$ '3 C)K 8 c.yL S11EPP lOo V GcuEESl <VG PER 'KC lO A/o ANAL ySES) ev)a R.oo ATIG, EIJ I) 4 ~ Qpg 3Qf PSX C $0 ~ p5 p $ >RESS kRQSE <>~QQ p p %3tPH tc 0 M, =
1NAc + oj> 9 lcc = 553 o'5'l lo.or= Z.9,1"l9 lilf 1OOe.OO
Calculation 3< fit Illlllllllllllllllllllllllllll Sheet Proiect Prepared By: Date WPPSS E ui . Seismic H drod amic Re ual. J.E. owski 4 22 83 Subject Checked By: Date Re ual Z'ystem 0 tc 82044 1P. 01 F Analysis No. Rev. No Sheet No. 018001 d.3.z.z7 Fz~.= r ~Z-9 Br ZZ S9 x iz..cs (p s" m) F<< - (Lr o~Loo,) ~~~, (zsqio.oi')yA>%(+g= VS'i g Lg p z
~~~~?5'~ ~~~~~~
2.
~zest 2. ~S. Ws8 g FsT> = 737 IIja. (~ o - /OSdg-F~g(g g~ ~3 z fz Q (.QN.OWL ~~~ pJw.)
j.
! Fzg+ F~.z ) <<( + Fscac. ,'1s+ Z.QI4 cjly~FE IL(zzS9+iqsg) + lGS7 )+ lv3a (a~i 9 UPI'o rR, /san. Qo =C o I~ Sf/ fop. Sa rk dMl Y SoLV WGHStCH = PT = l4FB t hhhX +ass +Ll Ag 41 2ht. 'FA g Ir Alo PlMSHSt0NS FOR- Cozen SEgV h O(DM lted.'l>~ earS - <.l+
gg I, Iq to I+) = . 334 Co(A&t+0 f(O~ 0 1005.00
Calculation Sheet llllllllllllllllllllllllllllll Project Prepared By: Date MPPSS E ui ment Seismic H drod amic Re ual. J.E. kowski 4/22 83 Subject Checked By: Date O System Job No. File No. 82044 1P.01 F Analysis No 1 1 Rev. No. Ol't Ml - 4.9.3.36 5"Sz (r%$ +lo ol).//so) ~
~~~~+. Ztt'-',lS.7>)0.Z) D (IHgZ= s'R4+ ssB.Pg, Zd ) zg g i~~~~
~~~~Pl pg = E>i5'7~~~~~
~~~~/AA= l,rs3~55/)(7) j.) P). l6,0 t yl = j+'f-eZ. mf /-ss-- bs~tss/.I. )=~~~~
~~~~IKS Wl.S4 = I~ 4F r~) Ko 575 + /4A.vz + lcm~~~~
~~~~- /z. s/s~~~~
~~~~( ao/ am> ov ps't Holt~ 3s(sw s,7 its.>sX.so+) w(..ssq3~~~~
~~+)oixs (rop A 3o7) eoL'g SHE I (s+ /e) t = 1-s~~ + s~$
l OCd.00
Calculation B A D t Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Proiect Prepared By: Date WPPSS E ui ; Seismic H drod amic Re ua1. J.E. Rakowski 4 22 83 Subject Checked By: Date 1 System Job No, File No. 82044 1P. 01 F Analysis No. Rev. No. Dl b~ I c2.P,3 gg p~t-w gN E+ A. ~F mo ~R.l~w vzc INmztq: S<l-l = (~pc +'DSD,) + gv
~~~~%Ay StH - II69 W I.S f IS<7 PSX'339)~~~~
Il E.RttCCIL + DE.RO uJEtr" H V QcL,T' ST'26.95 llr 'r ( l+I Qcl-) ZZa.Z PS X 4Al, ( S(g ~ S)q ) = 2S'9tt PS l ADD SIIEAR Sa(JESS Dug. >0 TOgQQ E (= pM>>+l9+< 4339 psz c ls;cDD psz l'Ew l3isc H~v't sec lr x z.. Azoic . (I S+S)
$0 rE: QC t-R--tl C.u L Pre ht l Sit t=ag tX A/O BFc AUSE. po HwQRogyNhM tc Iagg C y C, t I al 6 g ~ pE g. IEPCF 5.
~~~~Prepared By: Date Calculation Sheet Checked By Date~~~~
~~~~~'I Project WPPSS-Seismic l2- S-82 f~~~~
~~~~Requal ification Job No. 82044 File No. IIIIIIIIIIIIIIIIIIIIIIIIIIII Subject A rr 0 . rw7~"r Sheet No dr8oor-Q+ REFERENCES~~~~
1. 8" Cylinder, Dwg. No. C-26096, Flick-Reedy Corp.

2. 10" Cylinder, Dwg. No. C-26045, Flick-Reedy Corp.

3. 12" Cylinder, Dwg. No. C-26093, 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, AISC, 8th Ed.

( 9. Cygna Calculation, 82044, QID 361106, Dated 12/7/82, Rev. 2.

10. Cygna Calculation, 82044, QID 361104, Dated 7/23/82, Rev. 0.
~~~~QID 018001 APPENDIX A~~~~
~~~~SUMMARY~~~~
OF A/0 MODEL USED IN PIPING ANALYSIS
Calculation Sheet llllllllllllllllljlllllljlljll Project System C S'ob 8~>- s VpN ~c A~a f~ Prepared By: Checked By: No. Sheet No. File No. Date N OT,oj i 3 z4/z 5 p) op L Cot Ft U ( tM CeNV~oV y M@ (EHD RELAAS<) 5 TABAC.[ERAL lhEPA QEk DtREc.r~5 g) gC1UAb gTRLIC'TIJIZE (9 +x
~~~~-v Qz qx yz - e~AVz gx Pn ~y +v Qe -v 1005 00~~~~
Calculation 1 ~ e Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII By,'ate Project System Analysis No. Uv 8X cqP I'5 O'Ae c Rev. No. ATo Prepared Checked 8y: Job No, Sheet No. gga g ~File No. Deke 0 r. 6 I /F WIIO + %tloQ Q VAivE. EARS Jl 8 ~ y~ (24 v4tva) IO, pig Oui,'4T Ag =Ay= Ap = fs w 2I 4 Jx~= Iot Os'l
~~~~~v~ = I/.Z "~~~~
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~~~~4 lo p 255~~~~
~~~~- +~~~~
I y<> lmrO IH, tgog 2.I(a 19 4,22. (4 C< -..ES IH .'3l 5 C~ = sit 6 Eve
~~~~=25<<> PK F = II.Q +IO PSZ A = Z!r.S (. IK . dOdch, ~ C&)~~~~
~~~~Q3$ EtVILKE 7 OFFSETQ E = S Lg- tk.stS~~~~
~~~~'.o" yh~mLrss, e Stoic .t'E.E l r.s~s".ltt .)~~~~
Qy roke L<kyK,~ S (B r ~8 $g Fard. ls yo yyo< Qy, NQ4)
Calculation y'k Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Prepared By: t Date e Pfs5 Es Checked By: Date 6l P >/ A6. Acyl A. or-'.s Ap Job No. File No. P bT'OI 3btt Gb~ 34tto Sheet No. A 33
+5 SHAF' OFFSET II R i@ID LIN g l4 +8 Log& (I +.5o l AW SZS 7 bS SI+ ~P Pg SHEAF~ = A= +el iw = 'j.,5Z (hi 5.o+
g)v = 5 )5 i.za>> I PZ. Cy = l, Iz.5 g.zr Cq i. I Z-5 i. z.C R - 2.'I X-(O~FZ= llew/ I6 WL i+ I~. 12.'g S Ql Dt:ivE RoD Z.AI A >= Z.Lft P~= Zgt lg 24( IP a 4G (AJ
~~~~.'7Z- I~ .92 IN C.g = t-"p = ~78 IP -52~~~~~
~~~~Ht& g g E. = poXIO ~W Q= (Zg(d t'llZEP.~~~~
~~~~< c.yuNDE:g PUT Q=o + h&p IS.S ~~~~~
~~~~Eyy~~~~
~~~~=I+> = '7Q lb' Ir'005 tt.x,= 4 gq = 5, 2.~~~~
~~~~Ax= Qy= Ap=(r~~~~
~~~~~~=%= +~~~~
00
Calculation 3'. rii IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Sheet project Prepared By: Date Subject Checked By: Date System Job No. File No. Analysis No. Rev. No. Sheet No. APPENDIX B <t" AIR CYLINDER BUSHING PRESSURE EQUATTONS 100 s 00
Calculation a T J Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII P Ps> Q&j'sF'hecked A IR CML(40Ea Ea
~~~~'MtA Prepared By:~~~~
~~~~Job No. By.~~~~
+~
~~~~g ~ P4~ "" File No. Deke~~~~
~~~~~ (~~~~~~
Analysis No. 0 +co 1 Rev. No. APP~VlL~ 8 - C .l/~ AMALySIS Fog . u BuSnldS S - Lo O guSHI y & PRES,SQ g.5, 5LlSH iHG PORC f. A RsA Skl H cfog ek'yG d k cd c cULA Y o e\- lrdkhyk F~ ( +m c:Qe=v(c L,r-B~e,~ Ce< e = ~(i dA FdP Scd'Chy 'lt Ig 6 lO Il Ajg p 2'.0't5 ~ 'Z LA >k '5T cAGE P @ ))ATE VE.-O~KV~ &HFDF L~~ IS, tAykiMykged( di IS VtM I Mu M ~ IQ g~ga vE IN ~CH c Q>p,
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Calculation T I s ig t a Sheet H IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: v 0 , Date
~~~~<I'K 3 gl I'F S5 >~~~~
c.st'Z044 P. Subject AiR. t-M lN PEf'OS'N >AC System Job No. ~ File No. CF-P GP.OI F Analysis No. Rev. No. bi'K<> 1 AIPEAPM 6 FOQ C~ lU &OP " 1'.jV P RP I JU OjwlV F'oo( POP: lo 4o'3 z.0 18'
~~~~~larsal A@~~~~
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~~~~'a T 9 I= SI2-SS 1'AGE.~~~~
100 d,00
Calculation i Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII prepared By: irr \ fl . Date N Pf'S p I Subject h tE aYLINO&R BOSH thlC fWESSURE Checked By: Job No.
~~~~$ v'A ( ~ File No.~~~~
Date CsP eW ~ Analysis No. Rev. No. 0l Bool PPPt=V DIX 8 f'G. 3/3 END OF t'-VL,>HOP/
~~~~~6t IS.S 40 (~g)~~~~
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~~~~'l oFiMB<Ib~. I-t = I-I'7 PE (.+~~~~~
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: Date GS Clef>&84r AcJi= rra Subject Checked By: Date A R2 MQe
~~~~"'" dele W Job No.~~~~
Zdd File No. dQ I t"- Analysis No. Rev. No. Sheet No. Cr8 0 /8ddr A+CJ /4 2 P6 fQ EK7RAAd W~J44 A>P+rJ 6 r x, 8 WPP4dd C4 AVQ rr/PF'C.Yrn/ 4
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Calculation i~'j~ a B = Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Date QPP~~- E ///Ai - r 8 n Date AiA>L Cz~ R 8 ru 8 - /2 System Analysis No. 0/8dd/ Rev. No. Sheet No. A/P~rJcliv f <h. Cbrit(8 ~ 6'Z'8nlkCQ Chef/5/7 /qg 9 P CY/4tj4& Ed'KT ~JDCfl ) C. Qwuze <'/r" eudis) 4~i04
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QID 018001 5.0 CONTENTS 5.1 Response Spectra 5.2 Walkdown Sheets 5.3 SRM Sheets 5.4 Load Comparative Sheets 5.5 Revised BGR Inc. Piping Analysis Accelerations
QID 018001 5.1 - RESPONSE SPECTRA
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5.2 Walkdown Sheets E UIPMENT UALIFICATION WALKDOWN VERIFICATION FORM EPNg CSP-V.- l IIIIIIIIIIIIIIIIIIIIIIIIIIIIII OZDg t'. l I 0 ( BLDG FLOOR EL QO ) COORDS MFR QX F COMPONENT EL 5 O~ DSCRP o" FLY moog zoG+43 SERIALg MAT'L PSI 3 oF LBS SIZE ASME CLASS YOKE ORIENTATION MOUNTING CONDITION J To AXIS OF PIPE ( ) NO OF BOLTS
~~~~/j TO AXIS OF PIPE ( )~~~~
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~~~~E UIPMENT UALIFICATION PAGE 1 OF~ WALKDOWN VERIFICATION FORM~~~~
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user numb er 43, date!time 02/10/83 09: 14 function PIN -SRM MASTER EQUIPMENT LIST-EPN COMPOSITE EP N 2-CEP-AO-4A 2-CEP-V-4*+ MTRACT MFQ MODEL SERIAL NUMBER 68 NBBB ABBB '73354165 DESCRIPTION AIR OPERATOR FOR CEP-V-4A LEVEL EC USE HOURS SAFETY FUNCTION ACCURACY 2 A 2 3 1. 0 Ble F A/E DRAWINQ AE ZONE BLDQ ELEV DETAIL ZONE ROOM M543 8 49T H. 5/5. 4 R32 SEIS. QUAL ENV. QUAL QUAL STATUS TM FREG QID HL TEST ANL F/0 C AQINQ DBE C SEI S ENV Y 01 A P 10 018001 MESSAQE PROJECT TITL.E PREP E BY DATE CBBC~KB~ DATE W i~'9~ JOB HOc FILE NO SBKBT BC
user nuiiioer '~v '0 ll4i.'H/BE/ cfog lW.'tel function FEN -SR M MASTER EQUIP MEiNT L E ST- t +i EPN COMPOSETE EPN 2-ROA-V-1 2-ROA-V-1+ "ONTRACT MFQ MODEL SERIAL NUMBER 8 B250 0657 7229-1 DESCRIPTION
84. 0" R BLDG ESO VALVE LEVEL USE HOURS SAFETY FUNCTION ACCURACY 1 -0 4320 B2i D A/E DRAWING AE ZONE BLDG ELEV DETAIL ZONE ROOM M545 F3 R 578 N. 7/5. 7 R73 SEIS. QUAL ENV. QUAL QUAL STATUS TM FREG GID HL TEST ANL F/0 C AQENQ DBE C SEIS ENV N 02 0 A P 14 361101 MESSAGE y
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user numoer 08'ce/'clme vol Hc/c4 I t: 0/ funct'ion FIiV -SRM MASTER EQUIPMENT LIST-COMPOSITE EPN 2-ROA-V-2 2-ROA-V-2+ CONTRACT MFG MODEL SERIAL NUMBER 68 B250 0657 7229-2 DESCRIPTION
84. 0" R BLDG ISO VALVE LEVEL EC USE. HOURS SAFETY FUNCTION ACCURACY 2 A 1 0 4320 B2. D A/E DRANING AE ZQNE BLDG ELEV DETAIL ZONE ROOM M545 F3 R 578 N. 7/5. 0 RZ3 SE IS. QUAL ENV. QUAL QUAL STATUS TM GID HL TEST ANL F/O C AG ING DBE C SEIS ENV N 02 0
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REA-Ftt-IA AKh"FN-IA+ H545 J5 J127 54-26 I/2"1770 2 a 33 AEACTOA BUILDING FXHAUST FAN R 572 HE 2/4 ' 2"22A P ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ t~~ ~ ~ ~ ~ ~ 1 ~ ~ ~ ~ t ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ I~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0 ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ BKA-FN-IA+ H54 5 JS I tt 33 REACTOR UUILDING EXHAUST FAN R 592 HE 2/4+2 P ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ t~~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ f~ ~ ~~ ~~ ~ ~ ~~ ~ ~ ~ ~ ~ ~~~ ~ ~ ~ t~ ~ ~ ~ ~ ~ ~~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ fIEA=F tf-1U AEA-FN-IO+ H545 J5 J127 54-26 I/2"1770 2 33 REACTOR BUILDING EXHAUST FAN R 572 HE 2/4 ' 2022A P ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0 ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~,t ~ ~ 4 ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ t~~~~~0~~~~~~~~~~~~~~~~~~~~~~~ '
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~~~~6. 0 DRAYINGS USED FOR PXQUALIFICATION Contents BIF Drawing A-208293, Cylinder Support Bracket for 8 x 15 Cylinder Operator, 24" Valve.~~~~
BIF Drawing A208195, Cylinder Support Bracket for 10 x 15 Cylinder Operator, 30" Valve. BIF Drawing A-208274, Cylinder Support Bracket for 12 x 15 Cylinder Operator, 30" Valve. Fli~V, - Reedy Corp. Drawing C-26095, Certified Dimension for Model A83B Cylinder, 10" Bore, 57 5/8" Stroke. Flick - Reedy Corp. Drawing C-26096, Certif ied Dimension for Model A83B Cylinder, 8" Bore, 46 3/8" Stroke. FliCK - Reedy Corp. Drawing C-26093, Certified Dimension 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 TRANSMITTALS USED FOR REQUALIFICATION
AlgllessweeettlwstslgltesaepaasR>> t w1 jw
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- --GE5fSMO,'018001 Design Criteria and 03.8009, (A/0 an 2P~ameeer fata'), "~;~4"...~. ~e'leeon~ ~D"...-.Pflam,'"Coal K. Hsieh, CES/SDAO, -Specialty Co. and
~~~~{A/0 Design Crit:eria) ZD 018004 a d 018009,~~~~
< . Pagoda~'..t +- ...,,5.-, Tt gecons John kfa'r't'in%of Miller 'and"J.R. Rakowski of Cy~na~nrdpMarwices. Air'roducts ) 12/23/82, Ari Cylinder Side WPI+ M and BushQ.ng~eads'>>t Lead.Crireri t<>'
~~~~Cyl~ngeg c) 2/10/83, Bushing Naterxa3~~~~
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~~~~Subject:~~~~
~~~~/ID inf018001 and 0180 'Acr-4pera@r)"-' "wpi'ec: ~--gD~O~~~~
~~~~Participants:~~~~
a
~WE Ole <<J<<<<JJ ~ Konstantinow of Miller. F ~
~~~~V~ V Ra ond Hsihh of CES SDAO mw~~~~
,'of r 'J ts s ~ e Item Comments J u t Req'tf Action ~J }C, I called 0)eg 'ibo&uMR detailed informa'trop."of 'the sj~V oper~aor" (P', 8" hand.lg-'~.Eo~e)'for.,'.the 18",24"; hir'ylinder 6
a
~~~~1. The air and spring cyli;nder>>6p'er'htor,,is'not.inthe Miller's catalog and,it,.~i s.a. special design~'P.~~~~
~~~~v W ar~~~~
~~~~2. The sizes of the air cylinder's...are,::~~~~
fw
~
~~~~(i ~~~~~
~~~~~~ '~~~~
OD ID 10n bore,.... '10'A25".;.,'~; . -= 9.;9K .": . m 6n . bore--- ~28,5,".' '5'. SPj'<<JVJJ<<<< se J IIJf r The matef'i'al is ~<<<<w equivalent4to'"ASTM ru 4. A519': '~ w<<a<<~JJ<< a wa a<<VJ Jv ~ J<<JJa
-~ . pr
3. Miller Fluid Power does.not calculate IIELD the GG lo'cation'f'he ai>> cylinder. In oftrJ case, BIF calculated tlieJ Ctl '",
~~~~f 1 ocatio o +e+." 8"",'rjd 3a', J '~k M~yl'inders>.~~~~
~~~~'4,,'J fw" The'pring inside the cylinder..yas designed"bywti3ers, p>>'.~~~~
~~~~and there is no record in the file 'indicating'who desj.gn'ed~~~~
~~~~'I 7."~~~~
the spring, MFP ordered, the spring'ith this infoRnation; ie preload, final"VdSf> Itforf< 'ftVoRep
5. Oleg gave. e ncaa.l-sye~tyf. -company which~dt.sigrted , ggs=
I most ofj'their hir-sp~;cylindeC's'iiot necessagi3> <he one h wdofg esd-ntbee;spri gs onf, 6018001 and'rgg)8009). J 6.'leg prhmised to seiul'fse':scmes'ketches of theicraf ra'rjd '9c J' spring ~yonder ctes<ign.' c
~~~~<<8 e Signed:~~~~
~~~~a Page~~~~
~~~~;f r,~~~~
~~~~V Distribution: ~ f1 e } 102030~~~~
~~~ t Communications iB B =ti h r & l Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Company: <<)P, vb" Pelecon ~onference Report PtoIect. lob4o.
~~~~lc,r, ~ p., g Xlgte: q Sebf>> l.~~~~
~~~~~ID 8018001: and 0180'09 (Air Cylinder Operator) '~~~~
~~~~of of of I re Req'd Action By~~~~
, ~ 1 r fa .7. Basically, ihg. assembly. of,.theingegpa] components of an ajr-s'pqing.,cy]ipder.Be";,j pre]opded,.corn'pressed spring -.w'it)-a'concentrate.,jp'ring stpp'ybe'(welded'to the end I cap.plhtqf'os'nerend-ofittjepiston".':. 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;hepiston,".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.
~~~~v~ Ln apse the,drive rod:js removed-in~thedirection which causes 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-tudeof. this.'hruusk.~ A,ske)ch of g e.',air=spring cylinder ~ ...: operator.'is fly++,gpss.,
~~~~as'6'ei.ow':~~~~
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t i'<)(r ) r'n Co mmunicati@tta'--',-'=-':=" .a.ni Mar'Va R eport ~," aa
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~~~~='IIIIIIIIIIIIIIIIIIIIIIIIIIIII I ~ re ~r~,rarer~~~~~~
~~~~0 Company: CES .....A,.Jemooa.......... 't r r~~~~
"".' 9 C~~nrerencm~Report ~ a mors, r project: Job No.
~~~~82044 Subject Washington Public Power~~~~
~~~~Participants:~~~~
/ID ¹018001 and Supply System wow wire 44 ~e~ ~err PAN 018009-'sAO r Rick-R~ cap&o. Awe ee'oteew of H%F 8 Par nd iisteh- CES SDAO'f Item Gomments- ReqMAction By Dwg. ¹C-26096'rawn'ry,F1ickrReldy'orpnoration',(I'1iller Fluid Power Div.), indicated'thatboth.the "fait. "c'toshdu (CSP-V-3,4 and 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 mentioned in 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'hiroughthe"BIF"record award cnonfiriiii d 'that the in/or-mation containelqin'w'g." ¹C'-'26096 'fs.ihcorrrec't". 'Therae should be two types'f ski'inrg'ene.foi',the "fail'cl'ose" ;'design which has a sprin'g jYrelOrad of 1'500¹'ndifiiia1 load-of 3,000¹; the other type o7 s)nhg is 'fora"the "fail open" desig'n which has a 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 could be exerted on -thepiston. -This is sufficient to overcome both the spring...final..load (],/50'.,and. the;seating torque of 1478¹,-,'l6ck aTso .'pointed'ut that all'he valves 'orce and its ai'r",cyTiiiher ope'razors-jtave+een -tested for the operability (to open-and close).- From thts Telecon is cant be concluded"than"t-the valves, EPN'.¹CSP-V-5,6,9 (the fail open design) which'PPSS ajTe'ad(I rFc'eivEd; are properly designed except the reco'rd of the spring forces (inside the air cylinder). are not show'n 'correct'ly. Rick indicated he willi send me the required information to clear up the spring forces problem.
~~~~2. Rick will also send me the support brackets of the 6", 8" i and 10" bore air cylinders.~~~~
r coy rerrrr 6 %4'wwH r eaerrerr areal m Ae'&w444 AA1%%a %r r% err ~ I ~ Ir+ r Ar ne Kerr e Signed: Rage ...1 ~f- .- Oistributlon: ~e ~ ~rr~ 1030.00
~~~~. -RtP Communications~~~~
~~~~~~ jk=3. f ~E % P, r~1 EE Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Company:~~~~
*~
~~~~Itj Teiecon x ct Conterence Report Project: Job No.~~~~
~~~~Subject:~~~~
~~~~QID f01mjOT-.:antn~~~~
~~~~< E ISm'ime: )E Ml 1 dt <E E % <~~~~
~~~~piece'.~~~~
~~~~Participants:~~~~
".~r 1C, Comments Req'd Action By 3~ I 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" and nfail open" designs). We concluded that the CG locations of the 6" bore air cylinder'fai'1 op'e'n<<des'ign, Dwg. 8 A-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 (fail closed design) and'wg.- imIA-206765 (fail open design), both have the identical CG location"yn.,the,gylingens.; There are possibly two mistakes about <he; CG.;location on the 8" bore air cylinder. First, the "fail closed" and "fail open," designs could not hav'e the same CG .location because the "spr'ing and'the. spring storpi tu%e're'.lo'cated o'n 'the opposite-and of the"cyAnder'o'f""the 'tW<o 'QeEsigns.'ote that the spring and the spring stop tube are located at the op'p'oui te'end." of. the air'rr1j t~" ~tI;<he'"two.'"designs have a A E differ'ent'ocation 'o'f th' air'~hl'et "(at" <he."opposite end). Second, the CG of the 6" and 10." bove c'ylinders pre both loBte'd'near'he center of 'the air cyl'in~Ier".E ""Hot'lever,, the 8" 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 find thyrse"'ca'1'culatioris;- he.pr'okised Cb. i4'nd, me a'=letter stating that the"CG '-loca't'idn oY'the 'f"'"b'ore'fr'rcyfindev" h'ave both the "fail open and fail closed designs and can be assumed to have the same proportion as that of the corresponding 6" bore cylinder (fail open design) and the 10" bore cylinder (fail 'gg&
~~~~i closed design), respectively.~~~~
~~~~4. The time needed to close or open the butterfly valve is appro imately two seconds (estimated).~~~~
Sighed: E<. Oistribution:
Communicaboas;=,.-,=-.-:.;.-.
~~~~'4! k3 epo >>>>gq>>fj!I ~ r>> jjc>>l,>>>>>>~~~~
llllllllllllllllllllllllllllll jf Company: Telecon "0 Conference Report Project: o No. 82044 Washington Public-Power Supply System Date: 10/6/82 Subject Time: 10:50 A.M. (ID 8018001, 018009.;(Air Cylinder Operator) Pia'e'- "
~~~~'"'DAO '-~~~~
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Dave Pf 1am f Co i1 S eci al Co . Ra ond Hsieh CES/SDAO of Item grist ~ -Comments Req'd Action By Dave exp)ained,toI me ghat,the,,spjing,manufacturer Hses the. following rulies'.'i',."'designsngi'the>>spgng's': ', '..',
~~~~a. For low cycle..spring'esign:.. ;:, .~~~~
>>>>>>yf,f >>,,>>,>p,fn~>>>t <jr ~ 'aqua =f0.45 Fu'Fb-"'='ultimate:"tensile: Stren'gtlT'f>t'";-
~~~~x " '~ "~<<b!'ateria'])'~~~~
~
~~~~b. FOr high'r CJJCle Spy!ing deSign: ir .r."<<.~~~~
~~~~" ""I, " ',.'~~~~
to" 0;35'Fu -: '<<; 3a,'I ot<<', .'!:?c t;b ~ f ~ t.!'-'0.3 max-. 3P Dave indicated::i'fr hef lffere,ifesi gnsyg. the'se, spry ngs'f th'e as r cylinder for W)PSS,ten y'ea'rs,'ago;.he wil;1, use these safIIe,rules I
~~~~2. The most comiIIon,used,,'material for the. sprsng,wpj,ch 'Cojl;;~~~~
~~~~Specialty provides.,to Hjl,.per,rFluid. Power', is AISI 51608'.Which has an Fu of 196 'ksi.~~~~
~~~~3. The bar diametep, fprf.fpe*:10",3"="ang5.,",bore.'air.'cy'lirfgr.'are:~~~~
4, Dave mention'ed pe,,foesp,.t know, th'e:fatsgue'l i.fe .in'foriiiat)'on of the .sprig .. 'HIsaid that,i;t;.,j s .very'pnusua1.'to, hear .that springs fai,lied in, le j,stress, cycles .(j ersz.than JoDI;000'.cy'cl es) when designed..'to th'e gu',lisf menQioned iri:,(1),;above.;;.',"
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Item Comments a Rett'd'ction By RBO ha oriana? veri faICari0ri ~aragaa iaIr..aha above referenced files which specify imcojnglete i,, status. These:sh'H 1 'be &organ%'zed 'into complete packace format 3q@ fa,l.ed ip, tpq,. RBQI QID',.binders. ', The completed packages are <forthcoming from the Area Of f ices"-i n~5he -foem"'o& Reezsiorf:-R ~these Revision 1 requatjification packages will supersede Revision 0 in RBO QID files. NH Zt is noted that nond of'hese incomplete packages Ig > a <,- (Revision 0) hpve,'bqen qubmittep- to the~ctS.
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ML17277A649

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Dear Mr. Schwencer:

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4.1 CONCLUSION

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Dear Sir:

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3.1 INTRODUCTION

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