Text

Qualification of Purge & Vent Valves at WPPSS-2, Vol 4: Rev 4 to Equipment Seismic & Hydrodynamic Requalification of 24-Inch Cylinder Operated Butterfly Valves for CSP-V-3, 4,5,6 & 9 & CEP-V-3A & 4A.
	ML17277B223
Person / Time
Site:	Columbia
Issue date:	11/08/1983
From:	Fernandez L, Khanachet F, Michael Scott; CYGNA ENERGY SERVICES
To:	;
Shared Package
ML17277B221	List: ML17277B220; ML17277B222; ML17277B223; ML17277B224;
References
	361106, NUDOCS 8312300162
	Download: ML17277B223 (710)
	v • d • e

Final A'< ~. ~

Qualification IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Report PRO~~ - Equipment Seismic/Hydrodynamic Requalification JOB NO: 82044 CALC NO: OT.Ol F ~

CKXENT- Washington Public Power Supply System QXD NO: 361106 TXTLE: .Equipment Seismic and Hydrodynamic Requalification of 24" Cylinder Operated Butterfly Valves for:

CSP-V-3,4,5,6, and 9 CEP-V-3A, and 4A I'i

~J.apW g Ili-"'.'b5 g~ u-tl~

PREPARED BY:

DATE n

3EVXENED BY: ZC ~

adz I 6983 DATE APPROVED BY:

kl-Ll-q DATE I

I REVXSZON- 4 Edwin/ &erne A v'~ <~.

g uJ. 4sc~M ~/i%a aaiaSO0>aa SSii>1 PDR ADOCK 0500039T A PDR

J

,I t

WASH(a 10'. ('l.'BLlC PO(VER S(al'l'LY SYt! l'EM SU PF LlER TRAYSabllT1'AL FOR i1 (AREA W(TH(N HEAVY BOROER TO BE COMPLETEO BY SUPPL(ER)

To THK ATTENTIQN DF Oenni S ArmStrOn PACK OF 1 MNP 2 Mgcfc'ta)P Tfbt!tz(I(HAsE AcENT/BUYER/coNTRAcT ADM!t!P)

ADDRESS! TRANSMITTALNO C

ouzp. essmsc na Ener H

Servi drod namic Re ual ..

Q NKW g R K.SU SM ITTAL 1111 I AQDRFSs! 1 200 Jadwin Suite 565 Ri'chl and MA REQUESTED DATE THF FOI I OWINC PUDI ICATIONS/QRAWINCS ARK SUSMITTKO FOR! OF RCTURN!

QAPPROVAS Q RSVICPI OF C*CN Q INFORUATIIIN NO,OP RCPAO UCISSCS Q OISTIIISUTION CONTRACT NO!

NO,OP PRINTS OF EACH PO NO!

CU SIP IT Tao cv Faeaz Khaoachet WORK ORDER NO!

Pro ect Mana SPEC NO!

SUSVKNQOR! CONT~.O. NO,! SPCC SECT NO!

ITEM PUBLICATION OR REV WPPSS NOO DRAWINC NOR NO, PUBLICATION OR DRAWltlCTITLE MANUFACTURER ACTION Revise s. for 018011 361106 Revi ed . for 611 6 C na Transmittal 716RB COMMENTS! (USK ADDITIONALSHKCTC IF REQUIRED) TO SK REVIEWED SY 4 ~ VCD BY! (PURCHASINC ONI Y) TRANSMITTED SY! (PV RCHASINC ONLY)

NAM FDS ! TITLE 0 ACTION LKC KND!

A < APPROVED FOR PUBLICATION I ~ INFORMATION ONLY

<N ~ APPROVED AS NOTED FOR FABRICATION HA a NOT APPROVFA7 WP'770

I

't~

'f \

qID g 361106 REVISION STATUS REPORT PRE'D BY APPROVED DATE BY DESCRIPTION REV'0 BY L~4.~mA~ LZZ'uq (o/p( t 54 c4 U Zlhf og'UMMAg,'f g Eev]se m4c788LF. aP ccwT8~75 Rcviktd Cw'tive Ca.lt. '5 l'cftc<C neW Cyl<<~<~ C(a a~8

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$ pcs'o d ~~~ c P~~

g

~

ptelacacts tOr <<~

aa 8 fy efhett.

c~ gm ss-s IHc4~c Cence dS~a4 6/ 9/83 tm co~~S C~~

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l5 NAev 4 2.) LoAC(A<A+ QOMPA4

1.0 REQUALIFICATION CERTIFICATION

REVISION+ 1.1

%WASHINGTON PUBLIC POPPER SUPPLY SYSTEM REQUALIFICATIONCERTIFICATE WNP.

QlD5 361106 CQMroNKNTNos CSP V 3 CSP<<V-4, CSP-V-5, CSP-V-6, CSP-V-9, CEP-V-3A 6 CEP-V-4 24" Cylinder Operated Butterfly Valves MANURACTURKRc BXF A-206765 MQQKLNQ aaUlraCKNT CLASSInCATIOW QZ ACTIVK SKISMIC QUALIFICATION RKMRT RKStKRKNCKs C crna Re ort Ot.01 F ID 361106 "24" C linder-0 crated Butterfl Valve" Reauired action: 1) Remove A-307 Ear Bolts and replace with A-325.,

2 Reinforce valve ear rou with 4" shear lates to qualify air operators for reauired fatiaue cvcles.

THK ASOVK 5KISMIC QUALIFICATIONRKSORTS HAVK SKKN RKKVALUATKQIN ACCOIIQANCKWITH THK CLIRRKNT NRC SKI5MIC ANO CRITKRIAa I ~ IKKK5TANOARQS 544 (I575) 5 USNRC RKOULATORVOUIQKS lACe Io100 L

STANOARO RKVIKW ~NS KSW 5 IIL~

k~g~

~

iikla~

THC ASOVK COMSONKNT HAS SKKN I'OUNQ ACCKRTASLKFOR tCAFORMINO ITS INTKNQKQSAFETY RKLATKQFUNCTION ll->>&

WHKN SUSlKCTKQ TO THK tLANTStCCIItICVISRATORY LOAQ5 rRKFARKQ SY RKVIKWKDSY

%MOD k.l 3~ %Pe

'" ala ss AftltOVKDSY

~ ~ NB~~~m DAYK

$ 44 IS$ 74

2. 0 SQRT FOE1(S) AND REFERENCES REVISION+

WASHINGTON PUBLlC POWER SUPPLY SYSTEM I i~dh Fk Qualification Summary of Equipment IIIIIIIIIIIIIIIIIIIIIIIIIIIIII QID4 361106 Ref. No.

I uNT NANEI TYPE NSSS: GE 1Y' Z AyE I I~ CLMNPONENT NANEI 24" C 1 .0 er. Butterf <<TalVe~ENT Np.C P-V-CEP-V-3A & 4A I~ SCOPES Q NSSS 8OP

z. IIDEL Nu48ER: PUANTITY'.

YENOOR. SIP 4o IF THE CQ4%HENT IS A CABINET OR PANEL, NANE ANO ICOEL NO OF THE DEVICES INCLUOEO:

N/A 5 FHYs IcAL DEscR IPT ION APPEARAIgE But ter f1 Valve wi6h 8 " C 1 0 erato

b. DIIIENSIDNSI 24". nominal diam t

~ 8475 - Valve Assv; 676N 0 erator & bracket 8UILDING, Reactor ELEyATION. Maximum elevation: 495 'CSP-V-3A & 4A) 7o FIELD MOUNTING CONDITIONS: BOLT (MO B(ZE Q MELO (LEMBTH )

8 e SYSTEI4 IN IVANICH LOCATEO. Containment Su 1 Pur e S stems FUIcTIpNAL pEscRI PTIpN Primary Containment iso 1 ation, orevention of the release of radioactive material to the environment.

c IS THE EOUIR4ENT REOUIREO FOR: Q, HOT STANSY Q COLD SHUTOOIN Q 8PTH Q NEITHER 9B PERTINENT REFERENCE DESIGN SPECIFICATION:

I I IM IS E UIFHENT AVAIlh8LE FOR INSPECTION IN THE PLANT:

Q YES Q NP PAGE I OF 5

REVISION+ 2. 2 I

Quaiification Summary of Equipment (Continued)

QIDO 361106 Ref. No.

IV EOUIPMENT DUAL IFICATION METHOD:

Q TEST X ANALYSIS CCMBINATION OF TEST 4 ANALYSIS PUAL IF ICATION REPORT 24" C linder-0 crated Butter f1 Valve*

(No, TITLE 4 DATE): OT. 01.F Revisi;on 3, June, 1983 15 COMPANY THAT PREPARED REPORT'oMPANY THAT REv I EIfED REPCRT Wa shin ton Public Power Su 1 S stems

Plus original valve analysis 3,"4 V VIBRATION INPUT:

1. LOADS CONSIDERED: a. SEISMIC ONLY bG HYCROOYNAMIC ONLY co g CCHBINATON OF (e) AND (b)

2. METROS OF CtÃGINING RRS:

A g AIISOLIITE SIM g SRSS Q OINER ISPECIFYI 3 REQUIRED RESPDNsE sPEcTRA (ATTAcH THE GRAPHs): Section '5. 1 of QID 361106 4G ~ DAMP I NG CORRESPONDING TO RSS:

Q OBE 5 REPUIRED ACCELERATION IN EACH zPA Q SSE'IREGTIDN:

DTHER (sPEGIFY) ~on 5 Attached F/B %

SSE S/S ~ Attached F/B R V %

6 ; MERE FATIGUE EFFECTS OR OTHER VIBRATION LOADS CONSIOERED7 Q YES Q NO IF YES, DESCRIBE LOADS CONSIDERED AND H(N THEY. HERE TREATED IN OVERALL PUALIFICATION FR%RAM:

lat d were com ared to the not A

ctures ana zed were art of the ressure boundar NOTE: IF MORE THAN ONE REPCRT, CIMPLETE ITEMS IV THROUGH VI I FOR EACH REPCRT PAGE 2 OF 5

2.3 Qualification Summary of Equipment (Continued)

QIDO 361106 Ref. No.

Ylo IF UALIFICATION BY TEST THEN COiPLETEIs N/A I

Q SiNGLE FREQUENCY Q MULTI-FREPUEICY Q RAHM4 2 Q SINGLE AXIS Q MULTI-AXIS Q SINE BEAT 3 NO OF QUAL IF ICATION TESTSs OBE SSE OIIIER (EPEE(ETI 4o FREQUENCY RANGE 5o NAT(RAL FREQUENCIES IN EACH DIRECTION (S IOE/SIDE, FRONT/BACKS VERTICAL) s S/S 0 F/B 0 ~

Y 0 6o METHOD OF DETERNI NING HATIRAL FREQUENCIES Q LAB TEST Q IN SITU TEST Q ANALYSIS I

lo TRS,ENVELOPING RRS USING MULTI~EQUEHCY TEST:

Q YES (ATTACH TRS 4 RRS GRAPHS)

Q HO Bo INPUT g LEVEL TESTs CBE S/S 0 F/8 0 I

SSE S/S 0 F/B 0 0 9o LABCRATORY )CUNT I NGs SILT (IIO, 5 IZE I Q IIELO (LEEOOI I IOS RJICTICNAL OPERABI LITT VER IF I EDs Q YES Q NO Q HOT APPLICABLE I 'I ~ TEST REULTS INCLUDING MCOIF ICATICHS MADEs l2o OTHER TEST PERFORMED (SUCH AS AGING OR FRAGILITY TEST, IICLUOIHG RESUI.TS) s NOTEs IF QUALIFICATION BY A CQ4BINTATION OF TEST ANO ANALYSIS, ALSO COI4ELETE ITEM VII

'AGE 3 OF S

REVISION 2.4 Qualification Summary of Equipment (Continued)

QIDC 361106 I I~ IF QUAL IF ICATION BY ANALYS IS, THEN C04PLETE:

Ref. No /k'>

I~ METHOD OF ANALYSIS:

STATIC ANALYSIS QX EQUI VALENT STAT IC ANALYSI S DYNAMIC ANALYSI S Q T IMEWI STORY RESPONSE SPECTRlH 2 NATURAL FREQUENCIES IN EACH DIRECTION (SIDE/SIDE, FRONT/BACK, VERT ICAL):

S/S 10.81 Hz, F/B 26.1 Hz V )100 3 MODEL TYPE:

Q 3D 2D Q 10 Q FINITE ELEMENT Q BEAM Q CLOSED FORM SOLUTION 4NQ COMPUTER CODES:

FREQUENCY RANGE AND NON OF MODES CONSIOEREO:

HAND CALCUIRTI ON S OTHER 5 METHOD OF CCIBINING DYNAMIC RESPONSES: Q ABSOULTE SIR

[jg SRSS Q (SPECIFYI 6 DAMP ING: OBE SSE : AIA '

SUPPORT CONS IOERATIONS IN THE MODEL' B CRITICAL STRUCTIRAL ELEMENTS: GOVERN I NG LOAD OR RESPONSE SEISMIC TOTAL STRESS A I DENT IF I CAT ION LOCAT ION CINBI NATION STRESS STRESS ALL(NABLE Valve Ears CSP-V-364 EIAEID-BIIAB1 15743 19538 (PS

'6880,

)

Ear Bolts CSP-V-364 pipe-normal 15777 18382 66001) (PS )

Drive Rod CSP-V-4 .,rod-.normal 8543 33019 86400 (PSI)

I Ear Bolts CSP-V-6 pipe-normal 57543 58884 66000 (PSI)

MAXIMLM ALLOWABLE B MAX CRITICAL DEFLECTION TO ASSURE DEFLECTION LCCAT I ON FUNCTIONAL OPERABII.ITY E

0 01" Valve disk: radial approx 1/8" radial deflection clearance (OlrtP(37 PQ $ 7RGSSC.S AGE. ~SEb QIC'PCS.

~ RCCGL<~rioMZ M47"

&LICH'TCE/ Pdg rg~ /2&guFFe~ (SC Can< 5;SJ I/<C.UES. SEE QA~LA7/&I P<R D E>O~SB/~

PAGE 4 OF 5

Revision + 2.5 Qualification Summary of Equipment (Continued)

NQID 361106 Vill. REFERENCES D-207110-H, D-207110-G,(Valve Data Sheets)

A-206767gl8", 24" 6 30" Butterfly Valve - General C-26096,"Certified Dimension for Model A-83-B Cylinder"

2. MPPSS 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-IR64 (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 4TR-'74-7 by McPherson Assoc., Inc., "Design R Seismic Analysis 24" Cylinder operated Butterfly Valve." (Rev. 1) 1/5/76.

letter to Cygna Energy Services, GE-02-RVH-018, 12/17/82.

f'li

5. WPPSS

~.,V- nice d ~g g~,~ ll-il-ga REFERENCES CONTINUED ON PAGE 2.6 Completed By t ~tCowMl Reviewed By

/PE '~, >//a Page 5 ot 5

Calculation aL JLrm's Sheet IHHHHHIHNIHHHHHH Project Prepared By: Date Washin ton Public Power Su 1 S stem L.C. Fernandez 5/27/83 Subject ' Checked By: Date Equipment Seismic/Hydrcdynamic

~

Requal. + z~ s5 CSP & CEP 82044 . OT.01.F AR atyete + rp. Rev. No. Sheet No.

QID 361106 2 2.6 SECTION 4.4 /c~~~J e//s/mg e/y/j r REFERENCES (CONTINUED):

6. Cygna Energy Services Communications Report, R. Ricappito, BIF Valve, and J. Rakowski, CES, "BIF Valve Dimensions",

2/11/83.

I'

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 1nstitute of Steel Construction, 8th Edition, 1980.

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.

I

12. Cygna Energy Services, "Equipment Seismic and Hydrodynamic Requalification of 30" Cylinder Operated Butterfly'Valves for CSP-V-1, & 2, and CEP-V-1A, & 2A," File No. OS.Ol.F, QID No. 361104, Revision 1, 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.FI QID No. 361106, Revision 3, June, 1983.

iooe oo

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'000 00

3.0 TABLE OF CONTENTS TABLE OF CONTENTS QXDO 361106 SECTjON TXTLE 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 2 4.3.2 Calculations jk~ 46 +Appendices 4~4 References 1 5.0 Appendices 5.1 Response Spectra 5.2 Walkdown Sheets 5.3 Valve Local Coordinate Systems 5.4 SRM Sheets 5.5 Final Pipe-Mounted Equipment Response G-levels 6.0 Drawings Revision cf.

TABLE OF CONTENTS QID5 361106 CON'T SECTION TITLE NO OF PAGES 7.0 Transmittals, Prior Calculations and Reports 7.1 Communication Reports & Correspondence 37'8 7.2 Old Requalification a SQRT Forms 7.3 BIF Report 7.4 McPherson Associates Analysis

4. 0 CALCULATIONS -'YGNA jggUALIPICATION ANALYSTS
0 SECTION 4. 0 REQUALIPICATION ANALYSIS
Calculation "3 t.
~t ill Cover IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Sheet Project Job No. 820 gg Eaui ment Seismic Is H drod amic Requalificatiok' OT.Ol/F Client Gale. Set No.
No. of Sheets Washin ton Public Power Su 1 S stem Subject Seismic Qualification of 24" Cylinder Operated Butterfly 5,'4A Valves QTD 361106, EPN gCSP-V-3,4,5,6 6 9, and CEP-V-3A 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 tI 4/fS/V Sources of Oats See sheets 4.3.r7 and 4.3.~b Sources of Formulae 8 References See sheets . 4. 3. 47 and 4. 3. 4 5 Remarks None Originators Checkers Olstrfbution Revision No.
4 Supersedes Calculation Set No.
J. Bakowsjci D. Searle gppSS-2 Project File-1 Revision 5 M. Kuntz L. Kaner Approved By. Date:
M. Scott LC Fernande df~/ZZ Q. <a.aaL~
Calculation
Fbi Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By

Qate 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 Analysis 4.3.1 . Introduction 4.3.2 Calculations 4 ' References 1001 00
Calculation
~~'K0 i F~ Sheet 111IIIIII!11111111111111111111 Project Prepared By: Date Subject Checked By: Date System Job No. File No.
Analysis No. Rev. No. Sheet No.
SECTION
4.1 CONCLUSION
S tccs 00
Calculation A kM IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Sheet project WPPSS Equipment Seiqmj.c Prepared By: Oate H drod name.c Re alxfzcation 6'9 83 Subject Checked By:
BZF Valves/Miller Operators y~~ .6'/9/83 System Job No. File o.
CEP 6 CSP 82044 1T.01.F Analysis No. Rev. No. Sheet No.
361106 4.
1.1 CONCLUSION
S Seven 24-inch BIF 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:
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) .
e Calculation f*i Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: Date Subject Checked By: Date System Job No. File No.
Analysis No. Rev. No. Sheet No.
SECTION 4.2 SUMK&Y OF RESULTS
Calculation
~~ t. i' IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Sheet Prepared By: Oate WPPSS, MECHANICAL EQ Z Subject 24" Butterfl Valves Checked By. '"'a so&
System Job No. File No.
CSP 6 CEP 82044 OT.01.F Analysis No. Ftev. No. Sheet No.
361106 +Z
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.
'F000.00
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Calculation f4'='g,' . Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII WPPSS EQ Prepared By:
m'D Subject Checked By; Date 8
System 82044 OT.01/F Analysis No. Rev. No.
361106 34//dh-d. 2-
~/sos>
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 AXSC criteria and the yield stresses at temperature (340'F) from. PG. 9 of REF. 4 for conservatism.
Le'ver. 8 l8 L eEL l.r. >.t Lax.rt yean SraS ~ t0 Fy '.'/ Fy Otc Vy Fy o,eq Fy F'
~ H T E/Z z tiI L (I'Si) iHe'HR. 8 erto~c SHe'rta.
8 un~. 8 t.shad. 0 LLONlo 7,tattoo
~~X - 'I I'IO Hdrtr I Rzwm 90< oo0 8 Yiooo 36ooo Sk,'too MCoa SyI-0t7( i 6R Zo / / phoo Jlilog I7,vga //,t/0 HATH 1 - Z9S'-4o-sZ-IS qSjoo'o op )oooo / Fi00Q '/SikoD Q /foe 55- 3o7 9,ohio 43,Boo /3,9//0 9,3ko 0 2,37O / '/,)oo 8-s~ - /oil (r ~ vm~o) jsiooo 2 t ooQ ) Q)ooo 3Z 40o 84 too 8j ooo /P,coo /B)Moo a),lao /C,J'yo PR,Ceo 13,Sea 3 I,7 VV /9,mo ooo /4 oo //Zoo RiEFo./ 'ko.
I I.4 FAc~ra. gePt ~Ni g Qr.sld,~ Czl r emA, ~C" 5 SIP%It,'6 5 Got T At.t.owe Iran vitKt=.M t-t'o~ At'Sc, STYLI EO., Ssc.. l.5'.Z.Z, 1005.00
SECTION 4.3 ANALYSIS
0 Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Prttjezt WPPSS Subject ~
Mechanical E ui ment ualificationPrepared Checked B By:
ZP '10 24" Butterfl Valves System 82044 'T.01/F Analvsis No. Rev. No. Sheet No.
361106 361106 45 EQUIPMENT REOUALIFICATION 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-ceived from Burns 6 Roe. Since theseloads were initial-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.
,I Calculation S ~ Zs Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII
'QNSS Mechanical Equipment QualificationPrepared By.
1/10/83 Subject 24" Butterfl Valves
"" s(~also System Job No. File No.
CSP CEP 82044 OT.01 F Rev. No.
3&1106-4,+ 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 QTiD 361104 (30" valves/10" operators). Hand calculations which check selected por-tions of computer output pre, 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.
Calculation
t. Ft i Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII
, Oate Pro'ect WP)SS Mechanical E ui ment ualification Prepared By:
1 10 Subject 24" Butt rf Job No. File No.
System Rev. No.
361106 cf.g 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 r'emaining 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 calculati.ons, 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 yi.eld.
Stress contribution from dynamic loads on the valve
'and operator were 'relatively small. Further, as shown in the figures:
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~g)
Proiect MPPSS Mechanical E ui ment ualificationPrepared By 1 10 83 Subject Checked v V 3lso(bs System Job No. File No.
Analgsgg(. Rev. No.
361106 -+Q I'he 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'f the valve. Valve flange dimensions are given below. Note the relatively large internal radial clearance of 1/8 inch.
Z Stress analysis of the valve extended stxuctures are given in this report. Air operator operability is addressed in QTD 018001.
The design data used in the analyses are given in Summary Table 1.1 (pipe-orientations and elevations are taken from the appropriate PIC?D'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 ~ 3504 Final ~ 18504 Fail Closed Preload ~ 15004 Final 30000
2) Cylinder C.G.'s shown on the following sketches r'epresent data received from BXF in the communi-c~tion 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"
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24" Butterfly Valve !
System Job No. File No.
CSP & CEP 82044 OT.01/F Ahatys's No 361106 Aev. No. 361106-'feb 7 8*
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82044 OT.Ol F Analysis No. Aev. No. Sheet No.
4. 3. 2 . CALCULATIONS I
4.3.2.1 NATURAL FRE UEHCY CALCULATIONS Perform natural frequency calculations for the fol-lowing four operator configur'ations:
Grou T. - Fail 0 en'PN's CSP-V-5 ' )
and 9 Case T. Valve Open Case II Valve Closed Grou II - Fai:1 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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24" Butterfl Valves sibaiaa System Job No. File No.
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61106 361106 <<4 g
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Calculation Akdir~h Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII
, Date Protect WPPSS Mechanical E ui ment Qualification Prepared By: I Subject Butterfl Valves Checked B Oate /
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'T.01/F Rev. No. Sheet No.
361106 361106 - Q- -P 4,3 z.2 Ro Ll 8IH 0 I~EQwtrt 0> Ftj'oN FtGUR,E f.3
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. F13 Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII t
CAS Mechanical Equipment Qualification 1/10/83 Checked B: Date Subject 24" Butterfl Valves 984 85 System Job No File No CSP and CEP 82044 OT.01 Rev. No Sheet No.
361106 A.S Z,Z 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 Edi'tion, 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 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.
Calculation L~k ~.r~t Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By:
1 10 83 24'utter f1 Qu,itject Ualves Checked "" ~i'soles System Job No. File No.
CSP and CEP Analysis No. Rev. No. Sheet No.
361106 AI-VOBIS S TR~ A< DF vhLu'E AM > Ajk aPBm'To%. >PoiiewT g go~ Coij BR&-9 Iy Q>D OIgoo]
I) duo ZluuiJtOP Ptl& +FEE hIJAt yes AN n t~e STREs~ mh> F~~tpy wo E;~ Faiepkii. Y 1ZP~uzu 7 Ohl OV KIKTGRIJuJ t" Ihl THF Z-Awt5 PI~YioA.
ATRIA L.MEED tujTH, '.pp/ '
her r= EAA7vau 7(( I & ((I Z<d7(I((Ad( /3.$
J or g 7(+6 S(AP Jl (Z SVAED5
~AS oui.Y 33 PER.CEPIT T~g QLi.oep6~. ply~~ .
wHi AIS & ~$ SQFFie l~v Foi2 Au, apjv's,.
CAc.t U44 Tlo& pccso&Q ~ 'tt ]n
(. <EP -v- 34) II L (ch Q ~
Lyon - ~~sa) LcC = I4'R (Z.)S ]3.3E 2%i W Z< ihr
'4=4X.('( 'tel((
(AI = (((Ao Fz-- P<
)zing(, IA.( ) =.v((,($ 9 Id~
- Soils ~am g I Z.7$
F(( = Lh((((. Leer) V)Aa ~ (
i'( 444 14XI. +4)
Lga(( L ZS+Z.
0 Fzz = +Ao $ z - 39RU (z) >sz4." F~7Z =
'-IIT-'(((AAQ(IS ua Z.
l2C l (,o (
p 4IF xW FoR 8 rt II.aS (33(a M'I(t= IISb "Etr gT(g) F'Oit- IO" ZE I~4 "~ g47"
<~>>>V4 TIP E. camr~lP PTroN sEE stF RPr~ Hc~~dPpr tIF,p F~I)+F t +(( I-II(UZI
(
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Calculation A ~de Fbi Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII project WP preeeree By: Ij~J>ete.
Subject Checked By. Date 24" Butterfl Valves Job No File No.
CkP and CEP 82044 OT. 01 F Anatvdia No. Rev. No.
361106 84I aC -4.
37. TH E Iovnt- LOAC OV THF a Gute I0 TN.
u QEc.~og 5Q+ oF Ft'-~ Ax b F~.Q . (0 I
F~TZ, Ipctl If+7
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=
FC.LEvts I Fc. y QTR ZA+ul
~ ~
AEEUMe UPPER LlMIT OF ej~ lEJ'a 'SRE7 FRR AREA Z%
33 THa Hmoak, F~< = t'g+g, eA -GH4'OO 3 L~- zi.E MaViS f.~ltae7 +L9ES 1 7yte9 5
~
" 'I tie to = lA+W/~.~" -- Z'I+7 P espy MI
+ =7'99 J>>E yyv +Q= R7I7 PRE < I ly t'~a/e.
.. CPrtS $ PIP ARE GeaP FOE.Pc t t) P<VE. I.ave.a, THPo SE TH& SENT I)0& l-oR@u.F Mgg Ag D 0~I'jtIA~I REACVIc 4 Fd ~CA- Ojtl TIIa. pRIy F <EuFW (Q WPIR PESFPCTIuF QgEC T(cNS e= Gx oAx PYIjAHtt ~ Ft = )q 8 LG FsT e
~ I20)
LOA b Ft'ult-l Ill CREA 5E. TR F /t4tAl FoRCB IP THE Pff,em -PRIV E. LE.'tiM [bled E.UER, 'T H 5 INtU M, 'To@.4 Q9 OlM'TIFF l E'OE.R TRAP )Utah IS ZI4 S
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~~ t.oa.
S~k6LE. IM MiG t:m~~ t'omrxrON'.
lccd.ce
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L. ~a. Jh.fk'i Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: i Date on Subject Checked B
'r I Job No.
C8P and CEP 82044 . OT.01/F Analysis No 361106 Rev."No.
a(lloS- .-
hnR-X bio R.hn AL I ac E oe PRtV E LEVER; FgT C05 8 y FC, pig 8 zsz9 Ls (.m~aufz')
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kkEA au ~ brp.rc ~w~
d A~AI .
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IIIIIIIIIIIIIIIIIIIIIIIIIIIIII, Sheet Project Prepared By: i Oate Checked B Oate 2"
Subject te Valv s CSP and CEP 82044 OT.01/F Analysis No.
361106 Rev. No. Sheet No.
361106 - -2 EVr C*y 6 Ir'-(d 6 r TRESS S&A-~tat O. 4+$
'Q '5m t v- t-5
(.IZ5 IP F~<t = m ~ z. = Iz, ze'7 LG Oct@
6 gag = FIILG ~ Z7I 3$ I Ag q- 3 Zen F'3 I OW y4RSIH =58 g
?
Sea.p-a, amp OV Kajtt = (.3S
~fg F'OP-I- t5EPP tP to r tg.g S. CON'Ti Cg).
Meal suAFz .
FR&.tw tNAP-M ANR<y SIS 'Se ~> mt'S AoT A /4GHO S>~~5MC Co ~PoblF uy, pgpLg2-E Fof< E>PELo pp LojjOS.
STD-EW = ALFSO ~p vt &wta t" %r-=@oE. +
STRE~> DUF Tv 5+~~ OF FsY to J3EPIDl~r" dF +7Z .
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Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project WPPS Mechanical E ui ment ualification Prepared By:I 1 10 83 Subject II Checked B ""sa /
System CSP and CEP 82044 OT.01/F Analysis No. Rev. No. Sheet No.
I. <z,gV t.2 S" 5 =zI~ Z.Sty (jI+ S.Vg IO~
(o.eel ~
6.3z I o,hj IV jgo t l.ZS 7 Vc~ g~ Q <tazp-g CD 7<- 2'L,l~t (.i.zs) 7Z$ 7 Psg x.'z '5 Fee ~a. FRam Rc . n8 PPec c f fs P.
+ 70SS 1 = PESOS l8
+pv s . 7s'os /g'ro f's'z
s. 'f'7
)'E.4't L(3Z,. ~'lII~.S~ = '7'7'7 j Ig - L5 14, ~j S-t,4<>)
0- = 8~ "IS'I'f ~ (.mj~mE) - '1l58 PS~
l.~ l C~N mQORZiuEt.g AGO >N Q SH fhR, S~:-S CS
.-7Z33 +"Q'jo = '91Z l PS I 0 (Lf,5cro g/<
q = ~ls8 F~ ZI 79'000.00
Calculation A'-'~.F.> Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII h . Date Pro ect GPSS Mechanical E uinment ualificationPrepared ByI I gC 1 10 83 Subject Checked 8 . Date
.,24" 3 V v 8 SorS5 System Job No. File No.
Rev. No.
'361106 -4,+-gS 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 torque. The stress in Ref. 4, page 53, is 10753 PSI and i.s therefore acceptable. For the 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 TabG.e 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.
1000.00
.Calculation L ha.5 a Sheet F.'IIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Mechanical -E uipment QualificationPrepared By 1/10/83 Subject Checked y: Oate 24" Butterfl Valves System Job No. File No.
82044 OT.01 F Rev. Nd. S"eet o.
36] ] 06 y '5 Z9 Method XIi Use the north,'east and vertical operator acce'lerations 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 2: 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 QTD 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'he trunnion pins are shown below, along the cylinder axis, for +2-axis g-loading:
+I LaCAl cLALS an clews/inlvc 5k&
LI l I a~A alve cars Qclspniclgtl jc F~ EiaAl ope~r
~ - cu'I)dlreaSDiv
Calculation a iii IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Sheet Pro'ect GPSS Mechanical E ui ment ualificationPrepared By 1 10 83 Subject Checked B:
2 " Butt r Valve Job No. File No.
Rev. No.
361106- 4.+- 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 trunniok pins.
A5d seating torque stresses. 7.tZS F~ - L<~ w@
TNo Foll'tS Ag.E cPrrlcAt. I PT A TH b BQSHt~& hPh j' 8 O'T TH a.
<~~inc.~& MEEPO PIP>E ZaA, MA = F (.Lp,> is.s')
gp, = MACp Za ,Ll~qw Cp BZs td Qo-wut
'l.(.ZS Fc. I3$ 3tH Cg, qg = HgCp l.ct a51 tj Ag V g fl Z- H ll4
Calculation i'.=~ Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: Date M
Subject Checked By: Oate 24"'utterfl V lv s System Job No. File No.
Analysis No. Rev. No. Sheet No.
36xi06, 361106- "5 f le At.I.V:
FmZ. NIg e O'1498ttitt~
AA XA b4 (op As >Bs su~ ARE,R Cn.~S
~G DQI P y QPIAtC, Cmf aggpsTg SElSWIC 9'/0 A Vte. FoRCES 4N V ALV6, C.+8 A ~A P-~APE Jehss /5 r I FPHEss QQDPL UJAs F+EF'A<F->
TH& PIPING hlioPQ. 'TO CAu:LILATE,'%ESPcrftjSE C-MV~ (SeE ATT.PtcHAIEIIT ) . THE YAL9 E EA-R SYSTatA SrttuSt4 Ptttt TOkafogAg fiZq iaII ITy Z Pg,lg Ct OPED IV ~H.E. MOOE'L A~ 9 SEES FoRt ES A<I) . 94mt=NWS W~t-L ALSO 86 OLtl'(J'T FO P CoM tlat&)b N IN 70 tj ALg& Elk 5 TEE, -SFS, TH I-'poch Tfogg TRtIslaul ctws Q Nl, 1 (SEE LdAICCRR'It..DEF At HEXT +) Mg zp g -+ ~NI A- P,k +St A ~A S
(Wseu a~ TS)
+A
+
g'AP-ttf Hatt T3 =+
Qz z~s, goQ g:f (sea A~Vcuvm)
TdP Itt TEIIS(0 II L+I WIIQI ttII IS + (APPEtIOIy. Bg
P
. Calculation A'd~r~ Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By 1 10 83 24 'utterfl
.Subject Valves Checked 8 No.
'ob File No.
Date System CSP and CEP Analysis No. Rev. No. Sheet No.
361106 D CooRDIN TE SYSTEM ( LOCAL) 1000,00
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Date ISS Mechanical E ui ment ualification Prepared B 24 'utterfl Subject Valves Checked Job No File No.
5 '5d System CSP and 82044 OT.01 F Rev No Sheet No.
Anafy~is No. Z. 3611 Fog CE 5 DUF 7g T'o C t-'iE.
e sa
= 4t IO 7.S(,
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7~AT Fp = Les) Fc.p 5 A/o O.+A F~ ~IO" A/o E
FC Z +TuAFT It ZD tb 1
dt 'l.S D =~~L~, +4~3 J p 100 IOZ
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Date 1 10 8
'utterfl Subject 24 Valves Checked B Job No File No.
s System 82044 Rev. No. Sheet No.
ll f~Stt.g StR ES5 OQE 'To IvtZ.
zP d~ - Hz., 9p- Z.= 'Nz
z. 'pA zV ] gtP.n t Pz+~~
ui s,4 (l.f, LEFT .EPEE TEHSMINl+) QPH&N ML=+)
S SLEo + + "P Fc =
~ b 1004.00
K t
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Checked By.
~ C jt~ Date Oate 8 Bd System 'ob No File No.
CSP and CEP Analysis No. Rev. No. Sheet No.
3(el I 44-c/gm PCS~ ziairrr 5'HE&,~ PoPCC, +$ . 7D 'P~ QN FPCH Ebb. IA THF Z- R<<~ . PIaaCT iad .
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Fzz (DF
(-F -D~4 iW XF ~t Fz= FL-zz=b+ x~$ ) = Arx wF~
t 05 GAFF:. - fg '$%LO,
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Z -$ 'f'5 OiRFCWtaP)5 /ESPY CTIVGI P Si < Sg gR~
GIM lt AR St)EA< PaP<S'8 dtlTPItT +cog PfF I-jHAt PtAjtjC INh4rSV U5'(itic THE Nto Pf't tN APpFA) pp. 5 FOP. VWr- F~~r gC 5EP 0<4'a Sm poor.g, R,.%,, pig (p)=o)
Q~, ~~Dzr ~~ta-4.3~a BE~ Pt~ & 5'TRES> CT FW+-Cauvgp,:
~teil K 1
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OT.01 F bt.lint - 4, Rev. No. Sheet No; o Jl:
~gJNN ~W 2l sl Qs, - s( oi )~ QL gs
- s~,Q.p (y z~ z g~)
3 3 3
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1 QZ I.S =0,$ 0 l)) I.7S (-3f )o 1?.
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P4 E To 5) S) 49,9z. 0, kg.
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tl2.
gAtz sl4EAPc 5 Tfze55 8;'ULMNs = Bii + +m 3 jllECTojz SUM
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Q~A Checked B Date
'utterflv Valves
'ubject 24 Syitem Job No. File No.
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/l ' -$ 7 Pat. TS Hc I DIAG l3RJICtCE.Y5'O EARS:
5OVt qFhlwIOU IS, PU 6- T QOI.~ 58&hiZ IS PU E )SQ)V3 0
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CSP and CEP 82044 OT.01 F Analysis No.
61106 Rev. No.
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TA F-SF ppQA Tto p5 ARE Te 5&. QG&b TO FINb THr FctEMS A< b w ortaur s dU &K EAR S DUE I HE CEA,P MJS(8H~, AAA D QFA=ttiU g mQQQE FOE~ 5I PO g CIAt.t.t QLJ}- Ytc AJ OP dPCkP TtA '5W FOR ISSE lla &aTHSR Nle PHOO I t Z.
SEE FORCES g U~t~E,T Otr'-Ia~'T0-'7rog IH Lt"C4t ce otiblH A tEQ> PE,xT pACE, tp = Toua(ok keogh t.oZAL A~tS 4 3
'PE - ZNls>>T Q+ = F Z Te3 a0 F6R,eq + "Aa2e2 e-FSR2e,.
FTgle3 4 Ogpu ee3 0 RIela j2e2 tWSR$ e FTA(e3 + Nggp,RH, 3
$R (INAge2+ aNaae )
l 3 Ft~E.D = + +AoZ.~ "ST. > > <r>@i<4 <'~SP.Z<~
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Calculation a Fbi Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By:
1 10 8 Checked B 24 Butterfl Valves Job No. File No.
CkP and CEP Analvaia No. Rev. No.
361106 34)lldk-cf, Fo ACE.S OA uppoRT ARS BUS Tc LoOAL -Aditi> Act'.EZRA>os P.M5 l jJ 8E Lee L coo Ihj A t-i = S,'25't V.s~<z 9$ (N F aces ae.~ Ã TH-a LOC,At I,Z,K . 4/d A.XIS SVS~ I
~Ae WPzi l5 e~
y~ FAct XrS 6~a ZS.S j
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gk lit)Z ~<tjo(+T OF gkACKE l (0 7H'f C 1,2(3-hjttS PIG.ECTIoHQ
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3
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: , Date MPZSS Mechanica1 E ui ment ualiH.
Subject Checked By I~ ~ ~ 5 56 System Job No. File No.
CSP and CEP 82044 OT.O Analysis No.
361106 Rev. No.
GC(lo(- .-
FOLIC+ Otic TA trOPP 0N ~49 ". ZF +'p (Ahl f>)
~I Tg I "mi +~a $
i
+
"IjaR PRoM P I.oacE BPLP +ATE Qt- >H Q. OPERA TO@
k+
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= (LgooalcC ~+MA (+roKCECA HARV,T J Lr
'4/~)- g tLgab + Lcm) W~ )
Lhasa 4 I <cc wAo+PI g I oPEv Cts Ry ZS 4a ZS 4o'Og l%.9 & Z I.5 t 00s.cs
0 Calculation Sheet sf'IIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: . Oate Checked 8: Oate 24'utterfl Sub(ect Valves System Job No. File No CSP and CEP 820 0 Analvsis No. Rev. No. Sheet No.
361y106 94lI 5z = FA~.z +r.ggz. = jwe~+>gn)g.z.
~P FtCF-b = +5Rz, ++net, + ~sTz
'R duT Ot= AHF BE~&I
( ~V" 6
= g~.'-t.poz t- Froze- te-<z Rwp<4 0 0
=-(Npo~NgR)gz 8~ 'Ngqgptep~ w s$ gRg ToF'EN%M Ih
<<<<~ =(uJAo > I m%2. w F~~q)e~ - Wr'~A~3'- gag++
4 ~LEFT Buy
= ( Wpg +wgp
+g )ga esgtlS 1000.00
Calculation aaa ~h,rsi Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project WPPSS Mechanical E ui ment uglificationPrepared By:
1 10 83 Subject Checked Date tt n1r. 3 85 System Job No. File No.
Anatvsis No. Rev. No. Sheet No.
361106 361106-4' set Condition Stresses The 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 BGR piping analysis, Sec. 5.5)
EPN' 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 0.59 E
Component stresses are given in Table 1.2.
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36110 - 4.5-4 Section49.5'- Fati e Anal si.s 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 ATSC Manual for Steel Con-struction. The following assumptiibns 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. Tf the operating loads (i.e. seating torque effects) are al-ready included in the stress analysis it will be con-to use the calculated stress value. As long 'ervative as no failures occur, the operating stress does not need to be extracted.
4) The aXhwable 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.
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7) Bracket bolting is assumed to be properly tightened and will not be considered for fatigue per Section B3.1 of the AXSC Manual.
The table on the following. page gives the calculated stress range, stress category, and allowable for thecritical components. The fol-lowing page gives excerpts from Appendix B of the AISC Manual showing the descriptions of the relevent stress categories.
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Fati ue Anal sis (cont.)
STRESS STRESS STRESS STRESS 1.5 x ALLOW ITEM TYPE (PSI) RANGE (PSI CATEGORY (FROM AISLE)
TRUNNION PIN 410 DRIVE ROD SEE TA LE 1.2
~ SUPPORT EARS SEE TAB E 1.2 9127 1 e,ZS4' A 90000 MAIN SHAFT 8064 1 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 4478] + 60 13494 cycles).
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Base metal with roHed or cl caned sur- T or Rev. ~
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faces.
Bu0t-up Base metal and weld metal in mem- T or Rev. B members beis, without attadunents, built up of plates or shapes connected by contin-uous full-or partial-penetration groove.
weldsor continuous fdiet weMs paraHei to the direction of appHed stresL Calculated flexural stress, fs, in base Tor Rev.
metal at toe of welds on girder webs or fhnges adjacent to welded transverse stiffen era.
Base metal at end of partial. length welded cover plates having square or tapered ends, with or without waids across the ends.
Mechani- Base metal at gross section oi'igh- T or Rev. B cally strength-bolted friction-type connec-fastened tions, ezcept connections subject to conn ec stress reversal and aziaHy loaded joints tions which induce outwf-plane bending in connected material.
Base metal at net section of other me- T or Rev. D chanicaHy fastened joints.
~
Base metal at net section of high- T or Rev. B strength bolted bearing connections.
Attach-ments Shear stress on nominal area type shear connectors.
of stud- (z".,s )
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~~REFERENCES:~~
gc~~ erylss D-207110-F., D-207110-G,(Valve Data Sheets)
A-206767,18"," 24" 6 30" Butterfly Valve - General C-26096,"Certified Dimension for Model A-83-B Cylinder"
~~2. 'tijPPSS 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 gTR-74-7 by McPherson Assoc., Inc., "Design R Seismic Analysis 24" Cylinder operated Butterfly Valve." (Rev. '1) 1/5/76.~~
1
~~5. WPPSS letter to Cygna Energy Services, GE-02-RWH-018, 12/17/82.~~
Calculation
'h Ã.'.',~ Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: Date Washinaton Public Power Su 1 S stem L.C. ernandez 5/27/83 4
Subject Checked By: Date Equipment Seismic/Hydrodynamic Requal. + z~ s5 System Job No. File No.
82044 OT 01 F
~aiysie Ao. Rev. No. Sheet No.
QID 361106 2 4, 3, 44t, SECTION
~~4.4 REFERENCES~~
~~(CONTINUED):~~
~~6. Cygna Energy Services Communications Report, R. Ricappito, BIF Valve, and J. Rakowski, CES, "BIF Valve Dimensions",~~
2/11/83. a 7 ~ Cygna Energy Services, Project Manual Design Criteria, DC-l, 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. "AZSC Manual of Steel Construction", American Institute of Steel Construction, 8th Edition, 1980.~~
~~Preliminary Transfer of Final Burns & Roe Piping Loads for cEV-V-11,2,3,4,5,6 and CEp-v-3A64A, 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-1A, & 2A," File No. OS.01.F, QID No. 361104, Revision 1, 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"~~
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
sbasi c csp34 tm BASIC Compiler Ver sion 5. 4b 0001:00 REM+++++ BIF VALVE AND AIR OPERATOR SEISMIC STRESS 0002r00 REM%%%%%%%+%%%%%%% CSP-9/AO-~4 0003:00 REM++SAME ORIENTATION FOR EPN 3h4,SAME PARAMTERS, VARY G'S 0004:00 REM 000S:00 var var i,j,k ~ integer lrod>lcg,x,phi,lave,ablt,li,l2,e1,e2,e3,e4,e5 ~ real 0006:00 0007: 00 var f st 2, ca, a, cb, b, aa, ab, di, d2, c 1, i 1, c2, i 2~r ea1 i i 0008:00 var lr odo, cgo, dr,d, abush, pbush=real 1 1 0009:00 var fcof, fco, ma,mb, si ga, si gb, fcdr, fcdrf,maf, mbf=real 0010 t00 var dear, fcear,fr, fi i,f22,la, ci12,ci21,stt3,semi~real 0011:00 var sem2,set3,ses1,ses2,sr, taui1, tau22, tauear,aear~r eal 0012:00 var btens, taubl t, set3f,semif,sem2f,fcearf, frf,fi if~real 0013:00 var f22f,stt3f,sesif,ses2f,srf, tau1f, tau2f, taurf~real 0014: 00 var taubf, bt f, dsr, dtaur., dtaub, db ten, dsa, dsb, dpb~real 0015:00 var sdraf,sdr bf,pbushf, taui if, tau22f~real 0016:00 var wao,wbr,f tr i,watr 1,si,sif,s2,s2f,mi,mi f,m2 r eal 0017:00 var m2f, t3, t3f, t t3, t t3f, br >wtot~real, 1
0018:00 var- bsi sbs2sbt3sbmi tbm2sbt ter eal 0019:00 dim real av(3) 0020:00 dim real wa<3) 0021:00 dim real wb<3) 0022:00 REM 0023:00 REM +++ BURNS 7 ROE EAR FORCES ARE bs1 etc TURN ON WITH K 1+++
0024:00 REM 25:00 REM 26:00 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, .?S, 1.95, 1.25, .7 0030:00 2 data 25,14.46,.531,53.,7.125,.31,1.5,2.5 0031$ 00 3 data 1150 875t 46s 648s 138<2 41si 4 0032:00 4 0033+M 5.
data data
~ s ~ ~
399~277~5 25~8 5~28 '~15
~
~
40.,10.96,26.5,.30.5,2.075
'e~
875
~
0034:00 6 data 90.,90.,180 '0.,90 '90.
0035t00 7 data 90.,180.,90.,180 '90.,90.
0036t00 REM DATA A%7 FOR VALVE/GLOBAL-6 ORIENTATIONS AND WEIGHT VECTOR 0037:00 restor e 0038: 00 read di, d2, el, i 1, c2, i 2 0035';00"res%ore 2 0040:00 read lrod,lcg,x,phi,lave,abl/t,11,12 0041:00 r estor e 3 O'Iu'Gb! A
'042:00 read fst2,ca, i a,cb, ib,aa,ab ATTACHMENT 0043.:00 r estore. 4 0044>00 react wao,wbr, e1, e2, e3, e4, e5 gOB yg 8 0045:00 restore 5 PQ Q Pi6f 2'~LE 0046:00 read lrodo,lcgo,ldr,d,abush 0047'.00 r estor e- 6 man Mo.~
0048.: 00 .read. a( 1, 1), a(2, 1), a(3, 1), a< 1,2), a(2,2), a< 3,2) 0049:00 restore 7 0050:00 read a<1,3),a(2,3),a<3,3),av(1),av(2),av<3) 51:00 text O,h INPUT GLOBAL ACCELERATIONS h 52:00 input b(1) sb(2) sb<3) 53:00 print 0054:00 text O,h INPUT DATA h 0055:00 print 0056:00 pr int "GLOBAL G-LEVELS ," sb< 1) b(2) t b(3) y LES ";a<1,1),a(2,1),a(3,1)
UT GLOBAL ACCELERATIONS
.66,2.99,3.76 INPUT DATA GLOBAL G-LEVELS
'lORTH VECTOR ANGLES
~ 2. 66 90 2
90
'9 3 '6 180 VERTICAL VECTOR ANGLES= 0 90 90 VECTOR ANGLES ~ 90 'ST 180 90 HEIGHT VECTOR At'lGLES = 180 90 90 LOCAL G-LEVELS
-1 . 01471E-5 2. 99 -1.43433E-5
-1 01471E-5
~ -1 14059E-5
~ -3.76
-2.66 -1 14059E-5
~ -1.43433E-5 3PERATING DRIVE ROD STRESS AT A 5525.52 OPERATIt'IG DRIVE ROD STRESS AT B 8542.57 3PERATING CYLINDER BRG PRESSURE -98.4646 3PERATING VALVE EAR TENSILE STR 3795.21 3PERATING VALVE EAR SHEAR STRES 244 962
~
3PERATING EAR BOLT SHEAR STRESS '963.25 3PERATING EAR BOLT TENSILE STR 2615:86 AMIC COMPONENTS
>RIVE ROD TENSILE STRESS AT A 15094.5 DRIVE ROD TENSILE STRESS AT B 23086 '
3USHING PRESSURE 294 '09 VALVE EAR TENSILE STRESS 14765.9 PALVE EAR SHEAR STRESS 967.76 MR BOLT SHEAR STRESS 11706.8 R BOLT TENSILE STRESS 14229.2 FIXED PLUS DYNAMIC COMPONENTS
)RIVE ROD TENSILE STRESS AT A 20620 ~ 1 DRIVE ROD TENSILE STRESS AT B 31628.7
~USHING PRESSURE 392.874 JALVE EAR TENSILE STRESS 18561 F 1 JALVE EAR SHEAR STRESS 1212.72 WR BOLT SHEAR STRESS 14670 MR BOLT TENSILE STRESS 16845.1 3'I P.5 cvcw>
ATTACHMENT
3
<JT GLOBAL ACCELERATIONS
~6,2 '9,3.76 INPUT DATA GLOBAL G-LEVELS, = 2 ~ 66 2.99 . 3.76 CNORTH VECTOR ANGLES = 90 90 180 VERTICAL VECTOR ANGLES~ 0 90 90
&ST VECTOR ANGLES ~ 90 180 90 JEIGHT VECTOR ANGLES ~ 180 . 90 90 LOCAL G-LEVELS
-1.01471E-5 2.99 -1 ..43433E-5
-1 ~ 01 471 E-5 -1 . 14059E-5 -3. 76
-2. 66 -1 . 14059E-5 -1 . 43433E-5 3PERATING DRIVE ROD STRESS AT A 5525.52 3PERATING DRIVE ROD STRESS AT B 8542.57 3PERA'TING CYLINDER BRG PRESSURE -98.4646 OPERATING EAR WELD TENSILE STR 4338.59 3PERATING EAR WELD SHEAR STRES '19.72 3PERATING EAR BOLT SHEAR STRESS 2963.24 3PERATING EAR BOLT TENSILE STR 2615.86
.WI C COMPONENTS I
)RIVE ROD TENSILE STRESS AT A 15094.5
)RIVE ROD TENSILE STRESS AT B 23086.2 3USHING PRESSURE 294 '09 R WELD TENSILE STRESS 16435 '
."AR WELD SHEAR STRESS 2053.24 R BOLT SHEAR STRESS MR BOLT TENSILE STRESS 11706 '
14229.2 JOB NO.
ammo.
~
FIXED PLUS DYNAMIC COMPONENTS
)RIVE ROD TENSILE STRESS AT A 20620.1
$ iiPET iiO.~
)RIVE ROD TENSILE STRESS AT B 31628.7
'USHING PRESSURE 392.874 R WELD TENSILE STRESS 20773 '
.AR WELD SHEAR STRESS 2572.96 R BOLT SHEAR STRESS 14670 MR BOLT TENSILE STRESS 16845.1
T GLOBAL ACCELERATIONS i6,2.99,3.76 INPUT DATA GLOBAL G-LEVELS ilORTH VECTOR ANGLES = 90 2.66 2 90
'9 3.76 180 VERTICAL VECTOR ANGLES= 0 90 90 MST VECTOR ANGLES = 90 180 90 AEI GHT VECTOR ANGLES = 180 90 90 LOCAL G-LEVELS
-1.01471E-5 2 ~ 99 -1.43433E-5
-1.01471E-5
-2.66
-1 14059E-5
~
-1.14059E-5
-3 '6
-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 3795 21.
~
QPERATING VALVE EAR SHEAR STRES 244.962 QPER*TING EAR BOLT SHEAR STRESS 2963 25
~
OPERATING EAR BOLT TENSILE STR 2615 86
~
906.782 s 1150 t3f~-2 ~ 57873E-3 nl,f~-7906. 15 v2f=<<6234. 1 t t3f~-12328.8 DYNAMI C COMPONENTS DRIVE ROD TENSILE STRESS AT A 15094.5 DRIVE ROD TENSILE STRESS AT B 23086 '
3USHING PRESSURE 294 '09 VALVE EAR TENSILE STRESS 14765.9 PALVE,.EAR, SHEAR STRESS 967.76 R BOLT SHEAR STRESS 11706.8 R BOLT TENSILE STRESS 14229.2 sid s2d 2711 2541
'7
'6 t3d= 1798.16 nid~ 59281.6..
a2d=E 22662 6F t:t3d~ 68555.7 ED PLUS DYNAMIC COMPONENTS E ROD TENSILE STRESS AT
~~20620 ~ 1 DRIVE ROD TENSILE STRESS AT 8 31628.7~~
~USHING PRESSURE 392.874
)ALVE EAR TENSILE STRESS 18561 F 1 VALVE EAR SHEAR STRESS 1212.72
II
\
1 8
EAR BOLT SHEAR STRESS 14670 EAR BOLT TENSILE STRESS 16845.1 sl t~ 3618.06 s2t= 3691.76 1798.16 67187.8 28896.7 ttat= 80884.5 CVQMA ATrACHMENT wacko.~h~~~'C vaz wo. <<~'~
smv wo.~~
4* H 4
UT GLOBAL ACCELERATI Ol'JS
. 96,3 17,4
~ ~ 19 INPUT DATA
)LOBAL G-LEVELS 2.96 3 17
~ 4 ~ 19
)ORTH VECTOR ANGLES ~ 90 90 180 VERTICAL VECTOR ANGLES= 0 90 90
%ST VECTOR ANGLES ~ 90 180 90
)EIGHT VECTOR ANGLES ~ 180 90 90 LOCAL G-LEVELS
-1
.1
~ 12915E-5
'2915E-5 3 '7
-1 20926E-5
~
-1.59836E-5
-4 '9
-2 96
~ -1.20926E-5 -1.59836E-5
)PERAT ING DRIVE ROD STRESS AT A 5525. 52
)PERATING DRIVE ROD STRESS AT B 8542.57 iPERATING CYLINDER BRG PRESSURE -98.4646
)PERATING VALVE EAR TENSILE STR 3795 21
~
iPERATING VALVE EAR SHEAR STRES 244.962
)PERATING EAR BOLT SHEAR STRESS 2963.25
'iPERATING EAR BOI T TENSILE STR 2615 86~
ANI C COMPONENTS DRIVE ROD TENSILE STRESS AT A 16003 ~ 2
'RIVE ROD TENSILE STRESS AT B 24476
'USHING PRESSURE 312.133
'ALVE EAR TENSILE STRESS 15743
"*LVE EAR SHEAR STRESS 1034.29 R BOLT SHEAR STRESS 12511.6
~~AR BOLT TENSILE STRESS 15776.8 FIXED PLUS DYNAMIC Cast ONENTS RIVE ROD TENSILE STRESS AT A 21528 ~ 7~~
~RIVE ROD TENSILE STRESS AT B 33018.6 USHING PRESSURE 410. 597
'ALVE EAR TENSILE STRESS 19538 ~ 2 ALVE EAR SHEAR STRESS
.'AR BOLT SHEAR STRESS 1279 '6 15474.9 AR BOLT TENSILE STRESS 18392 '
Eiilib JOB NO.E~~~~
m.a ~o.~4~~i ~
SHEcT NO
II UT GLOBAL ACCELERATIONS rgl u L~~b '~KJ~Lb
'6,3.17,4.19 INPUT DATA 3LOBAL G-LEVELS 2.96 3 ~ 17 4 ~ 19 lORTH VECTOR ANGLES ~ 90 90 180 VERTICAL VECTOR ANGLES= 0 90 90
&ST VECTOR ANGLES ~ 90 180 90 JEIGHT VECTOR ANGLES = 180 90 90 LOCAL G-LEVELS
-1 . 1 291 5E-5 3. 17 -1.59836E-5
-1.12915E-5 -1 20926E-5
~ -4.19
-2 96
~ --1.20926E-5 -1.59836E-5
)PERATING DRIVE ROD STRESS AT A 5525.52
)PERATING DRIVE ROD STRESS AT B 8542.57
)PERATING CYLINDER BRG PRESSURE -98.4646 OPERATING EAR WELD TEl'lSILE STR 4338.59
)PERATING EAR WELD SHEAR STRES 519.72
)PERATING EAR BOLT SHEAR STRESS 2963.24
)PERATING EAR BOLT TENSILE STR 2615.86
<MI C COMPONENTS
)RIVE ROD TENSILE STRESS AT
~~16003.2~~
)RIVE ROD TENSILE STRESS AT B 24476
)USHING PRESSURE 312.133 AR WELD TENSILE STRESS 17548.3 R WELD SHEAR STRESS 2194'.4 R BOLT SHEAR STRESS 12511 '
lAR BOLT TENSILE STRESS 15776.8 FIXED PLUS DYNAMIC COMPONENTS
)RIVE ROD TENSILE STRESS AT A 21 528 ~ 7
)RIVE ROD TENSILE STRESS AT B 33018 '
,'USHING PRESSURE 410 '97
~~AR WELD TENSILE STRESS 21886 '~~
~~AR WELD SHEAR STRESS~~
~~AR BOLT SHEAR STRESS 2714 '2 15474.9 AR BOLT TENSILE STRESS 18392.7~~
~os ~o.~~~~
plea wo ~+
GHQ~T No.
cs 4 T GLOBAL ACCElERATIONS 96,3.17,4.19 INPUT DATA GLOBAL G-LEVELS 2.96 3.17 4.19 ilORTH VECTOR ANGLES ~ 90 90 180 VERTICAL VECTOR ANGLES= 0 90 90
=*ST VECTOR ANGLES ~ 90 180 90 AEIGHT VECTOR ANGLES = 180 90 90 LOCAL G-LEVELS
-1 12915E-5
~
"1 12915E-5 3
-1
'7 -1.59836E-5
-4.19
'6
~ '092~E-5'2
-1.20926E-5 -1.59836E-5 3PERATING DRIVE ROD STRESS AT A 5525.52
'3PERATING DRIVE ROD STRESS AT B 8542o57 3PERATING CYLINDER BRG PRESSURE" -98.4646 OPERATING VALVE EAR TENSILE STR 3795.21 3PERATING VALVE EAR SHEAR STRES 244.962 OPERATING EAR BOLT SHEAR STRESS 2963.25 3PERATING EAR BOLT TENSILE STR 2615 86
~
"906 '82 1 150 t3f~-2 '7873E-3 Aif=-7906.15
~2f=-6234.1 t t3f=-12328. 8 DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 16003 '
DRIVE ROD TENSILE STRESS AT B 24476 3USHING PRESSURE 312 '33 JALVE EAR TENSILE STRESS 15743 HALVE EAR SHEAR STRESS 1034.29 R BOLT SHEAR STRESS 12511 '
MR BOLT TENSILE STRESS 15776.8 si M 2874.49 CVGRA iZd 2832
'.3d~ 2000.96
'4 ATTACHMENT aid= 65975.4 JOB NO.J~~~
nZd= 24418 ' Faa~o ~~o <
~~t3d~ 72951.2 SHEET NO.~~
.ED PLUS DYhNNIC COMPONENTS E ROD TENSILE STRESS AT A 21528. 7
)RIVE ROD TENSILE STRESS AT B 33018.6
'USHING PRESSURE 410.597
>ALVE EAR TENSILE STRESS 19538.2 JALVE EAR SHEAR STRESS 1279.26
~ AR RAI T RHPAP Ri RFRR 474.0
W ~ ~ ~ W ~ ~ ~ ~
R BOLT TENSILE STRESS 18392o7 3781 '8
<<2t= 3982.44
'1t=
t3t= 2000 '6 73881 '
30652.9 85280 ATTACHMENT JOB MO.~~~
FILE NO.~~~~ ~
SHaaV WO. ~<-
'I T GLOBAL ACCELERATIONS EQE.R.GSQCV (&ld<cobcs CS+- ~-~)
r0,1 97i1.71
~
INPUT DATA
)LOBAL G-LEVELS 2' 1 ~ 97 1.71 IORTH VECTOR ANGLES = 90. 90 '1 80 VERTICAL 'VECTOR ANGLES 0 90 90
!AST VECTOR ANGLES = 90 180 90 FREIGHT VECTOR ANGLES ~ 180 90 90 LOCAL G-LEVELS 1 ~ 0681 1E-5 1 . 97 -6.52313E-6 1 . 06811E-S -7 51495E-6
~ -1.71
~
2~8 -7.51495E-6 -6.52313E-6
)PERATING DRIVE ROD STRESS AT A 552S.52
)PERATING DRIVE ROD STRESS AT B 8542.57.
iPERATING CYLINDER BRG PRESSURE -98 4646
~
)PERATING EAR WELD TENSILE STR 4338 59 ~
iPERATING EAR WELD SHEAR STRES 519.72
)PERATING EAR BOLT SHEAR STRESS 2963.24 iPERATING EAR BOLT TENSILE STR 2615.86 Pli C COMPONENTS RIVE ROD TENSILE STRESS AT'A 9945.23 iRIVE ROD TENSILE STRESS AT B 15210.7
'USHING PRESSURE 493.975
'.AR MELD TENSILE STRESS 10668 '
~~AR MELD SHEAR STRESS 1296.94 AR BOLT SHEAR STRESS 7394.64~~
'AR BOLT TENSILE STRESS 14365 '
FIXED PLUS DYI'NNIC C(EXPONENTS RIVE ROD TENSILE STRESS AT A 15470 ~ 8 RIVE ROD TENSILE STRESS AT B 23753.2 USHING PRESSURE 292.44
'AR MELD TENSILE STRESS 15007.2 AR
.AR WELD SHEAR STRESS BOLT SHEAR STRESS 1816 '6 10357.9 AR BOLT"TENSILE STRESS 16980 '
. Q'ggl)i:]4 ppgggPRY gQB N0.~44~
FLENa
~~'HEETNO A-tb
"sp4 PUT Gl OBAL ACCELERATIONS 6 P>>< ., E;V~BC.nreS ds&I-3) 14,1.40,1.5 INPUT DATA GLOBAL G-LEVELS 1 ~ 14 1 ~ 4 1 ~ 5
)ORTH VECTOR ANGLES = 90 90 180 VERTICAL VECTOR ANGLES= 0 90 90
~~-AST VECTOR ANGLES = 90 180 90 HEIGHT VECTOR ANGLES = 180 90 90 LOCAL '-LEVELS~~
-4.34875E-6 1.4 -5 '2204E-6 "4.34875E-6 -5.34057E-6 -1.5
-1 ~ 14 -5.340S7E-6 -5.72204E-6 3PERATING DRIVE ROD STRESS AT A 5525,52 3PERATING .DRIVE ROD STRESS AT B 8542.57 3PERATING CYLINDER BRG PRESSURE -5'8.4646 3PERATING EAR WELD TENSILE STR 4338.59 3PERATING CAR WELD SHEAR STRES 519.72 3PERATING EAR BOLT SHEAR STRESS 2963.24 3PERATING EAR BOLT TENSILE STR 2615 86
~
'MIC COMPONENTS VE ROD TENSILE STRESS AT A 7067. 68
)RIVE ROD TENSILE STRESS AT B 10809.6
)USHING PRESSURE 137.85 WR WELD TENSILE STRESS 7558.92
~~AR WELD SHEAR STRESS 940 '09 R BOLT SHEAR STRESS lAR BOLT TENSILE STRE~ 5364 6129~~
'3
'4 FIXED PLUS DYNAMIC COMPONENTS
)RIVE ROD TENSILE STRESS AT A 1255'3.2
)RIVE ROD TENSILE STRESS AT B 15'3S2.2
)USHING PRESSURE 236.315 R WELD TENSILE STRESS 1'1897 '
R WELD SHEAR STRESS 1460.53 R BOLT SHEAR STRESS 8327.37 R BOLT TENSILE STRESS 8744.9 CYQ 3A JQ8NO. ~~~~~
Ra.ERO. OT'Oi >
BREST RO.k~~
sbasic csp5 tm BAS I C Compiler Version 5.4b F001 '00 REM+++++ BIF VALVE AND AIR OPERATOR SEISMIC STRESS 4++++
0002:00 REM3f%%%%%%%%%%%%%% CSP~/AO 5 0003!00 REM 0004!00 var i,j,k = integer .
~
0005!00 var Irod,lcg,x,phi,lave,ablt,li,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 lrodo,lcgo,ldr,d, abush, pbush~r eal 0008!00 var fcof, fco, ma,mb, siga, si gb, fcdr, fcdrf,maf, mbf~real 0009!00 var dear, frear, fr, f 1 1, f22,la, c i 12, c i 21, st t3, semi~real OO1O:OO var sem2,set3,sesi,ses2,sr, tauii, tau22, tauear,aear~r eal 0011:00 var btens, taubl t, set3f,semif,sem2f,fcearf, frf,f11f~real 0012!00 var f22f, st t3f, sesi f, ses2f, srf, taui f, tau2f, taurf~r eal 0013:00 var taubf,btf, dsr,dtaur,dtaub,dbten,dsa,dsb,dpb~real 0014!00 var sdraf,sdrbf,pbushf, taui1f, tau22f~r eal 0015:00 var wao,wbr,f tri,watrl >'si >sif! s2,s2f,mi,mi f,m2=real 0016!00 var m2f, t3, t3f, t t3, t t3f, br,wtot=real 1
0017!00 var bsi,bs2,bt3,bmi,bm2,bt t3~real 0018!00 dim real av(3) 0019!00 dim real wa(3) 0020:00 dim r eal wb(3) 0021 j 00 REM 0022!00 REM 4~4 BURNS 7 ROE EAR FORCES ARE bsi etc TURN ON WITH K~i+ww 0023:00 REM 0024:00 REM 025!00 dim r eal a(3,3)
J26$ 00 dim real b(3) 027:00 dim real glc(3,3) 0028!00 1 data 7.5~ los .75> 1 95i 1 25s 7~
0029!00 2 data 25,14.46,.531,53.,7. 125,.31,1.5,2.5 0030: 00 3 data 0 , 875,.46,.648,.138,2.41,1.4 0031!00 4 data 399,277,5.25,8.5,28.5,15.,6.875 0032!00 5 data 40.s10 96s26 5s30 5t2 075
~ ~ ~ ~
0033!00 6 data 42.5,47.5,90.,90.,90.,0.
0034:00 7 data 47.5,137.5,90 '180 '90, ,90 ~
0035!00 DATA 6%7 FOR VALV&'GLOBAL-GORIENTATIONS 'EM AND WEIGHT VECTOR 0036!00 restore 0037!00 read di,d2,c1,i1,c2,i2 0038!00 restore 2 0039!00 read lr od,lcg,x,phi,lave,ablt,l1,12 0040200 restore 3 0041!00 read fst2,ca,ia,cb,ib,aa,ab 0042.00 restor e 4 0043'00 read wao,wbr,ei,e2,e3,e4,e5 0044!00 restor e 5 0045!00 read lrodo,lcgo,ldr,d,abush 0046:00 restore ATTACHMFNT 0047!00 read a< 1, 1), a(2,1), a(3, 1), a(1,2), a<2,2), a(3,2) 408 NO.
0048!00 restore 7 0049:00 read a( 1,3),a(2,3),a<3,3),av(1),av(2),av(3) FlLE NO. +T'~
0050! 00 text O,h'NPUT GLOBAL ACCELERATIONS 5 SHEET NO.
A-IZ
~51 $ 00 input b( 1),b(2),b(3)
~52!00 print 53!00 tex.t O,h INPUT DATA h
~5 LfT GLOBAL ACCELERATIONS
.26,3.44,5.42
~ ~
INPUT DATA 3LOBAL G-LEVELS
<ORTH VECTOR ANGLES 2.96 42.5 3.44 47.5 5
90
'2
)ERTI CAL VECTOR ANGLES= ~
90 90 0
&ST VECTOR ANGLES 47.5 137.5 90 dEI GHT VECTOR ANGLES 180 90 90 LOCAL G-LEVELS 2.18234 -1.31225E-5 3 '6169 1.99974 -1 31225E-5
~ -3.99606
-1.12915E-5 3.44 -2.06756E-5
)PERATING DRIVE ROD STRESS AT A 5048.35 3PERATING DRIVE ROD STRESS AT B 7721 ~ 14
)PERATING CYLINDER BRG PRESSURE -98.4646 3PERATING VALVE EAR TENSILE STR 4664.25
)PERATING VALVE EAR SHEAR STRES 297.614 3PERATING EAR BOLT SHEAR STRESS 3600 ~ 17 3PERATING EAR BOLT TENSILE STR 1340.69 AMIC COMPONENTS
)RIVE ROD TENSILE STRESS AT A 21519. 6
)RIVE ROD TENSILE STRESS AT B 32912 8 ~
3USHING PRESSURE 419. 724
)ALVE EAR TENSILE STRESS 20190.5
)ALVE EAR SHEAR STRESS R BOLT SHEAR STRESS 1312 15882
'1 MR BOLT TENSILE STRESS 19507 FIXED PLUS DYNAMIC COMPONENTS
)RIVE ROD TENSILE STRESS AT A 26567.9
)RIVE ROD TENSILE STRESS AT B 40633 9 ~
'USHING PRESSURE 518.189
)ALVE EAR TENSILE STRESS 24854.8
'ALVE EAR-SHEAR-STRESS 1610.53 R BOLT SHEAR STRESS 19482.2
!AR BOLT TENSILE STRESS 20847.7 ATTACHMENT JOB NO.
FILE NO ~OPdl F SHEET NO.
E e 5 UT GL'OBAL ACCELERATIONS
>6,3.44,5.42 i AVuQ kleig ~%
INPUT DATA GLOBAL G-LEVELS CNORTH VECTOR ANGLES 2.96 42.5 3.44 47.5 5
5'0
'2 VERTICAl VECTOR ANGLES= 5'0 5'0 0 ST VECTOR ANGLES 47,5 137.5 90 AEIGHT VECTOR ANGLES 180 , 90 90 LOCAL G-LEVELS 2 ~ 18234 -1 31225E-5
~ 3 ~ 66169 1 ~ 99974 -1 31225E-5
~ -3. 99606 .
-1 1 291 5E-5
~ 3. 44 ~ -2.06756E-5 3PERATING DRIVE ROD STRESS AT 'A 5048.35 3PERATING DRIVE ROD STRESS AT B 7721 1'4 ~
3PERATING CYLINDER BRG PRESSURE 5'8.4646 OPERATING EAR. WELD TENSILE STR 5107 51 ~
3PERATING EAR WELD SHEAR STRES 631.431 OPERATING EAR BOLT SHEAR STRESS 3600.17 3PERATING EAR BOLT TENSILE STR 1340.69 WI C COMPONENTS DRIVE ROD TENSILE STRESS AT A 21515' 6 DRIVE ROD TENSILE STRESS AT B 32912.8 3USHING PRESSURE 419. 724 R WELD TENSILE STRESS 22736e7 R WELD SHEAR STRESS 2785.52 R BOLT SHEAR STRESS . 15882 MR BOLT TENSILE STRESS 19507 FIXED PLUS DYNAMIC COMPONENTS
)RIVE ROD TENSILE STRESS AT A TENSILE STRESS AT B 40633 9 26567.5'RIVE ROD ~
'USHING PRESSURE 518 '89 MR WELD TENSILE STRESS '7844'.2
.:*R WELD SHEAR STRESS 3416 95 ~
R BOLT SHEAR STRESS 19482. 2 MR BOLT TENSILE STRESS 20847.7
t cc 5 UT GLOBAL ACCELERATIONS 6,3 '4s5 42
~
INPUT DATA GLOBAL G-LEVELS
<ORTH VECTOR ANGLES ~ .
2 '6 42.5 3.44 47 '
5.42 90 VERTICAL VECTOR ANGLES= 90 90 0 ST VECTOR ANGLES = 47.5 137.5 90 WEIGHT VECTOR ANGLES = 180 90 90 LOCAL G-LEVELS 2 '8234 -1 31225E-5
~ 3 '6169 1 ~ 99974 -1.31225E-5 '3.99606
-1 12915E-5
~ 3.44 -2.06756E-5 3PERATING DRIVE ROD'TRESS AT A 5048.35 OPERATING DRIVE ROD STRESS AT B 7721.14 3PERATING CYLINDER BRG PRESSURE -98.4646 OPERATING VALVE EAR TENSILE STR'664 ~ 25 3PERATING VALVE EAR SHEAR STRES 297.614 OPERATING EAR BOLT SHEAR STRESS 3600.17 3PERATING EAR BOLT TENSILE STR 1340 69~
-906.782
~
-2.57874E-3
~
t3f=-2.57873E-3 nlf= 9.89667E-2 n2f=-6234. 1
'.t3f~-22103 '
DYNAMIC COMPONENTS
)RIVE ROD TENSILE STRESS AT A 21519 6 ~
)RIVE ROD TENSILE STRESS AT B 32912 '
3USHING PRESSURE 419.724 JALVE EAR TENSILE STRESS 20190 '
)ALVE EAR SHEAR STRESS'
.BOLT SHEAR STRESS 1312 15882
'1
=AR BOLT TENSILE STRESS 19507
-id~ 3865.34 32d= 3020 7
".3d= 2325.44*
>id= 76145
>2d~ 31369.7
~~t3d= '84539.5 ED PLUS DYNAMIC COMPONENTS E ROD TENSILE STRESS AT A 26567.9~~
)RIVE ROD TENSILE STRESS AT B 40633 9 ~
'USHING PRESSURE 518. 189 (ALVE EAR TENSILE STRESS 24854 8~
'ALVE EAR SHEAR STRESS 1610 . 53
tC 5UL'I btlCHtC b I tCC55 lYRVZ 2
~
"=AR BOLT TENSILE STRESS 20847.7 si t~ 4772. i 2
~2t= 3020 7 2325 76i45
'4
~
37603.8
~~t~r= i.06643E+5 JOB MO.~2~<@~~
FlLE Ng. < <.6I.F'HERT NO
0 sp5 UT GLOBAL ACCELERATIONS E.REFQ $ 9~/
0,2.69,5.32 INPUT DATA GLOBAL G-LEVELS'ORTH 2'
42.5 2.69 47.5 5
90
'2 VECTOR ANGLES VERTICAL VECTOR ANGLES= 90 90 0 ST VECTOR ANGLES 47.5 137.5 90
'jEIGHT VECTOR ANGLES 180 90 90 LOCAL G-LEVELS
~~2. 06437 -1 0261 5E-5~~
~ 3.59413 1 . 89165 -1 . 026'1 5E-5 -3.92233
-1 . 0681 1E-5 2. 69 -2.02942E-5
)PERATING DRIVE ROD STRESS AT A 5048.35
)PERATING DRIVE ROD STRESS AT,B. 7721 ~ 14
)PERATING CYLINDER BRG PRESSURE -98.4646
)PERATING EAR WELD TENSILE STR 5107,51 1P ERAT ING EAR WEt.D SHEAR STRES 631 . 431
)PERATING EAR BOLT SHEAR STRESS 3600.17
)PERATING EAR BOLT TENSILE STR 1340 69
~
~M I C COMPONENTS LVE ROD TENSILE STRESS AT A 20924.4
)RIVE ROD TENSILE STRESS AT B 32002.6
'USHING PRESSURE 408 '16 R WELD TENSILE STRESS 21934 '
~~AR WELD SHEAR STRESS 2693.88 R BOLT SHEAR STRESS 15359.5~~
~~AR BOLT TENSILE STRESS 16131.4 FIXED PLUS DYNAMIC COMPONENTS RIVE ROD TENSILE STRESS AT~~
~~25972.8~~
'RIVE ROD TENSILE STRESS AT B 39723.7 USHING PRESSURE 506.581
.'AR WELD AR MELD .SHEAR,.STRESS TENSILE STRESS 27042.1 3325.31 C'1QMA
~~AR BOLT SHEAR STRESS 18959.6 A7YACB9RH47 "AR BOLT TENSILE STRESS 17472.1 IFILE SIO.~~
gHERTN0.8 11
UT GLOBAL ACCELERATIONS
'>,1 '~1.71 INPUT DATA lLOBAL G-LEVELS ~ 5'7 1 ~ 4 1,. 71 IORTH VECTOR'ANGLES 42.5 47 ' 5'0
'ERTICAL VECTOR ANGLES= 5'0, 90 0
~~AST VECTOR ANGLES 47 ' 137.5 90 JEIGHT VECTOR ANGLES 180 90 5'0 LOCAL G-LEVELS~~
~ 715158 -5 '4057E-6 1. 15526
~ 655321 -5.34057E-6 -1 . 26075
.3.70025E-6 1.4 -6 '2313E-6 IPERATING DRIVE ROD STRESS AT A 5048.35
)PERATING DRIVE ROD STRESS AT B 7721.14 OPERATING CYLINDER BRG PRESSURE -5'8.4646
)PERATING EAR WELD TENSILE STR 5107.51 OPERATING EAR WELD SHEAR STRES 631.431 OPERATING EAR BOLT SHEAR STRESS 3600.17 PERATIl'lG EAR BOLT TENSILE STR 1340.65'WI C COMPONENTS r
E ROD TENSILE STRESS AT A 6855' 1 8
'RIVE ROD TENSILE STRESS AT B 1045'0 7 ~
USHING PRESSURE 133.784 AR WELD TENSILE STRESS 7323.31 AR WELD SHEAR STRESS 892.936
.'AR BOLT SHEAR STRESS 5091 . 16 AR BOLT TENSILE STRESS 7595'.75 FIXED PLUS DYNAMIC COMPONENTS RIVE ROD TENSILE STRESS AT A 115'07.5 voodoo.
RIVE ROD TENSILE STRESS AT B 18211 9 ~
USHING PRESSURE- 232.249 AR WELD TENSII E STRESS 12430.8 AR WELD SHEAR STRESS 1524.37 AR BOLT SHEAR STRESS AR BOLT.TENSILE STRESS 8691 85'40.43
'3
~as wo.~4<<<
SHEET NO.~~
~ ~
isbasi c csp6 tm BASI C Compiler Version 5.4b JOi'00 REM>>>>>>>>>> BIF VALVE AND AIR OPERATOR SEISMIC STRESS 0002:00 REM>>>>>><<>>>><<<<<<<<<<>><<>>>> CSP-V/AO-6 >><<>><<<<>>>>>><<<<<<>><<>><<<<>><<<<>>>>>><<>><<>>
0003:00 REM 0004too var i,j,k = integer 0005:00 var lrod,lcg,x,phi, lave,abi t,l1,12,ei,e2,e3,e4,e5 ~ real 0006:00 var fst2, ca, ia,cb, ib,aa,ab,di,d2,ci, ii,c2, i2 real 0007:00 var lrodo,l cgo,1 dr,d, abush, pbush~real OOOS:0O var fcof, fco, ma,mb, siga, sigb, fcdr, fcdrf,maf, mbf=r eal 000900 var dear, fcear ', fr, f 11, f22, la, c i 12, c i 21, st t3, semi=real 0010:00 var sem2, se t3, sesi, ses2, sr, taui 1, tau22, tauear, aear~r eal 0011:00 var btens, taubl t, set3f,semlf,sem2f,fcearf, frf,fiif~real 0012too var f22f,stt3f,ses1f,ses2f,srf, tauif, tau2f, taurf~real 0013:00 var taubf,btf, dsr,dtaur,dtaub,dbten,dsa,dsb,dpb=real oo14:oo var sdr af,sdrbf,pbushf, tau11f, tau22f~real 0015:00 var wao,wbr, f tr f,watr 1, si, sl f, s2, s2f,mi,mi f,m2=real 0016:00 var m2f,t3,'t3f,tt3,tt3f,lbr,wtot~real 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 bsi etc TURN ON WITH K~1>>>>>>
0023: 00 REM 0024:00 REM 025:00 dim rea'i a(3,3)
'26:00 dim real b(3) 27:00 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 ~ s 875> ~ 46'48s 138<2 4isi 4 ~
0031:00 4 data 399<277>5 25ts 5t28 5t15 s6 875
~ ~ ~ ~ ~
0032:00 5 data 40.,10.96,26.5,30.5,2.075 0033 i 00 6 data 90 '90 s0 so s90
~ ~ ~ ~ 90 ~
0034:00 7 data 90.,0.,90.,180.,90.,90.
0035:00 REM DATA A%7'OR VAI VEf'GLOBAL-G ORIENTATIONS AND WEIGHT VECTOR 0036:00 r estore 0037:00 read di,d2,ci, i l,c2, i 2 0038:00 restore 2 0039:00 read rod, cg,x,phi, ave,abl t, 1, 12 1 1 1 1 0040'00 restore 3 0041:00 read fst2,ca, ia,cb, lb,aa,ab 0042:00 restore 4 0043:00 read wao,wbr,ei,e2,e3,e4,e5 0044:00 restore 5 ATTACHMHN7 0045:00 read irodo,lcgo,ldr,d,abush 0046:00 r estore 6 Voe Na, 0047:00 read a(1, 1 >, a(2, 1), a(3, 1), a< 1,2), a(2,2), a(3,2) Ri.ENO. <~ ~i 0048:00 restore 7 SHEEi NO.
0049-!00 -read a( 1,3),a<2,3),a(3,3),av( 1),av(2),av(3) 0050:00 text 0,8c INPUT GLOBAL ACCELERATIONS 5 "051 i 00 input b(1),b<2),b(3) 52: 00 print 53too text O,h INPUT DATA h 54!00 pr int 0055:00 print "GLOBAL G-LEVELS 0056:00 print "NORTH VECTOR ANGLES
'; b( 1 ), b(2), b(3>
~ ";a(i,i),a(2,1),a(3,1)
<<'MQI ~ MV Pl I II 4 0060 t00 for i~i to 3 008'1 !01 for Jpi to 3 0062!02 a< J q i )~a< J, i ) +2.+3.1'416/360 ~
'0063!02 gl c( J, i )~b( i ) icos(a(j, i ) )
064!02 next J 65!01 next 66!00 f'r j=i i to 3 367!01 av(j)~av(j>+2.+3.1416/360.
0068t01 next J 0069!00 pi int 0070:00 text O,h LOCAL G-LEVELS 5 0071!00 print 0072!00 pr i n t gl c(1, 1), gl c(1,2), gl c(1,3) 0073!00 pr int gl c(2,1),gl c(2,2),gl c(2,3) 0074!00 print glc<3yi)yglc(3,2),glc<3,3) 0075!00 REM WEIGHT COMPONENTS 0076!00 for J~i to 3 0077!01 wa(j)~ao+cos(av(j))
0078!01 wb(j)~broncos(av<j))
0079!01 next J 0080!00 phi~phi+2.+3.1416/360.
0081:00 la~lave/2 0082!00 ci12 ci/i2 0083!00 c i 21 ~c2/ i 1 0084!00 aear~li+12 0085:00 REM CALCULATE EAR FORCES USE ShR LOADS AS OPTION LATER 0086:00 REM FIXED COMPONENTS ARE ALWAYS THERE 0087:00 1 br =1 rod+1 cg 0088!00 watr i~1 br~a(1)/1 rod 0089:00 si f~b(1)+watr 1 0090!00 wtot~ao+wbr 091: 00 s2f~b(2)+wa(2)+f st2 92!00 t3f~a< 3)+wb(3) 093!00 mi f~-(wa(2)+wb(2)+ f st2) +e5ma(3) +(e3+ cg) ~b(3) +e4 1
0094!00 m2f~(watri+wb(1) ) we5~a(3) we2mb(3) we 1 0095:00 <coffel t t3f~atr.iwe3+<wa(2)+fst2) +e2+wb(1>+e4+wb<2) hei 0096!00 fcdrf cgMa(1)/lr od 1
0097:00 maf~fcdrfw< lr od-i3.5) 0098!00 mbf~fcdr f+7.125 0099:00 sdr af ~f s t2/aa+ abs(maf wc a/i a) 0100!00 sdrbf~f st2/ab+abs(mbf +cb/i b) 0101!00 ego~a<1)/1 rodo 0102!00 pbushf~f cof +(1 dr+d)'/(d+abush) 0103!00 REM STRESSES FROM FIXED COMPONENTS 0104!00 dear~( d 1 wdi+d2+d2> ++. 5 0105!00 set3f~abs( t3f/(4+aear) )
0106!00 semi.f ~abs(mi f/(2+d2+ae ar ) )
0107!00 sem2f~abs(m2f/(24di +aeat ) )
0108!00 fcearf~tt3f/<2%dear ) CY 0109:00 frf~x+fcear f ATTA 0110!00 f i if~-< fcearfwsin(phi )-frficos(phi) )
0111!00 f22f~fcearf+cos(phi )+frf+sin(phi ) JOB NQ.
0112:00 st t3f~abs( f 11 f+1 a+c i 12)+abs( f22f +1 a+c i 21) vaa No. 4 0113:00 ses1f~abs< si fwc i 12+1 a/4.)
0114!00 ses2f~abs(s2f +c i 21+1 a/4. ) SHEET NQ.~
0115:00 sr f=se t3f+seml f+sem2f+sesi f+ses2f+st t3f 0116!00 REM EAR SHEAR
"'17200 taui if~abs(sif/<4+aear) )+abs< f if/aear) 1 18200 tau22f~abs(s2f/(4+aear ) )+abs< f22f/aear) 19!00 taur f~( taui 1 f+taui 1 f+tau22f+tau22f) ++.5 120! 00 taubf=taurf+aear/abl t 0121:00 REM EARBOLT TENSION 0122:00 bt f~( se t3f+semi f+sem2f )+aear/abl t 0123!00 print 0124!00 print"OPERATING DRIVE ROD STRESS AT A ";sdraf n>>sinn nt i n 0" flPCPdTTNl PlOTL JC DAn %TUCANA dT A " <<arknhC
0 0
Va Av VV
~ pa ~ ~ ~ v vo 4oso ~ ~ o ~ ov vosa v v +vv v I
~ ~ vosvv ~ ~ ~ v y aevi 'v I, 0126!00 print" OPERATING CYLINDER BQG PRESSURE ';pbushf 0127!00 print" OPERATING VALVE EAR TENSILE STR ";st f 0128!00 print" OPERATING, VALVE EAR SHEAR STRES "; taurf
'4129!00 print" OPERATING EAR BOLT SHEAR STRESS ";taubf aiso$ oo p! int"OPERATING EAR BOLT TENSILE STR ";btf 31! 00 print 32!00 REN i33$ 00 REN. CALCULATE VARIABLE COMPONENTS 0134:00 REM 0135:00 dsr~o.
0136'00 dtaur=O.
0137:00 dtaub 0 ~
0138!00 dbten=0.
0139!00 dsa=o.
0140!00 dsb=a.
0141!00 dpb 0.
0142!00 for j~l to 3 0143!01 fco 1 cgoeuao+gl c(1, j ) r odo 0144!01 pbush~f co+(1 dr+d)/(d+abush) ll 0145!01 f t! i~l br~ao+gl c(1, j)J'1 r od 0146'Oi si~f trl+wbr +gl c(1, j) 0147!01 s~totwglc(2,j) 0148!01 t3~tot+glc(3,j) j)
0149!01 ml~~tot+gl c(2, +e5~ao+gl c(3, j) +(e3+1 cg) ~br+gl c(3, j ) +e4 0150! 01 m 2~(f tri+wbr +gl c(1, j) ) +e5-(wao+e2+wbr hei)+gl c(3,J) 0151 $ 01 t t3=f tr 1 we3+wbr+gl c(1, j ) we4+gl c(2, J ) +(wao+e2+wbr+e 1 )
0152! 01 fed> ~l cg~ao+gl c(l, j)i'1 rod 0153:01 m a=fcdr 4<1! od-13.5) 0154!01 m b~fcdr+7.125 0155!01 siga=ma+ca/'ia 0156:01 s i gb~becbl i b 157:Oi REN CALCULATE, EAR TENSION 58!01 se t3~abs( t3/'(4+aear)
$ 59!01 ~abs(mi/'(2wd2waear ) ) )'emi 016D! 01 sem2=abs(m2t'(2+dl +aear ) )
0161:Oi fcear ~t t3/(2wdear) 0162!01 fr~x+fcear 0163!01 f 1 i~-< fcear+sin(phi )-fr icos(phi ) )
0164!01 f22 fcear+cos(phi )+fr+sin(phi )
0165!01 st t3 abs( f 11+1 a+c i 12)+abs( f22+1 a+c i 21) 0166!01 sesi~abs(si +c i 12+1 a/4 ) ~
0167!01 ses2 abs< s2+c i 21 +1 a/4. )
0168!01 sr~se t3+seml+sem2+sesi+ses2+st t3 01 69!01 REN EAR SHEAR 0170!01 taui l~abs(sir'< 4. +aear ) )+abs( f 11/'aear) 0171! 01 tau22 abs(s2/'(4.+aear ) )+abs(f22/'aear )
0 1-72! 01- tauear ~< tau11+tau 1 1+ tau22+tau22) ++.5 0173!01 taubl t~tauear+aear/abl t 0174!01 REM EARBOLT TENSION 0175:01 btens (se t3+semi+sem2) +aeart'abl t 0176!01 dsa~dsa+s i ga+s i ga 0177!01 dsb~dsb+sigbwsigb ATTACHMENT 0178001 dpb~dpb+pbushwpbush 0179!!01 dsr~dsr+sr %sr JOB No.
0180! 01 dtaur~dtaur + tauear+tauear FLEgo 6 .bl 01.8.1.! 0,1 .dtaub dtaub+taubl t+taubl t 0182! 0 1 dbten~dbten+btens+btens SHEE f i4C.WC-
"'3$ O1 next .J 84! 00 REN COMBINE STRESSES 85!00 dsa~dsa++ ~ 5 186!00 dsb~dsb++.5 0187'00 dpb dpb4+.5 0188ioa dsr,=dsr +w. 5 0189!00 dtaur~dtaur ++.5 0190200 dtaub~dtaub++. 5 n! os nn~
h 1
VJ I4 ~ MV Vu '4 C I ~ W l. e ~ ~ ++ ~ 4 0192! 00 pr int 0173!00 text 0,8c DYNAMIC COMPONENTS 5 oi94!00 print
'0295:00 print "DRIVE ROD TENSILE STRESS AT A";dsa 0196!00 print "DRIVE ROD TENSILE STRESS AT B4;dsb 97!00 print "BUSHING PRESSURE 'fdpb 98!00 print "VALVE EAR TENSILE STRESS 3 dst f 99! 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 dsa~dsa+abs(sdraf) 0203:00 dsb+abs(sdt'bf) 'sb 0204!00 dpb~dpb+abs(pbushf) 0205!00 dsr ~dsr +abs< srf )
0206!00 dtaur~dtaur+abs< taurf) 0207!00 dtaub dtaub+abs( taubf )
0208!00 dbten~dbten+abs(btf )
0209:00 print 0210!00 text O,h FIXED PLUS DYNAMIC COMPON 0211!00 print 0212!00 print "DRIVE ROD TENSILE STRESS AT A';dsa 0213!00 print "DRIVE ROD TENSILE STRESS AT 8'dsb 0214:00 print "PUSHING PRESSURE 'dpb 0215!00 print "VALVE EAR TENSILE STRESS ".dsr 0216:00 print "VALVE EAR SHEAR STRESS "idtaur 0217! 00 print "EAR BOLT SHEAR STRESS ";dtaub 0218:00 print "EAR BOLT TENSILE STRESS "idbten 0219!00 end 0220!00 0221200 0222!00 223!00
'z4:ao z25!00 End gf pl c!gr am iosNO. '4 FlLE No.
SHfETHO.~
csp6 NPUT GLOBAL-ACCELERATIONS
~ 39<3 33s5 85 ~ F
)~r'UT DATA GLOBAL'-LEVELS WORTH VECTOR ANGLES ~
11.39 5'0 3
90
'3 0 5 F 85 VERTICAl VECTOR ANGLES= 0 90 90 ST VECTOR ANGLES = 90 0 5'0 LOCAL G-LEVELS
-4.34494E-5 3.33 -2. 2316E-5 "4. 34494E-5 -1.27025'E-5 5. 85 11.39 -1 27029E-5
~ -2.2316E-5 OPERATING DRIVE ROD STRESS AT A S048 35~
3PERATING DRIVE ROD STRESS AT,B 7721 14~
3PERATING CYLINDER BRG PRESSURE -98.4646 3PERATIhlG VALVE EAR'ENSILE STR 4664.2S 3PERATIh(G VALVE EAR SHEAR STRES 297 614
~
3PERATING EAR BOLT SHEAR STRESS'600 ~ 17 3PERATING EAR BOLT TENSILE STR 1340.69 DYNAMIC COMPONENTS .
ROD TENSILE STRESS AT A 16811 vE ROD TENSILE STRESS AT B 25711.4 BUSHING PRESSURE 327.887 fALVE EAR TENSILE STRESS 17822.1 VALVE EAR SHEAR STRESS WR BOLT SHEAR STRESS 1 154 '2 13963.6 R BOLT TENSILE STRESS 57543 FIXED PLUS DYNAMIC COMPONENTS 3RIVE ROD TENSILE STRESS AT A 21855' 4
>RIVE ROD TENSILE STRESS AT B 33432.5
~USHING PRESSURE'ALVE 426.352 EAR TENSILE STRESS 22486.4 fALVE EAR.SHEAR STRESS 1451 3
=AR BOLT SHEAR STRESS 17563.7 MR BOLT" TENSILE STRESS 58883.7
I l
0
6 7 GLOBAL ACCELERATIONS
.35',3.33,5.8S .
INPUT DATA GLOBAL G-LEVELS 11.39
~ 90 3
90
'3 0 5 '5 4ORTH VECTOR ANGLES VERTICAL VECTOR ANGLES= 0 5'0 5'0 ST VECTOR ANGLES = 90 0 5'0 LOCAL G-LEVELS "4.34494E-5 3.33 -2.2316E-S
-4.34494E-5 -1.27029E-5 5.85 11.39 -1.27029E-5 -2.2316E-5, OPERATING DRIVE ROD STRESS AT
~~5048.35 OPERATING OPERATING DRIVE ROD STRESS AT B CYLINDER BRG PRESSURE 7721 '4~~
-98.4646, OPERATING EAR WELD TENSILE STR 5107.51 OPERATING EAR WELD SHEAR STRES 631 '31 OPERATING EAR BOLT SHEAR STRESS 3600 17
~
OPERATING EAR BOLT TENSILE STR 1340 69
~
<ANI C CONPONENTS VE ROD TENSILE STRESS AT A 16811 DRIVE ROD TENSILE STRESS AT. B 25711 ~ 4 BUSHING PRESSURE 327.887 PR WELD TENSILE STRESS 21586 '
R MELD SHEAR STRESS 2445'.05 PR BOLT SHEAR STRESS 135'63.6 R BOLT TENSILE STRESS S7543 FIXED PLUS DYNANIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 21859"4
>RIVE ROD TENSILE STRESS AT B 33432.5
~USHING PRESSURE 426.352 PR WELD TENSILE STRESS 26693.7 R WELD SHEAR STRESS 3080.48 PbR BOLT SHEAR STRESS 17563.7 R BOLT TENSILE STRESS 58883.7 JOB BO.~~'~
ma No.~d.~~t. F SHEET bio.~
0 6
UT GLOBAL ACCELERATIONS
.39,3.33~5.85 INPUT DATA
)LOBAL G-LEVELS 11.39 3.33'0 5.85
)ORTH VECTOR ANGLES = 90 0 jERTICAL VECTOR ANGLES= 0 90 90 ST VECTOR ANGLES = 90 0 LOCAL G-LEVELS 4.34494K-5 3.33 -2.2316E-S
.4.34494E-5 -1.27029E-5 5.85 11.39 -1 '7029E-5 -2.2316E-5
)PERATING DRIVE ROD STRESS AT A 5048.35
)PERATING DRIVE ROD STRESS AT 8 7721 ~ 14
)PERATING CYLINDER BRG PRESSURE -98.4646
)PERATING VALVE EAR TENSILE STR 4664.25
)PERATING VALVE EAR SHEAR STRES 297 614
~
)PERATING EAR BOLT SHEAR STRESS 3600.17
)PERATING EAR BOLT TENSILE STR 1340 69
~
-906.782
-2.57874E-3
=-2.57873E-3
>if= 9s89667E-2 i2f=-6234 1 F
~~t3f=-22103. 8 DYNAMIC COMPONENTS iRIVE ROD TENSILE STRESS AT A 16811~~
'RIVE ROD TENSILE STRESS AT B 25711 4 ~
lUSHING PRESSURE 327.887
'ALVE"'EAR TENSILE STRESS 17822.1
'ALVE EAR SHEAR STRESS "AR BOLT SHEAR. STRESS 1154 '2 13963.6 AR BOLT TENSILE STRESS 57543
.id= 3019.58
.2d= 3954.6 3d= 7699.63 i)d= 2.44083E+5 2d=-58968.3---
t3d~ 78875.3 ms~.~~
vmxo.~ '~~'"
F "=D PLUS DYNAMIC COMPONENTS SHEET Ho.
E ROD TENSILE STRESS AT A 21859 '
VE ROD TENSILE STRESS AT B 33432.5 USHING PRESSURE 426.352 ALVE EAR TENSILE STRESS 22486.4 ALVE EAR SHEAR STRESS 1451.93 AR BOLT SHEAR STRESS 17563.7
~
'a
R BOLT TENSILE STRESS 58883e7
~15= 3926.36 s2t= 3954.6
'.3t= 7699.64~
2.44083E+5
~
65202.4~
= 1.00979E+5
~
I \
E I N'
~
T GLOBAL ACCELERATIONS 11.37,3.18,5.83
~QP Q ggQf INPUT DATA GLOBAL G-LEVELS 11.37 3. 18 5.83 IORTH UECTOR ANGLES ~ 90 90 0 VERTICAL VECTOR ANGLES~ 0 90 90 ST VECTOR ANGLES ~ 90 0 90 LOCAL G-LEVELS
~~4. 33731E-5 3 ~ 18 -2.22397E-5~~
.4 33731 E-5
~ -1 21 307E-5
~ 5.83 11.37 -1.21307E-S -2.22397E-5
)PERATING DRIVE ROD STRESS AT A 5048 35
~
)PERATING DRIVE ROD STRESS AT B 7721 ~ 14
)PERA'TING CYLINDER BRG PRESSURE -98.4646 OPERATING EAR WELD TENSILE STR 5107.51
)PERATING EAR WELD SHEAR STRES '31 '31
)PERATING EAR BOLT SHEAR STRESS 3600 17
~
)PERATING EAR BOLT TENSILE STR 1340 69
~
PII C COMPONENTS I
>RIVE ROD TENSILE STRESS AT
~~16053 '~~
'RIUE ROD TENSILE STRESS AT B 24553.2
)USHING PRESSURE 313 '17
~~AR WELD TENSILE STRESS 20967~~
~~'AR WELD SHEAR STRESS 2365.96~~
~~AR BOLT SHEAR STRESS 13489.8~~
'AR BOLT TENSILE STRESS 57426.5 FIXED PLUS DYNAMIC COMPONENTS
'RIUE ROD TENSILE STRESS AT A 21102. 1 RIVE ROD TENSILE STRESS AT 8 32274.4
'USHING PRESSURE 411.582 40B No. ~444 AR WELD TENSILE STRESS 26074.5 Rmre.AMP
~~AR WELD SHEAR STRESS 2997.39 $ HEET NO.~~
AR BOLT SHEAR STRESS 17090
'.AR BOLT TENSILE STRESS 58767.2
0 I
1
~~sp6 INPUT GLOBAL ACCELERATI ONS.~~
69,3.09,1.48 QPg fP i dT'ATA GLOBAL G-LEVELS (ORTH VECTOR ANGLES =
2.69 90 3
90
'9 jERTICAL VECTOR ANGLEM 0 90 90
&ST VECTOR ANGLES = 90 0 LOCAL G-LEVELS
.1 ~ 02615E-5
.1.02615E-5 3 '9
-1.17874E-5
-5.64575E-6 1 '8 2.69 -1.17874E-5 -5.64575E-6 jPERATING
~~PERATING DRIVE ROD STRESS AT A DRIVE ROD STRESS AT B 5048 7721 ~~~
'514 3PERATING CYLINDER BRG PRESSURE -98.4646
'PERATING EAR WELD TENSILE STR 5107.51~
jPERATING EAR WELD SHEAR STRES 631 ~
EAR BOLT SHEAR STRESS 3600 17.
431'PERATING
~
)PERATING EAR BOLT TENSILE STR 1340.69 DYNAMIC COMPONENTS ROD TENSILE STRESS AT A 15599 '
E ROD TENSILE STRESS AT B 23858.3
'USHING PRESSURE 304 '56
,;AR WELD TENSILE STRESS 16110 '
R WELD SHEAR STRESS 1976 '1.
.AR BOLT SHEAR STRESS 11271 AR BOLT TENSILE STRESS 14173.8 FIXED PLUS DYNAMIC COMPONENTS RIVE ROD TENSILE STRESS AT A 20647.7 RIVE ROD TENSILE STRESS AT B 31579 '
'USHING PRESSURE 402.72 AR WELD==-TENSI'LE STRESS 21218.3
'AR WELD SHEAR STRESS 2608.24 AR BOLT SHEAR STRESS 14871 '
AR BOLT TENSILE STRESS 15514 '
0 VVVj ~ VV .PI IIII W41VIII Vl VIVII PI'%VLC'V'OYllf,yOYICIyOYIOI sbasic cep3a tm
-BASIC Compiler Versian 5.4b
)01:00 REM>>>>>>>>>> BIF VALVE AND AIR OPERATOR SEISMIC STRESS v002:00 REM>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> CEP-V/AO-3A >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>
0003:00 REM 0004:00 var i, j,k = integer 0005'00 var 1rad, I cg,x,phi ave,abl t, l 1,12,ei,e2,e3,e4,e5 = real
> 1 0006ioo var fst2, ca, ia,cb, ib,aa,ab,di,d2,ci, i i,c2, i2 real 0007:00 var lrado,lcgo,ldr>d, abush, pbush~reai 0008:00 var fcof, fco, ma,mb, si ga, sigb, fcdr, fcdrf,maf, mbf~real 0009:00 var dear, fcear,fr, f11,f22,la, ci12,cI21,stt3,semi~real 0010:00 var sem2,set3,sesi,ses2,sr, taui1, tau22, tauear,aear~real 0011:00 var btens, taubl t, set3f,semif,sem2f,fcearf, frf,fiif~real 0012!00 vat f22f,stt3f,sesif,ses2f,srf, tau1f, tau2f, taurf~r eal 0013:00 var taubf, btf, dsr, dtaur, dtaub, dbten, dsa, dsb, dpb~real 0014:00 0015:00 var var sdr af,sdrbf,pbushf, taui if, tau22f~real wao,wbr, f tr i,watr 1, si, si f, s2, s2f,mi,mi f,m2~reaI 0016:00 var m2f, t3, t3f, t t3, t t3f, br,wtat=real 1
0017:00 var bsi,bs2,bt3,bmi,bm2,btt3 real 0018:00 dim real av(3) 0019:00 dim real wa(3)
OO20:OO dim real wb(3) 0021: 00 REM 0022:00 REM >>>>>> BURNS 7 ROE EAR FORCES ARE bs1 etc TURN ON 4IITH K~1>>>>>>
0023:00 REM 0024:00 REM 0025:00 dim real a(3,3) 026:00 di'm real b(3)
J27: 00 dim real glc<3,3).
028'0 i. 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 , 875,.46,.648,.138>2.41,1.4 0031:00 4 data 399,277,5.25,8.5,28.5,15.,6.875 0032!00 5: data 40 ~ ~10 ~ 96s26 ~ Ss30 ~ Sr'75 0033:00 6 data 90.,90.,0.,90.,0.,90.
0034'0 7 data 180.,90.,90.,90.,180.,90.
0035'00 REM DATA 6&7 FOR VALVE/GLOBAL-G ORIENTATIONS AND WEIGHT VECTOR 0036:00 restore 0037too r ead, d1,d2,c1, i i,c2, i 2 0038:00 restore 2 0039:00 0040: 00 read rod, cg,x,phi, ave,abl r
1 estor e 3 1 1 t, l 1,12 0041:00 0042'00 read fst2,ca,ia,cbyibyaa,ab restore 4 CYGRA 0043: 00 read wao,wbr,ei,e2,e3,e4,e5 ATTACHPilENT 0044:oo restore 5 Voa No.
0045:00 read Iroda,lcgo,ldr,d,abush restor e 6 FILE NO. 4 ~
0046:00'047:00 i'ead a(1, 1), a<2,1), a(3, 1), a(1,2), a(2,2), a(3,2) 0048:00 restore 7 SHEET. NO. W&
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 input b(1),b(2),b<3)
"52:00 print 53i00 text 0,& INPUT DATA &
54:00 pf int 055:00 print "GLOBAL G-LEVELS "Ib< 1') sb<2) sb(3) 0056too print "NORTH VECTOR ANGLES ~ ";a(1,1),a<2,1),a(3,1) 0057:00 pr int "VERTICAL VECTOR ANGLES= ";a(1,2),a(2,2),a<3,2) 0058:00 print "EAST VECTOR ANGLES = ";a(1,3),a<2,3),a(3,3)
ilation complete '
INPUT GLOBAL ACCELERATIONS
'? 4.57,1.26,.86 INPUT DATA
~
GLOBAL G-LEVELS 4.57 1 ~ 26 .86, WORTH VECTOR ANGLES ~ 90 90 0 VERTICAL VECTOR ANGLES= 90 0 90 ST VECTOR ANGLES = 180 90 90 WEIGHT VECTOR ANGLES = 90 180 90 LOCAL G-LEVELS
-1.74332E-5 -4.80652E-6 .86 "1.74332E-5 1.26 -3.28064E-6 4 '7 -4.80652E-6 ~ -3.28064E-6 3PERATING DRIVE ROD STRESS AT A 477. 198 OPERATING DRIVE ROD STRESS AT B 821 '58 3PERATING CYLINDER BRG PRESSURE -3.75613E-4 3PERATING VALVE EAR TENSILE STR 1136 52
~
3PERATING VALVE EAR SHEAR STRES,89 ~ 1706 3 ERATING EAR BOLT SHEAR STRESS 1078.68
%TING EAR BOLT TENSILE STR 525.595
@i f~-3. 4591 E-3 32f= 474 t3f~-2. 57873E-3 ni f~-3258. 67 n2f~-5.29623E-3 r.t3f= 4929 17 ~
DYNAMIC COMPONENTS
)RIVE ROD TENSILE"'STRESS AT A 4341 .57
)RIVE ROD TENSILE STRESS AT B 6640 . 18 PUSHING PRESSURE 84.6795
)ALVE EAR TENSILE STRESS 4711.31
>ALVE EAR SHEAR STRESS 285 '35 R BOLT SHEAR STRESS 3458.89 MR BOLT TENSILE STRESS 22999.3
~id= 779.831 a2d= 851 76
'.3d~ 3089
>id= 97498.6
'1
>2d 22785 19965.7 FIXED PLUS DYNAMIC COMPONENTS
>RIVE ROD TENSILE STRESS AT A 4818.76
)RIVE ROD TENSILE STRESS *T B 7461 ~ 64
'USHING PRESSURE 84.6799
VALVE EAR TENSILE STRESS 5847.84 VALUE EAR 'SHEAR STRESS 375.106 EAR BOLT SHEAR STRESS 4537.57 EAR BOLT TENSILE STRESS 23524.9 779.835 1325.76
.3089.32 a1i= 1.00757E+5 w2t= 22785 tt3t= 24894.9
m ilation cmpiett 3.OBAL ACCELERATII6 4.57)1 26)&.86 INPUT DATA LOBAL 0-LEVELS > 4.57 1.26 .86 3RTH VECTOR ANGLES 90 90 0 BTICAL VECTOR NGLEN 90 0 90
)ST VECTOR ANGLES -"1&0 90 90
=IGKT VECTOR NGLES > 90 180 90
.OCAL Crt9lELS 1.74332E-5 -4.&0652E-6 -.86 1.74332E-5 1.26 -3.28064E-6 4.57 "4.80652E-6 -3.28064E-6
?ERATIHG DRIVE ROD STRESS AT A 477.198
?ERATIHG DRIVE ROD STRESS AT 8 821,458
'ERATIHG CYLINDER BRG PRESSURE
-3.75613'ERATING EAR MELD TENSILE STR 1326 01 ~
'ERATING EAR MELD SHEAR SIRES 189.188
'ERATIHB EAR BOLT SHEN STRESS 1078.68
c TING EAR BOLT TSSILE STR 525,595 N4NIC CNRNEHTS RIVE ROD TENSILE STRESS AT A 4341.57 RIVE ROD TENSILE STRESS AT 8 6640.18 iSHING PRESSURE 84.6795 8 MELD TENSILE STRESS 6247,02
>R MELD SHEAR STRESS 606.65 8 BOLT SHEAR STRESS 3458.89
%R BOLT TENSILE STRESS 22999.3 I U
.IXED PLUS 9NNIC CNRNEHTS ALIVE ROD TEHSILE'STRESS AT A 481&.76 IIVE ROD,TEHSILE STRESS AT 8 7461.64 iSHING PRESSURE 84.6799 8 MELD TENSILE STRESS 7573.03
)R MELD SHEAR STRESS 795.838 8 BOLT SHEAR STRESS 4537.57
)R BOLT TENSILE STRESS 23524.9
0 I
sbasic cep4a tm
-BASIC Compiler Version 5.4b 0001:00 REM<<<<>><<<<BIF VALVE AND AIR OPERATOR SEISMIC STRESS 0002:00 REM<<<<<<<<<<<<<<<<<<<<<<<<<<<<>> CEP-V/AO-4A <<<<<<<<<<<<<<<<<<<<<<<<>><<<<<<<<<<<<<<<<>><<<<<<<<
,0003:00 REM 0004:00 var i,j,l< ~ integer 0005:00 var lrod,lcg,x,phi,lave,ablt,11,12,el,e2,e3,e4,e5 ~ real
.0006:00 var fst2, ca,ia,cb,ib,aa,ab,di,d2,cl,ii,cZ>i2 real 0007:00 var lrodo,lcgo,ldr,d, abush, pbush~real 0008i00 var fcof, fco, ma,mb, si ga, ai gb, fcdr, fcdr f,maf, mbf~real 0009:00 var dear, fcear,fr, fil,f22,1a, ci12,ci21,stt3,semi~t eal 0010:00 var sem2,set3,seal,ses2,sr, taui 1, tau22, tauear,aear~r eal 0011'00 var btens, taubl t, se t3f, semi f, sem2f, fcearf, fr f, f f~real 1 1 0012:00 var f22f,stt3f,sesif,ses2f,srf, tauif, tau2f, taur f~real 0013:00 var taubf, bt f, dsr, dtaur, dtaub, dbten, dsa, dsb, dpb real 0014:00 var sdraf,sdrbf,pbushf, taul if, tau22f~real 0015500 var wao,wbr,f trf,watri,si,sl f,s2,s2f,ml,mif,m2 real 0016:00 var m2f, t3, t3f, t t3, t t3f, br,wtot~real 1
0017:00 var bsl,bsZ,bt3,bml,bmZ,btt3~real 0018:00 dim real av(3) 0019:00 dim real wa(3) 0020!00 dim real wb(3) 0021 too REM 0022:00 REM <<<<<<BURNS 7 ROE EAR FORCES ARE bsi etc TURN ON WITH K~1<<<<<<
0023:00 REM 024:00 REM 125:00 dim real a(3,3) 026:00 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 , 875,.46,.648,.138,2.41,1.4 0031:00 4 data 399,277,5.25,8.5,28.5,15 '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.,90.,90.,90.,-128.,-38.
0035:00 REM DATA 68c7 FOR VALVE/'GLOBAL-G ORIENTATIONS AND 4IElGHT VECTOR 0036:00 ~
reatore 0037:00 read di,d2,ci,ii,c2,i2 0038ioo restore 2 0039:00 read lr od, cg,x,phi, ave,ab'1 t,11,12 1 1 0040:00 restore 3 0041:00 read fst2,ca,ia,cb,ib,aa,ab 0042:00 restore 4 A~ACHRIENT 0043:00 read wao,wbr,el,eZ,e3,e4,e5 0044:00 restore 5 gaS NO.
0045:00 read lr odo,lcgo,ldr,d,abush FILE No.
0046>00 restore 6 0047:00 read a(1,1),a(2,1),a<3,1),a(1,2),a(2,2),a(3,2) SHEET HO.L +
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
>51: 00 input b(1),b(2),b(3) 52 00 print 053ioo text O,h INPUT DATA 5 0054:00 pr in t 0055ioo print "GLOBAL G-LEVELS, ~ "; b(1), b< 2), b(3) 0056:00 print "NORTH VECTOR ANGLES ~ "la(1,1),a(2,1),a<3,1) 0057:00 pr int "VERTICAL VECTOR ANGLES~ ";a(1,2),a<2,2),a<3,2) 0058:00 print "EAST VECTOR ANGLES ~ ":a(1.3).a(2.3),a(3.3)
0 0
0059$ 00 pr int "WEIGHT VECTOR ANGLES ~ ";av(1),av (2), av(3) 0C60$ 00 print 0061:00 for i~i to 3 0062$ 01 for j~i to 3 0063$ 02 a(j si)=a(j,i)+2.%3.1416/360.
064:02 glc(J,i)=b(i)icos(a(J,I))
065$ 02 next J 066$ 01 next i 0067$ 00 for j=i to 3 0068 Oi av( J')=av( j ) +2.+3.1416/360.
0069$ 01 next int j
0070$ 00 pr 0071$ 00 text O,h LOCAL G-LEVELS h 0072$ 00 print 0073:00 print glc( 1,1),glc(1,2),glc(1,3) 0074:00 print glc<2, 1),glc(2,2),glc(2,3) 0075:00 print glc(3, 1),glc(3,2),glc<3,3) 0076:00 REM WEIGHT COMPONENTS 0077$ 00 for j~i to 3 0078:01 wa(j)~ao+cos(av(j) )
0079$ 01 wb(j)~broncos(av(j))
0080:01 next J 0081500 phi~phi+2.+3.1416/360.
0082$ 00 la=lave/2 0083$ 00 ci12 ci/i2 0084$ 00 c i 21~c2/i 1 0085!00 ae area l 1+] 2 0086$ 00 REM CALCULATE EAR FORCES USE EkR LOADS AS OPTION LATER 0087$ 00 REM FIXED COMPONENTS ARE ALWAYS THERE 0088$ 00 lbr~lrod+lcg 0089"$ 00 watr 1~1 br ~a< 1)/l rod 0090$ 00 sif~b(1)+watr 1 4)91 $ 00 wtot~ao+wbr J92$ 00 s2f~b(2)+wa(2)+f st2 0093$ 00 t3f~a(3)+wb< 3) 0094$ 00 mi f~-<wa<2)+wb(2)+f st2) +e5~a(3) +(e3+1 cg) ~b(3) we4 0095'00 m2f~(watr 1+wb(1) ) +e5~a(3) +e2~b(3) hei 0096$ 00 tt3f~atri+e3+<wa<2)+fst2)+e2+wb(1) we4+wb <2) we 1 0097:00 fcdr f~1 cg~a(1)/1 rod 0098:00 maf~f cdr fw( r od-13. 5) 1 0099"$ 00 mbf=f cdr f+7. 125 0100$ 00 sdraf~f st2/aa+abs(maf +ca/i a) 0101$ 00 sdr bf~fs t2/ab+abs(mbf +cb/i b) 0102$ 00 fcoffel ego~a(1)/1 rodo 0103$ 00 pbush f~f cof +( dr +d)/(d+abush) 1 0104$ 00 REM STRESSES FROM FIXED COMPONENTS 0105,'0,0. dear~(di+di+d2+d2)++.5 0106$ 00 se t3f~abs< t3f/(4+aear) )
0107$ 00 f semi ~abs(mi f/( 2%d2+ae ar ) )
0108:00 sem2f =abs(m2f/< 2wdi wae ar ) ) g~AQH SRBNT f f 0109$ 00 c ear ~t t3f/(2+dear )
0110'0 "fr f~xwfcear f Zo Oiii:00 f f~-( fcear f+s in(ph i ) -fr ficos(ph 1 1 i ))
JOB NO 0112$ 00 f22f~fcear f+cos(phi )+frfwsin<phi )
0113$ 00 st t3f~abs(f 1 i f+1 a+c i 12)+abs< f22fwl a+c I 21) f 0114$ 00 sesi f~abs( s1 +c i 12%1 a/4. )
PlL,E NO SHEET y~Q, ~
0115$ 00 ses2f ~abs( s2f +c i 21 %1 a/4. )
0116$$ 00 sr f~se t3f+seml f+sem2f+ses 1 f+ses2f +s t t3f 17:00 REM EAR SHEAR
$ 18$ 00 tau 1 1 f~abs(s1 f/(44aear) )+abs< f 11 f/aear )
119$ 00 tau22f~abs(s2f/(4+aear) )+abs(f22f/aear) 0120:00 taut f=( tau11 f+taui 1 f+ tau22f wtau22f ) ++.5 0121$ 00 taubf~taurf+aear/abl t 0122$ 00 REM EARBOLT TENSION 0123$ 00 b t f~( se t3f+ semi f+sem2f ) +ae ar/ab1 t 0124:00 print
0125! 00 pc'int" OPERATING DRIVE.ROD STRESS AT A 'sdraf 0126 200 pr int" OPERATING DRIVE ROD STRESS AT B ";sdrbf 0127! 00 pr in't" OPERATING CYLINDER BRG PRESSURE ";pbushf
~
0128200 print"OPERATING VALVE EAR TENSILE STR "lsrf 0129:00 print" OPERATING VALVE EAR SHEAR STRES "i taurf 130200 print" OPERATING EAR BOLT SHEAR STRESS "; taubf 131200 print'OPERATING EAR BOLT TENSILE STR ";btf 132200 print 0133200 REM 0134:00 REM CALCULATE VARIABLE COMPONENTS 0135200 REM 0136200 dsr ~0.
, 0137200 dtaur~O.
0138!00 dtaub~0.
0139200 dbten~O.
0140: 00 dsa~O.
0141! 00 dsb=O.
0142200 dpb=0.
014320D for J~i to 3 0144201 fco lcgo+wao+glc(1,J)f'lrodo 0145:01 pbush~fco+<ldr+d)t'(d+abush) 0146201 f tr i~i br~ao+gl c(i,j)/1 rod 0147201 si~f tri+wbr+gl c(1,J) 0148201 s2=wtot+glc(2,J) 0149201'150201, t3=wtot+glc(3,J>
mi~~tot+gl c(2; J) we5~aowgl c(3,J) +<e3+1 cg) ~brwgl c(3,J) +e4 0151! 01 m2~(f tr 1+wbrwgl c(i,j) ) +e5-<waowe2+wbr+ei) +gl c(3,J )
0152201 t t3 f tri+e3+wbr+gl c(i,j)+e4+gl c(2,J) +(wao+e2+wbr+ei) 0153:Oi fc dr~ c g~ao+g l c ( 1, J ) t'1 r od 1
0154201 ma=f cdr+< rod-13. 5) 1 k 0155201 mb~fcdr+7.125 0156:01 s i ga~a+c~i a 1572Di s f gb=mb+c bl i b abaci 158:01 REM CALCULATE EAR TENSION 0159201 se t3 abs( t3/(4+aear ) )
0160 01 semi~abs(mli'(2+d2waear))
0161 201 sem2=abs(mM(2+di+aear)>
0162201 fcear~tt38'(2%dear) 0163201 fr~x+fcear 0164201 f i i~-<fcearwsin(phi )-frescos(phi ) >
0165201 f22~f cear+c~-ph-W+4 r+s i n(ph i >
0166:01 st t3 abs< f 1 1>i 12)+abs< f22+1 a+c i 21) 0167201 sesl=abs( sl wc i 12+1 a/'4. )
0168'.01 ses2 abs(s2+ci21+1 M4.)
0169: 01 sr~set3+seml+sem2+sesi+ses2+stt3 0170 201 REM EAR SHEAR f
..0$ .7,1 0.1- tauif'=abs(si/'(4. +aear) )+abs( 11/aear) 2 f
0172201 t au22=abs( sM(4. +aear ) ) + abs( 22ae ar )
0173201 tauear =( tau11+taui 1+ tau22+tau22) ++.5 0 1'7.4: 01 taubl t~tauear+aear/abl t 0175! 0.1 REM EARBOLT TENSION 0176201 btens~< se t3+sem1+sem2) +aear/abl 0177201 dsa~dsa+siga+siga t CYaMz 0178201 dsb=dsb+sigb+sigb ATTACHINBNT 0179:01 dpb~dpb+pbush+pbush JOB NO.
0180:Oi dsr,=dsr+sr+sr FILKNO. D 0 0181201 dtaur~dtaur+ taueat +tauear ni 82:01 dtaub dtaub+taubl t+taubl t SHEET N0.8=~
.83201 dbten=dbten+btens+btens
~ 2 84'$01 next 85: 00 J'EM COMBINE STRESSES 0186200 dsa~dsa++.'5 0187:00 dsb~dsbw+.5 0188200 'dpb~dpbw+.5 0189:00 dsr~dsr++.5 0190200 dtaur~dtaur++.5
0191 !00 dtaub dtaub++.5 01'92:00 dbten~dbten++.5 0193:00 pr int 0194t00 text O,h DYNAMIC COMPONENTS h 0195!00 print 196:00 print "DRIVE ROD TENSILE STRESS AT A";dsa 197 i 00 print "DRIVE ROD TENSILE STRESS AT B")dsb i98:00 print "BUSHING PRESSURE "idpb 0199t00 print "VALVE EAR TENSILE STRESS ";dsr 0200200 print "VALVE EAR SHEAR STRESS ";dtaur 0201:00 print 'EAR BOLT SHEAR STRESS ";dtaub 0202:00 print "EAR BOLT TENSILE STRESS 'dbten 0203:00 dsa~dsa+abs( sdraf )
0204:00 dsb dsb+abs(sdrbf) 0205:00 dpb~dpb+abs(pbushf) 0206!00 dsr~dsr+abs(srf) 0207:00 dtaur~dtaur+abs(taurf) 0208:00 dtaub~dtaub+abs(taubf) 0209:00 dbten~dbten+abs(btf) 0210:00 print 0211:00 text O,h FIXED PLUS DYNAMIC COMPONENTS h 0212:00 print 0213)00 print "DRIVE ROD TENSILE STRESS AT *"sdsa 0214:00 print 'DRIVE ROD TENSILE STRESS AT B"'dsb 0215!00 print "PUSHING PRESSURE "idpb-0216:00 print "VALVE EAR TENSILE STRESS "jdsr 0217 ! 00 print "VALVE EAR SHEAR STRESS "idtaur 0218:00 print "EAR BOLT SHEAR STRESS ";dtaub 0219: 00 print "EAR BOLT TENSILE STRESS "sdbten 0220: 00 end 0221:00 0222:00 223200 224:00 0225!00 0226:00 ++++++ End of program ++++++
CYGMA ATTACHMENT JOB No.
vaa xo.
~
ZO
<~UT GLOBAL ACCELERATIONS
~
35,1.34,.86
~ ~
INPUT DATA GLOBAL G-LEVELS 3.35 1 ~ 34 .86 NORTH VECTOR ANGLES ~ 90 -38 52 VERTICAL VECTOR ANGLES 90 52 142 ST VECTOR ANGLES
~ 180 90 90 VEIGHT VECTOR ANGLES ~ 90 -128 -38 LOCAL G-LEVELS
-1.27792E-S -5.11169E-6 -.86 2.63983 .824984 -3.28064E-6 2.06246 -1.05594 -3.28064E-6 3PERATING DRIVE ROD STRESS AT
~~477.198 OPERATING DRIVE ROD STRESS AT B 821 ~ 458 3PERATING CYLINDER BRG PRESSURE -3 75613E-4~~
~
3PERATING VALVE EAR TENSILE STR 1946 57
~
3PERATING VALVE EAR SHEAR STRES 128 033
~
3PERATING EAR BOLT SHEAR STRESS 1548.79 3PERATING EAR BOLT TENSILE STR 4771 ~ 17
'%HI C COMPONENTS VE ROD TENSILE STRESS AT A 4341.57 DRIVE ROD TENSILE STRESS AT B 6640 ~ 18 3USHING PRESSURE 84.6795 VALVE EAR TENSILE STRESS 5948.81 HALVE EAR SHEAR STRESS 379. 21 1 MR BOLT SHEAR STRESS 4587.24 R BOLT TENSILE STRESS 13246.5 FIXED PLUS DYNAMIC COMPONENTS
)RIVE ROD- TENSILE-STRESS AT A 4818.76
)RIVE ROD TENSILE STRESS AT 8 7461.64
'USHING PRESSURE 84.6799 JALVE EAR TENSI't.E STRESS 7895.38
>ALVE EAR SHEAR STRESS 507.244 R BOLT SHEAR STRESS 6136.03 AR BOLT TENSILE STRESS 18017.7 ATTACHMENT JOB NO.
RLENO ~otol Ã s~arr vo.~>~
3>cep4a GLOBAL ACCELERATIONS 5,1.34,.86 raut.-si0( Qacb)
INPUT DATA 3LOBAL G-LEVELS 3.35 1.34 ~ 86
<ORTH VECTOR ANGLES = 90 -38 52
)ERTICAL VECTOR ANGLES= 90 52 142 9bST VECTOR ANGLES = 180 90 90 JEIGHT 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
)PERATING DRIVE ROD STRESS AT A 477oi98 3P ERAT IN G DRIVE ROD STRESS AT B 821.458 3P ERAT ING CYLINDER BRG PRESSURE -,3.75613E-4 3PERATING EAR WELD TENSILE STR 2592.98
)PERATING EAR'ELD SHEAR STRES 271.64
)PERATI NG EAR BOLT SHEAR STRESS 1548.79
)PERATING EAR BOLT TENSILE STR 4771 '7
'MIC COMPONENTS
) E ROD TENSILE STRESS AT A 4341 .57
)RIVE ROD TENSILE STRESS AT B 6640 18 ~
3USHING PRESSURE 84.6795 MR MELD TENSII E STRESS 7493.12
~~AR MELD SHEAR STRESS 804.547 R BOLT SHEAR STRESS 4587.22 R BOLT TENSILE STRESS 13246.5 FIXED PLUS DYNAMIC CCNPONENTS~~
)RIVE ROD TENSILE STRESS AT A 4818.76
)RIVE ROD TENSILE STRESS AT B 7461.64
'USHING PRESSURE 84.6799 R WELD TENSI'LE STRESS 10086 F 1 i"-tR MELD SHEAR STRESS 1076.19 R BOLT SHEAR'TRESS 6136.01
~~AR BOLT, TENS.ILE STRESS 18017.7 JOB NO.~Z~~~
RLS NO N'of l-SHEET No ~~
lt V
i e
ep INPUT"-GLOBAL ACCELERATIONS
? 3.35,1.34).86 INPUT DATA GLOBAL G-LEVELS 3.35 1.34 ~ 86 lORTH VECTOR ANGLES 90 -38 52 VERTICAL VECTOR ANGLES= 5'0 52 142 ST VECTOR ANGLES 180 90 90 JEIGHT VECTOR ANGLES 90 -128 -38 LOCAL G-LEVEL'S
-1.2775'2E-5 -5.11165'E-6 .86 2.63983 .8245'84 -.3.28064E-6 2 '6246, -1 0555'4
~ -3 '8064E-6
)PERATING DRIVE ROD STRESS AT A 477.198
)PERATING DRIVE ROD STRESS AT B 821.458
)PERATING CYLINDER BRG PRESSURE -3.75613E-4
)PERATING VALVE EAR TENSILE STR 15'46.57
)PERATING VALVE EAR SHEAR STRES 128 033
~
ERATING EAR BOLT SHEAR STRESS 1548.79
%TING EAR BOLT TENSILE STR 4771 ~ 17
~~1 f~-3. 459'1 E-3~~
~~2f= 733 811 ~~~
~~3f= 532. 65'5 il f=-21826. 4~~
>2f=-3818.52 t3f= 6791.56 DYNAMIC COMPONENTS RIVE ROD TENSILE STRESS AT A 4341.57 RIVE ROD TENSILE STRESS AT B 6640 USHING PRESSURE
'8 84.675'5
'ALVE EAR TENSILE STRESS ALVE EAR SHEAR STRESS 5948.81 379.211 CVGMA
'.AR BOLT SHEAR STRESS 4587.24 AiTACHMENT AR BOLT TENSILE STRESS 13246 ' 408 NO ~ZOW id= 775' 831 smwo ~aV.o .V 2d= 1869.64 3d~ 1566.33 swear No.~L id~ 59205.9 2~ 12442.3 23258.6 FIXED PLUS DYNAMIC COMPONENTS RIVE ROD TENSILE STRESS AT A 4818.76 RIVE ROD TENSILE STRESS AT B 7461.64 I IRH FNA PRCRRI IRF A4.8799
VALUE EAR TENSILE STRESS 7895.38 VALUE EAR SHEAR STRESS 507.244 EAR BOLT SHEAR STRESS R BOLT TENSILE STRESS 6136 '3 18017.7 779.835 2603.45 2099.02 nit= 81032.3 a2t~ 16260.8 tt3t= 30050.1 f
APPENDIX B VALVE/AIR OPERATOR MODEL FOR FINAL PIPING RESPONSE G-LEVEL CALCULATION.
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S-13('cr COMIPONENT c~~ od5T MODE, -. SERIALI 2 5.3 MAT'L I ig< PSI 8 275 'F Lss A/r.. sIzE Z(
ASHE CLASS r'/
YOKE ORIENTATION r'O NIOUNTING CONDZ TZON AXIS OF PIPE ( 9 No OF BOLTS I
// TO AXIS OF PIPE
/
( L)~
rg/ c BOLT TY'PE WELD TYPE 6
/. <
SIZE BOLT q YOKE LENGTH (FLANGE TO FLANGE)
PIPE MOUNTED YES(~ NO ( )
PERMANENT OBSTRUCTION (WITHIN 2") YES ( ) NO (
IS COMP BETWEEN CONT & 1ST ANC (FULL 6 WAY ANC) YES
~ (4 NO ( )
DO MULTIPLE SUPPORTS EXIST BETWEEN CONT & COMP YES ( ) NO (W Y
~~
GLOBAL CO-ORDINATE VALVE .STEM ORIENTATION SYSTEM PERATDR EPH +rA MANUFACTURER C')i'GNA ODEL NO SERIAL No ATTACHMENT YPE SIZE ORDER NO JOB NO MG~F )
RLSHO.O~W.
OTOR EPN MANUFACTURER SHEET NO.ML=D.
ODEL NO SERIAL NO D No IHS CIASS I-PHASE ( ) 3-PHASE ( ) AC DC COJQMNTS: . Definition '(N/F ~ Not Found) g C E.P-il~&-3A Q,'harv~
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Prelect P aoa err Br Date 5 =
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CheClreC By 'r'. @~~I t Z 2<I/8Z Job No. File No.
=- .- c sP 52 Analysis No, Rev No. Sheet No VJ A LIC. t'm P ATTACH[AI-MT U IL V' OPLiA~OL or'Errrg ;rOrJ'.
sos N0.3529"K can v - 3A pe RL,a No.~~
SHEET NO.
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PID( 3Wleh-BLDG FLOOR ZL H. 5 5.9 'OORDS MFR 5T f COl"PONENT ZL ('i< DSCRP 2 Ft n:&SERIAL;. 9 MAT'L SA -5 I( 6C -"l~
('I MOD( Z,W ~
PSI +5 'F LBS~ID F SIZE 2 '(
ASMiE CLASS YORE ORIENTA ION MOUNTING CONDITION TO AXIS OF PIPE ( NO OF BOLTS Pr j/ TO AXIS O." FIPE (~)
I/ 4 BOLT TYPE V'ZLD TYPE 6 SIZE BOLT q t YOKE LENG. E: PIPE MiOUNTZD YES (~) NO ( )
{FLANGE T..'ANGE)
PERCENT OBS:x.UCTION (WITHIN 2 " ) YES ( ) NO (
I S COMP BETWE 's CONT 6 1 ST ANC (FULL 6 WAY ANC ) YES ( ) NO NO
(
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)
DO MULTIPLE Si.'".."'ORTS EXIST BETLiEEN CONT & C MP YES ( )
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FlLE NP (%@~IF OTOR .EPN MANUFACTURER SHEET NP ~~I ODEL NO SERIAL NO D NO IHS ClASS I-PHASE ( ) 3-PHASE ( ) AC . DC COMh1ENTS: Def ni i tion (N/F = Not Found)
P 4 4~~k.
h Seesae~vzoyz. a062Araa oaiMV.qriog PREPARED BY Pw.'. l'DATE
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII PeaaeaBr Oate e 5 ec. gP Subtect O
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'2 System Job No. File No.
csP Analysis No Rev. No, Sheet No.
lVAN LV AL.{~ Ci ow tJ
'J:
$ ov LE'w~gg o~. (fuvp<<oils ATTACHQBNT ca.io v -?ci $ 4A JOB NO.Q~~~
ftLE ce.f -v - "=A: NO.~OX'HEET NO. sW 0
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II guLPX tT quALL~CATtN CS rlAlJCCMN Y REF.CATION FORD
'~~iaQN MI7ifIB FiRS7 ANCHOR ~Em CQi%7AINNKN7: YH ( )NO ( )
su~ut~s w ~ =IZON RK CGOROENA i~
~
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( ) Mw, mra +A@1
! ~PEPK NGUNrcQ (SEA) ~~, ( ) ROOR MINicD, { ) MAIJ. NQUtPiH
) RACX, (+St ma": 'rna a LQu .CN. r- ~~~t mt=-)
( ) Qi~m (sr=- sx~iu)
~~~~7. AQJACQT =gULPHBPi'. LWCi PCMiBt="7~~~~
~~~~(~~".~, suepoa-~, emma~ m.) ( cascades)~~~~
~~~~a. a~t'ra cwoui7 mievt= t.cui.ca~ ( caspar)~~~~
~~~~ATTACH>~W~~~~
~~~~8) lL R'COKL NUr4IBKR JOB NO.~~~~~
No.-'~
Res
~"-RIAL "tUNSK No-M~ 'r iNSULA7iQH CLASS
/
(OW ON: WITHIN FIRST ANCHQR ~iv L.QiRTAiHHKNT: YH ( ) NQ ( )
SUIUI.'lS R. O =~~SATION CQQRQENAi~ Pl '7 M%FAC i LlRR P
'lGO~ HlJSU ZQCc &W ~ 7 +~ 2 S~ "t. NQNBH QA 7 OZS~arP).OX ra~~ HQUlPiENG CONDITIONS, S'A~iL 9 HAOE?
( ~SQLTS, NURSER? SIR? TYPC'?
( ) M~~, LB(~i TYPC'?
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( ) eu, (OESC+aZ: Nma a <m,i.CZ Ir >PP<~mt=-)
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(PIP%, SUPPORT>, S~i'iilRK "iC.) ( CESCRIBK)
~~~~a. RIGID C"NOUIT "=NiRNC= t.CCRC).CN? ( OESCGBK)~~~~
O'II'GNA TCR: ATTACHMFNT.
.tQOE HglSZq JOB NO. ~c"~
>> +
+~
RLENO.
S:-R~ .'luvea SHUNT Wa.~<>'
AllSULAT;QN AMASS I
) ASW<SLLY 1gS<SLLED S).S<lS)(
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' LOCATEON: METHJN r ERSI ANC/QR iQ I.QNI*ENM~".(I'm ( 'Q ( )
BUELQENG >==!"aiaN "t 8 COOROEe~a Z 'MUFACiJRH Z. 'tQOK NlMH -'ZC) 4 74
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ra~~ NQU~iNG CCNGETEONS, SK~wd NOE?
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~~~~7. AOJACH: =gULPNr~i'. Ei4fFAt.i POMiBH7~~~~
~~~~9. NGTCR:~~~~
@30K'Ul6FB xNStJLATiON CLASS
gUIPMDT gNL HCATECS MAt %"CMH V%IF.CATION FON vn: KQV-0-g tQCn 0'l MIiRIH FIRST ANCHOR ~tv CQNTAIBiilt='.l?t: YH ( ~
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0
( ) PZGR NGUlPiB, ( ) MALL i%U~i
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lCOKL HUiHFQ Ftl,a Xo.~>~F S>>=RIAL MJNSH SHEET NQ ~~i i'lSilLhTION QASS t
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( ) maw (s=- sr=-u)
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.. cRIAL ."lUMBR iNSULA) iQN CLASS
4 4
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~~~~2. 'ICGK NU) H N zVzzs-s~" l. NONsa~~~~
~ ~ ~ ~
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5.3 Valve Local Coordinate Systems CSP-V-3 CSP-V-4 CSP-V-5 CSP-V>>6
~ ~
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g~t r~~ s): CP~4 E-'(r
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FtLE tiQ.~~~
SHEET NO.~
~ ., a p+445&dSC 7d cdCA-L KO~Clsgpyg'.
Wsran 4w hJ3 Spy
- ATTACHPAEAT...
JOB NO. 3BQ9~~
FILE NO.CKC}l~l~
SHEET NO.M
'h (v
Q$p g ( pggyuao g> ',
g~;~ ~leis'3 RN~E~ 5~' Z'~~K ~I~IF~
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~~~~CVGNA-ATTAC'Ri'.",=A JOB 'I6.3~ i.~~~~
FILE tfo. ~. Cl/Z SHEET WO.MM
Calculation Ak0aPk Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By:
Subject 5lF ALVE M.tt-LEG o Checked By: f j
.!.+gri&
Oate r I System Job No. File No.
CE, ZC t'-I- d'7 .4t Analysis No. Rev. No. Sheet No.
~>4I I.Ob CzP-v- 4A JOAN.WH
( I-Avt>) (.Z-*)hS) (3-texts)
$o - 3E GAS NE(GHT j
VE RTjcht. go (So lO 52.
lo IZ.V I Q.Z.
9o ATTACHMENT JOB NO.M~B Flf.E NO.~~P sHEK7 No. MM
5.4 SRM Sheets II I
user number 43. date/time 02/10/83 09': 08 function NEX -SRM MASTER EQUIPMENT LIST-EPN COMPOSITE EPN ESP-V-3 ~SP-V-3+
CONTRACT MFQ MODEL SERIAL NUMBER 68 8~25 DI40 4 06764 N27235-i DESCR XPTXON 24" B Y CONTAIN EN SO VALVE EC,. USE HOURS SAFETY FUNCTION ACCURACY
~20 II A g Q A/E DRANXNQ SKIS. QUAL BLDQ ENV. QUAL H 'l*'
ELEV DETAXL QUAL STATUS TM ZONE FRKQ ROOM Q ID ST ANL F/0 C" AQINQ DBE C SKIS ENV Oi 9 C /Qhj;"..
~;c PROJECT +MS AI4'-~
V 4i TlTLE' PREPARED 8Y!
c, FgeJA808%
P'r DATE CHECKE B DATE 4 FILE ND. OT.O~. F Sgarr ~y, ~S'.'S,
user number'8 date/time 02/20/83 09'. 08 functian ~X -SRM MASTER EGUIPMENT LIST-EPN ~ 'OMPOSITE EPN 8 -4 ~SP-V-4~
CONTRACT MFQ MODEL SERIAL NUMBER 68 Q25D DMO
206'76 2'-35-2 DESCRIPTION 24 BFLY C AIN ISO VA VE EC HOURS SAFETY FUNCTION ACCURACY A ~320 B iF A/E DRAMINQ AE ZONE E-BLDQ'LEV DETAIL ZONE u-ROOM SEIS. QUAL ENV. GUAL QUAL TATUS TM FREG GID HL ST ANL F/0 C AQXNQ DBE C O~ 2. P 10 gt~i06 ..
MESSAQE 7$ TLS PRSPARSO SY:
t'- C. RA a4)ck OATS CHSCICKD OATS
l I
1 H
user number 43 date/time 02/i0/83 09: 08
-Function ~X ,
-SRM MASTER EQUIPMENT LIST-EPN COMPOSITE EPN MSP-V-5 -GSP-V-5+
CONTRACT MFQ MODEL SERIAL NUMBER b8 2200 DIIO 6 206'766 2723 b f DESGR IPTIQN 24" B Y GQN 4INMENT ISQL VA V lEVEL EC USE HOURS SAFETY FUNCTION ACCURACY R 4 g S a~SO BX,F A/E DRAMINQ AE ZONE ELEV . DETAIL ZONE ROOM-M5a3 C5 475 M. 7'/8. 3 R33 IS. OVAL H
SE TEST ANL F/0 G 9
ENV.
AGING QUAL DBE C'E QUAL STATUS S ENV TM GID P 3~106 MES QE C~f+ h,~ s~.
PROJECT T)TgE Q PREPARED SY:
~~~~t. g . Fe,~nr40Hr CATS CHECKED G~.~~~~
function NEX user nveber 43,'ate/time
-SRM MASTER EQUIPMENT LIST-02/10/83 09: 08 EPN COMPOSITE EPN 2~SP-V- 2-C P-V-6~
CONTRACT MFQ MODEL SERIAL NUMBER DWO A-206T65 DESCR IPTION Y CONTAINMENT ISOL ALV LEVEL EC USE HOURS SAFETY FUNCTION ACCURACY 2 A 1 3 4320 B ~ F A/E DRAWINQ AE ZONE BLDQ ELEV DETAIL ZONE ROOM M543 814 480 N. 5/7'. T R~
SEIS. QUAL ENV. QUAL QUAL STATUS TM FREG QID TEST ANL F/O C AQINQ DBE C SEI ENV N 0~ 2.
MES ACE pROJECT TITLE +
pgEPAAED BY:
Q. c. t=~dwNCM DATE'VECi:ED DATE gOS Na.

~~~~.-. ~~ ~54.~~~~

C n user number 43 date/time 02/10/83 09:10 t'unction fIN -SRM MASTER EQUIPMENT LIST-COMPOSITE EPN ESP-V~ -CS -V-9+
ONTRACT MFQ SERIAL NUMBER DMC A-2067 4 DESCRIPTION 24"BFLY VAC RELIEF TO SUPP CHAMB LEVEL EC USE HOURS SAFETY FUNCTION ACCURACY R A 1 g ~0 i. F A/E DRAMINQ AE ZONE BLDQ ELEV DETAIL '"ZONE ROOM M543 8 aea 9/5. 1 R33 SEIS. QUAL ENV. QUAL QUAL STATUS TM QID HL TEST ANL =.F/O C AQINQ DBE C ENV "
Y 01 P 10 SKI @+5~106
V use~ number 43 ~ date/time 02/10/83 09': 13 function FIN -SRN MASTER EQUIPMENT LIST-EPN COMPOSITE EPN
-V-3A PEP-V-3*+
CONTRACT NFQ MODEL SERIAL NUMBER DMQ A-206T64 N27235-3 DESCRIPTION 24" AO BLFY SUPP. CHANB EXHAUST EC HOURS SAFETY FUNCTION ACCURACY A 4320 ioF A/E DRAMINQ AE ZONE BLDQ ELEV DETAIL ZONE ROCN C14 R 495 H 5/5. 4 $ 32 SEI8. QUAL ENV. QUAL QUAL STATUS TN FREG GID HL TEST ANL 'F/O C AQINQ DBE C ~
SKIS ENV Y di 9 10 361106 CYC~NA PRO48CT T~LB Atll4U'l g,e ~
- ~o0&
PREPARES BY:
OAYG CMKCl:ZD OATS JOB MO~
PLL8 NO SHKHT 80. ~~" ~
0 a
,user number 43 date/time 02/10/83 09: 13 function fIN ~M MASTER EQUIPMENT LIST-COMPOSITE EPN 2- -V-4A -CEP-V-4A+
ONTRACT MFC MODEL SERIAL NUMBER 2 B250 DMC A-206T64 N27235-4 DESCRIPTION 24" 0 B Y SUPP. CHAMBER HAUST EC UBE HOURS SAFETY FUNCTION ACCURACY A 1 3 4~30 Bii F
~~~~/E DRAMINQ AE ZONE ELEV DETAIL ZONE RGQM M543 C14 495 H. 5/5. 4 R~~~~~
SEIS. QUAL ENV. QUAL QUAL STATUS TM QID HL TEST ANL F/0 C AGING DBE C BEIS ENV YP Qk ~0 3~6~/
MESSAGE Cg+9 j Pr p804KCT TITLE '~
p<<pa<<~ p.AR I":~0<>~>
P~
g Z3 nATS gyp';F69
5.5 Final Pipe-Mounted Equipment Response G-Levels
Sub)ecto W. O. 3900/4000 Washington'ublic Powor Supply System RECEI VED
"-".<<j~i".,,'::.'ueU.fication of Mechanical Pipe InHf dZ ]gg3 l!ounted Equipmentg Forwarding of
". ' Xn formation
,':.,i~,':~.<
CYGNA-RIGHLANO -"j; April 29 < 1983 m)r/P S'.:! BRHP 83-078
~~~~O<~J~ gC~~~~
~~~~w;P.;~~~~
'e
~~~~i. <<hopi~~~~
'wr..5>',,
Assistant Director
jg'.o-,"Washington puhlio poses Supply System ATTACHMENT"I 3000 George Washington Way Richland, Washington 99352 JOB NO.~ ~.OI. I-FgF NOe V~~
Attention~ her. B. A. Holmberg SHKSy WO.~
i
.-,'~.'.=",.; .:;.'eferences s (a) WPBR-83-17', dated 3/16/83.
~~~~i~gP~"-".j (b) WPBR-83-28, Gated 4/l2/83. 4 4/4/83'Vr~~~~
'~
(c) WPBR-83-29, dated 4/12/83.
(d) Te3.ecopy, B. A. Holmberg to
~e V '4 Ie J. Z. Verderber, dated
~
Centlemcns Zn response to the request of references (a)> (b) + (c) and (d) < this letter is fcr;carding refined valve accelerations.
The valve acceleration sheets for the five (5) CSP valves
~ represent the second iteration valves of the refinement task..
>>.;g"'qi'<...':
represent the first Valve.."'.,""..:";.-,',"".i.";i'P~>.'::
., sheets for the other four (4)
e~jj<<W~.'. iteration of the refinement task. Please inform the Noodbary'cg;,:
Office fur ther if efforts should be r.ade to reduce accelerations Very truly yours, ORIGINAL SIGHED GY 1 1 VFZDKRSEP r.. "'OW/S S.k.i/les Zohn i7 Verder ber
~
~
Pro5ect Engineering Manager .
CC: Mr. W. S. Chin - SPA 1 .~r/1 QHr. J. F ~ Rhodes - WPPSS - 1 v/1
~
ter. P. Buck - WPPSS - 1 ~/1 Nail Drop 575
~
,z CW"
ATTACHMENT Data forwarded with BRWP-83-078, dated April 29, 1983 Valve 0 Kale.. No.
CSP-V-1 125 8.14 '29 CSP-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 RClC-V-31 107 8 14.112A RHR-V-17B 31 8.14..121 RHR-V-53A 29 8 '4.62C RHR-'V-53B 31 8.14.121B
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6.0 DRAWINGS USED FOR REQUALIFICATION QIDC 361106 DRAWINGS SUBMITTED TO SUPPLY SYSTEM IN ORIGINAL PACKAGE Johnson Controls D-220-0310-IR-64 Rev 0 Flick-Reed Corp C-26096 Rev 0 BIF D-207110-H Rev B D-207110-G
~~~~Rev A A-206767 Rev C Bovee & 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~~~~
C4 Tsaaaa cva,caco LCTTICTto ~ >>C so O'L'IIS LKv'EII Ila>>s)assr Isl'EE4Dt
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7.0 PRIOR CALCULATIONS USED FOR REQUALIFICATION
.4I qIDrf 361106 7.0 TRANSMITTAL, PRIOR CALCULATIONS AND REPORTS CONTENTS 7.1 Communications Reports 7.2 Old Requalification and SgRT Forms 7.3 BIF Report: Dynamic Torque Calculations of Butterfly Valve (Sheets A-1 thru A-83)
WPPSS Supplementary Calculations (Sheets A-84 thru A-98) 7.4 McPherson Associates Report:
Design and Seismic Analysis of 24" Cylinder-Operated Butterfly Valve (Sheets B-l thru B-75)
Revision 3
~ekVQ > Ã +
'lllllllllllllllllllllllllllll QZDN 361106 7.1 Communication Reports & Correspondence
f Communications Ak za IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Report Company: CSS Telecon 0 Conference Report Project Job No.
5> Date:
v) P$ E g, Subject Time:
Place:
Il t.VK Q,C. StoQS
~~~~Participants:~~~~
Cf~- Qe Cg y-Item Comments Req'd Action By
~
~
5(P .VA4~ 6 -
FL AQ &6 PIWF N Sfa M >
tt 4 $ Q tc ~@&4 l~S Z (45 Z5 ~ It 0.4. "bz >8 lS
+I.HS CVGNA ATTACHMENT roe No.~~~
FILE NO. ~L~~
eHeev No.~~
Signed: Page , of Distribution:
102040
Washington Public Power Supply System P.O. Box 968 3000GeorgeWashington Way Richland, Washington 99352 (509) 372-5000 Oecember 17, 1982 GE RWH-82-018 Cygna Energy Services 141 Battery Street Suite 400 San Francisco, CA 94111 Attention: Mr. T. Wittig, Project Manager
~~~~Subject:~~~~
NUCLEAR PROJECT 2 CONTRACT C-0892 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 A~ACHMBN~
. RECElVED gPBXO.~~'~
Dc.C48 f982 RLE No-~~
SHEET NO.~
-CYG>JA-RICHLAND
Communications i~a.rn IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Report l CR-030 company: CES XI Telecon 0 Conference Report Projecb Job No.
82044 WPPSS Date 7 29 82 Subject 9:40 A.M.
/ID 361110 - 18" BUTTERFLY VALVE Place:
SDAO Participanth Dick Hickman Supply System Hal Reeser of CES SDAO of 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 faulted or upset allowables for RHR valves.
o Dick said we should complete the requalification analysis of the valves and flag the dynamic instability issue as a
,separate subject that Hill 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 shoul'd attempt to assure Chat our work does not conflict with the BIF effort.
Dick said we may contact GE direct. Our contact at GE for M. 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.
zosvo. r~~+
F}LE NO.
SHEET NO.
'I. I r.
or.o i. l-Sign Page .. 1 of, .1
'"" ""'" T. Witti'o, H. Abolhoda, F. Khanachet, P. Guglielmo, B. Schlafer, M. Rajan, J. Minichiello, P. Patel, Project Files (SD), (SF), (RB)
V P ~
I f
Communications Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII CR-027 Coinpany: CES Xl Telecon 0 Conference Report Project Job No. 82046 WPPSS Date: 7/2O/B2 Subject Time: P ~ Iii.
APPLICABILITY OF HYDRODYNAMIC LOADS- Ptace: 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 enon listing is not to be trusted.
2. For packages in analysis Cygna will trace down the P 5 ID to determine the appli'cabil.ity of hydrodynamic loads to line mounted equipment.
~~~~3. To accomplish this, Cygna will:~~~~
A
~~~~a. Check the line routing to see primary containment. If not, if it penetrates the hydrodynamic loads 0. f~g~~~~
~~~~.do not apply. FiLK~~~~
~~~~b. If the line penetrates the primaryscontainment, hydro- SHE No Zi~.~~~~
dynamic loads wi11 apply unCesa:
l.- 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.
4. If a line mounted equipment fails to qualify due to hydro-dynamic loads, estimate it's fragility level. 'his'informa-tion will be used by WPPSS when they receive the B 8 R analysis and examine actual pipe accelerations.
final'iping WS/sak W. Schlafer ~Q Page. of 2 L. Kammerzell, J. Read, P. Guglielmino, J. Minichiello, P. Patel, N. Rajaq, H. Abolhoda,4RRSIIII P. Curry, H. Reeser, T. Wittig, F. Khanachet
r Communications L+k.6i a Report lljljjlljjjlllllljlljjlljjljjj CR-027 company: CES Xl Telecon 0 Conference Report
'roject Job No.
WPPSS Oate:
~~~~Subject:~~~~
Time:
APPLICABILITY OF HYDRODYNAMIC LOADS Place:
~~~~Participants:~~~~
~~~~of of of Comments Req'd Action By~~~~
~~~~5. For packages whose analysis is complete and where hydrodynamic loads were not considered because the SRM said nNo":~~~~
~~~~a. Review the line as in 3 (first page of this telecon).~~~~
~~~~b. If we feel hydrodynamic loads really do apply, send a memo to the S. S. indicating the package may need'ewor'k.~~~~
~~~~c. Send memo to F. Khanachet requesting supply system con-currence that hydro loads do apply and added analysis is required.~~~~
boa NC. y7.al.t.
'FLE ~0.
SHg~ N0.2 sign~: W. Schlafer Page 2 of 2 Oistrlbution:
Communications L'hkd.~ ~) Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII CR-023 Company: gl Telecon 0 Conference Report Project Job No.
82046 MPPSS J01 20 1982 Subject Time:
9 A.N.
Hydrodynamic Loads
'an Particlpanth Dieao'f innachi el 1 o of.
of Item Comments Req'd Action By Ouring the conversation we discussed the following:
If attenuation data on hydrodynamic loads are not available,'ne 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 (line plus equipment) indicates otherwise. system'requency~~~~
3. If the equipment satisfies the allowable stress limi'ts, then one should perform fatigue analysis using the fatigue design curves given for Class 1 components. To calculate the 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.
A~>CHVBN7 boa No FIIP NO ~
~r~
SHiEV HO.~~'
Signed: P. K Patel Page . 1 of 1 Distribution: H. Reeser, Rajan, H. Abolhoda, P. Curry
I 4~
July 7, 1982 ;Ie <<yg Sygna Energy Sexvice voa~o. <~ II I ~ N ~ I <<~,P>>
225 Stevens Street FlLB NO.
Solana Beach, CA 92075 SHBBTNO.M~
Attention: Mr. "Bill" Schlafer Subj ect: Butterfly Valves for Nuclear Applications with IEEE Qualification Requirements
~~~~Dear Sir:~~~~
~~~~This information is provided in response'o your recent phone call.~~~~
1. 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 ur 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 ZEEE-344-1975.
It is almost impossible actuator vendors I
to obtain prices from IEEE qualified 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 208, depending upon the wording used in the engineer's resultant specification.
Re lacements for Valves Furnished Ori inall .on N-2723.2 14 18" BV's with electric oper-ators (See NODS 11/1/79)
$ 40,000 ea.
or $ 25,000 ea.
if if qty. =
qty. ~
1 14 Re lacements for Valves Furnished Ori inall on N-.27233 2 18" BV's with spring to ~o en cylinder operators
$ 60,000 ea.
or $ 45,000 ea.
if if qty.
qty.
1 2
1 600 DIVISION ROAD o WEST WARWICK.Rl CABLE: BIFWRWKRI ~ TWX 710 382.0402 02893 401 -885-1 000
~ BOX 21 7 ~
~ TELEX 927-631
Sygna Energy Service July 7, 1982 Page 2 Re lacements *for Valves Furnished Ori inall on N-27234 4 30" BV's with spring to close cylinder operators
$ 75,000 or 660,000 ea.
ea.
if qty.
if gty.
Re lacements for. Valves Furnished Ori inall on N-27235 4 24" BV's with spring to close cylinder operators
$ 60, 000 or 650,000 ea.
ea.
if if qty.
qty.
Re lacements for Valves Furnished Ori inall on N-27236 3 24" BV's with spring to ~o en cylinder operators or
$ 60',000
$ 50,000 ea.
ea.
if if qty.
qty.
~ 1
~ 3 1
We trust that this information will be of some help to you, and are sorry that our prices cannot be more precise.
Sincerely<
eorgh E. Sayer BV Sales Applications Engineer
~~~~Enclosures:~~~~
650.20-4 BPD-668-45-1 BPD-668-1 NODS-11/1/79 CYGNA ATTACHlHE)MT JOB NO. f2o4+
RtBMO. or'< ~
BHBBV BO.~~I.
P B LI TTKR FI Q, VALVES . MODEL 6CS l2' 2+THRU SHAFT PARTS I8 lo 7
+
W~>> aeI
+ IC
~ 2P. HEAT' NHRVNK 4 SEALED WtVS LaaCTITE IIANICALLYRETAINED AChlVSTAHLE SEAli FlELD IRREPLACEABLE WITMON REMOVING VhLVE FROH PIP'E LINE.
I.TEN S SECVRED WITII 5 M YLOK I NSERT DE~ON A-A ALTERNATE AIWUSTASLE VEE
'A PACXIN4 e
IT M ER I A MA RIAL I VALVE BODY CAS IRON ASTM AI26 C RUBBER S A BUNA-N ASTiVI 02000 3 C AMP ING R ING YP 04 ST.
4 CL MP I NG I NG OCK 304 ST. ST'YPE 5 HALF DOG POI T S I SC W 304. ST. ST' ST'YP 6 SHAFT BEARING INFORC D FLON BR 0 PH NO IC BACKED STUF NG BOX PACKING VE P ACK I NG BUNA-N 8 STUFF NG BOX GLAND CAST BRONZ ASTM B62 9 HEX HEAD CAP SCR W TYPE 304 ST.
IO OP RATOR SHAFT 304 S . ST'PE, II HALF DOCs POINT'ET SCREW 304 ST.- ST'YPE IRON ASTM A48 CL40 OR ST'AST l2 VALVE DISC DUCTILE IRON ASTM A 36 GR 65-45-I 3 WAS HE TYPE l8-8 4 -
DISC P IN 304 ST.ST'YP
~~~~5. KEY* ST.ST'T'L HEX NUT TYP 304 S .~~~~
7 THRUST CO LAR 303 ST. ST'YPE 8 THRUST BEAR ING COVE IRON ASTiVI AI26 ST'AST C
l9 H X HEAD CAP SC W TYP 304 ST.
20 0-R ING ST'UNA-N 2 THRUST B AR ING R INFORC D T ON DISC SEAT INCs RINC TYPE 3IG ST. ST'I ATTACHMENT JOSNO.S FILE NO.~~
~
SHEET NQ.M'
'l'ERS
w=
FEEOER5~ONTRO BPD-668 45'-
I
~l~
iA UNIT OP GENERAl SIGNAL AWIA BUTTERFLY. VALVES MODEL 0668 30" THRU l20 8
. PARTS ITEM 5 SECURED Z+
I '
WITH NYLOK INS.ERT 2 3
,Qs 8
JKZ~
THRUST ADJUST-MENT PARTS-0 ll MECHANICALLY RETAINED -ADJUSTABLK SEAT.
REPLACKABLE WITHOUT 'IELD REMOVING VALVE FROM PIPK LINK ITEM 27 HEAT SHRUNK AND SEALED WITH LOCKTITE 30'HRU 48'.V) ' '(FOR (FOR 54'HRU I20'.V)'TE MA ER I A MAT RIAL VALV BODY CAST IRON ASTM AI26 B RUBBER SEA BUNA-N ASTM D2000 ~
3 C AMP I NG R I NG 304 ST.
.4 C AMP I NG R I NG OCK 304 ST. ST' ST'YPE HA F DOG POINT S T SCR W TYPE 304 ST. ST' SHAFT BEARING REINFORCED TEFLON BRZ OR PHE'LIC BACKED 7 STUFF I NG BOX P ACK I NG V E P ACK I NG BUNA-N 8 STU ING BOX G AND CAST BRONZ STM B6 9 H X HE D CAP,SCR W TYPE 304 ST:
IO OPERATOR SH A." T 304 S . ST'YPE II STU HA 304 ST. ST'YPE IRON ASTM A48 GL40 OR ST'AST I2 VALVE DISC DUCTILE IROI'I ASTM A536 GR. 65-45-I l3 WASH R TYP l8-8 l4 304 ST.ST'YP Dl SC P IN I5 ST.ST'T'L KEY l6 H X. NU TYP 304 ST.
7 THRUST COL AR 303 ST. ST' ST'YPE I8 THRUS I B ARING" COV CAST IRON ASTM Al 6 G B I9 HEX HEAD CAP S W TYPF 304 ST.
0 0-R ING ST'UNA-N I THRUST BEARING P INFORCED. FLON PH OLIC BACKED
'Q 2 THRUST ADJUSTING SCR W TYPE 304 ST.
TYPE 304 ST. ST'L ST'3 JAM NUT 24 THRUST B AR ING PLAT STEEL ASTM A36 25 SEA S ILICON RUBBER 26 HEX H AD CAP SCR W TYP 304 ST.
7 SEAT NG EDG 3I6 ST.S ST'PE
. Fr<r tqo. m.~~
1-15-82 ETERS>>FEEDERS~ONTRQ SHEET N'a ~(
o'PD-668-I
0 LIMITORQUE CORPORATION ~ P. O. BOX 11318 ~ LYNCHBURG, VIRGINIA 24506 IEEE 323 (1974) and IEEE 382 (1972)
NUCLEAR QUAI.IFICATIONDATA FOR SAFETY RELATED SERVICE PHASE ONI.Y 'HREE O.C.
Nuclear Containment Outside Containment Containment-Inside or Outside (See Option 8 Price Adders)
(Standard Prices) ft (See Option 8 Price Adders)
Design Lite 40 years (2000 40 years (2000 40 years (2000 cycles)'40'F cycles)'20'F cycles)'20'F Ambient Temperature (Continuous)
Ambient Humidity 60-100% 30.100% 30 100%
Aging Motor Stator. only Entire Unit Motor Armature, Field 180'C for 100 hours0.00116 days 0.0278 hours 1.653439e-4 weeks 3.805e-5 months 165 F for 200 hours0.00231 days 0.0556 hours 3.306878e-4 weeks 7.61e-5 months at Coils, 8 Brush Box only
, 100% relative humidity 180 C for 100 hours0.00116 days 0.0278 hours 1.653439e-4 weeks 3.805e-5 months Total Radiation 2.04x1P rad s 2x10'ed s 1.0x10'ads (40 yrs. Integrated)
Seismic
""8.0 g's (SMB/SB) " 6.0 g's (SMB/SB) 16,0 g's (SMB/SB)
Ref: IEEE344 , 3.0
""6.0 g's (SMB/HBC) g's (SMB/HBC) "" 3.0 g's (SM8/HBC) 6.0 g's(SMB/HBC)
"'3.0 g's (SMB/HBC)
""6.0 g's (SM8/HBC)
'umber of transients 1 l I'ranslent Temperature 340'F (BWR) 250'F 340'F 300'F (PWR)
Test Humidity 100% (saturated) 100% (saturated) 100% (saturat Profile PWR/IEEE382-73, ANSI (yet to be published) Special Page 12. Table 1 BWR/IEEE382.73, ATTACHftBFHT Page 12, Table 2 Length ot Test 30 Days 15 Days 25 Hours Completed Test Date PWR-September 1974 February 1975 October 31, 1 (600456) (600481) (80009)
BWR-September 1972 (6000378)
During BWR test, 500 cycles were used as a design life per IEEE382.
During PWR test, 2000 cycles were used as a.design life of which 500 were Incorporated prior to test and 1500 after 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 Irradiating.
"As ot 7/26/75, seismic tests were completed to IEEE344-1975 for both SM8 and SB units to 8.0 g's vertical and 3.2 g's horizontal. Since no cross coupling was noted between axes, the test qualifies the SMBlSB to 6.0 g's In both vertical and horizontal axle. Maximum g level dwells In each ot the three axes quality the units for any mounting position. (Selsmlc Qualification Report No. 80021). Qualification extends through 35 Hz.
ttStandard Class"8" Insulated motors only.
"Standard units without spur attachments.
""Standard units with seismic support bracket and without spur attachments.
NOTE: SMC44 and SMC45 actuators are qualified for "Outside Containment" service per above levels based on their similarity to the SMB actuator.
NODS ~ 11/1/79
Communications Ah, Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Company: CES M Telecon 0 Conference Report Projecb 82046/CR-019 WPPSS Oate:
7/] /82
~~~~Subject:~~~~
Hydrodynamic Loads for Line Time:
1] . 20 Mounted Equipment R 'DAO Partlcipantc kness of Bechtel Norwalk CA W. Schlafer CESi SDAO of Item Comments Aeq'd Action By Called 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 (RXM) 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) Xn-Plant Vibration: Required Xnput Motion of sine sweep testing at 2 Octaves/Minute from 5 to 200 to 5 Hertz for 90 minutes at .75 g.
3. This type of environment is distinctly more severe and more correct than that proposed in the WPPSS interim dynamics criteria memo 5 856. Eventually WPPSS will need to be informed of curre practice such as this.
'ry ATTACHMH4T JOE NO.
NO. 0I .oI .F
'ILE SNEEr NO.~I'~
WS:lgn W. Schlafer Page ] of
'""""" "Messrs Kammerzell, Read, Reeser, Wittig, Minichiello, Gug ze mx.no, Boschr~~ Patel, Rajan, o o a, urry
CommUnications A'<. j'. ii Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII campany: OEB 5 Telecon a Conference Report Project Job No 82046/CR-018 WPPSS 6/29/82 EQ of BXF Butterfly Valves Time:
05 QXD 361104, 361106 Place: S DAO
~~~~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 BZF Butterfly Valves.
~~~~2. His recollection af these analyses was vague but~~~~
- did mention they, as consulting engineers, never tried to assure operability. Operability was the manufacturer's responsibility.
He recommended t
testing a similar valve.
AT7ACHMEN1'OB NO.
FlLB NO.J2T.o~
BNBBr NO. ~~
BS:1 n Bill Schlafer Page of oistributfon: L. Kammerzell r J. Read, H. Abolhoda P. Patel, P. Curry
Communications .
Report IIIIIIIIIIIIIIIIIIIIIHIIIIIII Company CES IK Telecon 0 Conference Report Project 82046 CR017 WPPSS 6/29/82 Subject Time:
EQ of BZF Butterfly Valves Place:
~
SDAO 4
QZD 361104, 361106
~~~~Participants:~~~~
Bill Schlafer ot George Sayer ot BZF, 401-885-1000 ot Item Comments Req'd Action By Called 'George Sayer, the BZF sales agent to get a budget price for BZF 18", 24n, 30n air-operated butterfly valves and an 18" motor actuated butterfly valve. These va1ves are similar to ones in WPPSS QZD files but do not use the same air-actu ators. The original BZF valve serial numbers (for refere'nce) 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 A~AgHMENT BS:lgn Signed: ol ch afer Page oistnbutlon: L. Kammerzell, J. Read, H. Abolhoda P. Patel, P. Curry
Communications'eport jjlljjjljllljjljjljljjlljljljl Company: CES H Telecon 0 Conference Report Project:
82046/CR016 NPPSS Date: 6/29/82 EQ of BIF Butterfly Valves QID 761104, 361106 Place: SDAO Bill Schlafer of CES, SDAO Allan Berger BIF 401-885-1000 of of Item 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) Bod/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 the Miller air cylinder d) For dimensional data to verify functional operabiLity of the motor'ctuated valve, con-tact Limitorque in Lynchburg, Vir BS:lgn A~ACHMERT FILE NO.
SHE&'NO.Z
~
sos No. ~r~'~
Of'.0 l.f
~
Signed: Bill Schlafer Page 1 of 1 Olstribution L. Kammerzell, J. Read, H. Abolhoda P. Pate , P. Curry
Memorandum ma.
-= iF 3kfk3 PROJECT MEMO:
IIIIIIIIIIIIIIIIIIIIIIIIIIIIII 7 ~ Oe To: Oate: <r(
~b No: 82046 WPPSS
~~~~Subject:~~~~
MXSSXNG DATA REQUEST Copies:
Project File (C~z~'Sb>>(('e'" 7.)
DE A//h'C - zuZr-9~ < l, 5'u'. 8A-ME hgrLL.Eg' Yt'-,
z'p~-~
DRA+Viu 8- z/l E3o P~ivE pg+p//+g 8 - z /l g 92- DAM/S ATTACH@
JOB pro $
N.oi.p
'LBgp.
>HER'ao.
NOTE: Please sign and return the attached copy of this memorandum as acknowledgement of receipt 'of this memo. THANK YOU.
Received by:
Date Received:
I I C
Memorandum IIIIIIIIIIIIIIIIIIIIIIIIIIIIII To:
P. Gugl ielmino 'une 17 , L9 8 2 J. Minichiello W. Schlafer, Pz.'ate 1 82046/SDM-003
~~
~~~~Subject:~~~~
ples:
Analysis for Operabil gmAcHM-~ r L. KammerzeLL gOB NO.~ oy.Chl. t:
J,. Read H. Reeser G. Shipway (Wyle)
Pll.a NO.
1 (.(1 T. Wittig SHEN'NO project pile Zn 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.L of the Design Criteria.
Zf an equipment in Group ZZ is expected to perform during the seismic and/or hydrodynamic event then the following requirements shall be met:
(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.
Zf the calculated stresses for any service loading are such that permanent defarmaticns 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 L'h'Ã ~ f~k Report llllllllllllllllllllllllllllll Company: tK Telecon 0 Conference Report Project Job No. 82046/CR-014 WPPSS 6/16/82 Subject Time: a m Wyle Data Bank Place:
ParticIP nts:
W. Sch1a fer of CESr SDAO G. Shipway Hyle, Norco of of Item Cornrnents Req'd Action By Asked George to initiate a search in their testing
'data bank for seismic or seismic/hydrodynamic tests on BIP 18", 24" I*'0" 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.~~~~
CVGVA Vaa R~NO ~
ATTACH.ilENT No.~<+
SHEH'O. MQf t WS:1gn Signed:
Oistributiorc W.Schlafer L. Kammerze11, J. Rea, H. o o a, Page ro3ec of z e
C r>
'" Ec -IVI=-D I
Communications LaLJk p
JU'f.l rt d )98 Report llll(lljllljjjjjjllllllllljl
,~,.r rt XN ptl:9+
Company
/'V Telecon 0 Conference Report Proje t kquiptttent Seismic/Hydrodynamic Requalif ~
i-
~ Job No.'2044 6/15 82 Subject Znterim Dynamic Loads C 11 00 o r'articipants'ime Richland Office Jim Foreman ZOS No. of Wyle Laboratories .
FlLB NQ ~o.o .
ot Item Comments Req'd Action By Jo'e 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 thatthe acceleration values 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 B&R 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 susoidal motipn at a justifiable damping value.
For example, for an SSE condition the amplifica-tion at 3% damping would be 50 divided by 3 = 16.7 This loading may be in some cases present a very conservative loading on'he line mounted component A somewhat more realistic input motion would be Signed: Page 1- ot
-- 3.
'istribution" andard Di , P~ggf A].ol de.-,. ka-to~. ~t t r'r
Communications L~~ k, i L. fz) c Ilillllllllllllllllllllllllltl Report Company: p Telecon 0 Conference Fleport Cygna/Ry1 e Project; Job No.
Equipment Seismic/Hydrodynamic 82044 Recualification Date:
~~~~Subject:~~~~
Time:
Interim Dynamic Loads Criteria and 11 00 Fatigue Criteria Place. RZ Ch1 and 0 X Ce Part>cfpants:
Joe Braverman of Burns and R e ATTACHMEN'P JOB NO. r~94 of Item Req'd Action By continuous sine beats of 12-15 ocsillations per beat as recommended by the TEEE-382 draft "Ameri-can Standard of Safety Relathd Valve Actuators".
The amplification for a 15 oscillation sine beat
~
at resonance for 3% damping is approximately 11.5.
Zf the static lbadings 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. Zt is felt that a combined test and analysis would be a feas-ible and cost effective approach.
Signed: g>~ Page of Standard Distribution 1020 00
e L Ul t) l l lul llCa Llvl lO Report Blllllllllllllljljlllllllllll h
~
'omPenyCyctna/gyl e g Telecon D Conference Report Project Job No. 82p44 EquiPment Seismic/Hydrodynamic Requali- Date: 6/15/82 r
SLrblect Time: 11, pp
.Interim Dynamic Loads Criteria and Fatigue Criteria P"": Richland Office Perticipants:
Joe Braverman Burns and Roe Jim Foreman o, N le Laboratories Item Comments Rett'rf Action By Burns and Roe is checking to see if fatigue cri-teria have been developed for WNP-2 and will noti-fy Cygna/Wyle not later than June 17, 1982 if such criteria exists.
CYGMA ArrACHMEm sos NO.XLu~<
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SHEET NO. 7 '~~
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Communications i'. fib Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Telecon 0 Conference Report CES Project "ob No. 82046/CR 008 WPPSS 6/11/82
~~~~Subject:~~~~
Time:
Qualification of Line Mounted Equip. Place: SDAO 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/ll/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 analytical and/or in-situ testing to be conducted ACHMENT which will yield. data needed for a more accurate B NO.~&!~
definition of the dynamic input to line mounted F Na. aeg'aal. a equipment. F
$ FFTNO. +.<~
3 ~ An examination of the preliminary horizontal OBE and SSE response spectra outside the containment building for a frequency of 8Hz, indicate that the g levels from Attachment 1 (of the Xnterim 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 resonan condition of the line mounted equipment which would result in even higher g levels for use in analysis.
Signed W. Schlafer Page 1 L. Kammerzell, J. Read, H. Reeser, J. Minichiello, P. Guglielmino, P.K. Pate M.K.S. Rajan, A. Abolhoda, P. Curry, Project
Communications d~F~ Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII company: CES g Teiecon 0 Conference Report project Job No 82046/CR-005 WPPSS Equipment qualification 1982 June 8
~~~~Subject:~~~~
Time:
Response Spectra It WPPSS E.g. Documents Place:
SDAO
~~~~Participants:~~~~
H. Reeser CES, Richland of J. Forman Wyle (CES, Richland)
W. Schlafer CES, SDAO Item Comments Req'd Action By Hal has asked Jim Forman to help Cygna obtain, the following information form WPPSS or from similar data available within Wyle:
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 c'ompilation of Response Spectra for OBE, SSE and combined hydrodynamic events recently received .by the BAO, SDAO and the SFAO are to be considered preliminary.~~~~
~~~~IIl l11 pd 4 i ffid 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 NRC concerning Equipment qualification.~~~~
cyGNA No.~+
boa PILE NO.~
No' gr,ot.P 1.I.So sHEsT Page of istnbubon: Kammerzel1, Read, Patel, Rajan, Abolhoda, Curry', Ninichiello, Guglielmino
~mace Reeser, PROJECT FILE IW
Communications L'h kd ~ F~l Report llllllllllllllllllllllllllllll Company: CES 5 Telecon 0 Conference Report Projecc '2046/CR-004 WPPSS Equipment qualification June B, 19B2 Subject Time:
am (ID File Review Place:
SDAO
~~~~Participants:~~~~
P. Gu lielmino of BAO W. hl f of S DAO of Item Comments Req'd Action By In the review of a /ID 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.
2. If the error is such that the equipment can still be qualified, note the error and the fact it does not adversly affect qualification, but avoid the expense of altering that portion of the analysis. j
~~~~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.~~~~
g~ACHMGbP Joa No.a~~~
Fg.a No.
SHEH'O. 7. I.)I W. Schlafer Page of oI""b""'n'ammerze11 R ad pat 1 Ra an Abol hoda Curr Minichi e11o Reeser PROJECT FILE
Communications ALAI.F; Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Company: CES 5 Telecon 0 Conference Report Project: Job No.
O4 WPPSS Equipment qualification Date June 3 1982
~~~~Subject:~~~~
Time:
m Place
~~~~Participants:~~~~
of W. Schlafer CES, San Diego of Item Comments Req'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.~~~~
Since WPPSS has generated combined response spectra for 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 understanding of the BMR's systems.
~~~~3. Hal will be our contact in Richland to submit our Action Plan and cost estimates for approval.~~~~
F08 PiL.e STREET ~
zo.~tM NO.~O.~i.:
NO W. Schlafer '"If w~ Page of Distribution: Kamiterzell, Read, Patel Rajan, Abolhoda, Curry, Guglielmino, Minichiello, Reeser, PROJECT FILE WS: ib
I II f
Communications I ts a. s L Report IIIIIIIIIIIIIIIIIIIIIIIIIIIIIl Company: Telecon D Conference Report CES Prolect: sob No. 82044 Date:
lFTNP-2 Eauiament Qualification 4 Subject Time; Weld size at Valve Flange/Ear Interface 2:00 .m.
Place:
Richland Participants Don Searle CES/RBO Rick Rica oito I - -
B F 4 01 885 1 0 0 0 of Iten: Comments Rett'd Action By Requested and received information concerning t e attachment of the rectangular shaped "ears" to the valve body flanges.
Rick informed me that all of these items were af-I fixed to the valve flange by means of welding.
a) 0'.31" fillet weld three sides b) 0.31" "J"/Groove weld on side flush with flange face Refe=ence: BIF Orde Yo: PN2723<, P?LE27235 BIF Assembly Drawing: A-206767 CYGNA ATTACHMFNT JOE NO.~~~
FILE NO. Oi ol.F EHEH'O. 1I ii SIgnec Page of T. Wittis. F. Ehanachet, D. A..strong., ?'. Scott, R. Hickuan, 10? Prospect File f:Q "~Bear'~ Or=ice Fi e
~~~~"I g ~~~~~
tae~v p iw t Iu, ~ %s ~ sar~ 1~
~
July 16,'974
~
~~
Conference Notes No. 258 9F.CE.I%ED JJVerde"bar Washington Public Power Supply System NPPSS Nuclear Project Ho. 2 Jgs.< )!jIg I jQpp Contrnct So. 66 .
Cpggg 0 e Date: PPerry --
-':roncich P lace: B.X-F DMurphy Prove.dence, Rhode Island HReh CVesy (PTS0)
CV PTS.O)
~~~~Purpose:~~~~
RLuken evXew Meeting RECamp JHagan Present: B. I P- .
HDoon RÃoodward Z P. .Cunningham - P oduct Engr-Butterfly Valves
~ e M. Masse - Engr. Product Mgr. - Butterfly Valves
~~~~G.F- MacDonald - Director Nuclear Q.A.~~~~
'6'. wolfe - Marketing anager - Butterfly Valves Burns and Roe SFox JVZa lavadia Dee Sheikh DSheikh J. V. Zalavadia BBedrosian RBaldwin .
~~~~Part Time EFerrari'6)~~~~
MKahn pf Notes: l. Documents to BZF db Burns and Roe Comments on Q.A. Manual-Burns and Roe letter BRBZF-68-74-011, dated 6YGNA March 19, 1974. RTVACHMENT
~~~~2. Seismic Calculations - B&R Comments JOB NO.~~'Q~~~~~~
wig WO.
Burns and Ro wo.v I.g< .
~~~~a. Cha e ontract Specification.~~~~
~~~~b. ubmit the~~~~
~~~~c. Submit the calculations for the detail of seating torque value, used in design calculations de~~~~
~~~~e. ~ Consider tio" cn~~~~
rCI r
Page 2 F
specification. The seismic calculations include, stress an lysis only. The analysis fo strain/deformation is also required as a. proof that there will'be no loss of function.
Su mit analysis or proof that radiation will not versly affect the yield point of the material.
Submit analysis and design for 72" and 84" valves considering normal. load with the combination of 4 SSE stresses shall be maintained within the normal .
allowable working stress limit as mentioned in paragraph 3.3.1.1 of specification. r ~~~~
3. Mandator Testin for Seismic ualifications r tested the same type of equipment for greater accelerations than Burns and Roe specified and that they will sub the test data for Burns and Roe review and approval
~~~~4. Stardvne Model used in Seismic Calculations ATTACHMEN'I FILENO.~~~~
~~.~~.+
7.'
EHEETNO.
(.3S'.
e~s.
e ce ins t 4 ll valv 7.
Burns and Roe asked BZP to submit the natural fundamental frequency of 18", 24", and 30" valves.
st nr this and Roo state~d that G "4 c~ ra~vj~wj-,a thej.
quot t=cn nd after t:PPSS's a>>nroval Burns .-.nd Roe wE notify G.';F i,= acMitionai woz's auth.ran'ed.
ll (B; infor.ml
..; ~
I
~ c'l.. ':h o ) Tu l i. <j,, '>7.~ by t'")hone that the ccs"
~. gy '4 JWINvrrNrr
4 Page 3 additional work will be $ 300.00).
~~~~8. General>>BX= Comments BZF indicated as follows:~~~~
~~~~a. If operation or accidental 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. Xf water or any other fluid is supposed to flow in the pipe, the sha t 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 required to operate the valves. But in case. of air
~ i.,
or steam it makes no difference.
~~~~9. ualitv Assurance Manual:~~~~
Burns and Roe stated that Burns and Poe comments on BIF Quality Assurance Manual was mailed to BIF on March 19, 1974 (BRBZF-68-74-0LL) and was classified "Not Approved". The response to these comments has not been rece'ved as of BXF stated that the BXF Plant is on vacation for this'ate.
2 weeks (July 1 thru July 12). Mr- MacDonald will start updating QA Manual on July 15 and he expects to complete by July 19, 1974. BIF will revise their Q.A. Manual and/or provide necessary supplements to the manual as per Burns and Roe comments. Burns and Roe comments were discussed.
Mr. MacDonald will call Mr. Sheldon Paige of Burns and Roe on July 15, for the clarification of the following Burns and
~.Roe commeocs:
~~~~a. Corrective action~~~~
~~~~b. Audit of Purchase Regs./P.O.'s/change order~~~~
~~~~c. Compliance to supplier Quality Control Prog A~ACH58ENT~~~~
~~~~d. Complia'nce to Lower Tier Procurement~~~~
~~~~e. Welding Process Sheet Form N-152 (BIF) and t fpk%P~~~~~~
~~~~of Contract Specification 17A-30 and 17A-31~~~~
~~~~10. Inservice Insaection Re irements ru.s Na.~~~~~
SHEET N>
Burns and Roe questioned regarding the requirements of "calibration blocks" in accordance with the 'draft of the 1974 Edition of ASME Section XI, Article X>>3000 "Preparation for Calibration" for Znservice Inspection. BIF stated that the speciaL calibration blocks are not required. Thev will submit detailed method of Xnservice Inspection with Standard Calibration blocks.
Xtc.: 0;" s3 tn BX.- b.: BCR Decision on BXF uot.aiion on ca'culations on natural I'" ~" t !('"<' ~ '<<t ~ s' i' <<if'r( Qil" V' ' ~ ( f to'%~0 ~iO
'<<r
~ s % tfre<< ~ 1 e ~
Page 4 12 a~
~~~~b. Submission of revised Q;A. Nanual (Xtem No. 9)~~~~
.Inservice Inspection Reauirements (Xtem No." 10)
II@ .
JJV/JVZ/dc+ Prepared by J.~
I Submitted by cc: Mx- J. E. Woolsey - WPPSS -3 Nr. P. C. Otness - BPA -1 ATTACHSfEHY
"3 a Fjh
'llllllllllllllllllllllllltlll QID5 361106 7.2 Old Requalification & SQRT Forms
V/PPSS NUCf EAR PLANT UNIT 2-zbiio8 SEISMIC AND HYDRODYNAMIC LOADS REqUALIFICATION CERTIFICATION JOB NO. 2808 EQUIPMENT NAME- '4" Cylinder Operated . SPEC. NO:
Butterfly Valve E(UIPMENT NO< CSP V 3t 4 g 5 g 6 g 9; CEP<<V-3A,4A LOCATION:
491'0",
Reactor Bldg, El. 482'0", 479'0", 473'0" 488'0",
El. '491'0",' 491'0" E(UIPMENT CLASSIFICATION: g ACTIVE PASSIVE SHSMIC QUALIFICATION REPORT
~~~~REFERENCE:~~~~
~~~~l. cylinder'operated Report No. TR~-Y, Design and seismic analysis of 24" butterfly valve (rev. dated~~~~
~~~~2) 4/17/78, by McBherson Associatek, Inc., Trans 24~~~~
2. Dynatech Project No. BIF-14 Deflection Analysis of Butterfly Valves by Dynatech R/D Co. 4/12/76, Trans 1313 THE ABOVE SEISMIC QUALIFICATION REPORT(S) HAVE BEEN REEVALUATED AND REqUALIFIEO MHERE NECESSARY TO SHOW THAT THE ABOVE-MENTIONED COMPONENT
'S CAPABLE OF PERFORMING ITS INTENOEO SAFETY FUNCTION UNDER ALL THE.
APPLICABLE LOADING COMBINATIONS INCLUDING THE POOL DYNAMIC LOADS.
CYGNA APPROVEO:
MO.~L'REPARED:
ATTACHMENT DATE:
~08 No.~."
FILENQ. + ~'~
sHEav
mensch San dose, California Pro ~ 'WNP-2 F(ie No washington Public Power Supply Syst: em Qjent +ashington Public Power Supply System
. i-yGblA Tag No.: CSP-V-3",
CSP-V-4
~mAc HIVE>> CSP-V 5 CSP-V-6 NO.S-~
JOB PILE NO.~
<<I;geT
'j.et.
NO;~~
t-a*
CSP-V-9 CEP-V-3A CEP-V-4A-
.. Class I, Active linder 0 crated Butte
~ ~ =~
a Original qualification method a
.A., Static..analysis .........
Re-evaluation results h A. -. The natural frequencies were riot calcuated.
B.. Valve operability .was v'erified.by deflection'Icalculation.
C.. Caleu3.ated stress margins are within allowables.
D 'RS used in analysis
~ -. not envelop the interim SQRT crit ia.
Conclusion A T d butterf1v nes ant.
comply with interim SQRT requirements.
e se sm.c coefficients used in the analysis do not envelop the interim. SQRT requirements.
Recommendatxons A. Analyze valve to SQRT requirements.
V. Comments on the original analysis Accelerations used were 3g horizontal and 2g vertical..- They were combined using SRSS.'he B. natural freq encxes .Were not evaluated.
II
'Max~ critical-"deflection-was,D.A)64'a.,0,50"pallowabl I . ~
Revision Prepared By/Date Checked By/Date
.Ii Page I
-et -"" I
Tag no. CSP-V-3 CSP-V-4 CSP-V-5 CSP-V-6 ualification Sunna of E ui ment SP-V-9 CEP-V-3A CEP-V-4A I. Pl ant Name: WNP-2 T e:
~~~~1. Utflity: washin on Public Power PWR Supply System~~~~
~~~~2. NSSS: GE 3. A/f: Burns 6 Roe BWR 5, Mark EE II. ~C~~~~
~~~~1. Scope: [ 3 NSSS Xg BOP 2- Nodel Nunber: A-206765 guantity: 7~~~~
~~~~3. Vendor: BEP~~~~
~~~~4. If the componen. is' cabinet or panel, nan and model No. of the~~~~
~~~~. devfces fncluded: N/A~~~~
~~~~5. Physical Descri ption a. Appearance 'alve~~~~
~~~~b. Dimensions~~~~
~~~~c. Weigh. 399 lbs~~~~
~~~~6. Locatfon: Building: Reactor Bld ., Containment Bld .~~~~
482gQ>> 479gQ>> '473 '>> 488tQ>> 49lgQ>>
Elevation: 491'0" 4
~~~~7. Fie1d Mounting Conditions (jQ go1t (Mo. e hgize lie" j n MeId (Longe j~~~~
~~~~[3 Containment Supply Purge System~~~~
~~~~8. a. System fn which located: containment Exhaust pur e s stem Chamber exhaust, Containment~~~~
~~~~b. FunCtiOnal DeSCrfptiOn:Esolation a Vac. relief to Su al Chamber~~~~
~~~~c. Is the equipment required for [] Hot Standby [] Cold 'hutdown~~~~
~~~~[3 Both [3 Neither~~~~
~~~~9. Pertinent Reference Design Specifications:~~~~
2808-68 Am>CH~aN~
~
Prepared by:
Checked by: boa NO.~ 3/81 RGB NO.
M"'.oQ
.L.5 SMggt Mo
~~~~NOTE: game .bolts no't installed~~~~
U
,***III.Is Equipment Available for Inspection in the Plant: g3 Yes ., g g No IV: Equipment gsalification Method:
t; g Test P) Analysis 5 3 Combination of Test and Analysis gualification Report*:
Report.No. TR-74-7 (Rev. 2), dated 4/17/78, Design (No., Title and Date) a seismic Analysis od 24" c~linder Operst:sd enat Prepared Report: zcpnerson Assoc. Inc.
Butterfly Valve
. Coapany
~
Corpany tha RevieHed Report: Burns a Roe/NUTECH V. Vibration Input:
~~~~1. Loads considered: a- gQ Seisttnc only~~~~
~~~~b. t: g Hydrognamic only~~~~
" ~c.
gQ CodHnation of (a) and (b)
~~~~2. BBiethod of CorMning RRS: t. g Absolute Sum t,3g SRSS'* f 3 3- Required Response Spectra (attach the y aphs): Attached~~~~
4. Damping Corresponding to RRS: OBE SSE 5.. Required Acceleration in Each Direction: j g ZPA fQ Other attachment 1 DB: S/S . F/B I~
~~~~SSE 3 'g l. 3g~~~~
~~~~NOTE: XS more than one report: complete items XV thru VXX for each report.~~~~
~~~~NOTE-" Fbx-~2vB 'CSP=V=F.oaXy~~~~
~~~~NOTE: SCP-V-9, CSP-V-6 not installed ATTACHMENT JOB Nb. ~~'~~~~~
~>L,a Nb.~~olf eHBBINo.Z~ o
-2A-III. Is Equlpnent Available fnr Inspentlnn ln the Plant: fx'J Yaa ( ) Nn IY: Equipment gvalification Nethod: II I 3 Test QQ Analysis E 3 Combination of Test and Analysis qualification Report~:~t-<>egg 5&- Trarismitta'1< $ 3+
(NO., Title and Date) ~~~g4 'De/lee~ion-Analjrsi.st'4/1~2. ~
'ompany that, prepared Report:~b'n'~e'ch.c~Q'D Co.
Co~any tha. Reviewed Report: ~urns'. & Roe+Nutech, V. Vibration Input:
1.'oads..consid red: a. 5 3 Seismic only
~~~~b. t: g Hydrodynamic only~~~~
~~~~c. t. ) Corhination of (a) and (b)~~~~
~~~~2. Netho of Co~'ning RRS: t. 3 Absolute Sum {: 3 SRSS . t. 3~~~~
~~~~3. Required Response Spectra (attach the y'aphs):~~~~
~~~~4. Oarping Corresponding to RRS: OBE~~~~
~~~~~Saw~~ ~ SSK~~~~
5. Required Acceleration in Each Direction: t: 3 ZPA t: 3 Qther OBE S/S ~ F/B ~ Y a SSE S/S ea F/B ~ Y~
CYGWA ATTACHMENT OOS No.~~~
pll.e No.~>>~'
SHEH'NO.
HQTE: If more than one report complete items ?V thru VII for each report-3/81
YI- If gualification by Test, then Co~p1ete: gyA random
~~~~l. t. 3 Single Frequency L' HuIti<<Frequency: f 1 sine beat E3 2 [ l Single Rxis [g Multi<<Axis~~~~
~~~~3. No- of gualification Tests: OB{'SE Other spec1ey 4- Frequency Range:~~~~
~~~~5. Natural Frequencies in Each Direction (Side/Side, Front/Back, Vertical):~~~~
~~~~S/S ~ F/B %~~~~
~~~~6. Nethod of Determining Natural Frequencies l g Lab Test .. t: ) In-Situ Test g 3 Rna1ysis~~~~
~~~~7. TRS enveloping RRS using Hulti-Frequency Test [3 Yes (A.tach TRS 4 RRS graphs.',~~~~
~~~~f. 3.No e~~~~
8 Input g-level Tes: OBE S/S ~
SS S/S % V
~~~~9. Laboratory Nounting:~~~~
~~~~j ) Bolt. {Mo., Size ) {. 3 Meld {Length ) i3~~~~
~~~~10. Functional oper bility verified: f. 3 Yes I: 3 No f. g Not Applicable ll. Test Results including modifications made:~~~~
12<<Other test, performed (such as aging or fragility test, including results):
Note: If qualifica ion by a coahination of test and analysis a1so co late Item V!I.
12/80 4~ACHMauy dos NO.~Sz FILE gQ,+~0. FS SHEH'No ~~
4 VII- If gualification by Analysis, then complete:
~~~~1. Method of Analysis:~~~~
{. 5 Static Analysis {: g Equivalent Static Analysis g>-3g, g ~2g
{. 3 Dynamic Analysis: {. 3 Time-History 5 3 Response Spectrum
~~~~2. Natural Frequencies in Each Direction (Side/Side, Front/Back, Vertical):~~~~
~~~~Not Calculated s/s- F/B ~ V s~~~~
~~~~3. Model Type:. {. 3 39 {:32D . {:31D~~~~
~~~~{. 3 Finite Element {: 3 Beam Q g Closed Form Solution~~~~
~~~~4. {. ] Coaputer Codes: None Frequency Range and No. of modes considered:~~~~
{: 3 Hand Calculations 5- Method of Coahining Dynamic Responses: f. 3 Absolute Sum QQ SRSS
{: 3 Other:
+speci Ty)
~~~~6. Damping: OBE SSE Basis for the damping used: N/A 7- Support Considerations in the aadel: Pipe Mounted~~~~
~~~~8. Critical Structural Elements:~~~~
I Governing Load vPSX'PSX.
. or Response Seismi c Total Stress A. Identification Location Combination Stress Stress Allowa" I e Driver lever (a) Operating & SSE 40s444 45 000 Valve body (S.X.) Operating a SSE 17,330 18,000 Maxi adam Allowable Deflection B. Max. Critical to Assure Functional Opera-Defi ecti on Location bilityO&~&&&&~~&&&&&&~&W&W 0.064" Disk 0. 50 See V.C. Page 1/1-CYGNA ATTACHMENT JOB No.~Vga FlLE NO.~~~'~
SHKFT NO. 2 ~" 3/81
Attac<:ant 1 Static Seismic "C" calculations (Stick
~~todel)
CSE Level, 1/2% C=itical Caapinq, 8rec~eacr aacm~g 3nC above SSE Value ~ 2 v QBE Va ue Suil8 incr A-ea Elevxtioa t= t.)
Horizontal OS' Eo SSE i ontal
~
Ve 03~
tical, SS= ~
Reactor 653** 1.25 2 ~ 50 1 00 '
~ 00.
Buil~q 567 ~ 58 L.lo L.OO 2 00
~ <<8 eq~ 547 57 L 14 ~ 95 oO 52'00 ~ 57'8 1 l4 87 74 l, 36'.
L.36 470 i80 ~ 60' oO . 1.20 443 87 74 50 1 ~ 20 434 <<<< 1 QQ 2. 00 .40 80 Diesel Cen 414** 1. 00 2. QQ .40 . 80'
<<LQ 8=/15 Hc 472 3~ 5/ 60 7 0/1 2 '
6/L.6 2/3 Rad~ast 454 437 3
2 '/
'/.7090 6 4
4/l 4/l 4
8 "o5/~ 0 24/LL 5.0/2 0 AS/2 '
<<8 / 0 Rc -541 524 L $/L' 1 1/l, ~ L 3.0/3.0 2 '/202 lL Q(t
.2
~ 7/ 8 4.0/2 2'.4/l.6 500 L.O/.65 2.0/L.3 8/.65 3 . 5/L.:.
46o L.l/ 60 2. 2/1.3 L7/ 50 ~
3 4/1 i
~
~~~~L/S I:-I (~~~~
Reactor 3uiL4i.".q 492'l 480'-4" 5/8" 32 32 3.2 3.0 lL.3 3 p <<4~>> 467 '8" 3~0 l2'8 L.3 Co@<< 455'$" 4 0 3.0 1 3
<<8 Hc
~~~~From at additional's eleva (by NuTech) goB Noi No')LE SHPgf NO.~~~~
QIDN 361106 7.3 BZP Report
0 h
I y II t
B I F 1600 A UNIT OF GENERAL SIGNAL DIVISION ROAD NEST HARHZCKg R I 02893 QUALIFICATION OF PRIMARY CONTAINMENT BUTTERFLY ISOLATION VALVES UNDER LOCA CONDITION DYNAMIC TORQUE CALCULATION OF BUTTERFLY VALVE PREPARED FOR:
HASHINGTON PUBLIC POHER SUPPLY SYSTEM SIZES 3 0 g and 24 HPPSS CONTRACT NO. 68 BIF ORDER NO.: PN27234 Er PN27235 HPPSS XDENTIFXCATZON NO. CSP-V-"1 & 2, and CSP-V-3 8 4 Prepared by." Debendra K. Das ~l Date: 4ev. lO 1 0 82.
Checked by: Dezso Szila i Date: ~a, ro. /PgP REPORT NO. TR-27234 Anti TR-27235 Oyer 80,~20~q gg ~o.o SHEET t40. l~M'
~
~
~~~~1. Summary 2 Dynamic tor~e tables~~~~
~~~~3. Ref erences~~~~
~~~~4. Analytical Procedure and Plow Data (I) '.~~~~
Analysis I'.
b.
for 30 inch valve Hand Computation of several test cases for air flow Computer results and comparision with hand computation 25 28 (ZI) c. Hand computation of several test cases for steam flow 40
~~~~d. Computer results and comparison with hand computation 42~~~~
6. Analysis for Z4 inch valve (ZZZ) e. Hand computation of several test cases for air flow 53 f Computer results and comparision with hand computation 55 (IV) 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 ME-02-83-08-Oi Sheets 1 thru 9~~~~
~~~~b. LOCA Temp. Curve~~~~
~~~~c. LOCA Pressure Curve~~~~
~~~~d. MPPSS Letter dated 10/22/82 e BIP Plow Loss Coefficient K plot~~~~
~~~~f. BZF dynamic torcgxe Coefficient CT plot~~~~
h 1
'UMMARY This report contains the dynamic torque analysis of two butterfly valves of sizes 30, and 24 inch. The analysis is performed for LOCA Qoss 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 torque 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 torques developed under the specified flow conditions are less than the design torques used in the. original Seismxc and Stress analysis of these valves. Therefore the valves are safe against the action of dynamic torque in the event of a LOCA.
~~~~SUMMARY~~~~
OF RESULTS Table - 1 30 Inch Valve, airflow Time Angle cf Dynamic s dege Torque in-lb 1 0 90 (Pull 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 (FU11 closed) 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 No. TR-74-8 by McPherson Associates for this valve is 27800 in-lb. Therefore the design is safe.
Cj
~~~~SUMMARY~~~~
OF RESULTS Table - 2;. 30 Inch Valve Steam flow Time Anglec4 Dynamic S degas Torque in-Ib 1.0 90(Pull open) 11032 1.5 78 75 23175
~~~~F 0 67 50 18142, 2 5 56.25 14668 3 ' 45.00 12424 3 5 33 75 10580~~~~
4.0 22 50 7809 11.25 3867 5 0 9 0(Full cLosed) () 0 TNet= 22174 I
At full closed position the dynamic torque is zero and the net torque is due to seating and bearing friction.
L I
I I c C
~~~~SUMMARY~~~~
OF RESULTS Table - 3i 24 Inch Valve; Air flow Time Angle W Dynamic S degas Torque in-lb 1 0 90 9'ull open) 5525 78 75 11692 2 0 67 '0 . 9095 2.5 56.25 7428 3 ' 45. 00 6239 3 5 33 75 5430 4 ' 22 50 4043 4.5 11.25 2020 5 0 9. 0 (Pull closed) O-0
~~~~TNe't= 13808 in-lb~~~~
~~~~At full closed po'sition the'ynamic torque is zero and the net torque is due to seating and bearing friction.~~~~
Note: The design torque used in the Seismic analysis report No. TR-74-7 by McPherson Associate for this valve is 170(Qin-lb. Therefore the deisgn is safe.
'I
~ C l,o I 3
~
~~~~4~ g~~~~
~
'll f d
'll
~~~~SUMMARY~~~~
, OF RESULTS Table - 4 24 Xnch Valve, Steam flow Time Angle c4 Dynamic S degas Torque in-lb 1~0 909'ull open) 5425 1 5 78 '5 11394 2 0 67 '0 8921 56 '5 7213 3 0 45 F 00 6109 3 5 33 '5 5202 4.0 22.50 3842 11.25 1902 5.0 9~0 (Full.
closed) 0-0
~~~~TNet= 13808~~~~
~~~~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.'o. ME-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.
2~ ANSI/AWWA C504-80, AWWA Standard for Rubber-Seated Butterfly Valves. American Water Works ASsociation, Colo.
~~~~3. Beard,C., Final Control Elements, Valves and Actuators, First Edition, Rxmbac ,Pub catxons, 969.~~~~
Hutchison, J. W., ISA Handbook of Control Valves, 2nd Edition.
Torque and Sizing Calculation for'IF Butterfly Valves, No. D-214590, dated 1/9/75 for WPPSS Contract 468.
~~~~6. 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 OTR-0650-43, Hydrodynamic and Headloss Test of 12" - 150 Lb. Butterfly Valve with directly connected short radius elbow upstream, dated 2/24/82.
I 8~ B IF Drawings: 30 inch Valve General Arrangement Drawing A-206763 24 inch Valve General Arrangement Drawing A-206764
'NALYT1CAL PROCEDURE The valves analysed in this report are primary containment isolation Butterfly Valves used in the purge system. Valve sizes considered here are 30 inch and 24 inch.
During the normal operation these valves are in full open position and should close completely in case of an accident. Xn the event of a LOCA (Loss of Coolant Accident) the valves have to close against ascending differential pressure. During the closing operation the valve disc
~~~~illbe in semi-open positions and will experience fluid dynamic .forces due to uneven pressure distribution across the faces of the disc.~~~~
The pressure rise and temperature rise inside the containment with res-pect to time, is given in WPPSS addendum (reference 1) . The flow through the valve causes aerodynamic effect on the disc that gives rise to the dynamic torque. This dynamic torque is given by the formula:
TD ~ CT (bP) D (Ref o 2) ~ o o ~ ~ ~ o ~ ~ ~ ~ ~ ~ ~ (1)
TD Dynamic Torque (in.-Lb. )
CT ~ Coefficient of dynamic torque obtained from test (Dimensionless constant)(Ref. 7) h,P ~ Differential pressure across the valve (psi)
D ~ Disc diameter (in.)
During the closing operation of the valve CT and b,P will be changing for varying closing angles of the disc. The dynamic torque will tend to close the valve where ap the shaft bearing friction torque will oppose The bearing friction torque is given by the formula:
Th ~ rt D2 4
fb (d/2) b. p (Ref. 2)......
AVVACVMKM,
~20~q SHEET 40.3~:~
Tb ~ Shaft bearing friction torque (LB-in.)
D ~ Valve Port diameter (in.)
fb ~ Bearing friction coefficient (dimensionless constant) d ~ Shaft, diameter (in.)
$p ~ Differential pressure (psi)
Therefore the net unbalanced torque is T = TD Tb N
The differential pressure Qp ac'ross the valve shall be calculated from the data on volumetric flow rate under LOCA Condition supplied to us by WPPSS. The equation used will be the one for sub-sonic gas flow recommended by the Fluid Controls Institute:
P12 - p22 Q ~ 963 CV (Refe 3 and 4) ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ (3)
GTl Where Q = Gasflow in SCFH Pl ~ Valve upstream pressure (psia)
P2 ~ Valve downstream pressure (psia)
Specific gravity (air =1 at 60oP and 1 atm. pressure)
Upstream temperature in o Rankine Valve coefficient - 29.9D2 Valve Port diameter (in.)
K = Coefficient of flow (dimensionless constant) (Ref. 7)
WPPSS recommends that with the occurrence of LOCA inside containment, a signal is sent to the main control which automatically sends the valves to the failure mode. The time delay (instrumentation time) before the Butterfly valve starts to close is given to be less than one second. We have conservatively assumed this delay to be one full second. Time of closure from the fullmpen position to full-close position is four seconds.
This closure time was the original requixement of the valve operator and has been tested at B l F for several valves and is noted to be often less than four seconds and even as low as one and a half seconds. A smaller closing time will obviously cause less flow due to lower containment pressure and a lower dynamic torque. However, the maximum closure time of four seconds is used in this analysis. Therefore, from the onset of LOCA to the full closure of the valve the time duration is five seconds.
Using this time period
~ ~
we have abstracted the pressure and temperature response under a
~
LOCA condition from WPPSS curves of Reference 1, Fig.
6.2-2 and Fig. 6.2-3 . The drywell pressure and temperature are used which are considexably higher than the wetwell values; The enlarged plots for the period of interest are shown on pagesl0, and 11 ~ The specific volume and the volumetric flow rate of both saturated steam and air are also presented in WPPSS addendum, reference 1. These quantities are also plotted against time for both steam and air as shown in pages 10, thxu 15.
For saturated steam the specific volume or specific weight are obtained fro the steam table.
The period of closure of the valve has been divided into e'ght equal divisions each of 0.5 second duration representing 11.25 degree of closure of the butterfly valve at a unifoxm rate. This division facilitates in CYGNA AMiACNNKS'F Ng,g~do~9 esm r'o.i=~~~
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F 16
'I reading the interpolated values of pressure, temperature density and volumetric flow as can be seen from the plots on pages 10@ thru 15 Data obtained from reference 1, and the interpolated values are presented below. 8 equal intervals representing 11.25o rotation of the disc are consideredo TABLE -" 1 Time Angle Pressure Temp o Air Sat. Steam s deg~ psig oF density density Lbf/ft> Lbf/ft~
1.0 90 (Full open) 18 221 0 1295 0 0789 1.5 78.75 19 '* 234* 0.1325* 0.0818 2.0 - 67.50 20.7 243 0.1359 0.085 I
2.5 56.25 22 '* 249 '*' 0.1405* 0.0886 3.0 45.00 24.0 0.1460 0.1926 3 ' 33.75 25.4* 259* 0.1515* 0.0953 4 0 22.50 26.7 262 0.156 0 '984 4.5 11.25 27.9* 265* 0 '595* 0.1009 5.0 0.0(full closed) 28.9 268 0.1618 0.1033
interpolated from Page 10 Page 11 Page 12 For saturated graphs. steam from ste table at the given pressure Coefficient of flow Kv and the dynamic torque coefficient CT for different angles of valve opening are obtained from ithe test report reference 7.
B I F has conducted extensive test on different types of disc geometry and ATTACHMENT'f CYGN'A
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'E
~ g
disc and shaft orientation with respect to the direction of flow which are summarized in reference 6 and 7. The test medium is water and no air test is undertaken. Reference 6=is for two types of discs, namely, cast iron streamline disc and.fabricated flat plate disc. Measurements have been made for dynamic torque coefficient and flow coefficient for both flatside upstream and flatside downstream of the disc. The com-parison indicates that the disc orientation of flatside'down stream always causes higher dynamic torque. Reference 7 incorporates a directly connected short radius elbow upstream to study the effect of flow non-uniformity on dynamic torque. Several tests have been performed with yshaft vertical and shaft horizontal, counter clockwise opening and clock wise opening, with flatside upstream and flatside downstream. These test data are also compared with that of a straight pipe withou5 any elbow of the valve. A careful study of these experimental results in-up-'tream dicate th- ".e -os severe case is a vertical shaft orientation (i.e.
perpendicular to the plane of the elbow) wiQ flatside of the disc down<<
stream with a clockwise rotation of the disc.
This orientation results in approximately 30% increase in maximum dynamic torque coefficient than that obtained for a straight pipe. Zn this re-port this most severe case is used to obtain torque'oefficients at angle of valve opening. This approach results in higher torque
'arious values and represents the worst condition. The test data are presented in the tabular form.
l TABLE - 6 Time Angle(Q )
Sec. , Dege 1.0 90 0.55 0.275 1.5 78 '5 0-70 0.56b 2.0 67 50 l. 10 0 35 2.5 56.25 2 '0 0.175 3 ' 45.00 5.20 0.09 3 5 33.75 14 F 00 0.045 4.0 22.50 45.00 0 '2 11.25 170.00 0.01 5.0 0 ' :Closed 0.0 The volume and mass flow rate through the valve due to ascending differential pressure is presented by NPPSS in referencei. We note that this is the flow rate for valve in fully open position. However, the valve is closing gradually and the flow rate should decrease accordingly and when the valve is fully shut the flow rate should re-duce to zero. 'his would occur at the end of 5 seconds. Therefore, we have to obtain the percentage of full open flow corresponding to the appropriate percentage of opening. Reference 3 and 4 provide such in-formation. In reference 3, page 38, the flow characteristic of a butter-fly valve is presented. This is a plot of percent of flow versus percent open which shows an equal percentage curve for the firt 25% of flow a linear curve thereafter for the remaining 75% of flow. In reference 4, CYGNA A77ACHMES'F
r 0 ~ ~
page 166,the flow characteristic of Butterfly valve is shown to fall
'etween the linear and equal percentage curve. Therefore from these plots the fraction of maximum flow at a percentage opening can be de-.
tezmined. ,Before deciding whether to use the linear or;,equal per-centage curve some careful consideration has been given to determine which one should give the worst dynamic torque.- Upon some reflection it is observed from equation (1) that the dynamic torque increases when- the pressure drop increases. Zt is also apparent from equation (3) that the pressure drop is greater when the flow rate is greater. This is achieved by using the linear curve which predicts higher flow than ice equal percentage curve. Therefore on the basis of this argument following flow rates are established for different degree of opening of tahe Butterfly valve.
'..TABLE -7 For 30 inch valve Air. flow Angle Percentage Full open Flow Percentage Flow s degas open 5 ft3/s ft3/s 1.0 90 Full open 100 1614 9 1614. 9 1.5 78.75 87.5. 1625* 1423.6 2.0 67. 5 75 1646.4 1234.8 2.5 56.25 62.5 2669.5* 1043.4 3.0 50 1687 ' 843.6 3.5 33.75 37.5 1700* 63?.5 4.0 22.5 25 1709 9 427.5 4.5 11.25 12.5 1719.5* 214.9 5 0 0.0 Full 0.0 1734.3 0.0 Closed
~~~~Xnterpolated. Page 13 Re from graph 0 ~30~q y~,~o. O SHEET 40. l~~~~~
'N 1'ei-c f N Q 4
i'I'I ' k
-20 For the 24 inch HPPSS recOmmends that in ordeg to estqblish the flow rate same velocity as that of 30. inch. valve be used; Therefore following flow rates are obtained from the velocity data of WPPSS.
TABLE-8 For 24 incCc va1ve air flow Time Angled Velocity Full open Flow Percentage ft3/s flc s dege ft/s ft~/s 90 Full open 352 1015. 6 1015.6 1.5 78.75 -- (1); 1028* 899.5 2 ' . 67.5 358 9 1035.5 776.6 2.5 56.25 1052* 657.5 3 ' 45.00 367 8 1061.2 530.6 33.75 1070* 401.3 22.5 372 8 1075.6 268 9 4.5 11.20 1085* 135.6 5.0 0 ' F011 378.1 1090.9 0 0 closed Ref.l Pa e 14 (1) Not given
~~~~Xnterpolated from graph 24 inch valve I.d . 23 inch Area 2.8852 Ft2 CYGNA AMiACHMESY~~~~
C f
~ ~
For saturated steam flow data of WPP$ S some discrepanceis are observed.
Calculations presented on Sheet no. 7 of 9 and 8 of 9 and the table on
~
Sheet 9 of 9 indicate that the flow rate is decreasing with respect to
~
~
time especially at time 2 and 5 seconds. These data points are plotted on page 15 of this report. Since the containment pressure is rising with respect to time the flow rate should increase. This can be seen from the behavior of the air flow results. Therefore steam flow rates were re-calculated to establish the corrected flow rates. The results are as follows:
Reference 1. Sheet No. 7 of 9 and 8 of 9 30 inch valve saturated steam flow
~ 0.525 hP d ~ 29 Tif y d2 inch, K-, 6.0 Kv W V At.l sec. Qp 18 psi Pl ~ 32.7 psia
'4P ~ 0.55 Pg Y~076
= 12 68 ft3/Lhf V
W V ~ LO. 525 (.0.76) (29 ( ~t..18 [ . )= /
22 Steam flow - continued 5
At 2 Sec.
AP ~ 20.7 psi C
Pl cz 35.4 psia A,P ~ 0.585 Pl Y ~ 0 '4 11.7222 ft3/Lbf 20.7 0.525 (0.74) (29) 2 6.0(11.772) (11.772) 2082 ft /s Very close to WPPSS result.
At 3 Sec.
Same as WPPSS result = 2118.2 ft /s At 4 Sec.
hP ~ 26;7 psi Pl 41.4 psia AP ~ 0 645 Pl Y~0 718
v~
~ 10.165 ft3/lbf
,o. <<
26.7 0 525(0 718) (29) 6(10 165) (i 9. 165) =2132 ft3/s At 5 Sec. QP ~ 28.9 psi Pl ~ 43.6 psia 9
AP ~ 0.663 Pl Y > 0.712 V ,.9.683 ft3/lbf 28 '
l0.525(0.712) (29) 2 6(9 '83) (9.683)~21 ATTACHMENT'F
d""
4 l
23 These corrected values of steam flow rate is plotted earlier on page
~~~~15. Prom this plot the intermediate values are interpolated.~~~~
TABLE-9 30 inch valve, Saturated Steam flow Time Angle Pull open flow Percentage flow s deg~ ft3/s ft /s 1 90 2070 2070 0'.5 78.75 2074* 1814.8
.2.0 67.5 2082 1561.5 2.5 56.25 2097'A 1310.6 3 ' 45 2118.2 1059.1 3.5 33.75 2126* 797.3 4.O 22 50 2132 533.0 4.5 11.25 2139* 267.4 5.0 0.0 2147 0.0 From pages 21 & 22 and .
reference 1
~~~~Interpolated from the graph on page 15.~~~~
CYGMA AliACHMESV
SUHMARY OF RESULTS Table - 3i .
24 Inch Valve, Air flow Time Angle W Dynamic 8 dege Tor cue in-Lb 1 0 90 (FuLL open) 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 4i0 22 50 4043 11.25 2020 5 0 9 0(PuLL closed) O-0
~~~~TNet= 13808 in lb~~~~
~~~~At full closed position the'dynamic torque is cero and the net~~~~
,. torque is due to seating and bearing friction.
Note: The design torque used in the Seismic analysis report No. TR-74-7 by McPherson Associate for this valve is
~
': '70in-lb. Therefore the deisgn is safe.
I' tg l
24 The corrected values of Steam flow rate obtained for the 30 inch valve used to arrrive at the proper flow rate 'for the 24 inch valve based 'were upon the criterion of same velocities in both the valves. The results are presented below.
TABLE 10 25 inch valve, Saturated Steam flow Time Angle Full. open flow Full open flow Percentage s deg. fog 30" valve, fog 24" valve, flow, ft3/s ft /s ft /s 1.0 90 2070 1289.6 1289.6
,1. 5 78.75 2074 1291 1130.5 2.0 67.5 2082 1297 972.8 2 5 56.25 2097 1306.4 816 5 3 0 45 2118 ' 1319.6 659.8 3.5 . 33.75 2126 1324.4 496.7 22.50 2132 1328.2 332.1
'.5 11 25 2139 1332.54 166.6 5 0 0.0 2147 1337.5 0.0 From Page 23 Shown below VAt.YF Q Velocity in 30 inch 30" 30" same velocity in 24 inch valve A A30 4 63Z338.
Full open flow in 24 inch valve 930>> (A24) = 030 (0.62297)
A~
30
Mhen the valve shuts off completely the flow through the valve ceases and therefore the dynamic torque vanishes. Zn this position the dif-ferential pressure across the valve disc is the containment absolute pressure minus the atmospheric piessure. This is equal to the gage pressure inside the containment. Thus the necessary torque to com-pletely close the valve and maintain it in the fully-shut condition against the existing differential pressure is due to the sum of the shaft hearing friction torque and the rubber seat friction torque called, the seating torque.
'The shaft bearing friction tox'q'ue is'resented as equation 2 earlier.
. The seating torque is given by T ~ C D2 (Ref.2) ....... . ~ (4)
I Ts ~ Seating or unseating torque (in-lb)
~'
~ Coefficient of seating or unseating torque (Ref.5)
D ~ Valve part diameter (inch)
With all data availahle the necessary calculation is perforned using equation (1) through (4) . Dynamic torque is calculated for each angular e
position to determine its. maximum value and at what angle it occurs.
There are two valves (30 inch and 24 inch) and for each 9 sets of calculation has to be made. Furthermore two flowing media are con-sidered, namely, air and satruated steam. Therefore altogether it requires 36 sets of calculation. For this repetitive type of work a computer program is written following the methodology described ATTACHMENT'f earlier in the analytical procedure Section, Zn order CYGMA
~ gy ~2 pgg yQ 0
~0.0~
~q NEET NO.JL~
the computer program hand calculation of several test cases are per-(
formed in the beginning. Subsequently the computer results are presented including the input and output. Comparisions with the test cases show there is full agreement with the manual calculation thus verifying the validity of computer program.
SAMPLE CALCULATION
. VALVE SIZE: 30 Inch Medium: A c',~
Valve opening angle of gg degree occurring at 4. 0 second e
Inlet
~
pressure from pressure curve ~ ls.o +(4 7= 3> 7 l'>c4 Inlet temperature from temperature curve = gp f + +g,o (Sf g, Note that the higher pressure and temperature are used from the Drywell curves.
S Density from the density curve for air or from steam table for Saturated St.eam ~
'\
~~~~u. it@ S LLQ/ $ 6t Pull open uilume flow rate from flowrate curve = ICig 9~~~~
'6
+>/6 Percentage flow at percentage opening ( i)
'(= o K 64 SAqXio SS
~ass Specific gravity G ~ O,IS95 i.ski based on air wieght density 0Lpga
~ 0766 at, 60 F and 1 atm. pressure.
J Q.
Downstream pressure = 4 (0 E7 ) lo I >> o l.t~)l )(4'c;I )
qg~( y g = 31 08 psiu Therefore pressure drop dp - pl - p> i.(2 )so Dynamic torcpxe TD ~ CT ~ [f023 . CT ~
QS(Ref. 7 elbow effect plus most adverse shaft
~
'otation) orientation and disq
t JI 'I '4 ' + 'I f I
v l'
3
~ ~
'I
'b The shaft friction torque Th (29.IQ)
~ ~ S.go2.. cn lh (vastzszst~ sws(L)Q)
Therefore the net unbalanced torque is TN ~ T> - T~ ~ llol7- 0 ig-U
~
is a set of'alculation for one valve angle. 'his Similar calcualations are performed for differen4 angles and presented in subsequent pages.
,6.)
FRZLTZoo Yon,aua ZS g WLLC>ISLA SRa LL .
Nd FORTH I=A. CMCLlL475opf gF pygmy
'I sTMcYa E, F~M
.<~ T 7oRClo p T<iS APtM AeH
,ES CoNspggp7 gyp,
SAMPLE CALCUIATXON e
VALVE SIZE: 3 Qi Inch Medium: A c'.<
~
Va1ve opening angle of 7g 75 degree occurring at; i-S second
~ e Inlet pressure from pressure curve = ig.2, +t4'7= ~S'9 t'Sc o Inlet temperature from temperature curve = g.pg y +g,o - C9$ ~g, Note that the higher pressure and temperature are used from the Drywe11 curvese S
Density from the density curve for air3 or from steam table for saturated steam = o 1325'Lj/Q Pull open viLume flow rate from flowrate curve ~ t427 &3(6 Percentage flow at percentage opening'. '~<>7 )& 37<)= 1<~3 6 R/6 rate in SCFH Qs (5.la9y) ~O sao(<~ q) i<.p ( opq )
'low 8 3>~ >o4 'g>I, Valve coefficient "S-eS ~~ 9 f 0..'.IV)
SO 346 x to3.
C = o.7o v, o70 Specific gravity G = l335' l3 based on air wieght density 0 '766 at 60 P and 1 atm. pressure.
Downstream pressure Is = >>.~~ ( ~"ISSUE)to e qg$ {pq q$ )ty5 ( )(694) 3Z, ~ 2,$
$ 5j/
Therefore pressure drop dp - pl - p> i.667 )Si, Dynamic torose TD CT b, p 5 2 3098 CT- 54(Ref. 7 elbow effect plus in- Uo most adverse shaft orient ticn and d'sc rotation)
ATTACHMENT'
4., l rn k
II n ~
RUH UALVE ,-17A'18 SUN 07 NOV 82 '~ ZILCH VALVE,~ AIR, fLaW ENTER THE HUNBKR OF DATA SETS FOR EACH DATA SET ENTER THE FOLLOWING DATA IH ITS RESPECTIVE ORDER SEPERATED BY A CONCHA OR A BLAHKA I
A) UPSTREAM,PRESSURE IH PSIG B) UPSTRKAH TKHPERATURE IH DEGA F C) DEHSITY IN LB/FT443 D), ACTUAL FLOM RATE IN FT443/SEC E) LOSS COEFFICIENT F) TORQUE COEFFICIEHT ENTER DATA FOR SKT NOA i ?18 221 I
A 1295 1614 A 9 ~ 275 KHTER DATA FOR SET NOR 2
<.') ?19A2 234 A1325 '423A6 I t7 ~ 56
~ ENTER DATA FOR SKT NOA 3
?20+7 243 A1359 i234AS 1~1 D35
.~ ENTER DATA FOR SIT NO 4
?22A3 249+5 e1405 1043 ' 2A3 ei75 ENTER DATA FOR SET NOA 5
?24 255 A146 843+6 5A2
+09'NTER DATA FOR SET NO ~ 6
?25+4 259 +1515 637+5 14 A045 ENTER DATA FOR SET NOA 7
?26 ' 262 A156 427+5 45 ~ 02 ENTER DATA FOR SET NOA 8
?27+9 265 A1595 214A9 170 A01 ENTER DATA FOR SKT NOA 9
?28+9 268 A1618 0 CLa SF+
AMiACHNKf
I 4
NPUT IS, AS FQLLQMSi 0
T NQo P T RQ QA CT PSI DES+ F LB/FT443 FT443/SEC 18+0 221+0 Ooi295 ibi4+9 0+55 Oo275 19+2 234 ' 0+1325 1423mb 0 '0 Oi560 20+7 243 ' Oo 1359'234o8 i iiO 0 ~ 350
4. X,. 22 3 249+5 0+1405 1043+ 4 2i30 ~ 175 24+0 255+0 Oi1460 843+6 So20. 0 '90 25+4 259+0 Oo 1515 637+ 5 14+00'. 0 '45 26+7 262eO 0+1560 427o5 45+00 0+020 27+9 265+0 0+1595 214+9 170o00 0 ~ 010 28+9 268 ' 0+1618 0+0 t'lossa 0.0 i YQU M IW TQ NAKE ANY CHANGES?
IQ ATVACH EST kg ~, 0 q RLR ICL +T ~
3
I U U l U UU
' ~ U y'I U
30 CALCULATION AT ANGLE ~ gb DEG OCCURING AT TIME 1. 0 0
ABSOLUTE UPSTREAM PRESSURE Pi.'~ 32o7 PSI ABSOLUTE UPSTREAM TEMPERATURE Ti 68' DEG R FLOW RATE IN SCFH 9874936. FTeeW'HR VALVE COEFFICIENT CV ~ 34234+9
'PECIF'IC GRAVITY 6 ~ io69i CALCULATED DOMNSTREAM PRESSURE P2 ~ 3i ~ i PSI PRESSURE DROP ACCROSS THE VALVE -DP ~ i+620 PSI DYNAMIC TORQUE TD ~ fi020o LB-IN
CAI CULATXOH AT AHGLE ~ 7y. 75'EGAS OCCURIHG AT TIME ~ 1 5 S ABSOLUTE UPSTREAM PRESSURE Pi ~ 33+9 PSI ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 694 ' DEGAS R FLOM RATE IN SCFH ~ 885557ii FT443/HR VALVE COEFFICIENT CV ~ 30346 ~ 0
.SPECIFIC GRAVITY ~
G ~ i +730 CALCULATED DOWNSTREAM PRESSURE P2 ~ 32+2 PSI PRESSURE DROP ACCROSS THE VALVE DP ~ i'67 PSI DYNAMIC TORQUE TD ~ 23098 'B-IH
.Z I 4~
I
~ly 'I tv
~ 'I IT 4
~ ~ I
CAt CULATION AT ANGLE ~ 67' DEGAS OCCURING AT TIME ~ 2 0 SE ABSOLUTE UPSTREAM PRESSURE Pi ~ 35+4 PSI ABSOLUTE UPSTREAM TEMPKRATURK T1 ~ 703 ' DEBS R FLOW RATE IN SCFH ~ 7918319 'T443/HR VALVE COEFFICIENT .CV ~ 24207+7 SPECIFIC GRAVITY G ~ 1 ~ 774 CALCULATED DOWNSTREAM PRESSURE P2 33 3 PSZ PRESSURE DROP ACCROSS THK VALUE DP ~ 2i094 PSI DYNAMIC TORQUE'D ~ 18138+ LB-IN CYGMA A1VACHNKSY
W MMMMM ~ MMaO W MMM CALCULATION AT ANGLE ~ gl'Z,5'EGo OCCURING AT TIME ~ 2.i5 Sl ABSOLUTE UPSTREAM PRESSURE Pi ~ 37+0 PSI ABSOLUTE UPSTREAN TEHPERATURE Ti ~ 709is DEBS R
~ ~
FLOM RATE IN SCFH ~ 6929288'T43/HR VALVE COEFFICIENT CV ~ i674i+2 SPECIFIC GRAVITY G ~ li834 CALCULATED DOMNSTREAN PRESSURE P2 ~ 33+6,PSI PRESSURE DROP ACCROSS THE VALVE DP ~ 3o406 PSI DYNAHIC TORQUE TD ~ i4747 ~ LB-IN
t '
4 k I
4
'ALCULATION AT ANGLE ~ +5 DEGAS OCCURZNG AT TIME ~ S. 0 't ABSOLUTE UPSTREAM PRESSURE Pi. ~ 38+7 PSI ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 715e0 DEG ~ R FLOM RATE IN SCFH ~ 5814734+ FT443/HR "VALVE COEFFICIENT CV ~ 11133+9 SPECIFIC GRAVITY 6 ~ ie90b ~ .,
CALCULATED DOMNSTREAM PRESSURE P2 ~ 33 ~ 1 PSI PRESSURE DROP ACCROSS THE VALVE DP ~ 5+581 PSI DYNAMIC TORQUE TD ~ '2428+ LB-XN ATTACHMENT'NSET CYGNA
~~~~40. M~~~~~
CALCULATION AT ANGLE = 3p-'75 DEBS OCCURING AT TXHE ~ 3. 5' ABSOLUTE UPSTREAH PRESSURE Pi ~ 40ii. PSI ABSOLUTE UPSTREAH TEHPERATURE Ti ~ 7i9+0 DEBS R FLOM RATE !N SCFH ~ 4527766+ FT4'43/HR VALVE COEFFICIENT CV ~ 6785+6 SPECIFIC GRA VITY G ~ 1 e 978 CALCULATED DOMNSTREAH PRESSURE P2 ~ 30 ' PSI PRESSURE DROP ACCROSS THE VALVE DP ~ 9 '82 PSI DYNAMIC TORQUE TD ~ i0780 ~ LB-IN W&WW&WWWW ~MM~WMOOMM~O CY.GNA ATTACHN EST p3Q gy ~o.o pe % ~eO SHEET t40. M~~
CALCULATION AT ANGLE ~ 2,2 5 DEG ~ OCCURING AT TIME ~ c}..g SE 0
ABSOLUTE UPSTREAM PRESSURE Pi ~ 4i+4 PSI ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 722o0 DEGAS R FLOW RATE IN SCFH ~ 3i2i673+ FT443/HR VALVE COEFFICIENT CV ~ 3784 ~ 8
,SPECIFIC GRAVITY G ~ 2+037 CALCULATED DOWNSTREAM PRESSURE P2 ~ 25@2 PSI PRESSURE DROP ACCROSS THE VALVE DP ~ i6i f94 PSI
~ DYNAMIC TORQUE TD ~ 80i4o LB-IN
I,I k
Al
CALCULATION AT AHGLE gf Q5'EG OCCURING AT TIME = Q.S .
S ABSOLUTE UPSTREAM PRESSURE Pi 42,6 PSI DEGAS ABSOLUTE UPSTREAM TEMPERATURE Tf ~ 725+0 R FLOM RATE XH SCFH ~ 1608037+ FTff3/HR VALVE COEFFICIENT CV ~ i947o3 SPECXFXC GRAVITY 'G ~ 2 ~ 082
'CALCULATED DOWNSTREAM PRESSURE P2 ~ 26 ' PSX PRESSURE DROP ACCROSS THE VALVE DP ~ 16+054 PSX DYHAMXC TORQUE TD 3972, LB-IH
CALCULATION AT ANGLE ~ 0 DES+ OCCURING AT TIME ~ S 0 SE>
ABSOLUTE'UPSTREAM PRESSURE Pi = 43o6 PSI 0
ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 728 ~ 0 DEGAS R FLOM RATE IN SCFH ~ O. FTt43/HR VALVE COEFFICIENT CV Oeg .
SPECIFIC GRAVITY 6 ~ 2+ii2 o ~ ~~
('
PRESSURE DROP ACCROSS THE VALVE DP ~ Oe000 PSI DYNAHIC TORQUE. TD ~ Oe LB-IN .
k P
I. ~ <<E
/
Valve in full closed os/+ion. An le aG ~ Oo This oc'curs at 5.0 second Upstream pressure = 28.9 +'4.7 ~ 43.6 psia Downstream pressure ~ Atmospheric ~ 14.7 psia, valve fully shut.
downstream is exposed to atmosphere.
Differential pressure b, p 43.6 - 14.7 28.9 psi Plow rate is mero since the valve is fully closed. Therefore the dynamic torque is zero.
Friction torque at the shaft bearing is Tb ~~ (D )(fb d)Ap 8.
(Z~ l9) (a oah)(Z S)(Z8-y) (Ref. 5 )
S ss 9(,P Valve seating torque due to rubber. friction is T8 ~ D2K
(~~id) (2<3 = 2.aovv-c. C~-t.L Ref. 5 )
Net torque TN Tb + T Z2i74 4~- L4
- .Qbm TBSP,, RuSSER. F~TIoN C4BFFTCIENT K, 'WOUGH'6 BTA~~ Pg4N REF' ~ THw yaLua ZS FcR A Dt P qg P<z xmas(H i< ~CwVztC, AHA< THF VALVF - Op gg,9 pal THEMF+RE,
~ VH< VALUE Oi- 7~
ma m. os oeerr a'o.K<~
4 h',IE .*.w. $ ty
~ r 1
I Iiw
4o SAMPLE CALCULATION VALVE SIZE: '3 i Hedium: 5 a.+ u<o.$ ~ Q-earn ~
Valve opening angle of 78 gS degree occurring at 1 5 second Inlet pressure from pressure curve ~ l9.Z +t4 7= psc',o Inlet temperature from temperature curve = p.3g g ggo- C qy 4g.
Note that the higher pressure and temperature are used from the Drywell curves.
o Density from the density curve for air or from steam table for saturated steam o.o8ia LLg/Qa Pull open mme flow rate from flowrate curve ~ 2 074 &0j6 Percentage flow at percentage opening ~ ( M7Q )('~7S)= ~@4 8 8/6 Plow rate in SCFH Qs (t'o 533) )0 SaO(33 q) fi 28$ XI <~h~
aa.(-:tv)
Valve c'oefficient Cv 30 ~ 644 xlo .'V= o.vo 0'70 (aeq.7'pecific gravity 'G o a+8 '
t ~ 048 based on air wiegbt density 0,0766 at. 60oF and 1 atm. pressure.
L Downstream pressure I 2. ( ('..)C q) = ~2.227spsiQ, Therefore presscre drop 6p pl - p> l (70,6 PSi Dynamic torque TD CT Qp Q ~ 2,3i75 CT= 5$ (Ref. 7 elbow effect plus in- Up most adverse shaft orientat-'on and disc rotation)
I'L..'I'.
A w ~
f, t ll
~
~ '. 't- <
~
.41 SAMPLE CALCULATXON VALVE SIZE:
3'0'edium:
S~fv.wa.f~k Q e~
Valve opening angle of G7 5 degree occurring at Z,-o second Inlet pressure from pressure curve ~ 2o.7+14.7= 3~-g Psc'.a Xnlet temperature from temperature curve = z$ 3+ $ go g03 Note that the higher pressure and temperature are used from the Drywell curves.
0 Density from the density cuzve for air or from steam:table for saturated steam o. cd g LIg/ Q 3 Pull open Mume flow rate from flowrate curve ~ . 284 &3(6 Percentage flow at percentage opening ( gnS7 )(o.7S')= Igal g~ fk/6 sao(~s;4)
Plow rate in SCFH Qs = (S.42,])fQ P{>o>~
- c o133
~
x Io0 ~~ l4 9S2.
Valve coeffxcxent
~ ~
CV
'R9 V
2.9 9(?.9
)~
IQ x'4 2077x/o 'j= I~ l (g,gq7 Specific gravity 0 ~ 0 460 m i.fi based on air wieght density 0 0766 l at 60% and atm. pressure.
Downstream pressure I X a, 3s:g ( la C)"- - ) tb RC3(2$ 2')to~ ~~ ~~. - 33 3i )SCL Therefore pressure drop dp - pl - pg ~ 2 ~
0$ )SS Dynamic torque TD ~ CTLp g.3 ~ f.g)00 i,n- L4 CT= I (Ref. 7 elbow effect plus most adverse shaft orientation and disc rotation)
CYGMA AlVACHINES' gy,+~20 ~q SHEET 4O.M +
1 p
t i
nun VALVE . 17t28 SUN 07 NOV 82 . '3~ IMl:q VALVE
%VEAU'Lov4 FOR EACH DATA SET ENTER THK FOLLOWING DATA IH ITS RESPECTIVE ORDER SKPERATKD BY A COMMA OR A BLANKS A) UPSTREAM PRESSURE IN PSIG B) UPSTREAM TEMPERATURE IN DEGi F C) DENSITY IH LB/FT443
')D).
F)
ACTUAl FLOM RATE LOSS COEFFICIENT TORQUE COEFFICIENT IN FT443/SKC ENTER DATA FOR SET NOe. 1 Ti& 221 +0789 2070 +55 0 275 ENTER DATA FOR SET NO ~ 2
!T19i2 234 ~ 0818 1814+& o7 +56 ENTER DATA FOR SET NO+ 3 720+7 243 +085 1561+5 i+i o35 i'ER DATA FOR SET'Oo 4 22+3 249+5 ~ 0886 13iOo6 2o3 oi75 ENTER DATA FOR SET NO+ 5 724 255 +0926 1059+1 5i2 +09 ENTER DATA FOR SET NO+ 6 725+4 259 +0953 797+3 14 +045 ENTER DATA FOR SET NO ~ 7 726+7 262 +0984 533 45 +02 ENTER DATA FOR SET HO ~ 8 727 t9 265 o 1009 267 ' 170 +01 ENTKR DATA FOR SKT NO+
268 +1033 0 9'28+9 Ct.ogpu
~
AT) ACH NEST or.o event e'o.M~M
E INPUT IS AS FOLL6MS!
SET NOi P T RO QA PSI DEG+ F LB/FTt43 FT443/SEC
~
f8oO 221 oO Oe0789 2070+0 0+55 0 '75 f9o2 234 ' 'i08i8 f8f4+8 0+70 0+560 3 20+7 243+0 .'+0850 i56i+5 ~
i+f0 0+350 4K 2213 249i5 '+0886 i3i0.6 2o 30. 0 '75 24+0 255oO Oo0926 1059 ~ i 5+20 Oo090 25' 259oO 0+0953 797+3 f4+00 0 ~ 045 v .26 ' 262+0 Oi0984 533+0 Oi020
--'8 27 ~ 9 265+0 0~
f009'+f033
.Oo0'5+00 267+4 f70 F 00 Oo0i0 r
~
28o9 268i0 CLoSBQ OoO DO YOU O'SH TO MAKE ANY CHANGES?
?NO
I ~
CALCULATION AT ANGLE ~ $0 DEG ~ OCCURING AT TIME ~ I 0 SEC I
ABSOLUTE UPSTREAM PRESSURE Pi ~ 32+7 PSI ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 681+0 DEBS R FLOM RATE IN SCFH ~ i2657823+ FT443/HR VALVE COEFFICIENT CV ~ 34234 ~ 9 SPECIFIC GRAVITY G ~ 1+030
,CALCULATED DOWNSTREAM, PRESSURE P2 ~ 31ii PSI PRESSURE DROP ACCROSS THE VALVE DP ~ i+62i PSI DYNAMIC TORQUE TD ~ i1032o LB-IN ATPACHQEST N.~ O'~q RQ NO ~o..o SHEEZ NO. M~
>>>><<>>>>>>>>>>ao<<>> >><<>><<>><<>>>>>>>>>>>>>><<<<>>>>>>>>>>>>>>>>>><<>>>><<>>>><<<<>>>>a
' CALCULATION AT ANGLE ~ 7 f jg
> DEGAS 'CCURING AT TIME ABSOLUTE UPSTREAM PRESSURE Pi ~ 33+9 PSI ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 694+0 DEGAS R FLOM RATE IN SCFH ~ fi289048 ~ FTf43/HR VALVE COEFFICIENT CV ~ 30346' SPECIFIC GRAVITY G i 068 CALCULATED DOMHSTREAM PRESSURE P2 ~ 32+2 PSI PRKSSURE DROP ACCROSS THE VALVE DP ~ i+673 PSI DYNAMIC TORQUE TD ~ 23175+ LB<<IH
>>>>>> <<<<<<<<>> el ~
4
p I
V h
CALCULATION AT ANGLE ~ Co 7 5 DES'CCURING AT TIME ~ 2 g SEC ABSOLUTE UPSTREAM PRESSURE Pi ~ 35o4 'PSI ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 703 ' DEG ~ R FLOM RATE IN SCFH ~ '1001332bo FT443/HR VALVE COEFFICIENT CV ~ 24207+7
~ SPECIFIC GRAVITY G ~ 1+110 CALCQLATED DOMNSTREAM PRESSURE P2 ~ 33o3 PSI PRESSURE DROP ACCROSS THE VALVE DP ~ 2.095 PSI.
DYNAMIC TORQUE TD ~ 18142+ LB-IN
T )
CALCULATION AT ANGLE ~ 5't'. ZS DEG. OCCURING AT TIME ~ P.f SKC ABSOLUTE UPSTRKAM PRESSURE Pi ~ '7o0 PSI ABSOLUTE UPSTREAM TKMPKRATURK Ti 709o5 DEGo R FLOM RATE IN SCFH ~ 8703782+ FT443/HR VALVE COEFFICIENT CV ~ 16741 i 2 SPECIFIC GRAVITY G ~ 1 ~ 157 CALCULATED DOWNSTREAM PRESSURE P2 ~ 33+6 PSI
~ ~ PRESSURE DROP ACCROSS THE VALVE DP ~ 3o387 PSI DYNAMIC TG ~ UE TD ~ 14668+ LB-IN
~, /
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1
CALCULATION AT ANGLE ~ +g DEGAS OCCURXNG AT TIME ~ '3. O'EC ABSOLUTE UPSTREAM PRESSURE Pi ~ 38+7 PSI ABSOLUTE UPSTREAM TEMPERATURE Tf ~ 7i5e0 DEB ~ R FLOW RATE XN SCFH ~ 7300124'T443/HR VALVE COEFFICIENT CV ~ f f f33+ 9 SPECIFIC GRAVITY 6 ~ 1+209 CALCULATED DOMNSTREAM PRESSURE P2 ~ 33+ f PSI PRESSURE DROP ACCROSS THE VALVE DP ~ 5+579 PSI DYNAMIC TORQUE TD ~ f2424 'B-IN CYCNA ATTACHNESY
'I 1
I J
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4' I 'I
4q
&W~OHO&w~W~WWM~~&OO&WOWWWOOW&MMWW&wWWW~&WW&WW~M&WWW~&WW&woO
~ ~
CALCULATION AT ANGLE ~ 3'3 )5 DEGAS OCCURING AT TIME ~ --5'EC ABSOLUTE UPSTREAM PRESSURE Pi = 40oi PSZ ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 7i9+0 DEGo R FLOM RATE IN SCFH ~ 5662727 'T443/HR
'ALVE COEFFICIENT CV ~ 6785+6 GRAVITY G ~ io244 'SPECIFIC CALCULATED DOMNSTRPAM PRESSURE P2 ~ 30i6 PSI PRESSURE DROP ACCROSS THE VALVE DP ~ 9+502 PSX DYNAMIC TORQUE TD ~ i0580 ~ LB-IN k
0 D I 1"
CALCULATION AT ANGLE ~ ~2..5'EGAS OCCURING AT TIME ~ + 0 SEC
~
~
ABSOLUTE 'UPSTREAM PRESSURE Pi ~ 4i o4. PSI ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 722+0 DEGAS R FLOM-RATE IN SCFH ~ 389205i FT443/HR VALVE COEFFICIENT CV ~ 3784+ 8 r
SPECIFIC GRAVITY G ~ i+285 '
CALCULATED DOMNSTREAM PRESSURE P2 ~ 25ob PSI PRESSURE DROP ACCROSS THE VALVE DP ~ 15+780 PSI DYNAMIC TORQUE TD ~ 7809 ~ LB-IN
II
~ '
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0 CALCULATION AT ANGLE ( I- < 5 DEG OCCURING AT TIME 4' SEC ABSOLUTE UPSTREAM PRESSURE Pf ~ 42@6 PSI ABSOLUTE UPSTREAM TEMPERATURE Tl ~ 725i0 . DEBS R FLOM RATE IN,SCFH ~ 2000880 'T443/HR VALVE COEFFICIENT CV ~ 1947+3 SPECIFIC GRAVITY G ~ 1 ~ 317 CALCULATED DOMNSTREAM PRESSURE P2 ~ 27+0 PSI .
PRESSURE DROP ACCROSS THE VAI VE DP ~ f5 ~ 628 PSI DYNAMIC TORQUE TD ~, 3867'o LB-IN e
AliACHNES'F
(y ~
t A
A'
~ ~ f
~ i~
CALCULATION AT ANGLE ~ O-O DEBS OCCURING AT TIME ~ 5og SEC ABSOLUTE UPSTREAM PRESSURE Pi ~ 43o6 PSI ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 728+0 DES' FLOM RATE IN SCFH ~ 0. FT443/HR VALVE COEFFICIENT CV ~ 0 0
~
SPECIFIC GRAVITY G ~ ii349 PRESSURE DROP ACCROSS THE VALVE DP ~ Oo000 PSI DYNAMIC TORQUE TD ~ 0. LB-IN
~MTXAC 7oRAUt: lf'AWE's, fQoa g lv fgc,p gq CYGNA ATTACHMENT'),Q~PO~q SHKFt 4O.L ~
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SAMPLB CALCULATXON VALVE SIZE Inch Hedium: Aza.
Valve opening angle of 78.'?5'egree occurring at second Inlet pressure from pressure curve ~ 1'l ~ 2. +l4'7= Q'3 ~ Q )5C,Ow Inlet temperature from temperature curve = 2~4 p +go
~
Note that the higher pressure and temperature are used from the Drywell
~
curves.
Density from the density curve for air or from steam table for saturated steam ~ o.Iaaf LIg/ 6 ft I, Full open uiLume flow rate from flowrate curve = I 3 ~ '
+6(6 Percentage flow at percentage opening'. { Icl>> ){'$7S)= 896 < Sd(S Flow rate in sao (R3.p)
SCFB Qe (1.333)Io l<.p (Ggq) " g ' 6>F3ggIolo y6+(hr-Valve coefficient C IC,
~o~e Ig Jas III0 'I = c.vo {866.7.
Specific gravity G ~ O'I>>< ~ I 7S based on air wieght density 0.0766 at 60oP and 1 atm. pressure.
Downstream pressure I 33.) (-'-.=.;) to~
9C$ ( J$ .9e5 ) tO~ ~ ' 3~'~ f pgIQL Therefore pressure drop A,p - pl - p = 1.7I6 psi.
I DynamictorqueTD CThp g ~ iij'q2, CT= 5L',(Ref. 7 elbow effect plus in- U most adverse shaft orientation and disc rotation)
~
ATiACHNEM'
b k
h F
1 f"
'I a
SAMPLE CALCULATION
'ALVE SIZE: Inch Medium: Axe.
Valve opening angle of gg.Q,5 degree occurring at second e
Inlet
~
pressure from pressure curve = 2.Z 3 +l4'7= ~7 Psc'e .
Inlet temperature from temperature curve =2.gq.g+ +g,o 7gg,5 Note that the higher pressure and temperature are used from the Drywell curves.
4 Density from the density curve for air or from steam table for saturated steam o, IcIo5 LLg/ 6 ft pull open uiLume i'low 'rate from flowrate curve = Iog> '>(6 percentage flow at percentage opening'. ( I egg. )(o.CCC+ C 61.S gk(S Plow rate in SCPH Qa (I RCy) IO S~o( S7 )
~g~(> >)
= ~ XO 4. OCCAM.7 Valve coefficientC. 29 9m 2.9e[ 2.l) 'Io.qt IS Xlo 'V= 2'3
~ '
Specific gravity G o'l0cg ~ I.SSII based on air wieght density 0 0766 at. 60 F and 1 atm. pressure.
Downstream pressure IL 20 s7
~ 33I5IQ )$ QQ, Therefore prescore drop ap - pl - p2 3 4SB -
$ 5c, Dynamic torque TD CT 5p Q '7/2'7 CT= l7S(Ref. 7 elbow effect plus in- L4 most adverse shaft orientation and disc rotation)
S I
n I'II
'I e
I ~
I I
I I ~ . t
f7539 'UN 07 NOU 82 g $ XMCH. VALVC AIR. FLt.Q
~ ENTER THE NUMBER OF DATA SETS
'F9 ~
FOR EACH DATA SET ENTER THE FOLLOWING DATA IH ITS RESPECTIUE ORDER SEPERATED BY A,COMMA OR A BLANK A) UPSTREAM PRESSURE IN PSIG
~
B) UPSTREAM TEMPERATURE IH DEG ~ F C) DENSITY IN LB/FT443')
ACTUAL FLOW RATE IH FT443/SEC E) LOSS COEFFICIENT F) TORQUE COEFFICIENT ENTER DATA FOR SET HOo 1
?18 221 o1295 1015o6 'o55 'o275 ENTER
'F19o2 DATA'OR SET NO 234 oi325 899o5 o7 o56 ENTER DATA FOR SET HOo 3
?20o7 243 ~ 1359. 776o6 ioi o35 c.HTER DATA FOR SET NO ~ 4
?22o3'49o5 of405 657 ' 2o3 ~ 175 ENTER DATA FOR SET NOo 5
?24 255 o 146 530o6, 5o2 o09 ENTER DATA FOR SET Na. 6
?25o4 259 oi515 40io3 14 o045 ENTER DATA FOR SET HO ~ 7
?26o7 262 oi56 268 ' 45 o02 ENTER DATA FOR SET NOo 8
?27 9 265 ~ 1595 135 6 170 01 ENTER DATA FOR SET NO ~ 9
?28 o 9 268 o 1618 0 CLc 1ED
I A 1'p H I
4 >: t
~
'l V d
HE INPUT IS AS FOLLOWS+
/
SET NOi P T RO QA PSI DEGAS F LB/FT443 FT443/SEC 18oo 221 so 0+1295 1015+6 0+55 0+275 19+2 1
234oo 0 '325 899o5 0 '0 Oi560 3 20o7 243oo 0+1359 776ob idio 0 '50 22 0 3 249+5 0+1405 '57+5 2o30 Ooi75 5 24 ' 255oo Oii460 530+6 5+20 0 '90 25o4 259oo Ooi515 401 o3 14 F 00 0 '45 2bi7 262+ 0 0+1560 268 ' 45+00
'+020'765+0 0+1595 135+6 u'0 OO 0 ~ 010 28+ 9'68oo 0+1618 Dao CLC)SOD 0+0 90 YOU Mt ISH TO HAKE ANY CHANGES?
?NO
S N
h k
~ II W
57 CALCULATION AT ANGLE ~ QQ DEG>> OCCURING AT TIME ).Q SEC ABSOLUTE UPSTREAM PRESSURE Pi = 32>>7 PSI ABSOLUTE UPSTREAM TEMPERATURE T1 681 0 DEBS R FLOI4 RATE IN SCFH ~ 6210283>> FT043/HR VALVE COEFFICIENT CV = .21327>>8 SPECIFIC GRAVITY G u 1 ~ 691 CALCULATED DOMNSTREAM PRESSURE P2 ~ 31 ' PSI PRESSURE DROP ACCROSS THE VALVE DP 1 651 PSI DYNAMIC TORQUE 'TD ~ 5525>> LB-IN
4 Jl t f V II lf p
tt 4 P
k
<<<<~<<<<<<<<M<<<<<<<<<< <<<<<<<<<<~<<<<<<<<~<<<<~~<<O CALCULATIOH AT ANGLE ~ 7$ .7.g DEG ~ OCCURING AT TIME = I S SEC ABSOLUTE UPSTREAM PRESSURE Pi ~ 33+9 PSI ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 694o0 DEGAS R FLOW RATE IH SCFH ~ 5595381+'T443/HR VALVE COEFFICIENT CV 18905 0 SPECIFIC GRAVITY G m ii730, ~
CALCULATED DOMNSTREAM PRESSURE P2 ~ 32 ~ 2 PSI PRESSURE DROP ACCROSS THE VALVE DP = 1+716 PSI DYNAMIC TORQUE 'TD ~'1692+ LB-IH 0
~ ~
CYGNA ATTACHatEM'gg~.
0 .o~
esaav r o )~~~
A r ~ 0 a 1 lr ~
tt '1 V
~ ~
CALCULATION AT ANGLE ~ Q7 5 BEGS OCCURING AT TIME ~ 2'EC ABSOLUTE UPSTREAM PRESSURE. Pi ~ 35 4 PSI
~
ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 703 ' DEGAS R FLOM RATE IN SCFH ~ 4980051 'T443/HR .
VALVE COEFFICIENT CV ~ i5081 i 0 SPECIFIC GRAVITY G ~ 1+774 CALCULATED DOWNSTREAM PRESSURE P2 ~ 33+3 PSI PRESSURE DROP ACCROSS THE VALVE DP ~ 2oi36 PSI DYNAMIC TORQUE TD ~ 9095+ LB IN CYGNA AMiACHNKST Fgg gy, OT.
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l c."
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K 1
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CALCULATION AT ANGLE ~ Pa.'Lg DEGo OCCURING AT TINE ~ 2 ~ SEC ABSOLUTE UPSTREAH PRESSURE I
Pi ~ 37@0 'SI ~
ABSOLUTE UPSTREAM TEHPERATURE Ti ~ 709+5 DEGAS R FLOM RATE IN SCFH ~ 436650f FT443/HR VALVE COEFFICIENT CV ~ f0429' 5 SPECIFIC GRAVITY G i+834 CALCULATED DOMNSTREAM PRESSURE P2 = 33 ' PSI PRESSURE DROP ACCROSS THE VALVE DP 3 488 PSI DYNAHIC TORQUE TD ~ 7428'B-IH
~ ~
CYCNA Al i ACHNES'f
I CALCULATION AT ANGLE = QS DEGAS OCCURING AT TIME ~ Si 0 SEC
, ABSOLUTE UPSTREAM PRESSURE Pi ~ 38+7 PSI DEGAS ABSOLUTE UPSTREAM TEMPERATURE T1 ~ 715+0 R FLQM RATE IN SCFH = 3657300 FTI43/HR VALVE COEFFICIENT CV ~ 6936+3 SPECIFIC GRAVITY G ~ 1 ~ 906 CALCULATED DOMNSTREAM PRESSURE P2 ~ 33+0 PSI r
PRESSURE DROP ACCROSS THE VALVE DP ~ 5+698 PSX DYNAMIC TORQUE TD ~ 6239 'B-IN
0 h I HI t
t~
I 1
h s s ' q o>
) ~ ~ ~
CALCULATION AT ANGLE ~ 33.")S DEGAS OCCURING AT TIME ~ ~'~ SEC ABSOLUTE UPSTREAM PRESSURE Pi ~ 40+ i PSZ ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 7i9o0 DEBS R FLOW RATE XN SCFH ~ 2850i85o FT443/HR VALVE COEFFICIENT CV ~ 4227+3
~
)
SPECIFIC GRAVITY G ~ I.+978 CALCULATED DOWNSTREAM PRESSURE P2 ~ 30+2 PSI PRESSURE DROP ACCROSS THE VALVE DP ~ 9 'i8 . PSZ DYNAMIC TORQUE TD = 5430 LB-ZN AliACHNESY
0 a Q, It J P
II II I
W
CALCULATION AT -ANGLE ~ 22, b DEB+ OCCURING AT TIME ~ $ O SEC ABSOLUTE UPSTREAM PRESSURE Pi ~ 4ii4 PSI ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 722+0 DEBS R FLOM RATE IN SCFH ~ f963550 i FT443/HR VALVE COEFFICIENT CV ~ 2357+9 I
SPECIFIC GRAVITY ' ~ 2+037 CALCULATED DOWNSTREAM PRESSURE P2 ~ 24i8 PSI PRESSURE DROP ACCROSS THE VALVE DP ~ 16 ~ 613 PSI DYNAMIC TORQUE . TD = 4043m LB-IN
CALCULATIOM AT ANGLE ll'0 5 DEG OCCURIHG AT TIME ~ 4'~ SEC J
ABSOLUTE UPSTREAM PRESSURE Pi ~ 42 ~ 6, PSX ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 725@0 DEG ~ R FLOM RATE IH SCFH ~ i014658o FT443/HR VALVE COEFFICIEHT CV ~ i2i3o i
(
SPECIFXC GRAVITY G m 2+082 C
CALCULATED DOWNSTREAM PRESSURE P2 ~ 26+0 PSX PRESSURE DROP ACCROSS THE'VALVE DP ~ i'0i PSI DYHAMIC TORQUE . TD ~ 2020+ LB-IH .
AliACHINES'
Pt Met OP W w WW CALCULATION AT ANGLE ~ DEBS OCCURING AT TIME = 5 O SEC
'ABSOLUTE UPSTREAM PRESSURE Pi ~ . 43+6 PSI ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 728+0 DEGAS R FLOW RATE IN SCFH ~ Oo FT443/HR
~ ~
VALVE COEFFICIENT CV ~ 0 0 SPECIFIC GRAVITY G m 2 ii2 PRESSURE DROP ACCROSS THE VALVE DP ~ 0 F 000 PSI 0
DYNAMIC TORQUE TD ~' ~ .LB-IN
1w
/
4 I
~ ~
'alve in full closed os~4ion. An le aG 0o This occurs at 5.0 second Upstream pressure = 28.9 + 14.7 ~ 43.6 psia Downstream pressure ~ Atmospheric ~ 14.7 psia, valve fully shut downstream is exposed to atmosphere.
Differential pressure b, p ~ 43.6 -.14.7 ~'8.9 psi PLow rate is zero since the valve is fully closed. Therefore the dynamic . torque is zero.
Priction torque at the shaft bearing is Tb ~ (D2) (fb d) <p 8;
(q-3) (o oofI)(Z aS)f.aS 8) .'Ref. 5 )
in-lb Valve seating torque due to tubbes fniction is Ts ~ D2E Qtef. '5 )
Net torque TN Tb + Ts 138o8 ~n 4
SAMPLE CALCULATION VALVE SIZE Inch Medium: 8 ak uvo+~ Sf+a.w Valve opening angle of pg.7g degree occurring at ~ < second Inlet pressure from pressure curve = lg 2. +t4 7=
~ 9 ~
Inlet temperature from temperature curve = g.gg g +g,o that the higher pressure and temperature are used from the Dxywell.
curves.
4 saturated steam o.a sis '.Iy/g Density from the density curve for air or from steam table 9
for Pull open Wume flow rate from flowrate curve I7-'92 .
+2/6 7'ote percentage flow at percentage opening' ( I<92 )'t >>93" -I>>'S St/S rata in s~o (~~.y) -
Plow SCFS Qs (9 oaIs) Io fg.g (gqq ) V.oI>2IIIa gg he/
Valve coefficient'v 29.93> 29 9[ 21 ) Is.qai BIO S 0 70 Q6$
v faro Specific gravity'G o alI& ~ 'l 0483 based on air wieght density 0.0766 at 60P and 1 atm. pressure.
Downstream pressure I - q~,~ ( 7 o2.~z) to,
)'ag(
5 ~<<~~)C~99) = 3'>28 Psio, A
Therefore pressure drop ap '- pl - pg ~ I 76g, f76c, Dynamic toraue TD CT 5p > 3 ~ ll 394 CT= &(Ref. 7 elbow effect plus in- U most adverse shaft orientation and disc rotation)
ATTACHMENT'f CYGNA
~
SHEET lK),+~POP q gg.~o. o~=
t40.M+ ~
0 I ~
~ ~
SAMPLE CALCULATION VALVE SIZE: 2Q.. Inch Medium:
Valve opening angle of 22 S degree occurring at 4 second Inlet pressure from pressure curve ~ 2G"F +t4 7= $ i 4 k>co Inlet temperature from temperature curve' gG~ ~ gg,o-Note that the higher pressure and temperature are used from the Drywell curves.
4 Density from the density curve for air or from steam table for Saturated Steam c.c9Sd LLy/ fta Pull open 'atume flow rate from flowrate curve ~ 1'325 2 ~
'>/6
..Percentage flow at percentage opening ( '>26 2 3(c 26)- 382 os H'/6
=,
SRo (-li.4)
Plow rate in scFH Qs (f.i'Istr) [o4 -= 024gxio~
~g,~ ( 7>>)
2 ~
7 Xlb H, Valve coefficient 9n 269(2.1 ) 2.>5'79r(a '
Gv XS'9 6 c'4.7.
~S J specific gravity ~ o969 air density i.2893 based on lwieght G O 0 ~ 0766 at 60oP and atm. pressure.
I
--Downstream pressure I~ -.
=. 4s.q- ( > 4"-47) to QQ3 (2 3 Q7Q) (o$ (~ -'t3( 72 ) = 25' 42. pgiL Therefore pressure drop h,p pl - p2 0 ig 9S Dynamic toroue TD = CTLp > ~ 3844 CT= 02,(Ref. 7 elbow effect plus in- US most adverse shaft orientation and disc rotation)
%%A " e ~
CYGNA ATFACHNIEW,d~2o RLf NOo~LF SHKEZ fgo. M~+
e RUH WLVE ~
17;54 SUH 07 HOy 82 2.cf > hJCB V"~~t=
Pt.oW EHTER THE NUMBER OF DATA SETS FOR EACH DATA SET ENTER THE FOLLOWIHG DATA IN ITS RESPECTIVE ORDER SEPERATED BY A COMMA OR A BLAHKo A) UPSTREAM PRESSURE IH PSIG B) UPSTREAM TEMPERATURE IH DEGo F C) DENSITY IN LB/FT443 D) ACTUAL FLOW RATE IN FT443/SEC ')
LOSS COEFFICIENT F) TORQUE COEFFICIENT EHTER DATA FOR SET NOo 1
+f8 X 221 0789 1289 6 o55 '275 ENTER DATA FOR SET'Oo 2 T19o2 234 ~ 0818 ii30 ~ 5 o7 o56 ENTER DATA FOR SET NOo 3
?20o7 243 o085 972o8 ioi o35 ER DATA FOR SET HOo
?22o3 249o5 ~ 0886 816o5 2' oi75 ENTER DATA FOR SET NO ~ 5
?24 255 o0926 659 ' 5o2 'o09 ENTER DATA FOR SET HOo 6
?25o4 259 ~ 0953 496o7 14 o045 ENTER DATA FOR SET NOo 7
?26o7 262 ~ 0984 332oi 45 o02
=HTER DATA FOR SET NOo 8
~27o9 265 o1009 166o6 170 ~ Oi o
~~~~NTER DATA FOR SET NOo 9~~~~
'28o9 268,. o 1033 . 0 CYGNA
'AVVACHN8$}V
INPUT IS AS FOLLOWS'ET NO ~ P T ~ RO QA CT PSI BEGS F LB/FT443 FT443/SEC
,~
18+0 221+0 Oi0789 1289+6 Oo55 i 0 275 19+2 234+0 Oo0818 1130+ 5 0 '0 0 '60 20+7 243+0 0 '850 972o8 idio 0+350 4 22o3 249 ' Oo0886 816o5 2+30 0.175 24io 255+0 Oo0926 659+8 5+20 0+090 6 25+4 259io Oi0953 496+7 14+00 0+045
~ .. 26+7 262+0 0+0984 332+1 45ooo 0+020 27+9 265+ 0 0 '009 166 ~ 6 170+00 0+010 28+9 268 ' 0+1033 Ooo CLaSM O.O i
DO YOU W:.ISH TO MAKE ANY CHANGESV TNO
l V P
~4 %MMOOMWM R
CALCULATION AT ANGLE ~ DES'CCURXNG AT TIME ~ 1 b, SEC ABSOLUTE UPSTREAM PRESSURE Pi ~ 32+7 PSX ABSOLUTE UPSTREAM TEMPERATURE Ti 68i 0 DEG R
~
FLOW RATE XN SCFH ~ 7885763+ FT443/HR VALVE COEFFXCXENT CV ~ 2i327+8 SPECIFXC GRAVITY G = 1 +030
)
CALCULATED DOMNSTREAM PRESSURE P2 ~ 3iof PSX I
PRESSURE DROP ACCROSS THE VALVE DP ~ 'o62i PSI DYNAMIC TORQUE TD ~ 542So LB-IN
CALCULATION'AT ANGLE ~ QP-7y DEGAS OCCURING AT TIME ~
ABSOLUTE UPSTREAM PRESSURE Pi ~ 33+9 PSI ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 694+0 DEGAS R I
FLOM RATE IN SCFH ~ 7032328'T443/HR
'ALVE COEFFICIENT CV ~ i8905o0 SPECIFIC GRAVITY G ~ 1+068
~
~
CALCULATED DOMNSTREAM PRESSURE P2 ~ 32+2 PSI PRESSURE DROP ACCROSS THE VALVE DP ~ i'72 PSI DYNAMIC TORQUE TD ~ i 1394 e LB-IN
73
~
CALCULATION AT ANGLE ~ 67 S'EGo OCCURING AT'IME ~ Q~O 0
0 ABSOLUTE UPSTREAM PRESSURE Pi ~ 35+4 PSI
/
ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 703+0 4
FLOM RATE IN SCFH ~ 6238209+ FTlt3/HR VALVE COEFFICIENT CV ~ 15081o0 SPECIFIC GRAVITY G ~ 1 110 CALCULATED DOWNSTREAM PRESSURE P2 ~. 33+3 . PSI m
PRESSURE DROP ACCROSS THE VALVE DP ~ 2+095 PSI DYNAMIC TORQUE . TD. ~ 8921 ~ LB-IN 1AWI 4 ~ w CYGNA ATFACHNKSY
1
~ J
'ALCULATIONAT ANGLE ~ SC,.~g DEG ~ OCCURING AT TIME ~ 2'5' SEC
~
~
~\
~
ABSOLUTK UPSTREAM PRESSURE Pi ~ 37+0 PSI
~
ABSOLUTE UPSTREAM TEMPERATURE Ti ~ '709+5 DEBS R FLOW RATE IN SCFH ~ 5422430'T443/HR VALVE COEFFICIENT CV ~ i0429+5 SPECIFIC GRAVITY G ~ ioi57 CALCULATED DOMNSTRKAM PRESSURE P2 33.6 PSI PRESSURE DROP ACCROSS THE VALUE DP = .3 '88 PSI
. DYNAMIC TORQUE TD ~ 72i3o LB-IN V ~ ~
CYGNA ATFACHMNiY Ng,+~doge
~gy ~O.O SHEET 4O.M~~
C o ~
~ r MWWWMMMMMMMaO~M~MWW~M~~WMWM~M CALCULATION AT ANGLE ~ +3 DEGAS OCCURING AT TIME ~ >.a SEC ABSOLUTE UPSTREAM PRESSURE Pf ~ 3So7 'SI ABSOLUTE UPSTREAM .TEMPERATURE Tf ~ 7f 5+0 DEGAS R FLQM RATE IN SCFH ~ =
4547844m FT443/HR VALVE COEFFICIENT CV ~ 6936+3
\
SPECIFIC GRAVITY G. ~ f +209 CALCULATED DOMNSTREAM PRESSURE P2 = 33+1 PSI
~e PRESSURE DROP ACCROSS THE VALVE DP ~ 5+579 PSI
. DYNAMIC TOROUK TD 6109. LB-IN
CALCULATION AT ANGLE ~ 75 DEGAS'CCURING AT TIME ~ 3 ~ 5 ~
SEC ABSOLUTE UPSTREAM PRESSURE Pi ~ 40+ 1 PSI ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 7f9o0 DES+ R I
'FLOM RATE IN SCFH ~ 3527751+ FT443/HR VALVE COEFFICIENT CV ~ 4227' SPECIFIC GRAVITY G ~ i 244 o
. CALCULATED DOMNSTREAM PRESSURE P2 ~ 30+ b PSI PRESSURE DROP ACCROSS THE VALVE DP ~ 9+502 PSI DYNAMIC TORQUE TD ~ 5202m LB-IN
~ 1
~ ~
ATVACHNKSV
~
W ~& ~
WW OO W WW W W ~ ~ ~
W aO WW W &w40 CALCULATXON AT. ANGLE ~ 22. $6 DEG ~ OCCURXNG AT TIME ~ +' SEC ABSOLUTE. UPSTREAM PRESSURE Pi ~ 41 ~ 4 PSI ABSOLUTE UPSTREAM TEMPERATURE Ti 722 0 DEG R It FLOW RATE XN SCFH ~ 2425048+ FT443/HR VALVE COEFFICIENT CV ~ 2357i9 SPECXFXC GRAVXTY G ~ 1+285 CALCULATED DOMNSTREAM PRESSURE P2 ~ 25+6 PSX
/
PRESSURE DROP ACCROSS THE VALVE DP ~ i5o787 PSX
. DYNAMIC TORQUE TD 3842 LB-IN ATVACHMCSY
.CALCULATION AT ANGLE ~ Ili?-5 DEG'i QCCURING AT TIME ~ + $" SEC ABSOLUTE UPSTREAM PRESSURE Pi ~ 42 ~ 6 PSI ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 725+0 DEGAS R FLOW RATE IN SCFH ~ 1246622+ FT443/HR VALVE COEFFICIENT CV ~ 1213+1 SPECIFIC GRAVITY G ~ 1 +317 CALCOLATED DOWNSTREAM PRESSURE P2 ~ 27+0 PSI PRESSURE DROP ACCROSS THE VALVE DP ~ 15 o 631 PSI DYNAMIC TORQUE 7D .~ f902+ LB-IN
DEGAS CALCULATION AT ANGLE ~ 5 OCCURING AT TIME .~ 5 0 SEC
~
ABSOLUTE UPSTREAM PRESSURE Pi ~ 43ob PSI.
ABSOLUTE UPSTREAM TEMPERATURE Ti ~ 728 ' DEGAS R FLOW RATE IN SCFH ~ 0 FT443/HR VALVE COEFFICIENT CV = o O ll SPECIFIC GRAVITY 6 ~ ' e349 PRESSURE DROP ACCROSS THE VALVE DP 0 000 PSI DYNAMIC TORQUE TD ~ Oo LB-IN
~
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DESIGN AND SZXSHXC ANALYSIS ATTACHQKNY OP 24>> CYLINDER OPEMTZD BUTTERFLY VALVE FOR
~ xo.2~4~'t:
pgg ttO ~OOI .F.
QASHXNCTON PUBLXC POHKL SUPPLY SY AND Itin WO.G ~
BURNS AND ROE
~ e CUSTOMER P,O 68 SXr Saa aV MM-a-aias."'23 6-1-08 0 8
~ ~
p B S REPORT'NO TR 74 7 PN27235-L H27236-L ~
are 4
'3 PREPARED BY NcPHZRSON ASSCCXATZS< RfC~
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APPROVED BY
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4
DESIEf AND SEISMIC ANALYSIS OF 24~ CYLINDER OPERATED BUTTERFLY VALVE A-20676S 22 February 1974 Prepared Foz:
BIF NA A Unit OC t enezal Signal Corporation ATTAC
.ot.F Prepared By: 0 Thomas M. Riley John R. Henry
(<
A Unit a8 GeneraX 888np Ca+%ration Pnraheee,arier~N ~488-53 M he -son'~~elates, Inc.
oQrc ,a 'TR-.74-T-nna t aleile<
. McPhezson Associates, Inc.
400 Totten Pond Road 1faltham, Massachusetts 02154 wPfaaa aeon't~4arteaes 400 TOTTB4 PQNO ROAO ~ WAI.THAM,MASSACHLISKTTS021&
DESIGN AND SEISMIC ANALYSZS OF 24~ CYLINDER OPERATED BUTTERFLY VALVE A-206765 ATTACHSIENT Purchase BZF h Uait of general Signal'oryoratkon';
Order No. 84908-63 .
~ xo.M>KKD
~LLNy,~O ~ ol.F maat aaQ=~
(~i
.>x,iyqq v NcPherson As'socrates, Znc.
Repart 'Ãa. TR-74 RRV- 4 ~cJs~ J~s' FOR 24" VALVES BIF Contract No. BIF S.O. No. VaIve Ta 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
REVISlOH RECORD NUS REPORT TR 74 RKVlS!ON 1 12131l75 Page 3 a) Hat'1 was AS' 126 0 A 4&
b) Al la<able Stress Value corrected Page 5 a) Qrfve Levei was 8-1840054 b) Clevis was D-'46578 Page 9 a) b)
Hat'1 was ASTN A 126, Class C Corrected yield stress allowab e 0
c) Deleted AS'-48 Page 32 . a) Ref'. drawings were - 40054 4 D-l 57&
~ ~ 'v'ages 33, 35, 36 e 37 a) Mat'1 wa~H A-l2&
b) Corre 6uf'Stress'Qrkab> li
~ g
~ ~
TABLE OF CONTKlTS Section No. ~Pa e
~~~~~~Table of Contents Certification 1.0 Introductioa~~~~~~
~ ~
2.0 Summary of Results .
Conclusions 4.0 Refereaces .
~~4 Dc cv+4w~ tl~aa 6.0 Analysis 6.1. Cylinder Operator,semb 6 2 Cyliader Suypart EracR 23
~~
~ ~ '
~ $
Clevis Assembly an C ~ ~
Drive Lever
~ ~
6~4 Valve Body Support "Ears" and Associated 38 Hardware ~ ~
6.$ Shaft and Disc Assembly and 'Associated ' ~ 46 Hardware
~ ~
6 ' Valve Sizing and Stress Analysis Considering .
Combined Operating and Seismic Coad'tions
~ ~ ~ ~ ~ ~ op o<<
~ ~ eeooo Certification NcPherson Associates, Xnc. certifies that the 24" Butterfly Valve, A-206765, as shown on the customer drawings was
~
analyred in iccordance with 1fashington Public Power Supply System Specification No. Z808-68 and to the best, of our knowledge and belief, meets the requirements of Paragraphs 3.2 ~ $ .$ , and S.S ~ 2.4 of this document and Reference S of CYGMA ATTACHSIENT Section 4.0 of this report. ms eo. 'R~'5; 0 nLI w ~ooI.
waar ao.8=M 4 'crfA Jaha R./Lunary~~
f Q Reg'ii tered'Pro essional Engineer
~Mass;.. RegiaSiation No. 259Z9
~ ~ ~
J I
I,
~ 0
~ I~
Section 1.0 BiTRODUCTZON The purpose of this report is to determine the structural of a.24".Sutterfly Valve Assembly when subjected 'dequacy to seismic accelerations as described in Reference '1 and to insure the valve design is in accordance with Reference'f this report e ATTACHINKNT 405 No JH@,K The seismic plus operating analysis Is performed 'in accord- pasmo ~O oI. ~
e ante with Washington Public Pewet Supply System ~eeeiH,sa- OHKET NO.Q tion No. 2808-68, Reference 1, and all c applicable InfoTmation
~~~~~~as described in Section 4e0 of thi~ eport..~~~~~~
~ 5 ~ohio ~ ~ 0 0 0
~ ' ATTACHMENT Section 2.0
'HINARY OF RESULTS 0
~0 0
~0
~ ~
~g .J ~ ~
~ ~
~ ~ 00 ~ ~0 0
~ 0 0~0 00 ~ ~
WO AO 0( ~
~~~~~~sr~+~ aava~'<<24. sumacr 0~~~~~~
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~ 4 Section 3~0 ~ oo ~ oe CONCLUSIONS NcPherson Associates, Inc. concludes that all components for the 24" Butterfly Valve, as analyzed in this report, meet the requirements'of all governing specifications for seismic and operating considerations as defined in References lp and 3 of this report..
CYGMA ATTACHlNKNT
'I Section 4.0 REPERENCES
~~~~~~l. Washington Public Power Supply System 2808-68 ~~~~~~~
~~~~~~Specification No.~~~~~~
~~~~~~2. MF Drawings Drawin No. Revisien~~~~~~
. A(-206765 B . 24" Butterfly Valve-General A-900523 A-900524
~
. - 'ody, Arrangements Pabricated Body, fachining
.f ATTACHMENT A-900339
. - Disc, Fabricated~ .
A-900340 Disc, echined A-208293
~ -
.. Cylinder Support'racket
'perater B 000-522,B 000-522 Shaft c9' zl@~ Drive Lever Cb' ~~yg t Cldris P-206661 Miller glinfen
$. Section XEI, Nuclear Power Plant Components, ASME Boiler and Pressure Vessels Code, 1971 vitIf..Addenda.
~~~~~~4. 'irgil Noring Paires, Design of Edition The 0 i~face fillan I CO ~~~~~~~
54ac3Qne Ne Ye 'B 1965 ~
Elements, 4th
~~ \
d ~ ~
S. Raymond J'. Roark,. Pormu aa. or Stress and Strain, 4th Edition, McGraw Hill Book Co., 1965.
0' ~ ad
~ ~ e 2
~~~~~~6. Laddish Catalog No. SS.~~~~~~
d
~ ~ ~~ ~~ ~ ~
~~~~~~7. Grinnel, Piping and Engineering, 3rd Edition, 19'Zl.~~~~~~
~~~~~~8. 1963 Supplement to Screw Thread Standards for Federal Sezvices s~~~~~~
~~~~~~9. Baumeister 4 Marks, Standard Handbook for Mechanical Engineers, 7th Edition, bfcGxaw HilL Book 'Company.~~~~~~
~~~~~~s'0 ~ . Kent, 'Mechanical Engineers Handbook.~~~~~~
~~~~~~11. A.S.T.N. Standards - Part 2.~~~~~~
~~~~~~12. -A.S.M. Metals Handbook.~~~~~~
~~~~~~Timoshenko'nd Goodier, Theory of Elasticity, 3rd Edition, McGrav Hill Book Co., 1970.~~~~~~
14. Seely and Smith, Advanced:fechanics of Materials, 2nd Edition, John Riley 4 Son, Enc., 1966. cvaNA ATTACHlNENT NacHinery's Handbook, 17th Edition, The Xndustr9.al Press, 1964. ~ ~
Seatiaa VIIX Pv'assert Vessels Oivisiah t~tettative Rules, A.S.M.E. Boiler and Pressure Vessel Code, 1971,.
~
~~cecal Rubbers tahar,shing Co., ~ Standard Eiathematics Tables, Teel"th Edition.
18 ~ lfational Standard
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4.1 CONCLUSION

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