ML20024C146
| ML20024C146 | |
| Person / Time | |
|---|---|
| Site: | Columbia  |
| Issue date: | 06/30/1983 |
| From: | WASHINGTON PUBLIC POWER SUPPLY SYSTEM |
| To: | |
| Shared Package | |
| ML17277A650 | List: |
| References | |
| RTR-NUREG-0892, RTR-NUREG-892 NUDOCS 8307120313 | |
| Download: ML20024C146 (559) | |
Text
{{#Wiki_filter:_ _ _ _ - _ _ _ - _ _ . Washington Public Power Supply System
^
P.O. Box 968 3000 GeorgeWashingtonWay Richland, Washington 99352 (509)372-5000
)
s.. / The attached reports are the structural analysis of the purge and vent - valves and operators installed at WNP-2. The loads used in the analysis are the valve operating loads combined with the dynamic loads which would result from seismic and hydrodynamic events as determined by the piping analyses for the plant. There are three reports attached. They separately address: -
- 1) The 24-inch butterfly valves manufactured by BIF (identified as QID361106),
- 2) The 30-inch butterfly valves manufactured by BIF (identified as QID 361104), and
- 3) The air operators manufactured by Miller Fluid Power and supplied by BIF as a part of the valve assembly (identified as QID 018001).
These reports have been prepared by Cygna Energy Services for the Supply System's Equipment Qualification Group and are in their complete form in the Equipment Qualification files. However, in the interest of conserving space in the transmittal to the U.S. NRC, pages which are duplicated in the reports have been removed from all but one of the reports. Also, documents which have previously been submitted to the
.U.S. NRC are not attached as stated in the report.
g _ 8307120313 830622 gDRADOCK05000
WASHING 1t)N PUBLIC POWER SUPPLY SYSTEM SUPPL.lEll TITANS.illTTAL FOR.\1 (AREA WITHIN HEAVY BORDER TO BE COMPLETED BY SUPPLIER) TO tuE ATTENTION O,, Dennis Armstrong ,,aE 1 OF 1
,ooREss, 3000 GeMW'Ms ME"(En 'W"'Mf8Ml"a'rfd ^ "'" TRANSMITTAL NO. 0" sus;ECT: Equin. Seismic /Hydrodynnt ic Recuni NEw 0 arsu=~irra' PROM: Cvena Enerev Services oATE sueuiTTEo A/4/R7 AooREss, 1200 Jadwin. Strite 565. Richland. WA REauEsTEo oATE THE FOLLOWING PUBLICATIONS /OR AWINGs ARE sVBMITTED FOR: OF RETURN:
h A PPR OV AL REVIEW iN FORM ATION DisT RIBUTIO N CONTRACT NO: C-0892 No.OF PRINTS OFEACH NO.OF REPRODUCtBLE OF CM P.O. NO : SUBMITTED BY Fawaz Khanachet _ M.ef_m - 5 won g o,oE, uo, y,,gg, Assistant Proj ec.t'Managsr' s,E C, no , suSVENOOR: 'CO NT./P.O. NO.a SPEC. SECT.NO: J ITEM PUBLICATION OR REV. WPPss NO. OR AWING NO. No. PUBLICATION OR O R AWING TITLE MANUFACTURER ACTION 1 361106 3 Original Requal Rpt. for /7 QID 361106 2 T-644RB Cygna T-644RB I COMMENTS (UsE ADDITION AL SHEET. lF REQUIREO) . TO BE REVIEWED BY ~ ECElVED BY: (PURCH As4NG ONLY) TR ANsMITTED BY: (PU RCHAs4NG ONLY) NAME DATE - NAME DATE
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ACTION LEGEND, ' " A e APPROVED FOR PUBLICATION ,4 m INFORM ATION ONLY ON
- APPROVED AS NOTED POR P AsalCATION NA e NOT APPROVED W P 710 ma
Final A f. t * ' Qualification lilllllllllillllllllllllllllli Report PROJECT: Equipment Seismic / Hydrodynamic Requalification JOB NO: 82044 CALC NO: OT.01.F CLIENT: Washington Public Power Supply System QID NO: 361106 TITLE: Equipment Seismic and Hydrodynamic Requalification of 24" Cylinder Operated Butterfly Valves for: CSP-V-3,4,5,6, and 9 CEP-V-3A, and 4A G (s PREPARED BY: AN ' Mark scott 6/o/83 l DATE REVIEWED BY: - ' M >
- 4. Lourdes Fernandez 6/9/83 DATE APPROVED BY:- / MI # Fawaz Khanachet 6/9/83 e ,/ DATE REVISION: 3 SCI /K/ Sysm fcs/s[W- ,
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QID #__ 361106 i Q _ REVISION STATUS REPORT PRE'D BY APPROVED REV DATE BY DESCRIPTION REV'D BY O $ (e $1 - -4 .n,+. - Y-f IO/+7/t2, f.b vf -% W *"2' w ae = ~ ~any 4 REWSE Celc..TAsLE of 4- coursuTS Rev.u J est... ak n re tto.f '
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s REVISION /31 1.1 WASHINGTON PUBLIC POWER SUPPLY SYSTEM
,,.x REQUALIFICATION CERTIFICATE QID# 361106 d COMPONENT MO, CSP-V-3, CSP-V-4, CSP-V-5, CSP-V-6, CSP-V-9, CEP-V-3A & CEP-V-41 COMPONENT OESCR8FTiON, 24" Cylinder Operated Butterfly Valves MANUFACTURER:
BIF A-206765 MODELNO: EQUlPMENT CLASSIFICATION: ACTIVE PASSIVE SEISMIC QUALIFICATION REPORT
REFERENCE:
/
Cyana Report Ot.01/F, OID 361106 "24" Cvlinder-Ocerated Butterflv Valve" J Recuired action: 1) Remove A-307 Ear Bolts and rerlace with A-325.
- 2) Reinforce valve ear group with 15 " shear plates to cualify air operators for recuired faticue cycles.
o THE ASOVE SEISMIC AND 6 QUALJFICATION REPORTS HAVE SEEN REEVALUATED IN ACCORDANCE WITH THE CURRENT NRC SEISMIC ANO N CRITERIA:
- 1. IEEE STANDARDS 344 (1975)
- 2. USNRC REGULATORY QUIDES 1.s2.1.10e
- 3. STANDARD REVIEW PLANS 3JJ, S.10,M THE ABOVE COMPONENT HAS SEEN FOUNO ACCEPTABLE FOR PERFORMING ITS INTENDED SAFETY RElATED FUNCTION WNEN SUBJECTED TO THE PLANT SPECIFtc VIERATORY m LOAOS.
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i I i l I O I 2.0 SQRT FORM (S) AND REFERENCES
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REVISION b 2.1 WASHINGTON PUBLIC POWER SUPPLY SYSTEM V Ilmmimmitimmimi Qualification Summary of Equipment OIDe 361106 Rel. No.
- l. PLANT NAME:
2 TYPE PWR I. NSSS: GE 2. A/E: A0r"9 E RC P- - BWR 5. F*a rk TT 11 CCw oNENT NAME: 24" Cvl.0cer. But t er flv v lve a COMPONENT NO.CS P-V-3 . 4 . 5 . 6 . & 9k CEP-V-3A & 4A I. SCOPE: NSSS BOP
- 2. M) DEL NudBER: A-206765 QM NTITY: 7 j
- 3. VENDOR:
BIF 4 IF THE ComENT IS A CABINET OR PANEL, NAME AND MODEL NO. OF THE DEVICES INCLUDED: N/A
- 5. PHYSICAL DESCRIPTION: a. APPEARANCE: Butterfly Valve with 8" Cvl Ooerator
- b. DIMENSIONS: 24" UOm nal diameters
- c. WEIGHT: 847# - Valve Assy; 676# - Operator & bracket
- 6. LOCATION: BUILDING: Reactor ELEVATION: Maximum elevation: 495' (CSP-V-3A & 4A) d,;
7 FIELD MOUNTING CONDITIONS: BOLT (NO. SIZE ) WELD (LENGTH )
- 8. a. SYSTEM IN WHICH LOCATED: Containment Supply Purge Systems
- b. FUNCTICNAL DESCRIPTION: oMaiMed isoladon, Nevendon of the release of radioactive material to the environment.
- c. IS THE EQUlWENT REQUIRED FOR: HOT STANCBY COLD SHUTDOWN h BOTH NEITHER
- 9. PERTINENT REFERENCE DESIGN SPECIFICATION: WPPSS Soec. 2808-68
)
111. IS EOUlWENT AVAILABLE FOR INSPECTION IN THE PLANT: YES NO PAGE I OF $
REVIS ION . _3. 2.2 Qualification Summary of Equipment (Continued) OIDd 361106 h Rel. No. IV. EOUINE'ef CUALf FICATION METHOD:
] TEST X ANALTSIS C@8t NAfiON OF TEST & ANALYSIS CmLIFICATION REPCRT: 24" Cvlinder-Ocerated Butterfly Valve *
(No., TITLE & OATE): OT.01.F, Revision 3, June, 1983 1 15 COMPANY THAT PREPARED REPCRT: CVCna Ererav Services 1 l COMPANY THAT REviEwEO REPCRT: Washincton Public Power Sucolv Systems 1
*Plus original valve analysis 3,4
- v. vieRATicN INPUT:
l 1 LCA05 CONSIDERED: a. SEISMIC ONLY I
- b. HYCF00YNAMIC ONLY !
- c. CCN81NATON OF (a) AND (b) l
- 2. METH00 CF CCN8!NING RRS: A8 SOLUTE SO4 SRSS OTHER (SPECIFY) l
- 3. RE0utRED RESPONSE SPECTRA ( ATTACH THE GRAPHS): Section 5.1 of OID 361106 j 4 DA @ LNG CORRESPON0 LNG TO RSS: CBE O 55r S. RE00lRED ACCELERATION IN EA04 OlRECTION: ZPA OTHER (SPECIFY) Section 5.5 7 \ 15 OBE S/S . Attached pfg , y, SSE S/S = Attached F/8 v.
- 6. wERE FATIGUE EFFECTS CR CTHER VIERATION LOADS CCNS10ERE07 NO h YES I IF YES, DESCRIBE LOA 05 CONSIDERED ANO HOW THEY wERE TREATED IN OVERALL QUALIFICATICN FROGRAM:
l ! The calculated stress rances were comcared to the AISC allowables, as the structures analvred were not eart of the cressure boundarv. O NOTE: IF *CRE THAN ONE REPORT C@RLETE i TEMS IV TM OUGH dii FOR E ACH AEPORT PAGE 2 CF S
2.2 Qualification Summary of Equipment (Continued)
/
QID# 361106 Ret. No. VI. IF QUALIFICATION 8Y TEST. THEN COWLETE*: g 1 SINGLE FREQUENCY MULTI-FREQUENCY RAN004
- 2. SINGLE AxlS MULTI-Axis SINE BEAT
- 3. NO. OF QUALIFICATION TESTS: CBE SSE OTHER (SPECIFY) 4 FPEQUENCY RANGE:
- 5. NAYlRAL FREQUENCIES IN EACH DIRECTION (SIDE / SIDE, FRONT /BACK, VERTICAL):
S/S = F/8 = V=
- 6. METH00 OF DETEMINING NATIEAL FREQUENCIES:
LA8 TEST IN SITU TEST ANALYSIS
- 7. TRS ENVELOPING RRS USING HJLTI-FREQUENCY TEST: YES (ATTACH TRS & RRS GRAPHS) NO e)
(
%J
- 8. INPUT g-LEVEL TEST: OBE S/S = F/8 = V=
SSE S/S = F/8 = V=
- 9. LABORATORY MOUNTING:
BOLT (NO. , SIZE 1 WELD (LENGTH )
- 10. FUNCTIONAL OPERA 8ILITY VERIFIED: YES NO NOT APPLICABLE l 11. TEST REULTS INCLUDING MOOlFICATIONS MACE:
i
- 12. OTHER TEST PERF0*ED (SUCH AS AGING OR FRAGILITY TEST, INCLUOlHG RESULTS):
\
' NOTE: IF QUALIFICATION SY A C@ BlNTATION OF TEST AND ANALYSi$, ALSO COW LETE ITEM VII.
PAGE 3 0F 5
REVISION h 2.4 Qualification Summary of Equipment (Continued) QID4 361106 Ret.No. VI1 IF CUALIFICATION 9Y ANALYSIS. THEN C:FPLETE:
- 1. METHC0 CF ANALYSIS:
STATIC ANALYSIS X E0ulvALENT STATIC ANALYSIS DYMMIC ANALYSIS TIME-HISTORY RESPCNSE SPECTRIN
- 2. NATI.RAL FREOUENCIES IN EACH DIRECTION ($10E/Sl0E, FRCNT/8ACK. VERTICAL):
S/S . 10.81'Hz pfs . 26.1 Hz y. >100
- 3. MODEL TYPE:
30
] 'D
]10 FINITE ELEMENT hBEAM O c'osco rcaM so'urio~
4 COWUTER CCCES: FREQUENCY RANGE AND NO. OF MODES CCNSIDERED: HAND CALCULATIONS OTHER
- 5. METH00 0F cod 8tNING OYNAMIC RESPONSES: A850VLTE Stp h SRSS ](SPECIFY)
- 6. CAWING: OBE SSE BASIS FOR THE DAMPING USED: N/A*
7 SUPPORT CCNSICERATIONS IN THE MODEL: cire "touM_ed
- 8. CRITICAL STRI.CTLRAL ELEMENTS: GCVERNING LCAO OR RESPONSE SEISMIC TOTAL STRESS A. 10ENTIFtCATtCN LOCATICN CCNRINATION STRESS STRESS ALLOdA8({
Valve Ears CSP-V-3&4 pipe-axial 15743 19538 26880 (PSI) , Ear Bolts CSP-V-3&4 pipe-no rmal 15777 18382 66000 (PSI) Drive Rod CSP-V-4 rod-normal 8543 33019 86400 (PSI)! Ear Bolts CSP-V-6 pipe-normal 57543 58884 66000
!b i
(PSI)i MAXIMtB ALLCWABLE l 8 max. CRI TICAL DEFLECTION TO ASSURE CEFLECTION LOCATION FUM;TIONAL CPERABillTY
< 0. 01" Valve disk radial approx 1/8" radial deflection clearance
- Final response accelerations frca piping analysis were used.
pace 4 CF 5
Revision 2 2.5 Qualification Summary of Equipment (Continued) /Q #QID 361106 V Vllt. REFERENCES
- 1. BIF Drawings:
D-207110-E, D-207110-G,(Valve Data Sheets) A-2 0 6 7 6 7,18 " , 24" & 30" Butterfly Valve - General C-26096," Certified Dimension for Model A-83-B Cylinder"
- 2. WPPSS Unit 2 Drawings:
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-1A, 1B CEP-625-1.2 From Reactor Nozzle X-67 to SGT-Fu-1A, 1B D.220-0330 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 #TR-74-7 by McPherson Assoc., Inc., " Design & Seismic Analysis 24 Cylinder operated Butterfly Valve." (Rev. 1) 1/5/76.
- 5. WPPSS letter to Cygna Energy Services, GE-02-RWH-018, 12/17/82.
REFERENCES CONTINUED ON PAGE 2.6 Completed By g Qgpyg [ W , _ Date /i ,- aa'a'd 8Y )l. i ylpph_- y/'4 .., ;/;,/c 6//?/63 Page 5 of 5
r= = Calculation MW f a Sheet
,q lillllllllllllllllllllllllllli b
F ro!ect Preparec By d Date Washincton Public Power Supply System L.C.'Fernandez 5/27/83 Subject C - Date Equipment Seismic / Hydrodynamic Requal.hecked Br 4.,.p(2f g/,,/g5 sys em sob no poe no
* **r* % e Rev No Sheet No '
QID 361106 2 2.6 0 4W0 0$- 6,l/C & SECTION 4.4 # D '/ N I u REFERENCES (CONTINUED):
- 6. Cygna Energy Services Communications Report, R. Ricappito, BIF Valve, and J. Rakowski, CES, "BIF Valve Dimensions",
2/11/83.
- 7. Cygna Energy Services, Project Manual Design Criteria, DC-1, Rev. 1, November, 1982.
- 8. Cygna Energy Services, Equipment Qualification Walkdown
,_s Verification Forms, Revision 1, dated 1/5/83.
( ) k/ -
- 9. WPPSS, WNP-2, Safety Related Mechanical Equipment List Summary Sheets, dated 2/10/83.
- 10. "AISC Manual of Steel Construction", American Institute of Steel Construction, 8th Edition, 1980.
- 11. Preliminary Transfer of Final Burns & Roe Piping Loads for CSP-V-1,2,3,4,5,6 and CEP-V-3A&4A, received 4/13/83.
- 12. Cygna Energy Services, " Equipment Seismic and Hydrodynamic i 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.
l 13. Cygna Energy Services, " Equipment Seismic and' Hydrodynamic j{\ l Requalification for 8", 10" and 12" Bore Air Cylinder Operators," File No. 1P.01.F, QID No. 018001, Revision 0, May, 1983. j
- 14. 8,'SN RC , " Standard Review Plan, NUREG-0800"
- 15. Cygna Energy Services, " Equipment Seismic and Hydrodynamic Requalification of 24" Cylinder Operated Butterfly Valves for CSP-V-3,4,5,6, & 9 and CEP-V-3A & 4A," File No. OT.01.F, l QID No. 361106, Revision 3, June, 1983.
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lilitillilili;;om;iiiiiiii J TABLE OF CONTENTS QID# 361106 SECTION TITLE NO OF PAGES 1.0 Requalification Certificate 1 2.0 SQRT Forms ,7 3.0 Table of Contents - ' 4.0 Requalification Analysis - 4.1' Conclusions 1 4.2 Summary of Results 4 4.3 Analysis - 4.3.1 Introduction 2 4.3.2 Calculations 66 + Appendices ; 4.4 References 1 5.0 Appendices - !- 5.1 Response Spectra 2 ! 5.2 Walkdown Sheets 21 5.3 Valve Local Coordinate Systems 4 5.4 SRM Sheets. 7 , 5.5 ' Final Pipe-Mounted Equipment 8 Response G-levels 6.0 Drawings 9 Revision 3 l -) i
. - - - , , , , -..- ,. _ ---r,.--w-w-. --w.-ei.,w,
g___ _ _ [Tl#j t'Id tillllllilllilllill!!!Ill!!!! TABLE OF CONTENTS QID# 361106 CON'T SECTION TITLE NO OF PAGES 7.0 Transmittals, Prior Calculations - and Reports 7.1 Communication Reports ' & Correspondence 37 7.2 Old Requalificaticn & SQRT Forms 8 7.3 BIF Report 98 7.4 McPherson Associates Analysis 75 0 0
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** * *68% OO *6 9
- OS 9 hee e h eg m em, , , , ,
e SECTION 4.0 REQUALIFICATION ANALYSIS O 1 O e G P
Calculation
@MTJ A Cover s 111i1ll1111ll11111111111111111 ggg
~J Project Job N - 82044 Ecuipment Seismic & Hydrodynamic Requalificatioft ile No. OT.01/F Client Calc. Set No. 1 Washington Public Power Supply System No. of Sheets gg Subject Seismic Qualification of 24" Cylinder Operated Butterfly Valves QID 361106, EPN # CSP-V-3,4,5,6 & 9, and CEP-V-3A & 4A Statement of Problem The equipment qualification was performed based on calculations using valve and operator response g-levels transmitted by the A/E, (Final piping loads dated 3/31/83). Sources of Data O See sheets 4.3.65 and 4.3.66 Sources of Formulae & References See sheets 4.3.65 and 4.3.66 Remarks None originators Checkers Distribution Revision No. 3 Supenedu Wculation Set No. J. Rakowski D. Searle WPPSS-2 Revision 2 O M. Kuntz L. Kaner Proj.ect File-1 Approved By: Date: M. Scott LC Fernande:: .. ,/ <l
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*' BIF Valves / Miller Operators #
N M .. / /,, 6/9/83 System Jcb No File No CEP & CSP 82044 1T.01.F Analysis No Rev No Sheet No , 361106 3 4.1.1 l l CONCLUSIONS J 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:
- 1) Remove the existing operator bracket attach-ment bolts (A-307) and replace with an A-325 or A-490 bolt.
- 2) Reinforce the operator support ears with the addition of shear plates as shown on page 4.3-48 or 4.3-54 of 361106, Rev. 3 (this report).
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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. O O -
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TABLE 1.3 N"" ,) ~'/
- U ALLOWABLE STRESSES Since operability is required, the stresses for the faulted condition will be kept below yield *. The table below is based on AISC criteria and the yield stresses at temperature (340*F) from PG. 9 of REF. 4 for conservatism.
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- Subject
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24" Butterfiv Valves V ' W W- r -5 % System Job No Fue No CSP & CEP 82044 OT.01/F Analysis No Rev No. , Sheet No 361106 4 361106 - 4.5-1 EQUIPMENT REQUALIFICATION FOR QID 36110 BIF 24" CYLINDER OPERATOR BUTTERFLY VALVES 4.3.1 Introduction ew 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 & 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 responso 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 absoluta sum. Valve ear bending stress components due to any one response g-level component are combined by an absolute sum. (D A./
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g A LL f) Calculation Sheet lillilllllllllllllilllllillll! D FSS Mechanical Equipment Qualificationmem s' Meh ,Og D 1/10/63 Suegt Date 24 Butterfly Valves Checked v, By(,( ( N/a . /'i .e r a e" System Joe No Fue No CSP & CEP 82044 OT.01/F
#3Mi88 f 361106 - 4.3 2.
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 QID 361104 (30" valves /10" operators). Hand calculations which check selected por-tions of computer output are 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 P&ID's in section 6.0. Natural frequency calcu-lations are given for the air operator assemblies in Section 4. 3. 2.1. Preliminary analyses were performed which showed that, for operator response g-levels greater than ap-proximately 3 g's, the air cylinder sprir,g 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 beund g-levels which occur in the hydro-dynamic frequency range is approximately 6 degrees. Tnis flutter was evaluated to have no detrimental effect'on system safety function as noted in Reference 5. Valve operability was addressed in the folicwing manner. For the valves with Use Code 2, operability after the event can be assured by demonstrating that faulted con-dition stresses remain below elastic limits (see Summary of Results.
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24" Butterfly Falves ' ' 'w ' s 'l ' " 'E S ystern . Joe No File No CSP nnd CFP R90AA nT n1fy fSTidE Z 361106 4 6- 3 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 7673 parts of which are shown in figures 1.1 and 1.2, allow fN the following conclusions to be made for valve
'(,) operability: A) Figure 1.1 shows that thrust bearings are part of the shaft bearing design. This design prevents lateral movement of the disk in the direction of the shaft to eli-minate interference with the valve body when closing. Further, it is noted on Page 26 of Ref. 3 that frictional torques in the shaft bearing system are negligible. B) Figures 1.1 and 1.2 show a circular valve cross section having an internal rim within which the valve seats in the closed posi-tion. The only mechanism remaining to af-fect valve closing which can be postulated is our-of-round distortion of the section due to DBE piping loads and dynamic loads on the valve. These loads were accounted for in Ref. 4 in the overall valve sizing calculations, where analysis showed that the stress intensity in the 0.5 inch thick valve body remained below 1.2 Sm, or approximately 0.8 of yield. Stress contribution from dynamic loads on the valve 73 and operator were relatively small. Further, as shown ( in the figures: ex ::
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Calculation Mi&' M Sheet lill:!fillllllllllllllllill!!! O SS Mechanical Ecuipment Qualification "* N '* 1/10/83 Butterfly Valves 3 30!O3 S ystem Job No Fde No C99 nnd CEP A?O44 OT _01 / F Rev No. Agsg , Sheet No l The valve seat forms a heavily reinforced section made up of the valve body, internal hub and external flanges (including the mating flange of the piping). Hence the stress levels in this section are much lower than in the valve body and hence no distortion of the section could occur to affect seating of the valve. Valve flange dimensions are given below. Note the relatively large internal radial clearance of 1/8 inch. 2 Stress analysis of the valve extended structures are given in this report. Air operator operability is addressed in QID 018001. The design data used in the analyses are given in Summary Table 1.1 (pipe-orientations and elevations are taken from the appropriate P&ID'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 = 350# Final = 1850# Fail Closed Preload = 1500# Final = 3000#
- 2) Cylinder C.G.'s shown on the following sketches represent data received from BIF in the communi-cation report of Section 7.0 of QID 018001.
- 3) Closing torque values are taken from Ref. 3.
- 4) Valve component dimensions: (Ref. Feb. 10, 11/83 communication report - Section 7)/
Flange: width = 3.5", thickness = 1.78" Radial Clearance Disk / Seat 1/8" O l :a :e
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- 24" Cylinder Operated Butteryfly Valves QID# 361106 y 6
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- 24" Cylinder Operated Butteryfly Valves QID# 361106 0'.
Group I; Cylinder Operator Fail Open o o o a g g (Valves: CSP-V-5, 6, 9) S ['- vi
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7 4" Rtittorfl y Vnlvom System Job No File No ecp ana cup 82044 OT.01/F Analysis No Rev No Sheet No 161106 2- 361106-4.3- 9 4.3.2 CALCULATIONS 4.3.2.1 NATURAL FREQUENCY CALCULATIONS Perform natural frequency calculations for the fol-lowing four operator configurations: Group I - Fail Open V EPN's CSP-V-5 6) and 9 Case I Valve Open Case II Valve Closed Group II - Fail Closed l EPN's CSP-V- 3 and 4 and CEP-V-3A and 4A i Case I Valve Open Case II Valve Closed l l V
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B=41572.5(7[7) + 1364.99(19 1) = 12754.44 + 1042.85 = 13797.29 9 O B= = .000476 rad Deflection at Point "A" 8A' due to G B
= .000476(14.46)
= .0069 Total SA = .0069 + .000032 = .0069 g v, = =
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i ergss E Calculation [41dt'fd lililillllllllillllllillllllll Sheet l k$PSS Mechanical Equipment Qualification - 3h 3 l Subect Cnechec B Cate 24" Butterfly Valves [ 3[DO!dd ) S y stem Joe No Fue No ' CSP and CEP 82044 OT.01/F ) Analysis No Aev No Sheet No 161106 ' 361106 - 4, 6 - to
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Calculation ML% ri Sheet lililllillililllllllllllilllli NNSSMechanicalEquipmentQualification Sueiect lhh '")[Lyb Checked BC Date 24" Butterfly Valves F/ h, 30!6,5 System Job No File No CSP and CEP 82044 OT.01/F Analysis No Rev. No. , Sheet No. 4,3.E. 2 A PPRov1 M ATE VALyp ct (1 7 'E C MA G mT u n s 6 514 G P t%E utro 4 5 Flow RGuRC l.5 : r.
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"WFSS Mechanical Equipment Qualification"' "'(
NM U* 1/10/83 (('E Butterfly Valves d 3[$o[83 S ystem Joe No Fi!e No. CSP and CEP 82044 OT.Ol/F Analys s No Rev No Sheet No 361106 2 361106-4.3 - 2 2 4.3.2.3 STRESS ANALYSIS The procedures for the analysis of the subject valves are outlined below:
- 1. 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. G
- 2. Perform a fatigue analysis on significantly stressed components. Determine allowable alternating stress ranges from AISC 8th Edition, Appendix B, noting commentary.
The fatigue analysis is to be performed only for those EPN's subject to hydrodynamic loads. The number of respective load cycles is given below. 1 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 Cveles ! 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 #4 with 150 cycles can be
! used to conservatively bound combinations 3 and 4.
, x. x
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e m- Calculation (4 M'M Sheet lillililllllililllllilllililli Prepared B / / O P'O i eCt f'* h a Date WPP99 Mochnnien1 Ecninmont Ouali fi ca tion I CO'k 1/10/83 Suciect Checked By(l[l) Cate _ / / 24" Butterfiv Valves Wu S 36/63 S ys'em Jc0 P.o Fife No CSP and CEP 82044 OT.01/F Analysis No Rev No Sreet No 361106 L 361106 - 4. 3 - 24, key WAy EEn id 4 ncsss - Ec5 ,3 cu' % -u tr_. (EF 4., P4 'f., Ag= 0a 44-3 19 m, );, in a u - t. S
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- 1/10/83 Suoject Date 24" Rutrorfly vn1vns Checked W B'()"b 3[3d!63 Sys'em Job No Fde No CSP and CEP 82044 OT.01/F Analwsis No Rev. No Sheet No 36fl06 /- 36 t / 6 6. - 4 A- 7_7
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E[kSS Mechanical Equinment_ Qualification h ' 1/10/83 Suoject 24" Butterfiv Valves Checked B ' GM'/.G
] f Date / /
3/$0/05 System Joe No Fife No CRP nnd CFP R2044 OT.nl /F
# " " " Sheet N 3$ff08 i 361106 - 4. 3 2 8 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 celerations, change significantly for the new ac-the disc is acceptable. h l
Taper Pins l l The stress in these pins is due only to the seating torque. The stress in Ref. 4, page 53, is 10,753 PSI and is therefore acceptable. For the new, lower seating torque, the stress becomes 8710 PSI.
- Analysis for: Drive Rod, cylinder bushing pressure, I valve ears and valve ear bolts.
Method I: Use element forces and moments output from the piping analysis (Summary Table 1.1) and the absolute sum of stresses. The conservatism of SRSS summing of the component stresses cannot be assured l because the independence of the six element forces (/ moments) cannot be.de-termined without analysis of modal par-ticipation. O l l l
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cate N'fssMechanicalEquipmentQualification wareaeg L 1/10/83 Subiect Checkee (y [, [ Oate 24" Butterfly Valves NdX/4A .5 bb S y s*em Joe No Fue No CSP and CEP 82044 OT.01/F Rev No. Sheet No ggigg 5 361106 - 4,3.gg Method II: Use the north, east and vertical operator accelerations output.from the piping analysis. Absolute sum for stresses with each component then SRSS over re-sults for N.E and V. Noteh 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-7s fore the absolute sum will be used at this level. (d x 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/O parameters are shown for use in QID 361104. Analysis of Seating Torque Forces
- 1) Seating Torque loads control the stress in the valve lever arm, keyway, shaft and taper pins. These stresses were less than allowables for the valves of seating torque given in Ref. 3, for all valves.
- 2) For valve EPN's which are Fail-Open with Use-Code 2, no seating torque forces are applied during the faulted and upset conditions (CSP-V-5,6).
- 3) For the Fail-Closed valves, the forces at the trunnion pins are shown below, along the cylinder axis, for +2-axis g-loading:
st A cals (O %J 1 r
- k cn c.!cvis/ valve ah
.I L t cn .=aw halve e.ars am4A 9 i i gius:UDanomst. Force.frcm cpera cr nn x. - a.x!.y sirewow xe a
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F= =?. =1.M Calculation [ 4 p ; ril Sheet milimilmillimillilitil Protect Prepared By i FO . Date WPPSS Mechanical Eauipment Oualification UhK 1/10/83 Suc rect Checked ed. / # Cate 24" Rutterflv Vnives (J/ r/ V A' Ns d ?? 'd f. Syster1 Job No File No PCP nna cPP R?nAL OT.01/F Rev No. Sheet No Anal 1ssNo36 106 F- 361106- 4.'5- 4 2 4.M Upset 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 additi'onal 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 Section4.3.5. Upset g-levels (per revised B&R piping analysis , Sec. 5.5) EPN N V E 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 t l Component stresses are given in Table 1.2. l I I O
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Protect Precarec Byl PF) - Date WPPSS Mechanical Eculoment Oualification I Cu 1/10 / A3 Sueiect Checked B Date f / 24" Etittodi v Vnivon . . .513 0143 S / stem Job No Fi,e No esp nna cup 82044 OT.01/F Analysts No Rev No Sheet No 361106 T- 161106 - 4 5- 4 3 Section4.3.5 - Fatigue Analysis Discussion The operator and bracket assembly are not part of the pressure boundary, therefore, the fatigue analysis will be performed in accordance with Appendix B of the AISC Manual for Steel Con-struction. The following assumptions apply to the fatigue analysis. 1) (q
)
Faulted stresses (based on piping-analysis accelerations) will be used. This is necessary to insure operability after a design basis event.
- 2) The actual stresses used will be the ones calculated in Section 4 3.
- 3) If the alternating portion of the stress has been cal-culated separately only this part will be used. If the operating loads (i.e. seating torque effects) are al-ready included in the stress analysis it will be con-servative to use the calculated stress value. As long as no failures occur, the operating stress does not need to be extracted.
- 4) The allowable 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 AISC Manual.
The table on the following page gives the calculated stress range, stress category, and allowable for the critical components. The fol-loving page gives excerpts from Appendix B of the AISC Manual showing the descriptions of the relevent stress categories. O O
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N5'SSMechanicalEquipmentQualification*'*" h M k 1/10/83 Sub\ect 24" Butterfly Valves Cnecked B1(D j H, 6. . Date l l 3,/.50133 System Job No File No CSP and CEP _ 82044 OT . 01 / F
"**"' Sheet N 38ffd% L 361106- 4,3-zis Fatigue Analysis (cont.)
STRESS STRESS STRESS STRESS 1.5 x ALLOW ITEM TYPE (PSI) RANGE (PSI) CATEGORY (FROM AISC) TRUNN_ ION PIN Y 4108 8216 F ??500 O (/ DRIVE ROD (MAX) T - SEE TA BLE 1. 2 - A 90000 SUPPORT EARS T~ - SEE TAB 1E 1.2 - A 90000 I T 1127 19,150 A 90000 MAIN SHAFT 'M 8064 16.128 A 90000 NOTES: I (;) Assume shear stress on nominal area of a stud type shear connection. l l 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). m) l
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_ _ _ j ,._, JoDNo Fue No_ lilllilllllllllilililllll!!ill y_y1 .-7 ., System - Sheet No Analysis No ' O' Aev No IIO ~ ~ YAT:GvF hHAkYSTS (c ou r.h THE TASLE 8 Eko w H as BEEH CoHDEm Eb FROH A PPENb:x 8 0F Tt4 E Arsc t-t A HtA n u cP ATEEu C ONS T R Lrcrr o H. Tue cases asen nee Hazuo WrrH dn 8 R Roud. Stress General Cate-Condi- Situation Kind of gory. tion 8' IS Table B3) Plain Base metal with rolled or cleaned sur- T or Rev. A *p' - O, material faces. Built-up Base metal and weld metal in mem- T or Rev. B members bers, without attachments, built-up of plates or shapes connected by contin-uous full- or partial-penetration groove welds or continuous fillet welds parallel to the direction of applied stress. Calculated flexural stress, /s , in base T or Rev. C metal at tot of welds on girder webs or flanges adjacent to welded transverse stiffeners. Base metal at end of partial-length T or Rev. E welded cover plates hasing square or tapered ends, with or without welds across the ends. Mechani- Base metal at gross section of high- T or Rev. B cally strength-bolted friction-type connec-fastened tions, except connections subject to connec- stress reversal and axially loaded joints tions which induce out-of plane bending in connected material. Base metal et net se: tion of other me. T or hev. D chanically fastened joints. Base metal at net section of high- T or Rev. B strength bolted bearing connections. Attach- Sheer stress on nominal area of stud- S F j {,,/ , y y ments type shear connectors. toos ao
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Calculation dLnM Sheet (~N lilllilillllll!!!!!Illlllllll! U WashingtonPublicPowerSupplySystEm"8'Nh *?/zy/g 3 Sue!ect , Date ' Equipment Seismic / Hydrodynamic Requal.Checked 8(: ' O 3e 'e' 'ME System Joo No File No CSP & CEP 82044 OT.01/F Analysts No Aev No Sheet No / 361106 1 361106 - '*rr d. SECTop 4.4 b# f N k# 5/%h
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REFERENCES:
- 1. BIF Drawings:
D-207110-P., D-207110-G,(Valve Data Sheets) A-206767,18", 24" & 30" Butterfly Valve - General C-26096," Certified Dimension for Model A-83-B Cylinder" /'~N O
- 2. WPPSS Unit 2 Drawings:
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-1A, 1B CEP-625-1.2 From Reactor Nozzle X-67 to SGT-Fu-1A, IB D.220-0310 Support and Erection Isometric-IR64 (Johnson Controls)
- 3. BIF Report TR-27234 and TR-27235, "Dynsmic Torque Calculation of Butterfly Valve; Sizes 24 and 30 inch", dated November 10, 1982.
- 4. Report #TR-74-7 by McPherson Assoc., Inc., "Desi Analysis 24" Cylinder operated Butterfly Valve."gn &(Rev. Seismic
- 1) 1/5/76.
- 5. WPPSS letter to Cygna Energy Services, GE-02-RWH-018, 12/17/82.
A Q
.=.= -
pemegg!!g Calculation M eh'TJ Sheet illllillllllllilllllillllillli Project P?parec By M Cate O Washincton Public Power Sucolv System L.C. Fornandez 5/27/83
#' Equipment Seismic / Hydrodynamic Requa1." * '# g. pej U"g/yj73 S ySten! Joe No Fue No g + s.r.she Rev No Sheet No I /k .
OID 361106 2 4. 5. /4 1d-0 && O! h $l3Q 6/M r SECTION 4.4 I REFERENCES (CONTINUED) :
- 6. Cygna Energy Services Communications Report, R. Ricappito, BIF Valve, and J. Rakowski, CES, "BIF Valve Dimensions",
2/11/83.
- 7. Cygna Energy Services, Project Manual Design Criteria, DC-1, Rev. 1, November, 1982.
- 8. Cygna Energy Services, Equipment Qualification Walkdown Verification Forms, Revision 1, dated 1/5/83.
- 9. WPPSS, WNP-2, Safety Related Mechanical Equipment List Summary Sheets, dated 2/10/23.
- 10. "AISC Manual of Steel Construction", American Institute of Steel Construction, 8th Edition, 1980.
- 11. Preliminary Transfer of Final Burns & Roe Piping Loads for CSP-V-1,2,3,4,5,6 and CEP-V-3A&4A, received 4/13/83.
- 12. Cy Jna Energy Services, " Equipment Seismic and Hydrodynamic I l 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.
l 13. Cygna Energy Services, " Equipment Seismic and Hydrodynamic ' g Requalification for 8", 10" and 12" Bore Air Cylinder l Operators," File No. 1P.01.F, QID No. 018001, Revision 0, ! May, 1983.
- 14. USNRC, " Standard Review Plan, NUREG-0800" l
O
=..
O 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 f
1 l 1
-. _ . _ . _ _=
O sbasic esp tm 34
*- BASIC Compiler Version 5.4b 0001:00 REM ***** BIF UALVE AND AIR OPERATOR SEISMIC STRESS *****
0002:00 REM *************** CSP-V/AO-3/4 ************************** 0003:00 REM **SAME ORIENTATION FOR EPN 3&4,SAME PARAMTERS, VARY G'S 0004:00 REM 0005:00 var i,J,k n integer 0006:00 var I rod,1 cg,x ph i , l ave , abi t ,11,12, el , e2, e3,e4,e5 = re al 0007:00 var fst2, ca,la,ch,ib,aa,ab,d1,d2,ci,il,c2,12=real 0008:00 var 1rodo,1cgo,1dr,d, abush, pbush=real 0009:00 var fcof, feo, ma,mb, siga. sigb, fedr, f edrf ,maf , mbf=real 0010:00 var dear, fcear,fr, +11,f22,la, ci12,ci21,stt3,sem1=real 0011:00 var sem2, set 3,ses1,ses2,sa, tau 11, tau 22,tauear,aear=real 0012:00 var btens, taubit, set 3f,sem1f,sem2f,feearf, frf,filf=real 0013:00 var f 22f ,st t3f ,sest f ,ses2f ,srf , taulf , tau 2f , taurf =real 0014:00 var taubf,btf, dsr,dtaur dtaub,dbten.dsa,dsb.dpb=real 0015:00 var sdraf,sdrbf,pbushf, tau 11f, tau 22f=real 0016:00 v ar wao ,wbr , f tr 1,watr 1,51, si f , s2, s2f ,m1,m1 f ,m2=re al 0017:00 var m2f,t3,t3f,tt3,tt3f,1br,wtot=real 1 0018:00 var bst,bs2,bt3,bm1,bm2,btt3=real 0019:00 dim real av(3) 0020:00 dim real wa(3) 0021:00 dim ."eal wb(3) 0022:00 REM 0023:00 REM *** BURNS 7 ROE EAR FORCES ARE bs1 ete TURN ON WITH K=1*** 0024:00 REM 125:00 REM
.026:00 dim cral a(3,3) 0027:00 dim real b(3) 0028:00 dim real gic(3,3) 0029:00 1 - data 7.5, 10, .75, 1 95, 1.25, .7 0030:00 2 data 25,14.46,.53',53.,7.125,.31,1.5,2.5 0031:00 3 data 1150.,.875,.46,.648,.138,2.41,1.4 0032:00-4 data 399,277,5.25,0.5,28.5,15.,6.875 0033:00 5 data 40.,10.96,26.5,30.5,2.075 0034:00 6 data 90.,90.,180.,0.,90.,90.
0035:00 7 data 90.,100.,90.,180.,90.,90. 0036:00 REM DATA 6&7 FOR VALVE / GLOBAL-G ORIENTATIONS AND WEIGHT UECTOR 0037:00 restore 0038:00 read dl,d2,c1,il,c2,12 0039:00 restore 2 0040:00 read 1 rod, leg,x, phi, lave,ab1't,11,12 0041:00 restore 3 fgf 0042:00 read fst2,ca,la,cb,1b,aa,ab 0043:00 restore 4 ATTACl-WCMT 0044:00 read wao,wbr,el,e2,e3,e4,e'5 JOS NO. 82b44 0045:00 restore 5 pgggo,0"Cof/P 0046:00 read 1rodo,1cgo,1dr,d,abush 0047:00 restore 6 GHECTHO.g.{ 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) N l 51:00 text 0,& INPUT GLOBAL ACCELERATIONS & s v052:00 input b(1),b(2),b(3) 0053:00' print 0054:00 text 0,& INPUT DATA & 0055:00 print 0056:00 print " GLOBAL G-LEVELS = ";b(1),b(2),c(3) LES = ";a(1,1),a(2,1),a(3,1) l-
esdSN I*~UT GLOBAL ACCELERATIONS
? . 66,2.99,3.76 INPUT DATA GLOBAL G-LEVELS = 2.66 2.99 3.76 NORTH VECTOR ANGLES = 90 90 180 VERTICAL UECTOR ANGLES = 0 90 90 EAST VECTOR ANGLES = 90 180 90 WEIGHT VECTOR ANGLES = 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 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 OPERATING UALVE EAR SHEAR STRES 244.962 i OPERATING EAR BOLT SHEAR STRESS 2963.25 OPERATING EAR BOLT TENSILE STR 2615.86 D..AMIC COMPONENTS
( DRIVE ROD TENSILE STRESS AT A 15094.5 i DRIVE ROD TENSILE STRESS AT B 23086.2 BUSHING PRESSURE 294.409 VALVE EAR TENSILE STRESS 14765.9 UALVE EAR SHEAR STRESS 967.76 l EAR BOLT SHEAR STRESS 11706.8 EAR BOLT TENSILE STRESS 14229.2 FIXED PLUS DYNAMIC COMPONENTS l DRIVE ROD TENSILE STRESS AT A 20620.1 DRfUE ROD TENSILE STRESS AT B 31628.7 PUSHING PRESSURE 392.874 VALVE EAR TENSILE STRESS 18561.1 VALVE EAR SHEAR STRESS 1212.72 EAR BOLT SHEAR STRESS 14670 EAR BOLT TENSILE STRESS 16845.1 *"'i CYGNA ATTACHMENT JOB NO. 4204U1 FILE No,07.Ql/F _ SHEET NO.S*f- [
O b od34 - d IN 'JT GLOBAL ACCELERATIONS ' ;' 'C L < h1L6,)
?. s6,2.99,3.76 INPUT DATA GLOBAL G-LEVELS = 2.66 2.99 3.76 NORTH VECTOR ANGLES = 90 90 180 VERTICAL VECTOR ANGLES = 0 90 90 EAST VECTOR ANGLES = 90 180 90 WEIGHT VECTOR ANGLES = 180 90 90 LOCAL G-LEVELS -1.01471E-5 2.99 -1.43433E-5 -1.01471E-5 -1.14059E-5 -3.76 -2.66 -1.14059E-5 -1.43433E-5 OPERATING DRIVE ROD STRESS AT A 5525.52 OPERATING DRIVE ROD STRESS AT B 8542.57 OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING EAR WELD TENSILE STR 4338.59 OPERATING EAR WELD SHEAR STRES 519.72 OPERATING EAR BOLT SHEAR STRESS 2963.24 OPERATING EAR BOLT TENSILE STR 2615.86 O Di. A11C COMPONENTS DRIVE ROD TENSILE STRESS AT A 15094.5 DRIVE ROD TENSILE STRESS AT B 23086.2 BUSHING PRESSURE 294.409 y A EAR WELD TENSILE STRESS 16435.2 >
V 6 W EAR WELD SHEAR STRESS 2053.24 EAR BOLT SHEAR STRESS 11706.8 ATTACHMEgr. EAR BOLT TENSILE STRESS 14229.2 JOB NO. Afodd FIXED PLUS DYNAMIC COMPONENTS FILE NO. 00 SHEsTNC.A*I DRIVE ROD TENSILE STRESS AT A 20620.1 DRIVE ROD TENSILE STRESS AT B 31628.7 PUSHING PRESSURE 392.874 EAR WELD TENSILE STRESS 20773.8 EAR WE'.D SHEAR STRESS 2572.96 EAR BOLT SHEAR STRESS 14670 EAR BOLT TENSILE STRESS 16845.1 O b
codb24 If#UT GLOBAL ACCELERATIONS ? 36.2.99,3.76 INPUT DATA GLOBAL G-LEVELS = 2.66 2,99 3.76 NORTH UECTOR ANGLES = 90 90 180 VERTICAL VECTOR ANGLES = 0 90 90 EAST VECTOR ANGLES = 90 180 90 WEIGHT VECTOR ANGLES = 180 90 90 LOCAL G-LEVELS -1.01471E-5 2.99 -1.43433E-5 -1.01471E-5 -1.14059E-5 -3.76 -2.66 -1.14059E-5 -1.43433E-5 OPERATING DRIVE ROD STRESS AT A 5525.52 OPERATING DRIVE ROD STRESS AT B 8542.57 OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING VALVE EAR TENSILE STR 3795.21 OPERATING UALVE EAR SHEAR STRES 244.962 OPERATING EAR BOLT SHEAR STRESS 2963.25 OPERATING EAR BOLT TENSILE STR 2615.86 c1 -906.782 c2f= 1150 t3f=-2.57873E-3 m1f=-7906.15 m2f=-6234.1 tt3f=-12328.8 DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 15094.5 DRIVE ROD TENSILE STRESS AT B 23086.2 BUSHING PRESSURE 294.409 VALVE EAR TENSILE STRESS 14765.9 VALVE EAR SHEAR STRESS 967.76 EAR BOLT SHEAR STRESS 11706.8 EAR BOLT TENSILE STRESS 14229.2 hYh k sic,= 2711.27 ATTACHMENT 02d= 2541.76 t3d= 1798.16 , JOGNO.6Zo64 mld= 59281.6 FILE NO. OT Cl F m2d= 22662.6 SHEETNO.M*4 tt3d= 68555.7 F1XED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 20620.1 DRIVE ROD TENSILE STRESS AT B 31628.7 PUSHING PRESSURE 392.874 VALVE EAR TENSILE STRESS 18561.1 VALVE EAR-SHEAR STRESS 1212.72
EAR BOLT SHEAR STRESS 14670 , EAR BOLT TB4SILE STRESS 16845.1 sit = 3618.06
't3t= 1798.16 Cs2t=3691.76 m1t= 67187.O m2 28896.7 ,
tt3t= 80884.5 e O CYGNA ATTACHMENT JOBNO. AZO 44 FIL' N O. O T ol.F SHEETNO. 4-S < O
I csD3h IUT GLOBAL ACCELERATIONS
? . 9e,3.17.4.19 INPUT DATA GLOSAL G-LEVELS = 2.96 3.17 4.19 NORTH VECTOR ANGLES = 90 90 180 VERTICAL VECTOR ANGLES = 0 90 90 EAST VECTOR ANGLES = 90 100 90 WEIGHT VECTOR ANGLES = 180 90 90 LOCAL G-LEVELS -1.12915E-5 3.17 -1.59836E-5 -1.12915E-5 -1.20926E-5 -4.19 -2.96 -1.20926E-5 -1.59836E-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 OPERATING VALVE EAR SHEAR STRES 244.962 OPERATING EAR BOLT SHEAR STRESS 2963.25 OPERATING EAR BOLT TENSILE STR 2615.86 D .AMIC COMPONENTS l DRIVE ROD TEN 3ILE STRESS AT A 16003.2 DRIVE ROD TENSILE STRESS AT B 24476 BUSHING PRESSURE 312.133 VALVE EAR TENSILE STRESS 15743 UALVE EAR SHEAR STRESS 1034.29 EAR BOLT SHEAR STRESS 12511.6 EAR BOLT TENSILE STRESS 15776.8 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 21528.7 DRIVE ROD TENSILE STRESS AT B 33018.6 l
PUSHING PRESSURE 410.597 VALVE EAR TENSILE STRESS 19538.2 UALUE EAR SHEAR STRESS 1279.26 EAR BOLT SHEAR STRESS 15474.9 EAR BOLT TENSILE STRESS 18392.7 s2 - CYGNA ATTACHMENT
. JOB NO. MM FILE NC.dIOI[5 SHEET NO. M *O
s sp39 s IN UT GLOBAL ACCELERATIONE g, , g ,JC b i'
?. 86,3.17,4.19 _
INPUT DATA GLOBAL G-LEVELS = 2.96 3.17 4.19 NORTH VECTOR ANGLES = 90 90 180 VERTICAL VECTOR ANGLES = 0 90 90 EAST VECTOR ANGLES = 90 180 90 WEIGHT VECTOR ANGLES = 180 90 90 LOCAL G-LEVELS
-;.12915E-5 3.17 -1.59836E-5 -1.12915E-5 -1.20926E-5 -4.19 -2.96 -1.20926E-5 -1.59836L-5 OPERATING DRIVE ROD STRESS AT A 5525.52 OPERATING DRIVE ROD STRESS AT B 8542.57 OPERATING CYLItJDER BRG PRESSURE -98.4646 OPERATING EAR WELD TENSILE STR 4338.59 OPERATING EAR WELD SHEAR STRES 519.72 OPERATING EAR BOLT SHEAR STRESS 2963.24 OPERATING EAR BOLT TENSILE STR 2615.86 O D'. ti!C COMPONENTS DRIVE ROD TENSILE STRESS AT A 16003.2 DRIVE ROD TENSILE STRESS AT B 24476 BUSHING PRESSURE 312.133 EAR WELD TENSILE STRESS 17548.3 EAR WELD SHEAR STRESS 2194.4 EAR EOLT SHEAR STRESS 12511.6 EAR BOLT TENSILE STRESS 15776.8 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 21528.7 DRIVE ROD TENSILE STRESS AT B 33018.6 PUSHING PRESSURE 410.597 EAR WELD TENSILE STRESS 21886.9 EAR WELD SHEAR STRESS 2714.12 y EAR BOLT SHEAR STRESS 15474.9 '
V ' -- EAR BOLT TENSILE STRESS 18392.7 ATTACHMENT , JOS NO. 8 HLE NO. ON'b-SHEITNO O~ l g V
CODw4 IN NT GLGEAL ACCELERATIONS .
? ' 96,3.17,4.19 INPUT DATA GLOBAL G-LEVELS = 2.96 3.17 4.19 NORTH VECTOR ANGLES = 90 90 180 VERTICAL VECTOR ANGLES = 0 90 90 EAST VECTOR ANGLES = 90 180 90 WEIGHT VECTOR ANGLES = 180 90 90 LOCAL G-LEVELS -1.12915E-5 3.17 -1.59836E-5 -1.12915E-5 -1.2092dE-5 -4.19 -2.96 -1.20926E-5 -1.59536E-5 OPERATING DRIVE ROD STRESS AT A 5525.52 OPERATING DRIVE ROD STRESS AT B 8542.57 OPERATING CYLINDER BRG PRESSURE -96.4646 OPERATING VALVE EAR TENSILE STR 3795.21 OPERATING VALVE EAR SHEAR STRES 244.962 OPERATING EAR COLT SHEAR STRES2 2963.25 OPERATING EAR BOLT TENSILE STR 2615.86 c1 -906.782 c2t- 11E0 t3f=-2.57873E-3 m1f=-7906.15 m2f=-6234.1 tt3f=-12228.8 DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 16003.2 DRIVE ROD TENSILE STRESS AT B 24476 BUSHING PRESSURE 312.133 VALVE EAR TENSILE STRESS 15743 VALVE EAR SHEAR STRESS 1034.29 EAR BOLT SHEAR STRESS 12511.6 EAR BOLT TENSILE STRESS 15776.8 cid= 2874.49 CVGNA s2d= 2832.44 ATTACHMENT l t3d= 2000.96 mid= 65975.4 JOB NO* SIdWbd m2d= 24418.8 FILE NO. 07 OI*Er tt3d= 72951.2 SHEET NO. 4-6 F .ED PLUS DYNAMIC COMPONEt4TS DRIVE ROD TENSILE STRESS AT A 21528.7 DRIVE ROD TENOILE STRESS AT B 33018.e PUSHING PRESSURE 410.507 VALVE EAR TENSILE STRESS 19538.2 UALVE EAR SHEAR STRESS 1279.26 CAR Rni T 4HFAR RTRems ima74.o
~ ' '
hRhhthiss!Lh'sikkSS l h395.'h 51t= 3781.28 52t= 3982.44
)3t= 2000.96 dit= 73881.5 m2' - 30652.9 tt-.= 85280 l
i l - CVGMA ATTACHMENT JOB NO. 8IM FILE NO. 07 of.p SMSET NO. 4~9
ccp 3$) INSUT GLOBAL ACCELERATIONS E.Kf E GE NCY (C ucd Mc: f F- /- A'
?* ,0,1.97,1.71 INPUT DATA GLOBAL G-LEVELS = 2.8 1.97 1.71 NORTH VECTOR ANGLES = 90 90 180 VERTICAL VECTOR ANGLES = 0 90 90 EAST VECTOR ANGLES = 90 180 90 viEIGHT VECTOR ANGLES = 180 90 90 LOCAL G-LEVELS -1.Od?11E-5 1.97 -6.52313E-6 -1.0cE11E-5 -7.51495E-6 -1.71 -2.5 -7.51495E-6 -6.52313E-6 OPERATING DRIVE ROD STRESS AT A 5525.52 OPERATING DRIVE ROD STRESS AT B 8542.57 OPEPATING CYLINDER BRG PRESSURE -98.4646 OPERATING EAR WELD TENSILE STR 4338.59 OPERATING EAR WELD SHEAR STRES 519.72 GPERATING EAR LOLT SHEAR STRESS 2963.24 ' OPERATING EAR BOLT TENSILE STR 2615.86 D'. .MIC COMPONENTS DRIVE RCD TENSILE STRESS AT A 9945.23 DRIVE ROD TENSILE STRESS AT B 15210.7 BUSHING PRESSURE 193.975 84R WELD TENSILE STRESS 10668.6 EAR WELD SHEAR STRESS 1296.94 EAR BOLT SHEAR STRESS 7394.64 EAR BOLT TENSILE STRESS 14365.1
( FIXED PLUS DYNAMIC COMPONENTS l l DRIVE ROD TENSILE STRESS AT A 15470.8 ( DRIVE ROD TENSILE STRESS AT B 23753.2 PUSHING PRESSURE 292.44 EAR WELD TENSILE STRESS 15007.2 EAR WELD SHEAR STRESS 1816.66 EAR BOLT SHEAR STRESS 10357.9 EAR BOLT TENSILE STRESS 16980.9 - i CVGKA v.m.= maur a No.M 1 FILE No. 0T.01.9 SHEET NO.N l
/~'ap39 4 bdNPDTGLOBALACCELERATIONS QP5bT d.1/CI.4/>ES dM /~d)1
?1 14,1.40,1.5 INPUT DATA GLOBAL G-LEVELS = 1.14 1.4 1.5 NORTH VECTOR ANGLES = 90 90 180
- i. VERTICAL VECTOR ANGLES = 0 90 90 EAST VECTOR ANGLES = 90 180 90 WEIGHT VECTOR ANGLES = 180 90 90 LOCAL G-LEVELS
-4.34875E-6 1.4 -5.72204E-6
-4.34875E-6 -5.34057E-6 -1.5
-1.14 -5.34057E-6 -5.72204E-6 OPERATING DRIVE ROD STRESS AT A 5525.52 OPERATING DRIVE ROD STRESS AT B 8542.57 OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING EAR WELD TENSILE STR 4338.59 OPERATING EAR WELD SHEAR STRES 519.72 OPERATING EAR BOLT SHEAR STRESS 2963.24 OPERATING EAR BOLT TENSILE STR 2615.86 v F 'Vi!C CCNPONENTS ,
DRIVE ROD TENSILE STRESS AT A 7067.68 DRIVE ROD TENSILE STRESS AT B 10809.6 , BUCHING PRESSURE 137.85 l EAR WELD TENSILE STRESS 7558.92 EAR WELD SHEAR STRESS 940.609 EAR BOLT SHEAR STRESS 5364.13 EAR BOLT TENSILE STRESS 6129.04 FIXED PLUS DYNAMIC COMPONENTS l l DRIVE ROD TENSILE STRESS AT A 12593.2 DRIVE ROD TENSILE STRESS AT B 19352.2 PUSHING PRESSURE 236.315 EAR WELD TENSILE STRESS 11897.5 EAR WELD SHEAR STRESS 1460.53 EAR BOLT SHEAR STRESS 8327.37 l EAR BOLT TENSILE STRESS 8744.9
.CVGRA l l ATTACMMENT lJOSNC.82044
[ 81LE NO. 0I0I'O \ (d SHEE"HC. A'II
m sbasic esp 5 tm S-BASIC Compiler Version 5.46 v001:00 REM ***** 8IF VALUE AND AIR OPERATOR SEISMIC STRESS ***** 0002:00 REM *************** CSP-V/AO-L ************************** 0003:00 REM 0004:00 var i,J,k = integer 0005:00 var I rod ,1 cg,x , ph i ,l ave , abi t ,11,12,e l , e2, e3, e4, e5 = real 0006:00 var fst2, ca,la,cb,ib,aa,ab,dt.d2,c1,il.c2,i2=real 0007:00 var 1rodo,lego,1dr,d, abush, pbush=real 0008:00 var fcof, f eo, ma,mb, siga, sigb, fedr, fcdrf,maf, mbf=real 0009:00 var dear, fcear,fr, fil,f22,la, cl12,ci21,stt3,sem1=real l 0010:00 var sem2, set 3,sest ses2.sr, tau 11, tau 22,tauear,aear=real l 0011:00 var btens, taubit, set 3f',semif,sem2f,fcearf, f rf ,f11 f=r eal 1 0012:00 var f 22f ,st t3f , sest f ses2f ,srf , taulf , tau 2f , taurf=real 0013:00 var taubf,btf, dsr,dtaur,dtaub,dbten,dsa,dsb,dpb=real 0014:00 var sdr af , sdrbf ,pbushf , t au11 f , t au22f =real 1 0015:00 var wao,wbr,ftri,watri,s1,s1f,s2,s2f,m1,mif,m2=real 0016:00 var m2f t3,t3f,tt3,tt3f,1br,wtot=real i 0017:00 var bs1,bs2,bt3,bm1,bm2,btt3=real 0018:00 dim real av(3) 0019:00 dim real wa(3) 0020:00 dim real wb(3) 0021:00 REM l 0022:00 PEM *** 8 URNS 7 ROE EAR FORCES ARE bst etc TURN ON WITH K=1*** l 0023:00 REM 0024:00 REM 0025:00 dim real a(3,3) 326:00 dim real b(3) 0027:00 dim real gic(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 l 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.,10.96,26.5,30.5,2.075 l 0033:00 6 data 42.5,47.5,90.,90.,90.,0.
0034:00 7 da t a 47. 5,137. 5,90. ,180. ,90. ,90. l 0035:00 REM DATA 6&7 FOR VALVE / GLOBAL-G ORIENTATIONS AND WEIGHT VECTOR ! 0036:00 restore - l 0037:00 read dl,d2.ci,il,c2,i2 j 0038:00 restore 2 l 0039:00 re ad I rod,1 cg, x ,ph i ,1 ave , abi t ,11,12 1 0040:00 restore 3 0041:00 read fst2 ca,la,cb,ib,aa,ab 0042:00 restore 4 0043:00 read wao,wbr,el,e2,e3,e4,e5 0044:00 0045:00 restore 5 read Irodo,1cgo,1dr,d,abush ())[(]!hh k 0046:00 restore 6 ATTACHMENT 0047:00 read a(1,1),a(2,1),a(3,1),a(1,2),a(2,2),a(3,2) 0048:00 restore 7 JOB NO. 62044 0049:00 read a(1,3),a(2,3) a(3,3),av(1),av(2),av(3) FILE NO. CYIOIjE 0050:00 text 0,& INPUT GLOBAL ACCELERATIONS & SHEET NO. A-12
'51:00 input b(1),b(2),b(3) {
.J52:00 prirt 0053:00 text 0,& INPUT DATA &
's o 5 IUT GLOBAL ACCELERATIONS ? . 76,3.44,5.42 INPUT DATA GLOBAL G-LEVELS = 2.96 3.44 5.42 NORTH VECTOR ANGLES = 142.5 47.5 90 VERTICAL VECTOR ANGLES = 90 90 0 EAST UECTOR ANGLES = 47.5 137.5 90 WEIGHT VECTOR ANGLES = 180 90 90 LOCAL G-LEVELS 2.18234 -1.31225E-5 3.66169 1.99974 -1.31225E-5 -3.99606 -1.12915E-5 3.44 -2.06756E-5
- OPERATING DRIVE ROD STRESS AT A 5048.35 OPERATING DRIVE ROD STRESS AT B 7721.14 OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING VALVE EAR TENSILE STR 4664.25 OPERATING VALVE EAR SHEAR STRES 297.614 OPERATING EAR BOLT SHEAR STRESS 3600.17 OPERATING EAR BOLT TENSILE STR 1340.69 D..AMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 21519.6 DRIVE ROD TENSILE STRESS AT B 32912.8 BUSHING PRESSURE 419.724 VALVE EAR TENSILE STRESS 20190.5 VALVE EAR SHEAR STRESS 1312.91 EAR BOLT SHEAR STRESS 15882 EAR BOLT TENSILE STRESS 19507 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 26567.9 DRIVE ROD TENSILE STRESS AT B 40633.9 l PUSHING PRESSURE 518.189 VALVE EAR TENSILE STRESS 24854.8 VALVE EAR SHEAR STRESS 1610.53 l EAR BOLT SHEAR STRESS 19482.2 EAR BOLT TENSILE STRESS 20847.7 l
l CYGNA ATTACHMENT bT JOB NO. SDM FILE NO. 0TOf/F SHEET NO. MY
1 ? UT GLOBAL ACCELERATIONS 26,3.44,5.42
'. .,.4 2 , g [- g ;,-~
l INPUT DATA l GLOBAL G-LEVELS = 2.96 3.44 5.42 NCRTH VECTOR ANGLES = 42.5 47.5 90 VERTICAL VECTOR ANGLES = 90 90 0 EAST VECTOR ANGLES = 47.5 137.5 90 WEIGHT VECTOR ANGLES = 180 90 90 LOCAL G-LEVELS i l 2.18234 -1.31225E-5 3.66169 l 1.99974 -1.31225E-5 -3.99606 -1.12915E-5 3.44 -2.06756E-5 l OPERATING DRIVE ROD STRESS AT A 5048.35 l OPERATING DRIVE ROD STRESS AT B 7721.14 OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING EAR WELD TENSILE STR 5107.51 OPERATING EAR WELD SHEAR STRES 631.431 OPERATING EAR BOLT SHEAR STRESS 3600.17 OPERATING EAR BOLT TENSILE STR 1340.69 D VilC COMPONENTS DRIVE ROD TENSILE STRESS AT A 21519.6 DRIVE ROD TENSILE STRESS AT B 32912.8 BUSHING PRESSURE 419.724 EAR WELD TENSILE STRESS 22736.7 EAR WELD SHEAR STRESS 2785.52 EAR BOLT SHEAR STRESS 15882 EAR BOLT TENSILE STRESS 19507 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 26567.9 y. yA DRIVE ROD TENSILE STRESS AT B 40633.9 L U VJ N" PUSHING PRESSURE 518.189 EAR WELD TENSILE STRESS 27844.2 4774ggggg. 8 EAR WELD SHEAR STRESS 3416.95 JOBNO. 6fockf EAR BOLT SHEAR STRESS 19482.2 EAR BOLT TENSILE STRESS 20047.7 FILE N3* OIO/ F I SHEET NO. A*/4 I l
O t UT OLOBAL ACCELERATIONS
? 96,3.44,5.42 INPUT DATA GLOBAL G-LEVELS = 2.96 3.44 5.42 NORTH VECTOR ANGLES = 42.5 47.5 90 VERTICAL VECTOR ANGLES = 90 90 0 EAST VECTOR ANGLES = 47.5 137.5 90 WEIGHT VECTOR ANGLES = 180 90 90 LOCAL G-LEVELS 2.18234 -1.31225E-5 3.66169 1.99974 -1.31225E-5 -3.99606
-1.12915E-5 3.44 -2.06756E-5 OPERATING DRIVE ROD STRESS AT A 5048.35 .
OPERATING DRIVE ROD STRESS AT B 7721.14 OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING VALVE EAR TENSILE STR 4664.25 OPERATING VALUE EAR SHEAR STRES 297.614 OPERATING EAR BOLT SHEAR STRESS 3600.17 OPERATING EAR BOLT TENS 1LE STR 1340.69 p c1 -906.782 c2f=-2.57874E-3 t3f=-2.57873E-3 m1f= 9.89667E-2 m2f=-6234.1 tt3f=-22103.8 DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 21519.6 DRIVE ROD TENSILE STRESS AT B 32912.8 BUSHING PRESSURE 419.724 I VALVE EAR TENSILE STRESS 20190.5 VALVE EAR SHEAR STRESS 1312.91 EAR BOLT SHEAR STRESS 15882 EAR BOLT TENSILE STRESS 19507 sid= 3865.34 S2d= 3020.7 GNA i t3d= 2325.44 ATTACHMENT m& 69.7 JOB NO. 0YOAA tt3d= 84539.5 FILE NO. OT0l' F l SHEET NO. AS l Q F., SED PLUS DYNAMIC COMPONENTS l DRIVE ROD TENSILE STRESS AT A 26567.9 DRIVE ROD TENSILE STRESS AT B 40633.9 PUSHING PRESSURE 518.189 VALVE EAR TENSILE STRESS 24854.8 VALVE EAR SHEAR STRESS 1610.53
c D INPUT GLOBAL ACCELERATIONS LlPSET
? . *7,1.4,1.71 INPUT DATA GLOBAL G-LEVELS = .97 1.4 1.71 NORTH VECTOR ANGLES = 42.5 47.5 90 VERTICAL VECTOR ANGLES = 90 90 0 EAST VECTOR ANGLES = 47.5 137.5 90 WEIGHT UECTOR ANGLES = 180 90 90 LOCAL G-LEVELS .715158 -5.34057E-6 1.15526 .455321 -5.34057E-6 -1.26075 -3.70025E-6 1.4 -6.52313E-6 OPERATING DRIVE ROD STRESS AT A 5048.35 OPERATING DRIVE ROD STRESS AT B 7721.14 OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING EAR WELD TENSILE STR 5107.51 OPERATING EAR WELO SHEAR STRES 631.431 -
OPERATING EAR BOLT SHEAR STRESS 3600.17 OPERATING EAR BOLT TENSILE STR 1340.69 DV T11C COMPONENTS DRIVE ROD TENSILE STRESS AT A 6859.18 DRIVE ROD TENSILE STRESS AT B 10490.7 BUSHING PRESSURE 133.784 EAR WELD TENSILE STRESS 7323.31 EAR WELD SHEAR STRESS 892.936 l EAR BOLT SHEAR STRESS 5091.16 l EAR BOLT TENSILE STRESS 7599.75 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 11907.5 DRIVE ROD TENSILE STRESS AT B 18211.9 l PUSHING PRESSURE 232.249 EAR WELD TENSILE STRESS 12430.8 EAR WELD SHEAR STRESS 1524.37 p'%r ret ['. r c4d D (52Ltedh EAR BOLT SHEAR STRESS 8691.33 gggg. EAR BOLT TENSILE STRESS 8940.43 ' JOB NO. 82d44 FILE NO. OTd/ F SHET~NL.A~lb e
l
. .. ,sbasic csp 6 i (v'j tm S-BASIC Complier Version 5.46 )
J01:00 REM ***** BIF VALVE AND AIR OPERATOR SEISMIC STRESS.***** 0002:00 REM *************** CSP-V/AO-6 ************************** 0003:00 REM 0004:00 var 1,J,k = integer 0005:00 var t rod,1 cg , x ,ph i ,l av a , abi t ,11,12, e l ,e2, e3, e4, e5 = real ! 0D06:00 var fst2, c a , l a , cb , i b , aa , ab , di , d2, c t , i'1, c 2,12=r e al 0007:00 var I rodo ,1 c go ,1 de , d , abush', pbush=real 0008:00 var fcof, feo, ma,mb, siga, sigb, fedr, fedef,maf, mbf= teal 0009:00 var dear, fcear,fr, f11,f22,la, ci12,ci21,stt3,sem1=real 0010:00 var sem2,se t3,sest ,ses2,sr , tau 11, tau 22, tauear ,aear=real 0011:00 var btens, taubit, set 3f,semif,sem2f,fcearf, frf,filf-reel 0012:00 var f 22f ,st t3f ,sest f ,ses2f ,srf , taul f , tau 2f , taunf =real 0013:00 var taubf,btf, dsr,dtaur,dtaub,dbten,dsa,dsb,dob=real 0014:00 var sdraf,sdrbf,pbushf, tau 11f tau 22f=real i 0015:00 var wao,wbr,ftr1,watri,si,stf,s2,s2f,m1,m!f,m2=r.eal 0016:00 var m2f,t3,t3f,tt3,tt3f,1br,wtot=real 0017:00 var bst , bs2,bt3,bm1, bn2,bt t3=re al ~ 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 bs15etc TURN ON WITH K=1*** 0023:00 REM 0024:00 REM [s dim real a(3,3) -
\s>) 0025:00 126:00 dim real b(3) 9027:00 dim real gic(3,3) 0028:00 1 data 7.5, 10, .75. 1.95, 1.25, .7 0029:00 2 data 25,14.46,.5.' ,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.,10.96,26.5,30.5,2.075 0033:00 6 data 90.,90.,0 ,0.,90.,90. , 0034:00 7 ' data 90.,0.,90.,100.,90.,90'. .. . 0035:00 REM DATA 6&7 FOR VALVC/ GLOBAL-G ORIENTATIONS AND WEIGHT VECTOR 0036:00 restore ,
~
0037:00 read dl,d2,c1,li,c2,12 m 0038:00 restore 2 0030:00 read 1 rod,1 cg,x ,ph i ,l av e ,abi t ,11,12 , 0040:00 restore 3 ' l 0041:00 read fst2,ca,ia.cb,ib,aa,ab 0042:00 restore 4 0043:00 read wao,wbr,el,e2,e3,e4,e5 CYGPM 0044:00 restore 5 ATTACHMENT 0045:00 read 1rodo,1cgo,1dr,d,abush 0046:00 restore 6 j , g jpgg4 4 0047:00 read a(1,1),a(2,1),a(3,1),a(1,2),a(2.2),a(3,2) FILE NO. of.0i!P 0048:00 rectore 7 0049:00 read a(1,3),a(2,3),a(3,3),av(1),av(2),av(3) SHEET NO. 4*IS 0050:00 text 0,& INPUT GLOBAL ACCELERATIONS &
, 0051:00 input b(1),b(2),b(3) 52:00 print N 0053:00 text 0,& INPUT DATA & ,
0054:00 print 0055:00 print " GLOBAL G-LEVELS = *;b(F),b(2),b(3) 0056:00 print " NORTH VECTOR ANGLES = ";a(1,1),a(2,1),a(3,1)
0060:00har i=1 to 3 0061:01 for J=1 to 3 0062:02 a( J ,1 )=a( J ,1 ) o2. o3.1416/360. 0063:02 gic(J,1)=b(i>*cos(a(),i)) 0064:02 next J 0065t01 next i
'966:00 for J=1 to 3 J67:01 av(j)=av(J)*2.*3.1416/360.
0068:01 next J 0069:00 print 0070:00 text 0,& LOCAL G-LEVELS & 0071:00 print
- 0072:00 print gic(1,1),gic(1,2),gic(1,3) 0073:00 print gic(2,1),gic(2,2),9 1 c(2,3) 0074:00 print gic(3,1),gic(3,2),gic(3,3) 0075:00 REM WEIGHT COMPONENTS 0076:00 for J=1 to 3 0077:01 wa(J)=wao*cos(avCJ))
0078:01 wb(J)=wbr*cos(av(J)) 0079:01 next J . 0080:00 phl= phi *2.*3.1416/360. 0081:00 la=1 ave /2 0082:00 c i12=c1/12 0083:00 ci21=c2/11 0084 00 aear=11*12 0085:00 REM CALCULATE EAR FORCES USE B&R LOADS AS OPTION LATER 0086:00 REM FIXED COMPONENTS ARE ALWAYS THERE 0087:00 Ibr=lrod+1cg 0088:00 watr1=1br*wa(1)/Irod 0089:00 s1f=wb(1)+watrl 0090:00 wtot=wao+wbr 0091:00 s2f=wb(2)+wa(2)+fst2 92:00 t3f=wa(3)+wb(3) 9093:00 m1f=-(wa(2)+wb(2)+fst2)*e5-wa(3)*(e3+1cg)-wb(3)*e4 0094:00 m2f=(watrl+wb(1))*e5-wa(3)*e2-wb(3)*e1 0095:00 tt3f=wate!*e3+(wa(2)+fst2)*e2+wb(1)*e4+wb(2)*e1 0096:00 fedrf= leg *wa(1)/1 rod 0097:00 maf=fedef*(Irod-13.5) 0098:00 mbf=fedrf*7.125 0099:00 sdraf =f st 2/aa+ abs (maf *c a/ l a) 0100:00 sdebf=fst2/ab+ abs (mbf*cb/lb) ! 0101:00 fcof=1cgo*wa(1)/Irodo 0102:00 pbushf=fcof*(1dr+d)/(d*abush) j 0103:00 REM STRESSES FROM FIXED COMPONENTS I 0104:00 dear =(d1*d1+d2*d2)**.5 0105:00 set 3f= abs (t3f/(4*aear)) j 0106:00 sem1f= abs (m1f/(2*d2*aear>> 0107:00 sem2f= abs (m2f/(2*d1*aear)) #% A 0108:00 fcearf=tt3f/(2* dear) -gy%JEI M 0109:00 frf=x*fcearf 0110:00 f11f=-(feearf* sin (phl)-frf*cos(phi >> ATTACHMENT 0111:00 f22f=fcearf*cos(phi)+frf* sin (phi) JOB NO. A2fHid [ 0112:00 stt3f= abs (f11f*1a*ci12)+ abs (f22f*1a*ci21) F11E NO, dT".of/P 0113:00 sestf= abs (sif*ci12*1a/4.) 0114:00 ses2f= abs (s2f*ci21*1a/4.) SHEET NO. M "#EO 0115:00 srf= set 3f+semif+sem2f+sestf+ses2f+stt3f 0116:00 REM EAR SHEAR
**17:00 tau 11f= abs (stf/(4*aear))+ abs (f11f/aear) 18:00 tau 22f= abs (s2f/(4*aear>>+ abs (f22f/aear) 0119:00 taurf=(tau 11f* tau 11f+ tau 22f* tau 22f>**.5 0120:00 taubf=taurf*aear/abit l 0121:00 REM EARBOLT TENSION 0122:00 btf=(set 3f+semif+sem2f)*aear/abit 0123:00 print l 0124:00 print" OPERATING DRIVE ROD STRESS AT A *isdraf r999,nn noin&#ODCDATTNA hD T L JC D00 CTDCCC AT D " edeh4
......c..... . . . . . . . . , . , . . . . . . . , . , , . . . . . . . . , , . . .
0126:00 print" OPERATING CYLINDER BRG PRESSURE ";pbushf 0127:00 print" OPERATING UALVE EAR TENSILE STR ";srf 0128:00 print" OPERATING VALVE EAR SHEAR STRES ";taurf 0129:00 print"0PERATING EAR BOLT SHEAR STRESS ";taubf 0130:00 print"0PERATING EAR BOLT TENSILE STR ";btf k 0131:00 print
^132:00 REM
.33:00 REM CALCULATE VARIABLE COMPONENTS 0134:00 REM 0135:00 dsr=0.
0136:00 dtaur=0. 0137:00 dtaub=0. 0138:00 dbten=0. 0139:00 dsa=0. 0140:00 dsb=0. 0141 :00 dpb=0. 0142:00 for J=1 to 3 0143:01 fco=1cgo*wao*gic(1.J)/1rodo 0144:01 pbush=fco*(1dr+d>/(d*abush) 0145:01 ftrl=1br*wao*gic(1,Ji/Irod 0146:01 s1=ftr1+wbr*gic(1,J) 0147:01 s2=wtot5gic(2,J) 0148:01 t3=wtot*gIc(3,J) 0149: 01 m1=-wto t*gi c ( 2, J ) *e5-wao*gi c( 3, J ) *( e3+ 1 c g)-wbr*gi c ( 3,J ) *e4 0150 :01 m2=(f tr 1+wbr*gi c(1,J )) *e5-(wao*e2+wbr*e1)*gi c(3,J ) 0151:01 t t 3=f t r 1 *e 3+wbr *gi c ( 1, J ) *e4+ gi c ( 2, J ) *(wao*e 2+wbr*e l ) 0152:01 fedr=Icg*wao*gic(1,J)/Irod 0153:01 ma=fedr*(Irod-13.5) 0154:01 mb=fedr*7.125 0155:01 siga=ma*ca/la 0156:01 sigb=mb*cb/ib 0157:01 REM CALCULATE EAR TENSION
, Os 58:01 set 3= abs (t3/(4*aear))
.459:01 sem1= abs (m1/(2*d2*aear))
0160:0!-sem2= abs (m2/(2*d1*aear)) 0161:01 fcear=tt3/(2* dear) 0162:01 fr=x*fcear 0163:01 f11=-(feear*s!n(phi)-fr*cos(phi)) 0164:01 f22=fcear*cos(phi >+fr* sin (phi) 0165:01 stt3= abs (f11*1a*ci12)+ abs (f22*1a*ci21) 0166:01 se s1= abs ( s1 *c i 12*1 a/4. ) 0167:01 ses2= abs (s2*ci21*1a/4.) 0168:01 sr= set 3+sem1+sem2+sesl+ses2+stt3 0169:01 REM EAR SHEAR 0170:01 tau 11= abs (s1/(4.*aear))+ abs (f11/aear) 0171:01 tau 22= abs (s2/(4.*aear))+ abs (f22/aear) - 0172:01 tauear=(tau 11* tau 11+ tau 22* tau 22)**.5
-0173:01 taubit=tauear*aear/abit 0174:01 REM EARBOLT TENSION 0175:01 btens=(set 3+sem1+sem2)*aear/abit l
0176:01- dsa=dsa+siga*siga CYC= NA j 0177:01 dsb=dsb+sigb*sigb ATTACHMENT ! 0178:01- dpbadpb+pbush*pbush L 0179:01 dsr=dsr+s?*se JOB NO._^f 04d l 0180:01 dtaur=dtaur+tauear*tauear FRE NO. OI*OI E l 0181:01- d t au b=dt aub+ t aubi t* t aubi t SHEET NC. jp2/- 0182:01 dbten=dbten+btens*btens a183:01 next J S4:00 REM COMBINE STRESSES s- '0185:00 daa=dsa**.5 0186:00 dsb=dsb**.5 0187:00 dpb=dpb**.5 0188:00 dsr=dsr**.5 0189:00~ dtaur=dtaur**.5 0190:00 dtaub=dtaub**.5 nion.nn as+...sw .-.o a
..,.... os.... oo....--..
0192500 print 0193 00 text 0,& DYNAMIC COMPONENTS & 0194:00 print 0195:00 print " DRIVE ROD TENSILE STRESS AT A";dsa 0196:00 print " DRIVE ROD TENSILE STRESS AT B";dsb 0197:00 print " BUSHING PRESSURE ";dpb
~198:00 print "UALVE EAR TENSILE STRESS ";dsr
.99:00 print "VALUE 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=dsb+ abs (sd,rbf) 0204:00 dpb=dpb+ abs (pbushf) 0205:00 dsr=dsr+ abs (srf) 0206:00 dtaur=dtaur+ abs (taurf) 0207:00 dtaub=dtaub+ abs (taubf)
C208:00 dbten=dbten+ abs (btf) 0209:00 print 0210:00 text 0,& FIXED PLUS DYNAMIC COMPONENTS & 0211:00 print 0212:00 print " DRIVE ROD TENSILE STRESS AT A";dsa 0213:00 print " DRIVE ROD TENSILE STRESS AT B";dsb 0214:00 print " PUSHING PRESSURE ";dpb 0215:00 print "bALVE EAR TENSILE STRESS ";dse 0216:00 print " VALVE EAR SHEAR STRESS ";dtaur 0217:00 print " EAR BOLT SHEAR STRESS ";dtaub 0218:00 print " EAR BOLT TENSILE STRESS ";dbten 0219:00 end 0220:00 0221:00 0222:00 0223:00
!24:00 w225:00 ****** End of program ******
I CYGNA ATTACHMENT JOB NO. 020dd FILE NO. OY'OIh SHEETNO.A*N 9
CCD6 (S ) INPUT GLOBAL ACCELERATIONS M 11.39.3.33.5.85 livUT DATA GLOBAL G-LEVELS = 11.39 3.33 5.85 NORTH VECTOR ANGLES = 90 90 0 VERTICAL VECTOR ANGLES = 0 90 90 EAST VECTOR ANGLES = 90 0 90 LOCAL G-LEVELS
-4.344?4E-5 3.33 -2.2316E-5
-4.34494E-5 -1.27029E-5 5.85 11.39 -1.27029E-5 -2.2316E-5 OSERATING DRIVE ROO STRESS AT A 5048.35 OPERATING DRIVE ROD STRESS AT B 7721.14 OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING VALVE EAR TENSILE STR 4664.25 OPERATING VALVE EAR SHEAR STRES 297.614 OPERATING EAR BOLT SHEAR STRESS 3600.17 OPERATING EAR BOLT TENSILE STR 1340.69 DYNAMIC COMPONENTS F E ROD TENSILE STRESS AT A 16811 drave ROD TENSILE STRESS AT B 25711.4 -
BUSHING PRESSURE 327.887 VALVE EAR TENSILE STRESS 17822.1 VALVE EAR SHEAR STRESS 1154.32 EAR BOLT SHEAR STRESS 13963.6 EAR BOLT TENSILE STRESS 57543 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 21859.4 DRIVE ROD TENSILE STRESS AT B 33432.5 PUSHING PRESSURE 426.352 VALUE EAR TENSILE STRESS 22486.4 VALVE EAR SHEAR STRESS 1451.93 EAR BOLT SHEAR STRESS 17563.7 EAR BOLT TENSILE STRESS 38883.7 i i .- . CYGNA ATTACHMENT JOB NO.} 2044 FILE NO.DT*oll; SHEETNO. A*25 l-
cop 6 GLOEAL ACCELERATIONS
? .39.3.33,5.85 INPUT DATA GLOBAL G-LEVELS = 11.39 3.33 5.85 NORTH VECTOR ANGLES = 90 90 0 VERTICAL VECTOR ANGLES = 0 90 90 EAST VECTOR ANGLES = 90 0 90 LOCAL G-LEVELS -4.34494E-5 3.33 -2.2316E-5 -4.34494E-5 -1.27029E-5 5.85 11.39 -1.27029E-5 -2.2316E-5 OPERATING DRIVE ROD STRESS AT A 5048.35 OPERATING DRIVE ROD STRESS AT B 7721.14 OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING EAR WELD TENSILE STR 5107.51 OPERATING EAR WELD SHEAR STRES 631.431 OPERATING EAR BOLT SHEAR STRESS 3600.17 OPERATING EAR BOLT TENSILE STR 1340.69 DvNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 16811 DRIVE ROD TENSILE STRESS AT B 25711.4 BUSHING PRESSURE 327.887 -
EAR WELD TENSILE STRESS 21586.2 i EAR WELD SHEAR STRESS 2449.05 l EAR BOLT SHEAR STRESS 13963.6 l EAR BOLT TENSILE STRESS 57543 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 21859.4 DRIVE ROD TENSILE STRESS AT B 33432.5 PUSHING PRESSURE 426.352 y y EAP. WELD TENfiLE STRESS 26693.7 U N EAR WELD SHEAR STRESS 3080.48 EAR BOLT SHEAR STRESS 17563.7 ATTACHMENT EAR BOLT TENSILE STRESS 58883.7 JOH NO. 88044 FILE NC. OT*OI E SHEETNO.M-74 O
l 1 l ap6 INDUT GLOBAL ACCELERATIONS '
? .39,3.33,5.85 l INPUT DATA GLOBAL G-LEVELS = 11.39 3.33 5.85 NORTH VECTOR ANGLES = 90 90 0 VERT: CAL VECTOR ANGLES = 0 90 90 EAST VECTOR ANGLES = 90 0 90 LOCAL G-LEVELS
-4.34494E-5 3.33 -2.2316E-5
-4.34494E-5 -1.27029E-5 5.85 11.39 -1.27029E-5 -2.2316E-5 OPERATING DRIVE ROD STRESS AT A 5046.35 OPERATING DRIVE ROD STRESS AT B 7721.14 CPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING VALVE EAR TENSILE STR 4664.25 OPERATING VALVE EAR SHEAR STRES 297.614 CDERATING EAR BOLT SHEAR STRESS 3600.17 OPERATING EAR BOLT TENSILE STR 1340.69
.g(')
j i' -906.782 c2. -2.57874E-3 t3f=-2.57873E-3 m1f= 9.89667E-2 m2f=-6234.1 tt3f=-22103.8 DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 16811 DRIVE ROD TENSILE STRESS AT B 25711.4 BUSHING PRESSURE 327.887 VALVE EAR TENSILE STRESS 17822.1
- VALVE EAR SHEAR STRESS 1154.32 EAR BOLT SHEAR STRESS 13963.6
! EAR BOLT TENSILE STRESS 57543 old= 3019.58 c2d= 3954.6 i t3d= 7699.63 mid= 2.44083E+5 (yh%k m2d= 58968.3 ATTACHMENT tt3d= 78875.3 gg FILE NO. of.M. F
,/^'~ ID PLUS DYNAMIC COMPCNENTS SMEET NO. A 'Z5 L.)
! DRIVE ROD TENSILE STRESS AT A 21859.4 l DRIVE ROD TENSILE STRESS AT B 33432.5 PUSHING PRESSURE 426.352 t VALVE-EAR TENSILE STRESS 22486.4 VALVE EAR SHEAR STRESS 1451.90 EAR BOLT SHEAR STRESS 17563.7
EAF ECLT TENSILE STRESS 58883.7 sit = 3926.36 22t= 3954.6 t3t= 7699.64 m1t= 2.44083E+5 m2*= 65202.4 tt = 1.00979E+5 I l l O l - CVGNA ATTACHMENT Joe No. b2046 wa P$
/ (GcapA
/
11 iT GLOBAL ACCELERATIONS W EGfwCy
? 11.37,3.18,5.83 INPUT DATA GLOBAL G-LEVELS = 11.37 3/18 5.63 NORTH VECTOR ANGLES = 90 90 0 VERTICAL VECTOR ANGLES = 0 90 90 EAST VECTOR ANGLES = 90 0 90 LOCAL G-LEVELS' -4.33731E-5 3.18 -2.22397E-5 -4.33731E-5 -1.21307E-5 5.83 11.37 -1.21307E-5 -2.22397E-5 OPERATING DRIVE ROD STRESS AT A 5048.35 OPERATING DRIVE ROD STRESS AT B 7721.14 OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING EAR WELD TENSILE STR 5107.51 OPERATING EAR WELD SHEAR STRES 631.431 OPERATING EAR BOLT SHEAR STRESS 3600.17 OPERATING EAR BOLT TENSILE STR 1340.69 (h
t 1 D'. b1IC COMPONENTS DRIVE ROD TENSILE STRESS AT A 16053.7 DRIVE ROD TENSILE STRESS AT B 24553.2 BUSHING PE ESSURE 313.117 EAR WELD TENSILE STRESS 20967 EAR WELD SHEAR STRESS 2365.96 EAR BOLT SHEAR ETRESS 13489.8 EAR BOLT TENSILE STRESS 57426.5 FIXED PLUS DYNAMIC COMPONENTS hyhhk DRIVE ROD TENSILE STRESS AT A 21102.1 ATTACHMENT DRIVE ROD TENSILE STRESS AT B 32274.4 PUSHING PRESSURE 411.582 JOG NO. 820dd EAR WELD TENSILE STRESS 25074.5 FILE NO. om F EAR WELD SHEAR STRESS 2997.39 EAR BOLT SHEAR STRESS EAR BOLT TENSILE STRESS 17090 58767.2 SHEETNO. A*27 }0
csp 6 INPUT GLOBAL ACCELERATIONS &P{[T ? 2.69,3.09,1.48 IN.JT DATA GLOBAL G-LEVELS = 2.69 3.09 1.48 NORTH VECTOR ANGLES = 90 90 0 VERTICAL VECTOR ANGLES = 0 90 90 EAST VECTOR ANGLES = 90 0 90 LOCAL G-LEVELS . -1.02615E-5 3.09 -5.64575E-6 -1.02615E-5 -1.17874E-5 1.48 2.69 -1.17874E-5 -5.64575E-6 OPERATING DRIVE ROD STRESS AT A 5048.35 OPERATING DRIVE ROD STRESS AT B 7721.14 OPERATING CYLINDER BRG PRESSURE -98.4646 OPERATING EAR WELD TENSILE STR 5107.51' OPERATING EAR WELD SHEAR STRES 631.431-OPERATING EAR BOLT SHEAR STRESS 3600.17 OPERATING EAR BOLT TENSILE STR 1340.69 DYNAMIC COMPONENTS DR' ' ROD TENSILE STRESS AT A 15599.4 DRIVE ROD TENSILE STRESS AT B 23858.3 BUSHING PRESSURE 304.256 EAR WELD TENSILE STRESS 16110.8 EAR WELD SHEAR STRESS 1976.81 EAR BOLT SHEAR STRESS 11271 EAR BOLT TENSILE STRESS 14173.8 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 20647.7 DRIVE ROD TENSILE STRESS AT B 31579.4 py a a PUSHING PRESSURE 402.73 VU - M EAR WELD TENSILE STRESS 21218.3 EAR WELD SHEAR STRESS 2608.24 ATTACHEEN . EAR BOLT SHEAR STRESS 14871.2 JOB NC. 8f 04d EAR BOLT TENSILE STRESS .15514.5 FILE NO. Of*0I F SHEET NO. A-26 9
wwo,. . v....s - -. ... v ww . w.s n,wwww -
,.vs4- ,.vsue, vsse sbasic cep3a Ivl S-BASIC ompiler Version 5.4b 101:00 REM ***** BIF UALVE 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 1 rod,1cg,x, phi, lave,abit,11,12,el,e2,e3,e4,e5 = real 0006:00 var fst2, ca,ia,cb,ib,aa,ab,di,d2,ci,il,c2,12=real 0007:00 var 1rodo,1cgo,1dr,d, abush, pbush=real 0008:00 var fcof, feo, ma,mb, siga, sigb, fedr, fedrf,maf, mbf=real 0009:00 var dear, fcear,fr, f11,f22,la, ci12,ci21,stt3,sem1=real 0010:00 var sem2, set 3,sest,ses2,sr, tau 11, tau 22,tauear,aear=real 0011:00 var btens, taubit, set 3f,semif,sem2f,fcearf, frf,filf=real 0012:00 var f22f,stt3f,ses1f,ses2f,srf,taulf, tau 2f,taurf=real 0013:00 var taubf,btf, dsr,dtaur,dtaub,dbten,dsa,dsb,dpb=real 0014:00 var sdraf,sdrbf,pbushf, tau 11f, tau 22f=real 0015:00 var wao,wbr,ftr1,watri,s1,sif,s2,s2f,m1,m1f,m2=real 0016:00 var m2f,t3,t3f,tt3,tt3f,1br,wtot=real 0017:00 var bs t ,bs2,bt3, bm1, bm2,bt t3=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 bst etc TURN ON WITH K=1*** 0023:00 REM 0024:00 REM gg 0025:00 dim real a(3,3) I,
) 6026:00 dim real b(3) 427:00 dim real gic(3,3) 0028:00 1 data 7.5, 10, .75, 1.95, 1.25, .7 0029:00 2 da t a 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.,90.,0.,90.,0.,90.
0034:00 7 data 180.,90.,90.,90.,180.,90. 0035:00 REM DATA 6&7 FOR VALUE/ GLOBAL-G ORIENTATIONS AND WEIGHT UECTOR 0036:00 restore 0037:00 read dl,d2,ci,il,c2,i2 0038:00 restore 2 0039:00 read I rod,1 cg,x ,ph i ,l ave ,abi t ,11,12 0040:00 restore 3 fy l 0041:00 read fst2,ce,la,cb,ib,aa,ab kl A wa 84M 0042:00 restore 4 l 0043:00 read wao,wbr,el,e2,e3,e4,e5 ATTACHMENT 1 0044:00 restore 5 JOB NO. 020 4di 0045:00 read 1rodo,lego,1dr,d,abush 0046:00 restore 6 FILE NO.fDF. ollF
- 0047
- 00 read a(1,1),a(2,1),a(3,1),a(1,2),a(2,2),a(3,2) SHEET NO. 4 4 0048:00 restore 7 0049:00 read a(1,3),a(2,3),a(3,3),av(1),av(2),av(3) '
0050:00 tex t 0,& INPUT GLORAL ACCELERATIONS & 0051:00 input b(1),b(2),b(3)
'52:00 print ,
i (f s) J53:00 text 0,& INPUT DATA &
' ' 0054:00 print 0055:00 print " GLOBAL G-LEVELS = ";b(1),b(2),b(3) 0056:00 print " NORTH VECTOR ANGLES = ";a(1,1),a/2,1),a(3,1) 0057:00 print "UERTICAL 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)
Compilation complete co n . INFUT GLOBAL ACCELERATIONS
? 4.57,1.26,.86 d @ J-$L\ ( p. g y INPUT DATA GLOBAL G-LEVELS = 4.57 1.26 .86 NORTH VECTOR ANGLES = 90 90 0 VERTICAL VECTOR ANGLES = 90 0 90 '
EAST UECTOR 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 4.57 -4.80652E-6 -3.28064E-6 OPERATING DRIVE ROD STRESS AT A 477.198 OPERATING DRIVE ROD STRESS AT B 821.458 OPERATING CYLINDER BRG PRESSURE -3.75613E-4 OPERATING VALVE EAR TENSILE STR 1136.52 OPERATING VALVE EAR SHEAR STRES 89.1706 OPERATING EAR BOLT SHEAR STRESS 1078.68 OP"'ATING EAR BOLT TENSILE STR 525.595 cif=-3.4591E-3 92f= 474 t3f=-2.57873E-3 m1f=-3258.67 m2f=-5.29623E-3 tt3f= 4929.17 l DYNAMIC COMPONENTS hVh l
DRIVE ROD TENSILE STRESS AT A 4341.57 ATTACHMENT DRIVE ROD TENSILE STRESS AT B 6640.18 BUSHING PRESSURE 84.6795 JOS PN)* bEO # i VALVE EAR TENSILE STRESS 4711.31 FILE PH3. g,g,p VALVE EAR SHEAR STRESS 285.935 SHEET NO. O'b0 EAR BOLT SHEAR STRESS 3458.89 EAR BOLT TENSILE STRESS 22999.3 si d= 779.831 s2d= 851.76 t3d= 3089.31 mld= 97498.6 m2d= 22785 tt = 19965.7 FIXED PLUS DYNAMIC COMPONENTS O DRIVE ROD TENSILE STRESS AT A 4818.76 DRIVE ROD TENSILE STRESS AT B 7461.64 PUSHING PRESSURE 84.6799
VALVE EAR TENSILE STRESS 5847.84 VALVE EAR SHEAR STRESS 375.106 EAR BOLT SHEAR STRESS 4537.57 EAR BOLT TENSILE STRESS 23524.9 01t=779.835 s2t= 1325.76 t7 3089.32 mi s-= 1.00757E+5 m2t= 22785 tt3t= 24894.9 O i CYGMA ATTACHMENT ( 1 JOB NO. 02044 FILE NO. MOI F SHEET No. A-3/ O
Canpilation complete h M ADBAL ACCELEMTlWS
?4.57,1.26,0.86 INPUT CATA 6LOBAL G-LEVELS = 4.57 1.26 .86 NDRTH VECTOR M6LES = 90 90 0 VERTICAL VECTOR MGLES= 90 0 90 EAST VECTOR MGLES = ISO 90 90 JEIGHT VECTOR MGLES = 90 180 90 LOCAL 6-LEVELS
-1.74332E-5 -4.80652E-6 .86 -1.78332E-5 1.26 -3.20064E-6 4.57 -4.80652E-6 -3.28064E-6 DPEMTING DRIVE ROD STRESS AT A 477.lv8 OPEMilNG DRIVE RCD STRESS AT 8 821.459 OPEMTING CYLINDER BRG PRESSURE -3.75613E-4 DPERATING EAR WELD TENSILE STR 1326.01 GPEMTING EAR WELD SHEAR STRES 189.188 OPEMTING EAR BOLT SHEAR STRESS 1078.68 OPEMTING EAR BOLT TBtSILE STR 525.595 DMIC CDtPmENTS O DRIVE RDD TBiSILE STRESS AT A 4341.57
)
DRIVE R00 TENSILE STRESS AT 8 6440.18 BUSHING PRESSURE 84.6795 i EAR WELD TENSlLE STRESS 6247.02 ' EAR WELD SHEAR STRESS 606.65 , CAR BOLT SHEAR STRESS 3458.09 EAR BOLT TENSILE STRESS 22999.3 cveNN FIXED PLUS D M IC C3tP0NENTS ATTACHMENI! DRIVE ROD TENSILE STRESS AT A 4818.76 -JOB W. M04d._j DRIVE ROD TENSlLE STRESS AT 8 7461.64 FILE NO._7,0,,7 q ?USHING PRESSURE 84,6799 - SHEETNO. I EAR WELD TENSILE STRESS 7573.03 EAR WELD SHEAR S'RESS 775.838 CAR BOLT SHEAR STRESS 4537.57 EAR BOLT TetSILE STRESS 23524.9 9
sbasic cep4a % J) 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,k = integer - 0005:00 var 1 rod,1 cg,x ,ph i , l ave , abi t ,11,12, el , e2,e3, e4,e5 = real 0006:00 var fst2, ca,la,cb,ib,aa,ab,d1,d2,c1,il.c2,:2=real 0007:00 var 1rodo,1cgo,1dr,d, abush, pbush=real 0008:00 var fcof, feo, ma,mb, siga, sigb, fcdr, fedef,maf, mbf=real 0009:00 var dear, fcear,fr, f11,f22,la, ci12,ci21,stt3,sem1=real 0010:00 var sem2, se t3, ses t , ses2, sr , t au 11, t au22, t aue ar , ae ar=r e al 0011:00 var btens, taubit, set 3f,sem1f,sem2f,fcearf, frf,filf=real 0012:00 var f 22f , st t3f ,sesif ,ses2f ,srf , t mulf , tau 2f , taurf=real 0013:00 var taubf,btf, dsr,dtaur,dtaub,dbten,dsa,dsb,dpb=real 0014:00 var sdraf,sdrbf,pbushf, tau 11f, tau 22f=real 0015:00 var wao ,wbr , f tr 1,watr 1, s1, si f , s2, s2f ,m1,mi f ,m2=ce al 0016:00 var m2f,t3,t3f,tt3,tt3f,1br,wtot=real 0017,:00 var bs1,bs2,bt3,bm1,bm2,bt.t3=real 0018:00 dim real av(3) 0019:00 dim real wa(3) 0020:00 dim real wb(3) 0021:00 REM 0022:00 REM *** BURNS 7 ROE EAR FORCES ARE bs1 etc TURN ON WITH K=1*** 0023:00 REM [-s) 0024:00 REM V' .125:00 dim real a(3,3) 9026:00 dim real b(3) 0027:00 dim real gic(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.,-30. 0035:00 REM DATA 6&7 FOR VALVE / GLOBAL-G ORIENTATIONS AND WEIGHT UECTOR 0036:00 restore 0037:00 read dl,d2,ci,il.c2,i2 0038:00 restore 2 0039:00 read 1 rod,1 cg,x ,ph i ,l ave ,abi t ,11,12 0040:00 restore 3 0041:00 0042:00 read fst2,ca,ia,cb,ib,aa,ab restore 4 GNA 0043:00 read wao,wbr,el,e2,e3,e4,e5 ATTACHMENT 0044:00 restore 5 JOB NO. $7044 0045:00 read 1rodo,lego,1dr,d,abush 0046:00 nestore 6 FILE NO. OI^ OI 0047:00 read a( 1,1 ) , e.( 2,1 ) , a( 3,1 ) , a( 1,2) , a( 2,2) , a( 3,2 3 SH5ETNO. C E)- , 0048:00 restore 7 0049:00 read a(1,3),a(2,3),a(3,3),av(1),av(2),av(3) n050:00 text 0,& INPUT GLOBAL ACCELERATIONS & e51:00 input b(1),b(2),b(3) Os u052:00 print 0053:00 text 0,& INPUT DATA & 0054:00 print 0055:00 print " GLOBAL G-LEVELS = ";b(1),b(2),b(3) 0056:00 print " NORTH UECTOR ANGLES = ";a(1,1),a(2,1),a(3,1) 0057:00 print " VERTICAL VECTOR ANGLES = ";a(1,2),a(2,2),a(3,2) 0058:00 print " EAST UECTOR ANGLES = ":a(1.3) a(2.3) a(3.3)
0059:00 print " WEIGHT VECTOR ANGLES = ";cv(1),av(2),av(3)' 0060 00 print 0061:00 for i=1 to 3 0062:01 for J=1 to 3 0063:02 a(j,1)=a(J,1)*2.*3.1416/360. 0064:02 gic(j,i)=b(i)*cos(a(J,i)) 0065:02 next J 066:01 next i 0067:00 for J=1 to 3 0068:01 av(J)=av(j)*2.*3.1416/360. 0069:01 next J 0070:00 print 0071:00 text 0,& LOCAL G-LEVELS & 0072:00 print 0073:00 pr i n t gi c(1,1) ,gi c(1,2) ,gi c(1,3) 0074:00 print gic(2,1),gic(2,2),g1c(2,3) 0075:00 print gic(3,1),gic(3,2),gic(3,3) 0076:00 REM WEIGHT COMPONENTS 0077:00 for J=1 to 3 0078:01 wa(J)=wao*cos(av(J)) 0079:01 wb(J)=wbr*cos(av(J)) 0080:01 next J 0081:00 phl= phi *2.*3.1416/360. 0082:00 la= lave /2 0083:00 c i 12=c1/i 2 0084:00 ci21=c2/11 0085:00 aear=11*12 0086:00 REM CALCULATE EAR FORCES USE B&R LOADS AS OPTION LATER 0087:00 REM FIXED COMPONENTS ARE ALWAYS THERE 0088:00 lbr=lrod+1cg 0089:00 watrl=1 br*wa(1)/1 rod 0090:00 s1f=wb(1)+watrl '091:00 wtot=wao+wbr J92:00 s2f=wb(2)+wa(2)+fst2 0093:00 t3f=wa(3)+wb(3) 00 94 : 00 m1 f =-(wa( 2) +wb( 2) + f s t2) *e5-wa( 3) *( e 3+ 1 cg)-wb( 3) *e4 0095 : 00 m2f =(wa tr 1 +wb( 1 ) ) *e 5-wa ( 3) *e 2-wb( 3) *e 1 0096:00 tt3f=watr1*e3+(wa(2)+fst2)*e2+wb(1)*e4+wb(2)*e1 0097:00 fedrf=1cg*wa(1)/Irod 0098:00 maf=fedrf*(1 rod-13.5) 0099:00 mbf=fedrf*7.125 0100:00 sdraf=fst2/aa+ abs (maf*ca/la) 0101:00 sdrbf=fst2/ab+ abs (mbf*cb/ib) 0102:00 fcof=1cgo*wa(1)/Irodo 0103:00 pbushf=fcof*(1dr+d)/(d*abush) 0104:00 REM STRESSES FROM FIXED COMPONENTS 0105:00 dear =(d1*d1+d2*d2)**.5 0106:00 set 3f= abs (t3f/(4*aear)) v 0107:00 sem1f= abs (m1f/(2*d2*aear)) I ts* s A - 0108:00 sem2f= abs (m2f/(2*d1*aear)) A774ggggg7 0109:00 fcearf=tt3f/(2* dear) 0110:00 frf=x*fcearf JOB NO._ 82 0 0111:00 f11f=-(fcearf* sin (phi)-frf*cos(phi)) 0112:00 f22f=fcearf*cos(phi)+frf* sin (phi, FILE NO. OT odF 0113:00 stt3f= abs (f11f*1a*ci12)+ abs (f22f*1a*ci21) SHEET HO. 0114:00 sestf= abs (sif*ci12*1a/4.) -- 0115:00 ses2f= abs (s2f*ci21*1a/4.) 0116:00 srf= set 3f+semif+sem2f+sestf+ses.1ftstt3f 17:00 REM EAR SHEAR v118:00 tau 11f= abs (sif/(4*aear))+ abs (f11f/aear) 0119:00 tau 22f= abs (s2f/(4*aear))+ abs (f22f/aear) 0120:00 taurf=(tau 11f* tau 11f+ tau 22f* tan 22f)**.5 0121:00 taubf=taurf*aear/abit 0122:00 REM EARBOLT TENSION 0123:00 btf=(set 3f+semif+sem2f>*aear/abit 0124: 00 print
0125:00 print"0PERATING DRIVE ROD STRESS AT A ";cdraf 0126:00 print" OPERATING DRIVE ROD STRESS AT B ";sdebf 0127:00 print" OPERATING CYLINDER BRG PRESSURE ";pbushf 0128:00 print" OPERATING VALVE EAR TENSILE STR ";srf (vg G129:00 pr i n t" OPERATING 0130:00 print"0PERATING EAR BOLT VALVE SHEAREARSTRESSSHEAR";taubfSTRES " ; taurf 0131:00 print" OPERATING EAR BOLT TENSILE STR ";btf 132:00 print 0133:00 REM 0134:00 REM CALCULATE VARIABLE COMPONENTS 0135:00 REM 0136:00 dsr=0. 0137:00 dtaur=0. 0138:00 dtaub=0. 0139:00 dbten=0. 0140:00 dsa=0. 0141:00 dsb=0. 0142:00 dpb=0. 0143:00 for J=1 to 3 0144:01 fco=lego*wao*gic(1,j)/1rodo 0145:01 pbush=fco*(Idr+d)/(d*abush) 0146:01 ftrl=1br*wao*gic(1,J)/1 rod 0147:01 s1=ftr1+wbr*gic(1,J) 0148:01 s2=wtot*gic(2,J) 0149:01 t3=wtot*gic(3,j) 0150 : 01 m1 =-w to t *gi c ( 2, J ) *e 5-wao*gi c ( 3, j ) *( e 3+ 1 c g)-wbr *gi c ( 3, J ) *e 4 0151 : 01 m2=( f tr 1 +wbr *gi c ( 1, J )) *e 5-(wao*e 2+wbr*e l ) *gi c ( 3, J ) 0152:01 tt3=ftr1*e3+wbr*gic(1,J)*e4+gic(2,J)*(wao*e2+wbr*el) 0153:01 fedr=1cg*wao*gic(1,J)/1 rod 0154:01 ma=fedr*(Irod-13.5) 0155:01 mb=fedr*7.125 l 0156:01 siga=ma*ca/ia v '157:01 sigb=mb*cb/ib
,158:01 REM CALCULATE EAR TENSION 0159:01 set 3= abs (t3/(4*aear))
0160:01 sem1= abs (m1/(2*d2*aear)) 0161:01 sem2= abs (m2/(2*d1*aear>> 0162:01 fcear=tt3/(2* dear) 0163:01 frex*fcear 0164:01 f11=-(fcear* sin (phi)-fr*cos(phi)) 0165:01 f22=fcear*cos(phi)+fr* sin (phi) 0166:01 stt3= abs (f11*1a*ci12)+ abs (f22*1a*ci21) 0167:01 ses1= abs (s1*cil2*1a/4.) 0168:01 ses2= abs (s2*ci21*1a/4.) ! 0169:01 sr= set 3+sem1+sem2+sesl+ses2+stt3 0170:01 REM EAR SHEAR 0171:01 tau 11= abs (s1/(4.*aear))+ abs (f11/aear) 0172:01 tau 22= abs (s2/(4.*aear))+ abs (f22/aear) 0173:01 tauear=(tau 11* tau 11+ tau 22* tau 22)**.5 0174:01 taubit=tauear*aear/abit 0175:01 REM EARBOLT TENSION g%V kl A 0176:01 btens=(set 3+sem1+sem2)*aear/abit ws ITM 0177:01 dsa=dsa+siga*siga 0178:01 dsb=dsb+sigb*sigb ATTACHMENT 0179:01 dpb=dpb+pbush*pbush JO8 NO. Af o44 0180:01 dsr=dsr+sr*sr 0181:01 dtaur=dtaur+tauear*tauear FILE NO. OT Of[l 0182:01 dtaub=dtaub+taubit*taubit SHEET NO. S- I6 l
/~] .83:01 dbten=dbten+btens*btens
( / 0184:01 next j 0185:00 REM COMBINE STRESSES 0186:00 dsa=dsa**.5 0187:00 dsb=dsb**.5 0188:00 dpb=dpb**.5 0189:00 dsr=dsr**.5 0190:00 dtaur=dtaur**.5
0191:00 dtaub=dtaubno.5 0102:00 dbten=dbten**.5 0193:00 print 0194:00 text 0,& DYNAMIC COMPONENTS & 0195:00 print 0196:00 print " DRIVE ROD TENSILE STRESS AT A";dsa n197:00 print " DRIVE ROD TENSILE STRESS AT B";dsb
.98:00 print " BUSHING PRESSURE ";dpb 0199:00 print " VALVE EAR TENSILE STRESS ";dsr 0200:00 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 f. sdr bf )
0205:00 dpb=dpb+ abs (pbushf) 0206:00 dsr=dsr+ abs (srf) 0207s00 dtaur=dtacr+ abs (taurf) 0208:00 dtaub=dtaub+ abs (taubf) 0209:00 dbten=dbten+ abs (btf) 0210:00 print 0211:00 text 0,& FIXED PLUS DYNAMIC COMPONENTS & 0212:00 print 0213:00 print " DRIVE ROD TENSILE STRESS AT A";dsa 0214:00 print " DRIVE ROD TENSILE STRESS AT B";dsb 0215:00 print " PUSHING PRESSURE ";dpb 0216:00 print " VALVE EAR TENSILE STRESS ";dsr 0217:00 print "VALUE EAR SHEAR STRFSS ";dtaur 0218:00 print " EAR BOLT SHEAR STRESS ";dtaub 0219:00 print " EAR BOLT TENSILE STRESS ";dbten l 0220:00 end l 0221:00 0222:00
?23:00 .224:00 0225:00 1 0226:00 ****** End of program ******
l l
- CYGNA ATTACHMENT JOB NO. 62044 FILE NO. OY'Olbi SHEET NO. A' 3h O
op4a INPUT GLO8AL ACCELERATIONS
? " 35,1.34,.86 INPUT DATA GLOBAL'G-LEVELS = 3.35 1.34 .86 NORTH UECTOR ANGLES = 90 -38 52 VERTICAL VECTOR ANGLES = 90 52 142 EAST VECTOR ANGLES = 180 90 90
-WEIGHT VECTOR ANGLES = 90 -128 -38 LOCAL G-LEVELS
-1.27792E-5 -5.11169E-6 .86 2.63983 .S24984 -3.28044E-6 2.06246 -1.05594 -3.28064E-6 OPERATING DRIVE ROD STRESS AT A 477.198 OPERATING DRIVE ROD STRESS AT B 821.458 OPERATING CYLINDER BRG PRESSURE -3.75613E-4 OPERATING VALVE EAR TENSILE STR 1946.57 OPERATING VALVE EAR SHEAR STRES 128.033 OPERATING EAR BOLT SHEAR STRESS 1548.79
- OPERATING EAR BOLT TENSILE STR 4771.17 I
D %MI C COMPONENTS DRIVE ROD TENSILE STRESS AT A 4341.57 DRIVE RCD TENSILE STRESS AT B 6640.18
-BUSHING PRESSURE 84.6795 VALVE EAR TENSILE STRESS 5948.81 VALVE EAR SHEAR STRESS 379.211 EAR BOLT SHEAR STRESS 4587.24 EAR BOLT TENSILE STRESS 13246.5 FIXED PLUS DYNAMIC COMPONENTS t
DRIVE ROD TENSILE STRESS AT A 4818.76
. DRIVE ROD TENSILE STRESS AT B 7461.64 PUSHING PRESSURE 84.6799 VALVE EAR TENSILE STRESS 7895.38 VALVE EAR SHEAR STRESS 507.244 EAR BOLT SHEAR STRESS 6136.03 EAR 80LT TENSILE STRESS 18017.7 >
_CYGNA ATTACHMENT l JOB NO. 87% FILE NO. 07:01/F l q SHEET No. A- M !O i l
}
CeD4 lN GLOBAL ACCELERATIONS
? ? 35,1.34,.86 gp N MSL dCQ ~
GLOBAL G-LEVELS = 3.35 1.34 .86 NORTH ~ VECTOR ANGLES = 90 -38 52 VERTICAL VECTOR ANGLES = 90 52 142 EAST VECTOR ANGLES = 180 90 90 WEIGHT VECTOR ANGLES = 90 -128 -38 LOCAL G-LEVELS
-1.27792E-5 -5.11169E-6 .86 2.63983 .824984 ~3.28064E-6 2.06246 -1.05594 -3.28064E-6 OPERATING DRIVE ROD STRESS AT A 477.198 OPERATING DRIVE ROD STRESS AT B 821.458 OPERATING CYLINDER BRG PRESSURE -3.75613E-4 OPERATING EAR WELD TENSILE STR 2592.98 OPERATING EAR WELD SHEAR STRES 271.64 OPERATING EAR BOLT SHEAR STRESS 1548.79 OPERATING EAR BOLT TENSILE STR 4771.17 D"'Wi! C COMPONENTS l DRIVE ROD TENSILE STRESS AT A 4341.57 DRIVE ROD TENSILE STRESS AT B 6640.18 BUSHING PRESSURE 84.6795 EAR WELD TENSILE STRESS 7493.12 EAR WELD SHEAR STRESS 804.547 EAR BOLT SHEAR STRESS 4587.22 EAR BOLT TENSILE STRESS 13246.5 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENGILE STRESS AT A 4818.76 l DRIVE ROD TENSILE STRESS AT B 7461.64 PUSHING PRESSURE EAR WELD TENSILE STRESS EAR WELD 84.6799 10086.1 (Yhkk SHEAR STRESS 1076.19 ATTACHEENT EAR BOLT SHEAR STRESS 6136.01 ggo44 EAR BOLT TENSILE STRESS 18017.7 JOB .
FILE NO. SHEETNO. A 56 9
eceo EP? B) cep'45 INPUT GLOBAL ACCELERATIONS
? 3.35,1.34. 96 INPUT DATA GLOBAL G-LEVELS = 3.35 1.34 .86 NORTH UECTOR ANGLES = 90 -38 52 VERTICAL VECTOR ANGLES = 90 52 142 EAST VECTOR ANGLES = 180 90 90 WEIGHT VECTOR AN6LES = 90 -128 -38 LOCAL G-LEVELS
-1.27792E-5 -5.11169E-6 .86 2.63983 .824984 -3.28064E-6 2.06246 -1.05594 -3.28064E-6 .
OPERATING DRIVE ROD STRESS AT A 477.198 OPERATING DRIVE ROD STRESS AT B 821.458 OPERATING CYLINDER BRG PRESSURE -3.75613E-4 OPERATING UALVE EAR TENSILE STR 1946.57 OPERATING VALVE EAR SHEAR STRES 128.033
. ( 7PERATING EAR BOLT SHEAR STRESS 1548.79 - Q P' 4 TING EAR BOLT TENSILE STR 4771.17 c1f=-3.4591E-3 s2f= 733.811 t3f= 532.695 m1f=-21826.4 m2f=-3818.52 tt3f= 6791.54 l DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 4341.57 DRIVE ROD TENSILE STRESS AT B 6640.19 BUSHING PRESSURE 84.6795 i
l VALVE EAR TENSILE STRESS VALVE EAR SHEAR STRESS 5948.81 379.211 C GNA;j EAR BOLT SHEAR STRESS 4587.24 ATTACHMENT l EAR BOLT TENSILE STRESS 13246.5 JOSNO.6204 sid= 779.831 ,. FILE NO. oTo s2d= 1869.64 SHEETNO. A"E t3d= 1566.33 mid= 59205.9 l m2+ 12442.3 t = 23258.6 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 4818.76 DRIVE ROD TB4SILE STRESS AT B 7461.64 PitRHTNr, PRFARllPF Ad.4700
VALUE EAR TENSILE STRESS 7895.38 VALVE EAR SHEAR STRESS 507.244 EAR BOLT SHEAR STRESS 6136.03 EAR BOLT TENSILE STRESS 19017.7 sit = 779.835 s2'- 2603.45 t2 2099.02 mit= 81032.3 rn2 t= 16260.8 tt3t= 30050.1 i r l 1 l l t O l 1 I i CYGNA ATTACHMENT JOSNO. 82044 FILE NO. 0701. F SHEETHO A-4d 9
I l l l APPENDIX B VALVE / AIR OPERATOR MODEL FOR FINAL PIPING RESPONSE G-LEV" CALCULATION. O : i l i I l l l O l l l
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' WPPSS Mechanical Fquipnent Requalification prepared ey L.C. Fern @ 6/13/83 Subject Checked By-30" Cylinder Operated Butterfly Valves mP fDate 6/13/83 M.A. Scott '-
Systen: Job No Fde No CAC & CEP 82044 OS.01.F MstyTT*ty Ret No Sheet No OTn V;1104 1 4.1.1 4.1 Conclusions Four 30" BIF butterfly valves with Miller Fluid Power cylinder operators have been analyzed for structural integrity and operability to the seismic and hydrodynamic piping analysis loads. These Burns and Roe piping analysis loads are in the form of operator response g-levels. (see Ref. 9). All four EPN's, i.e., CSP-v-1, CSP-V-2, CEP-V-1A and CEP-V-2A qualify with the following modifications:
- 1. Manufacturer supplied A-307 bolts must be replaced with A-325 bolts.
- 2. Shear plates must be added to reduce the ear weld (mj stress (see sheets 4.3.30 through 4.3.48 ).
Valve operability was also demonstrated (see p. 4.3.20) while cylinder operability is addressed in QID No. 018001. t k i
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""'WPPSS Mechanical Equipment '## J . E . Rakowski* 3/25/83 enecaeo By- cate
"*'30" Butterfly Valves , ,/g, g j,u , ,,
system
- CSP & CEP 82044 OS.01.F Analysis No Aev. No Sheet No 361104 1 4.2.1
SUMMARY
OF RESULTS Parametric data for the four 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. O. L) 4 L)
=, :-
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SUMMARY
TABLE N [hLA ME TLit PATA i e 5 &
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$ E z m c CSP-V-I 7 Co *' A'eaueM r noumet 503 H j.% 3.67 f.?l _ (7 3
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'"hPPSS Mecha n'al Equipment QualificatEoE'#*" J.E. Rakowski '* 3/25/83 ;
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SUMMARY
TABLE 1.3 ALLOWABLE STRESSES Since operability is required, the stresses for the ( faulted condition will be kept below yield *. The table below is based on AISC criteria and the yield stresses at temperature (340*F) from PG. 9 of REF. 4 for conservatism. LEvCL A$6 Lins D
- t. & = . 6 F y a. 6 r . y F rzuosml.& ry .4 Fy a n ry o. w &
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Calculation L4 f. n 6 Sheet 7 llll111111111lllll1111llllll!I (J ) WPPSS Mechanical Ekluipnent Requalification * ' ' " # L.C.Fdddeg U 6/13/83 Suelect Checked By. %'k(Date 30" Cylinder Ocerated Butterfly Valves M.A. Scott 5/13/83 Sys!!m Job No. Fde No CAC & CEP 82044 OS.01.F
? r,; , Rev. No Sheet No EQUIPMENT REQUALIFICATION FOR QID NO. 361104 BIF 30" CYLINDER OPERATED BUTTERFLY VALVES 4.3.1 Introduction The four valves in this file are classified according to the parametric data given in Summary Table 1.1.
Since hydrodynamic loads apply (Ref. 7) fatigue analyses were provided for components with the highest stress range. O Q The analysis method calculates stress from north, vertical and east components of operator response g-levels. These l g-levels are the result of the Burns & Roe piping analyses. (Ref. 9) An SRSS analysis was set up in a computer program for each value assembly in its specific orientation. The SRSS is taken.at the maximum stress level due to seismic g-loading. l Operating loads due to seating torque force and dead I weight are combined with the seismic stress by absolute l sum. Valve ear bending stress components due to any one response g-level component are combined by absolute sum. l l l l l O l me ce l l
E: M s 4 Calculation M ei'fJ Sheet lililllllllllllillllllilllllli O
"#ESS Mechanical Equipment Qualification ""'"J.E.Rakowski 1/10/83 Sociect Cnecues By ,
Date
~
,30" Butterfly Valves L f. er :- e s n 'a
$ v s'em J00 NC Fr'e PT3 CSP & CEP 82044 OS.01/F "N S"" N "38f}0Q l 4.3.2 The computer analysis acklesses 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 QID 361104'(30" valves /10" operators). Hand calculations which check selected por-tions of computer output is shown in Appendix C. Appendix B of this section describes the air operator mass / stiffness model which was incorporated in the final piping analysis for calculation of operator re-sponse g-levels. The computer program includes an op-tion for using the valve ear forces and moments which are directly output from the piping analysis with the valve / operator codel included. This was not finally utilized, however, to qualify the subject equipment. The equipment locations and elevations were taken from the P&ID's in section 6.0. Natural frequency calcu-lations are given for the air operator assemblies in Section 4.3.2.1. Preliminary analyses were performed which showed that, for operator response g-levels greater than ap-proximately 3 g's, the air cylinder spring preload force would be exceeded and hence some disk flutter would occur when the valve is in the open position. The calculation in section 4.3.2.2 shows that the mag-nitude of the valve disk flutter vibration angle due to upper bound g-levels which occur in the hydro-dynamic frequency range is approximately 6 degrees. This flutter was evaluated to have no detrimental effect'on system safety function as noted in Reference i
- 5. '
Valve operability was addressed in the following manner. All valves have a Use Code of 1-3. It is noted that the g-levels pertaining to CSP-V-2 envelope CEP-V-1A and i
- s. CEP-V-2A.
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Calculation [41dt ' Sheet lillllilllllll!$fillllllllll V c, preca e: ey care WPY$tS Mechanical Equipment Qualification J.E.Rakowski 1/10/83 Suetect Checnec By . , cate 3d' Butterfly valves [ C , b u. ,- .ru a 'p c-S ystern Joe No Fue No CSP nnd CFP A?naa ng nifr
" " " shetN 3TIfd5 I 4.3.3 For valves CSP-V-1 and 2, which must operate from open to fail closed during an event, the following additional evaluations were made:
- 1) Dynamic flow torques were assessed per Ref. 3 and found to be less than the seating torque which controlled the equipment = tresses.
Furthermore these flow toraues tend to move the valve disk toward the fail-closed position, as noted in the above report.
- 2) The details of BIF drawing 206 7673 parts of which are shown in figures 1.1 and 1.2, allow g3 the following conclusions to be made for valve
( 1 operability: w/ A) Figure 1.1 shows that thrust bearings are part of the shaft bearing design. This design prevents lateral movement of the disk in the direction of the shaft to eli-minate interference with the valve body when closing. Further, it is noted on Page 26 of Ref. 3 that frictional ~ torques in the shaft bearing system are negligible. B) Figures 1.1 and 1.2 show a circular valve cross section having an internal rim within which the valve seats in the closed posi-tion. The only mechanism remaining to af-feet valve closing which can be postulated l is out-of-round distortion of the section due to DBE piping loads and dynamic loads on the valve. These loads were accounted for in Ref. 4 in the overall valve sizing calculations, where analysis showed that the stress intensity in the 0.5 inch thick valve body remained below 1.2 Sm, or approximately 0.8 of yield. Stress contribution from dynamic loads on the valve and operator were relatively small. Further, as shown (s) in the figures: l i 9M Z
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- 1. The valve seat forms a heavily reinforced section made up of the valve body, internal hub and external' flanges (including the mating flange of the piping). Hance the stress levels in this section are much lower than in the valve body and hence no distortion of the section could occur to affect seating of the valve. Valve flange dimensions are given below. Note the relatively large internal radial clearance of 1/8 inch.
- 2. Stress analysis of the valve extended structures are given in this report. Air operator operability is addressed in QID 018001.
The design data used in the analyses are given in Summary Table 1.1 (pipe-orientations and elevations are taken from the appropriate P&ID'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 Closed Preload = 2000 Final = 4800
- 2) Cylinuer C.G.'s shown on the following sketches represent data received from BIF in the communi-cation report of Section 7.0 of QID 018001.
- 3) Closing torque values are taken from Ref. 3.
- 4) Valve component dimensions: (Ref. Feb. 10, 11/83 communication report - Section 7)
.. Flange: width = 3.88", thickness - 2.625" Radial Clearance Disk / Seat 1/8" O *:C6 ;C l
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4.3.2. 2 A P9 L o y I H rrE VA L vP FL QTT G. G VA C WT U OG b 514 G P I M E u Slo 4.9 FCo4 FIGukE l.S :
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- Th e 73' d=*1 mA (v sts' .61 )
FRcM THE 5 Vec st p 10 sECTroW 5.E , FoL 9HM C YNikic loa cs: we . e p m, ETi (.15%7(E) /3 Du = 4&' d - $W .Lf.15+94.4 \ - .4I : . &' . o4-
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[41+ilfd lilllilllitill!!!!!!!Illllll'8 Sheet O DFSS Mechanical Equipment Qualification "" J.E. Rakcwski 1/10/83 e' Date
-N:/ /r Su5+0" Butterfly Valves -
ChechecBr/..( r e_ , ,t v 4 $ v s'em Job No File Nod CSP and CEP 82044 O S. 01/ F Anavs 40 Aev No Shect No k gmQy Gj% 2; 3_9e..ds JT ') 4.3.2.3 STRESS ANALYSIS d The procedures for the analysis of the subject valves are outlined below:
- 1. Recalculate the valve appurtenance stresses addressed in Ref. 4 using response g-levels from the Burns & Roe piping analysis. Incorporate the current seating torque given in Ref. 3.
Compare stresses to the lower yield strengths in Summary Table 1.3.
- 2. If faulted condition stresses exceed the upset g condition allowable stresses, repeat the analy-sis for the affected components using upset accelerations from the piping analyais,
- 3. Perform a fatigue analysis on significantly stressed components. Determine allowable alternating stress ranges from AISC 8th Edition, Appendix B, noting commentary.
The fatigue analysis is to be performed only for those EPN's subject to hydrodynamic loads. The number of respective load cycles is given below. LOAD COMBINATIONS & STRESS CYCLES The following table lists the load combinations and the nubmer of expected stress cycles for each com-bination. (From the design criteria) Combination Cveles ;
- 1. SRV Alone 3 (4500 ) =13500
- 2. OBE+SRV 50 g
- 3. OBE+SRV+ Chugging 2000 :
- 4. SSE+SRV+ Chugging /
SEE+7J 10 , i Note: Load combination #4 with 15560 cycles can be used to conservatively bound all combinations. l l eev e:
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Prosect Prepared By Date WPPSS Mechanical Ecuipment Oualification J.E. Rakowski 3/25/83 Sutiect Checaec By , , Date 30" Butterfiv Valves b 0. f.2 % oh ' N1'MT' System Joe No Feie N6 CSP and CEP 82044 OS.01/F Ana!ysis No Aev No Sheet No 361104 l 4.3.15 STRLD 40 6L V 51S of VALVE A0 & lilR. O P6TJTo R,. couTo4EuT S noi CoeLKLD l9 QtD Olloo l i) Tronuson PitG - 7LL' AJ u ro v I thS WE;E AuAty&cc. AuD TNi SWAL STizEss WAs Fown To 65 FitMAtiL Y ($ffN OfN T ON OV'EITu C 9 t4 G 10 THE 3-Avi5 f4Efc.Teo #. wucM AMA L V i!.E D wi Ttf AA/ Acc E/114TraN /M },Q THIS DtLEC Too rd 0F 15.1 *h, THE SHEAL STLESS U tU A S oaLY 15 PCLcENT of Tu E ALLOW Abt f. 7t/EMML rHL F1H S bli sd Pric IE.N T FoL ALL cPN 's.
,. er TH r.S CALCU L )~Trok feucWS . ,
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Fe wis = [ LFc. 4 fvTz cm,3 , y ASSdM E OPPER LIMIT OF g , el5g 'e "IuS7 FoA. A44 24( i 2.44 8d 4, 13 THI:> HLMBLL, Fs,z - (19 '1% iUA a = 531 C (soh tw El.C" Fu.svis [Im % g33,}I,;fM vt t TctEv:S: ~lI%4 /t.w' -- a +1 P5I z. 22,Wa@
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- h M"d'4 4 b !7I S ystem Joe No Fue Nf CSP and CEP R?nda OS.01/F Ana'ysis No Aev No Sheet No 361104 l 4.3.17 MAX NaRM AL Fot c f on D AtvE L EL/E C F57 C 5G + Fe, S19 9 = 1529 LS (EWVEto ff) l141 4 % + 6953 4 lb
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%=
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CSP and CEP 82044 OS.01/F Anaiys.s No Aev No Sheet No 4,3,yg 361104 I or ** ( = l . II.42 " l.2.S " i 3 s 2I = E. Sat id 5.73 lu pg - 6.cor 6.32 [ j (c : 10.18' Il li I,. , i.zs1 1.4rc rp5 c, roveer : :,,7 + % n n 4 (l.tr) Ccr4, fc e CD % - If = 13,7S9 U.izd - Gl4 PSI .u * $AiN'C 2 a.s4 CD %% Fe.ma. /Eom RG. op PA sc 43.& ( fG 4.'3.n: b A Fe, % g [2524 + 706 : '750f 66 Ypy g , TSOQ = l%90 V9T 1.17 (D M= li 41 l.6,.3_I M ll.183 = "791 1 lu-L5
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2==m Calculation Miej ; Tit Sheet lillllllllllllllllillilillllit o,n.ect PreCarec By Date WPPSS Mechanice.1 Eauinment Oualification J.E. Rakowski 1/10/83 Sunrect Checaec By bata [ f ' c"' ' ' ' ' - 30 " Butterfiv Valves 'M7/IT S ystgm JCC No Fue Na CSP nnd CFP 82044 n t nl /F gsg Rev No g Sheet N 4.3.20 Disc The stresses in the disc were shown on page 51 of Ref. 4 to be due almost entirely to the pressure load. Since the stress found in Ref. 4 of 4540 PSI will not change significantly for the new ac- { celerations, the disc is acceptable. Taper Pins The stress in these pins is due only to the seating torque. The stress in Ref. 4, page 53, is 11265 PSI and is therefore acceptable. For the new, lower seating torque, the stress becomes 8985 PSI. Analysis for: Drive Rod, cylinder bushing pressure, valve ears and valve ear bolts. Method I: Use element forces and moments output from the piping analysis (Summary Table 1.1) and the absolute sum of stresses. The conservatism of SRSS summing of the component stresses cannot be assured because the independence of the six element forces (/ moments) cannot be de-termined without analysis of modal par-ticipation. C O
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[41*i t'fd Sheet lillilillllilililllililllllill DYssMechanicalEquipmentQualification"'8" J.E. RakowskS 1/10/83 Suoject Cnecned By Date 30' Butterfly Valven L I r,ew,oA difD/ System Job No Fue No csp and CEP 02044 OS.01/F ShutN djgfg3 An No 4.3.21 Method II: Use the north, east and vertical operator accelerations output from the piping analysis. Absolute sum for stresses with each component then SRSS over re-sults for N,E and V. Noteh 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-
,m fore the absolute sum will be used at this level.
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( U 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/O parameters are shown for use in QID 361104. Analysis of Seating Toroue 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.
l 2) For valve EPN's which are Fail-Open with Use-Code 2, no seating torque forces are applied during l the faulted and upset conditions (CSP-V-5,6). I l 3) For the Fail-Closed valves, the forces at the i trunnion pins are shown below, along the cylinder axis, for +2-axis g-loading: 1 p1 wal wis i cm ~ 1 ( ) e u p.- cn c.levtshalve SJ6 1 LJ
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#jgff804 4.3.22 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 l force will oppose operator weight when the brackets hangs downward from horizontal pipes. Operator Drive Rod l Drive rod dyanmic stress is due only to g, because g and g forces are taken out by trunniod pins. Add seat $ng torque stresses. _ 7,, g " l l r c.F l Fc
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' WPPSS Mechanical Equignent Requalification M.A. Scott W '* 6/15/83 Subject TP"" Fernandez Checked By$.C.
Date 30" Cylinder Operated Butterfly Valves 6/15/83 Sy stem Joe No File No CSP and CEP 82044 OS.01.F _ Rev. No Sheet No
, _ QID 361104 1 4.3.30 Section 4.3.4 - Ear Support Weld Stress Comparison of a similar file (QID No. 361106) to this file noted the unconservative assumption of considering the bracket support ears to be a guided cantilever (fixed-fixed). The resulting ear weld stresses exceeded the allowable stresses. The ear weld stresses can be lowered by the addition of shear plates to stiffen the whole assembly. The resulting weld stresses (both existing and modified) are to be kept within the fatigue allowable stress, i.e., stress range. The allowable fatigue stress range from AISC for fillet welds in shear with less than 20000 cycles of loading is:
SR = (1.5) (15000) =22500 PSI This includes the 50% increase due to fewer than 20000 cycles. The weld stresses are calculated using faulted loads. These loads produce less than one percent of the total 15560 cycles of faulted /hydrodynami loading. Since the upset and emergency cond:tions are considerably lower in magnitude, small margins of overstress in fatigue will be tolerated fer faulted strees levels. The following allowables will be adhered to in the ear weld stress calculations. Allowable stress for welds for faulted conditions:
# allow = 1. 6 (0. 3) Fu = 2 8 8 0 0 PSI Allowable st.ress for welds subject to fatigue. This is 4 the allowable stress range of AISC Appendix B:
Callow fat =1.25 (1. 2
- 5) (15) = 14 KSI 1.25 = 25% increase due to previous comments 1.5 = 50% increase due to AISC commentary O
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W d :rsoAsiJu M //i: Y e.,J --- us - sys/C M" C*P-P C c riL/2 /rJ Che e h = = [5)[I. S ' 'T 76 h4 = M 376 N 5= 5
~P L- . _2ho'MY4.0 i -- .o0054s A Es i 2, un //2 e- *
=
I"7 88 =) SM $~r t c=crJ ~_ 5 ,3 %o r /6 -c n 2-- t r - A -- 3 -Ja ,J., L- 1
- . :. a v v A.. w 2.c . t , ,J; u c> n GEr C E".~. Pf2 i L.A Adi LY T W ' AL M 5Fie n e:. e +J 9. t J r _~. c p ~ - F .
- t :-
Calculation t% Ce t i Sheet HlHiiiiiiiiiiiiiiiiilillfill epare By #' U***
* '"' WPPSS Mechanical Equignent Fequalification M.A. Scott 6/15/83
'**30" Cylinder Operated Butterfly Valves L.C. Fe 6/15/83 System Job No Fde No CSP and CEP 82044 OS.01 F
--7 Rev No Sheet No.
GID 361104 1 4.3.37 foI58
, bc, 7._6I38(s).c,46l- _.L
- 4. is
. 1 a
n l_r v O w un~ - ~ n .n w l -re sh Mt, "weWu t d4 v n v .- c _ it a ,, - Z + N- = _Gh l - I s2 =:z9 k; - A d, Ag g,,,. 32 5 GOO 4 468 = / /48 4/fd { H$~~ Y17. / TO d'7?YT-. (a A Tf20 % c % W
~~F-o t t o u i J d $W L.oe, o M %
- tJ-%b.
t
;,W * *5 ;6 0 [, J 94 l
l AW ,,,,tND /h s% "& $ ?1Q $! %) m & &Je= u b "nmC ceNS:n: V, p .< l hs W r & 3&~k, -b bc 0 /OY wee.:r v- oc rawc
,v=-=nm n, = ~ x : .
- e. a h J ,
-- Calculation
[4BH fJ lililllillllllllillllllllillil Sheet 9 Pro,ect pgg gir al gyt Requalif1 Cation M.A. Scott #i *** 6/15/83 Sub!ect2.,0" Checked By J P Cate Cylinder Operated Butterfly Valves L.C. Fernandez 6/15/83 System Joo No File No CSP and CEP 82044 OS.01.F _ Rev No Sheet No OID 361104 1 4.3.38
~~FPeou keen 4 cc.<.,cL.'s Yu,i t> Fear ~- -eeoau A. Y eoa. r em e 6 s5
$g
- O I .9 : / . .? h t *2 I&
Tz= .6{4f.2.c,7ia' 10 A , = g.a L = g. 4 =.4.n ,a O bi rJT A 'FbcT lod o F T W~ S h NATC 15 T:>wve r of M G -A R_ McfDi ss y Me~ l F t T rA' "- (1 1 '7D < o u'mJ:.NrF ~ --3 . C m %m' ^ m e, o.a bl s s 1 h' f
=
T* ' 1 no
~
}' ;. A
- 2. l.s 7 ( 7 '
/'
y,,g . i.y}s W-~ '
= 4.917. T~
l E
~
' Fee n 4 t, +,<.S.,ct ,
e s k = 12 . A = 49n (e.L , ga ;g , - 7, i t.e2 (-f.vs) g Y 5\c -t \ = 7 964 ne :: l
Calculation M *h i Sheet llll'" ::mtill! WPPSS Mechanical Fouitznent Repualification M.A. Scot 6/15/83 Checked By: Subsect 30" CvlirviAr Oopratod But%rflv Valves [ @ ate T, _ C _ Fomnndo-r 6 /19 /R"4 System Joe No. File No CSP and CEP 82044 OS 01.F
*smu99pse Rev. No. Sneet No OID 361104 1 4.3.39
&*SPhk= #k fGl3 3 fZ$8),/34/6,auz 1 2a 2 (v.m)
% = -% ~ ble *~ lb, fIS S 3 0 * /5c//S
= -5bG90 + /3N/S * ~ / 72 7b TM Axi AL 1e-er ic ec Esc Tt n>J G e r-pyr:
A o <- C to tsr ev 4 Ech L -She - Q w-U = k *= /sd/5, 232[ a O* 4.74 i i _ YV W YGY/ & D / Y DD " l Ar&-A AW/% Di rz-GT 77 oM 'DdC ~73 ~5dd'd($ IS W kl / 7274 = z756 5 c. 2.7 / T&U T:=rrc cM oP r74 t/A-c. c.)c i S. 71-lDJ l l n-
Calculation t4 L a' a Sheet lillliitillllillllllilllilllli O'
"' '' WPPSS Mechanirml Equiptent Requalification '#*#
*~ M.A. Scott #' ** 6/15/83 Sveiect 30" Cylinder Operated Butterfly Valves Checked By. [j' Date L.C. Feutandez 6/15/83 System Job No cde No CSP and CEP 82044 CS.01.F Rev. No Sheet No.
OID 361164 1 4.3.40 r Towt L o u Strd B'b- lokh MT /* ara:_. I.c #b dMl ,AML ' C-D
- ro .aw a i: r--r w n nn nmi rc e mir 7 :t. A rJ6, c . Przar,0c.ec , & '?'BLta.J/rJ4 k ?cr Ar (o e oJ NF s dGC h =
2hM z(n.) 3;' 70 = 4'/. / 2 e/a iHr ra we.- < o u~ pJn ca +2 ed 6 c ,Jr2 iO r-MrJ p hl / , ,, m= .)nc, + i/4s +27&. -s /j R?i' ~;= w, w w._,,a, wm 2,zm ,= ,w 2')33 _- /3277 m:- d. $ C 0
% m =h*707f~5C6) u n,s n, - i, ~n -
nJ+,3 -rr+s m JA~e'c~ M MS r-e e-. =.p- n;u-:-
SJ '7" c~ar.M7 1 -tr% M dP';D*s'pl4 r_ s en ,
uJHici-/ c.0a Jt 2 3 e. uJ., ~77/c' A-c rum A.:_ rsre.f/w//J* -5772r2 eeeJr 60 i r#r J A-e c 2">-rA"5 LT u//>W ,
Calculation 4 L n ri Sheet ;
!!!!!!IIllll111lll111ll1111111 wJ Project wpss heal Equipnent Faqualification Prepared By M A h tt*. '
6/15/83 Sveiect Checked By- Y#Da'a 30" Cylinder Operated Butterfly Valves L.C. Fernandez 6/15/83 Systern Job No File No. CSP and CEP 82044 OS.01.F
. . , , , . . Rev. No. Sheet No.
QID 361104 1 4.3.41 TM -sTract Lej et., iO we' coceJex wm ut? --ro o'Y'm<.pm th L.o +==. is
'3canta M3 COT ~7HC /- / k'o r k = Sz e 9:6 T A- 14.10 =o .s:-
\
\l.* 6 90. S 4 4.'5 /.5 2/22Z t,s O
G f. 2 s' . zaad b4 n = Zl396 +2 44d(G)=5BCol8
-R,, - a, = e s c l a _ =zs ao s .. , a. a l
l SH cn ie. A eo ac. n /c 2'? Aya -- v3 ," _ I 2 2- 2. :. 3B kJ A 52 Lo-o mor u she_ ta 1-1 > ex, w
\
I
% = ,(t o. s ,f r - ger -
V 4./s/( 23.32 l e ~. (% )\ ') W $ l%OrJk TAT f-f s*-<t '
. tI '
hv" 687 g.s
= 62 &
- t ::
Calculation AL,, Sheet 111114;11ll111!!!!illI!!I1111 O "' ' WFPSS Mechanical Equignent Pequalification ' ' ' '
#' M. A. Scott 6/15/83 Suc r ect Checked By /,$ fate 30" Cylinder Operated Butterfly Valves L.C. Fernandez 6/15/83 System Joe No File No CSP and CEP 82044 OS.01.F
-m ,,, Aev No Sheet No THS A yr Aca tohb cra ~.E:~ uJ SL3 I c r7 / od [, * #67 [4) g 6,6. Ma
- e. 7s),.e vn, io -c e~- c~ -u , = u,ca raw w m<da /s m/N 5 27 C, G 7 :2G G/58 i u, c.-a- - - n-n n e
W 0.e [2o4
= -r- 6s +2a)* + (ps%c,z')]%
= s os. e -d/,a
~~Th rzssom A -5 nee =. W et, is M.-J Tus=t. >
- 30T.o 2 /'5 % ~P'sf 707(.sizS)
O
=.=
Calculation t4 Cd t i Sheet 11111111111!'1illlll11ll11011 p'%.)
'*" WPPSS Mechanical Equignent Requalification 21.A. Scott \ 6/15/G3 Subject Checked Sy. gG Cate 30" Cylinder Operated Butterfly Valves L.C. Fernandez 6/15/83 System Job No File No.
CSP and CEP 82C44 OS.01_F
- , . . . ~ Pev. No Sheet No QID 361104 1 4.3.43 Tsde- u)e:t ;;> MSSS. Oid i& S ~~/ W .-) W 6, k OP -7 W 5~ l0* S mi 25C.~77cN t.::r c4r c ac AM As Fo t.c o a . Cnsscan v'c r' ccu wr c.coc.x CW.AE'" W lT &D C, KCL c'., CR *.K ' ,
.a M,
-g y
4x4 >
.G -
TM7 Av&~A oF La35L."t> v . ~a- er t ,n ras.t O hp 2(co M ") - 15 >J
\ /
d 4-.,. % ./_4 a b ['Mb 2A v'G f2) ds A 4,a 4,a ' y a 46b [tok 47.14 4 ~_ :[4444 -92.[2-)
'4
- 4 4:7.2
= T&l
- 85 + /2 60 = 2 0 94 "/N O psu:> s h e O
t - cc nu
- t ::
Calculation [4 f.& i lillllillllllllllilililllllill Sheet
'*** WPPSS I4echanical Equignent Fequalification M.A. Scott ~-"i 6/15/83 Subi, et Checked Oy. e.TpOate 30" Cylinder Ooerated Butterfly Valves L.C. Fernandez 6/15/83 Systern Job No File No CSP and CEP R2044 m 01_P denemma:fde= Rev. No. Sheet No OID 361104 1 4.3.44
'THe' MM / ^./ JA / O Ad rarnJGit c" 4 o@ r3 S Y k ova a.J E w en GE ~r Ha- ?oWOU
--r-C' '
>S-ND C C t.J M / 4 . M aa / o J %
,N
$ WW = WY .2_._ Y
-> E 3 W= 4d6Nf? =409l d A
N i tn- M, - i-l? S d-M O b rA S trJ'E ( +4c' N (o u 7 O T" (0iTH 4 ht'~ h701 em hb S i EC
-e ' @/ + M4* = d 69 G 3/fJ
. Io S' Thy EL loa & Si-ec;. 'J f-r < 17 e'=
//400 7"5:~ Fefd ;Cid=r76 ur' Mb 05 o A.26 2 ra) eLrG A-r_. o N4 +Js- c.e M & M 4' = -. # s.. % - '.; a s '^)
(//,'300)(707 &
-/
=) OK". '// S Pi4. L" rz : ? TA~'
& r7sg cJ e t T;, M e O J r- 2 ~ ~ ~rr 3 .-f r' s o * .-r Thr-e Sdv? TM W L-D %= %
<fz e s a u r 7 r la, WmY /-/2r-~~~ M R L.~ M ~.
- s ::
Calculation 4L n i Sheet
,G lll!Illll1111111111lllllll11ll t]
Project h'ppss Wcal Equiptient Pequalificats. Prepareo By' M.A. Scott 4'() 6/15/83 sue ect # 30" Cylinder Operated Butterfly Valves L.C. Fe 6/15/83 System Job No. Fde No CSP and CEP 82044 h OS.01.F _ Rev. No. Sheet No QID 361104 1 4.3.45 T&f 5drAL M #7.) TantC M 6. W /S So= F6 d 2- , 3Nl La/id n T& M/n 4 0 A-D ~'D JT ~7D A7C /Aw oJe c rDwid AAJO F #fr4M~~ /x @ : 1 %. W: n [q = M, . b M c' _ U AA 24 T
=- se.o + s u + is s m [a s A )
l / / //. 5 3
= se o +41.1 - c79.1 = // 8 7 ~.J iJ Ta -tu , n eweiarz:, wp c:,
f= f/87* + 54/ = 12% A/d s., ~ c. . 4: .xn ~ an o.= m v.n.. r w a. - a ..
#O -S 772d*DS ("E NM
~~
To>sr::. 7 7 3j " 2 7 % 5"O ! d / N d O v
;;a ;;
i======= Calculation M %'Ta lillllllilllllllllllll!!(!Illi Sheet Project Prepared By: - Date e WPPSS Mechanical Mt2nent Recualification M.A. Scott 48 6/15/83 Subject Checkec By- ['(p Date 30" Cylinder Ocerated Butterfly Valves L.C. Fernand6z 6/15/83 System Job No Fde No CSP and CFP A?044 OS.01.F _,Q s 361104 "'*"~ Sheet N 1 4.3.46 Tus- M A-gr W u l _o A r:C. o4 M W '-. o* W o%N %A:nE!i /-e e 4e
- -o e Lev 33 5, e cer- rds- wsc R e m :, i , NJ m-m 'w e. r -t K r1oJ l :s BY S den t"~ W- ) =~'AM 01= W ~~4:.M i &c" 'WLA'TE* I: ~?/13I C.4 LL'/
/<-ruJ& H et A . as c dM.- MeM=snc.
A-5 M 4AJ bet.o4. L A-7s ' t
- 3. e.75. - ,
%. .pe s
c,.dc,/ = 6'59N '
/
4.76 s N r
'/ '
I'
-l to e ss- a a.ic.i a x <_
64G I d m =r e ow w rve-- Mouror-4 sdne cuoaa T Ei g (,J& I($ E99) = 2.4'ow ro c= -S*= L (4)#. . 2. 6 7 3 s
Calculation / t41% n Sheet ll111111111111111111111111llll (
" * WPPSS Mechanim1 Equiprnent Requalification "'#
8' M.A. Scott #8U6/15/83 Subject Checked By L.C. Fermndez #Y Date 30" Cylinder Operated Butterfly Valves 6/15/83 System Job No File No CSP and CEP 82044 OS.01.F QID 361104 1 4.3.47
,y ma creJa, w :. vgoa -ryis were > sc &
Osb
, &/ , 25o3c, , 9377 al/s 3 ,,47 THG~ }2er$ut.:7~i "hK f.-oA~b u.)6 JCb ~BC
$ YA d 4l , / 6/6 Abd 4
Tu (e.s /ard to.4e u.Jasun B E~ p 4 vg = 937724-/6I5*' = 9516 "here A 6/$. uJee:> u r e e d e, n 'er ci: r
- m, s. m.m -,-: -
%d %Y Q, %IS _ - 2 /655 L-5/id ' j
. ro .ws(D , y,a a fP d5 uJen?[ C & ar~b re A Y e>J
,- s- o w_, i or on ,4. cm wiw L- U.)S7 ~p M M*7"~ ?.4 / 7~1~I ~ / h r"d t i 2 '.)) /O
"#J """b C Wd A )5 g ,,
_m
'$ A he j lh, b f )
() ? _j _.. a= (s R G C+ d G
= 2 4.1 ne
M Calculation L4L E ra Sheet illllllllllllllllilllllll!!!Il O
'* ' WPPSS Mechanical Equiment Recualification M.A. Scott 6"' 6/15/83 Subiect Checked By cr" N ate 30" Cylinder Operated Butterfly Valves L.C. Fernandez 6/15/R~t System Joe No. File No CSP and CEP A'> 04 4 m _ n1 r h a , m is Rev No Sheet No OID 361104 1 4.3.48 -
I 4er LJo LA Ehd'I' C4.30 Rb ~BC (o46I 5.975 l 26 - = ."3 G>h,1 = 2 *) o76 m u.- +- - a - ae uso o t.d er
=_ C t, WOW 2- = 2kl3 d d 14.1
% venm m Aee tap
-r O u oJ t. d =I
* $n 4 79096 . Se26 y G bI G l A 2 4.I so.5
=
764 + 6 is = /3&c) Ma T tttr < c.s 4 4-< - L.OR a,d t-f5' uJ F ~5 r 5 -M
-t " J[/,3 4 /3@ e ZW l
N M tJL.f 7 h G.)22 *b Me~> , / C Tkid
-> /JCQQ
" ?('5/:.5)
#7 = /2.64'l %T
* ,v,,
~ ~s - o-
-n ,s --
a, e,
=,
w r q
'T W /-c-rt.)M 'F-;sL97L, Ur 2/iLJ 15 c .).Jye' AA; e 5 ,d-5 _- , #"
y ---
m 1Ell2llllllliMlll Calculation ST67T3 Sheet 111111111!!!!I11111111111!!!11 Pro #ect Prepared By Date WPPSS Mechanical Ecuiument Oualification J.E. Rakowski 1/10 / R3 Chechec By Subsect in" Entr,rflv VnIv,, L. c . Fmu, ,Date dM Sy: tem JoD No Fue No
- CMP nna crp 82044 O S. 01/F Analysis No Rev No . Sheet No 361104 1 4.3.49 Section 4.3.5 -Fatigue Analysis Discussion The operator and bracket assembly are not part of the pressure boundary, therefore, the fatigue analysis will be performed in accordance with Appendix B of the AISC Manual for Steel Con-struction. The following assumptions apply to the fatigue analysis.
- 1) Faulted stresses (based on piping-analysis accelerations) p)
( will be used. This is necessary to insure operability after a design basis event. l
- 2) The actual stresses used will be the ones calculated in Section 4 3.
- 3) If the alternating portion of the stress has been cal-culated separately only this part will be used. If the
, operating loads (i.e. seating torque effects) are al-I ready included in the stress analysis it will.be con-servative to use the calculated stress value. As long as no failures occur, the operating stress does not
. need to be extracted.
- 4) The allowable 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.
i 1 v .
--u~,.,,-.c-.~w. -- , -- - - aa. s .wwa
Calculation 3 (% rd lilllllillllllllllllilllllllli Sheet
~
Project Preparec By Date tmpqR %chnnien1 Fnninmone Onnli fi enti on J.E.Rakowski 1/10 / R 3 Suorect Checaed By Date ,, 30" Butterfly Valves l 0 few"A ~ ' O IM System Joe No File No CSP and CEP 82044 Os.01/F Rev No Sheet No pgggPga
- 7) Bracket bolting is assumed to be properly tightened and will not be considered for fatigue per Section B3.1 of the AISC Manual.
The table on the following page gives the calculated stress range, stress category, and allowable for the critical components. The fol-lowing page gives excerpts from Appendix B of the AISC Manual showing the descriptions of the relevent stress categories. O e k
Calculation [41*12 d Sheet Illl!llililllilillllilllilllil O Prmert Prepared By- Date WPPSS Mechanical Eauipment Qualification J.E. Rakowski 1/10/83 Sub,ect Checked By Date 30" Butterf1v Valves L. C . Fne. A. c ,fvln System Job No Foe No CSP and CEP 82044 O'S. 01 / F Rev No Sheet N ggisgp4 i 4.3.51 Fatigue Analysis (cont.) STRESS STRESS STRESS STRESS 1.5 x ALLOW ITEM TYPE (PSI) RANGE (PSI) CATEGORY (FROM AISC) TRUNNION PIN T 4108 8216 F ??500 l DRIVE ROD (MAX) T - SEE TA BLE 1. 2 - A 00000 SUPPORT EARS T~ - SEE TAB"E 1.2 - A 40000 t 9127 18254 A 90000 ! MAIN SHAFT a- 7158 14316 A 90000 NOTES: l t I (l) Assume shear stress on nominal area of a stud type shear connection. Note that this comparison includes all of the load combinations in one l conservative comparison using the maximum stress and the total number of cycles ( 3 x 4500 + 2000 + 60 = 15560) .
- O .
9000 Oc
- . . . . . . . . . . . . . ___-.-~n n
Pr;pired By D,tta Calculation Shest de Fyr_, y49&,t
/
___ CtheksdB Data
~
Prosect 0'PLV #' ~~ d ' Lk,Dj" 7 Job No Feie No N O1 h
^
Subsect _d -E P M7 '-" UJ T-- g- M& lilllllllllllllllllllllllllll! System -- $U Sneet No Analysis No SGu04 n,, so I 4.3.52 E4TI6(AE M H n L V3 TS f t o w r.h Tue raste s e s.o w a s., seen can oenses Flion A ?9ENb7x 3 0F THE Ar$C H s4 NLA H L OF STEEL C ONS TR uc Tr o M. Tuc cases asas nue uneva L1ITH AN 6 R R 04). i Stress General Cate-Situation Kind of gory. l Condi-j g;,, Stressa (See j Table B3) l Plain Base metal with rolled or cleaned sur. T or Rev. A & O, material faces. Built up Base metal and weld metal in mem. T or Rev. B members bers, without attachmenta, built up of l plates or shapes connected by contin-uous full- or partial penetration groove l I welds or continuous fdlet welds parallel l to the direction of applied streaa-Calculated flexural stress, /s , in base T or Rev. C metalat toe of welds on girder webs or flanges adjacent to welded transverse l stiffeners. l Base metal at end of partial-length T or Rev. E l welded cover plates having square or tapered ends, with or without welds across the ends. Mechani- Base metal at gross section of high- T or Rev. B cally strength-bolted friction-type connec-fastened tions, except connections subject to connec- stress reversal and axially loaded jointa l tions which induce out of-plane bending in l connected material Base metal at net section of other me. Tor Rev. D chanically fastened joints- , Base metal at net section of high- T or Rev. B strength bolted bearing connectsons. Attach-ments Shear stress on nominal area of stud-type shear connectors. S F 4 gIQ
. .~. -- - - -
Calculation [g W iira Sheet L) > llllllllllllllllllllllllllllll Projec' Precared By Date WPPSS Mechanical Equipment Qualification J.E. Rakowski 3/25/83 Subject Checked By Date 30" Butterfly Valve L.c F,s a y ,
/ 74 2 System JoD No. Fde No CSP and CEP 82044 OS.01/F Analysis N 361104
*** " 1 Sneet N 4.3 S
4.4 REFERENCES
- 1) BIF Drawings Drawing # Rev# Description a A-206763 F General Arrangement b CEP-625-10 From Reactor Nozzle X-3 to SGT-FU-1A, 1B c CEP-625-ll.12 H From Reactor Nozzle
/) ( X-3 to SGT-FU-1A, 1B d C-26095 Model A-83B Cylinder e A-206767 Valve Assembly f DOC-D-220-0310-IR-66 O Tube errection iso-metric g D-207110 F Valve Data Sheet h M-144 General Arrangment plan mis level k CSP-807-3.4 Containment purge air supply system O .U
, = . .
Calculation M1C Ta Sheet lillllllllllilll!!Illllllllill e i'**WPPSS Mechanical Equipment Qualifica$*[5N 'J.E. Rakowski 3/25/83 Sut:iect , e Date 30" Butterfly Valves Checked ByI- C . Pe twa.> A, Y/: 2 J: System Joe No. File No CSP and CEP 82044 OS.01/F Analysis N """~ sheet No. 361104 1 4.3.54 Reference cont'n Formulas for Natural Frequency and Mode Shapes, Robert D. Blevins Van Nostrand Reinhold Company 1979 Edition
- 3) BIF Report TR-27234 and TR-27235, " Dynamic Torque Calculation of Butterfly Valve; Sizes 24 and 30 inch",
dated November 10, 1982.
- 4) Report TR-74-8 by McPherson Assoc., Inc., " Design & O Seismic Analysis 30" Cylinder operated Butterfly Valve".
(Rev. 1) 12/31/75. i ! 5) WPPSS letter to Cygna Energy Services, GE-02-RWH-018, i 12/17/82. l l 6) WPPSS, WNP-2 SRM Equipment List Summary Sheets dated ! 2/10/83.
- 7) Cygna Energy Services, Equipment Qualification Walkdown Verification Form dated 7/14/82 and 7/19/82.
I 8) Cygna Energy Services, " Project Manual Design Criteria," DC-1, Rev. 1, 10/82.
- 9) Burns and Roe Revised Piping Analysis Loads for CSP-V-1 and 2 (dated 4/12/83) and CEP-V-1A and IB (dated 11/15/82).
- 10) Communications Report, R. Ricappito of BIF and J. Rakowski of CES, "BIF Valve Dimensions", 2/11/83 O
4' O
~
APPENDIX A COMPILED PROGRAMS AND RESULTS FOR CSP-V-1 CSP-V-2 i O l CYGNA ATTACHMENT l JOS NO. 8104 4 FILE NO. 05. W. F f SHEET NO.4 3 AI l O I
- . , _ _ -.. ,. --..-- . _- - , - . - . _ - . ~ . - . . _ . . , - , - - . _ - - . . - . _ . . . _ - - - - . _ _ _ _ - _ _ - . - - . --
tbasic csp 12 tm S-BASIC Compiler Version 5.4b
'901:00 REM ***** BIF VALVE AND AIR OPERATOR SEISMIC STRESS *****
0002:00 REM ************<** CSP-V/AO-1/2 ************************ 0003:00 REM *************** 10 INCH A0 PARAMETERS *************** 0004:00 REM 0005:00 var i,j,k = integer 0006:00 var I rod ,1 cg ,x , ph i , l ave , abi t .11,12, e l , e2 e3, e4, e5 = real 0007:00 var fst2, ca , i a , cb , i b , aa , ab , d t , d2, c i , i l , e:2, i 2=re al 0008:00 var 1rodo,1cgo,1dr,d, abush, pbush=real 0009:00 var fcof, feo, ma,mb, siga, sigb, fcde, icdrf ,maf , mbf=real 0010:00 var dear, fcear,fr, f11,f22,la, ci12,ci21,stt3,sem1=real 0011:00 var sem2, set 3,ses1,ses2,sr, tau 11, tau 22,tatear,aear=real 0012:00 var btens, taubit, set 3f,semif,sem2f,fcearf, frf,flif=real 0013:00 var f22f,stt3f,sestf,ses2f,srf,taulf, tau 2f,taurf=real 0014:00 var taubf,btf, der,dtaur,dtaub,dbten,dsa,dsb,dpb=real 0015:00 var sdraf , sdrbf ,pbushf , tau 11 f , tau 22f=real 0016:00 var wao,wbr , f tri ,wa tr 1,s t ,si f , s2, s2f ,m1,mi f ,m2=re al 0017:00 var m2f,t3,t3f,tt3,tt3f,1br,wtot=real 0018:00 var bst,bs2,bt3,bm1,bm2,btt3=real 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 bst etc TURN ON WITH K=1*** 0024:00 REM
'025:00 REM J26:00 dim real a(3,3) 0027:00 dim real b(3) 0028:00 dim real gic(3,3) 0029:00 1 data 9.5, 10.5, .88, 3.94, 1.50,1.34 0030:00 2 data 25,21.50,.488,48.,4.85,.627,1.75,3.0 0031:00 3 data 1847.,.875,.46,.648,.138,2.41,1.4 0032:00 4 cata 593.,321.,5.25,8.5,28.5,15.,7.75 0033:00 5 data 40. 16.25,26.5,43.,2.075 0034:00 6 data 135.,90.,135.,90.,180.,90.
0035:00 7 data 45.,90.,135.,90.,0.,90. 0036:00 REM DATA 6&7 FOR VALVE / GLOBAL-G ORIENTATIONS AND WEIGHT VECTOR 0037:00 restore 0038:00 read dl,d'2,c1,il,c2,i2 0039:00 restore 2 0040:00 read t rod,1 cg,x ,ph i ,l ave ,abi t ,11,12 0041:00 restore 3 0042:00 read fst2,ca,ia,cb,ib,aa,ab 0043:00 restore 4 {]'[(} ff,$( 0044:00 read wao,wbr,el,e2,e3,e4,e5 ATTA CHM. 'T^ 0045:00 restore 5 0046 00 re ad I rodo ,1 c go ,1 dr , d , abu sh JOB NO. SED 4" 0047:00 restore 6 i:lLE NO. 0L ol. F 0048:00 read a(1,1),a(2,1),a(3,1),a(1,2),a(2,2),a(3,2) SHEETNO. 43 Al 0049:00 restore 7 0050:00 read a(1,3),a(2,3),a(3,3),avC1),av(2),av(3) 151:00 text 0,& INPUT GLOBAL ACCELERATIONS & 9052:00 input b(1),b(2),b(3) 0053:00 print 0054:00 text 0,& INPUT DATA & 0055:00 print 0056:00 print " GLOBAL G-LEVELS = " b(1),b(2),b(3) 0057:00 print " NORTH VECTOR ANGLES = "ta(1,1),a(2,1),a(3.1) 0058:'JO print " VERTICAL VECTOR ANGLES = "ta(1,2),a(2,2),a(3,2)
0059:00 print " EAST UECTOR ANGLES ="ga(1,3),a(2,3)n[d,3) 0060:00 print " WEIGHT VECTOR ANGLES = ";av(1),av(2),av(3) 0061100 print 0062:00 for i=1 to 3 0063:01 for j=1 to 3 a(J,i>=a(J,i)*2.*3.1416/360. [_0064:02 1065:02 (_/166:02 next j gic(J,i>=b(i>*cos(a(J,i>> w067:01 next i 0068:00 for J=1 to 3 0069:01 av(J)=av(J)*2.*3.1416/360. 0070:Cl next J 0071:00 print 0072:00 text 0,& LOCAL G-LEVELS & 0073:00 print 0074:00 print gic(1,1),gic(1,2),gic(1,3) 0075:00 print gic(2,1),gic(2,2),gic(2,3) 0076:00 pr i n t gi c(3,1) ,gi c(3,2) ,gi c(3,3) 0077:00 REM WEIGHT COMPONENTS 0078:00 for J=1 to 3 0079:01 wa(j)=wao*cos(av(J)) 0080:01 wb(J)=wbr*cos(av(j)) 0081:01 next J 0002:00 phl= phi *2.*3.1416/360. 0083:00 la= lave /2 0084:00 cl12=c1/i2 0085:00 ci21=c2/i1 0086:00 aear=11*12 0087:00 REM CALCULATE EAR FORCES USE B&R LOADS AS OPTION LATER 0088:00 REM FIXED COMPONENTS ARE ALWAYS THERE 0089:00 lbr=1 rod +1cg 0090:00 watr1=1br*wa(1)/Irod 091:00 sif=wb(1)+watrl k 392:00 wtot=wao+wbr 093:00 s2f=wb(2)+wa(2)+fst2 0094:00 t3f=wa(3)+wb(3) 0095:00 m1f=-(wa(2)+wb(2)+fst2)*e5-wa(3)*(e3+1cg)-wb(3)*e4 0096:00 m2f=(watr1+wb(1))*e5-wa(2)*e2-wb(3)*e1 0097:00 tt3f=watr1*e3+(wa(2)+fst2)*e2+wb(1)*e4+wb(2)*e1 0098:00 fcdef=1cg*wa(1)/1 rod 0099:00 maf=f cdrf *(Irod-13.5) 0100:00 mbf=fedrf*7.125 0101:00 sdraf=fst2/aa+ abs (maf*ca/la) 0102:00 sdrbf=fst2/ab+ abs (mbf*cb/ib) 0103:00 fcof=1cgo*wa(1)/1rodo 0104:00 pbushf=fcof*(1dr+d)/(d*abush) 0105:00 REM STRESSES FROM FIXED COMPONENTS 0106:00 dear =(d1*d1+d2*d2)**.5 0107:00 set 3f= abs (t3f/(4*aear)) 0108:00 semif= abs (m1f/(2*d2*aear)) 0109:00 0110:00 sem2f= abs (m2f/(2*d1*aear)) fcearf=tt3f/(2* dear) CYGNA -- 0111:00 frf=x*fcearf ATTACHMENT 0112:00 f11f=-(fcearf* sin (phi)-frf*cos(phi)) 0113:00 f22f=fcearf*cos(phl)+frf* sin (phi) JOBNO. 32o44 0114:00 stt3f= abs (f11f*1a*ci12)+ abs (f22f*1a*ci21) FILE NO. 0$ AH S 0115:00 sestf= abs (s1f*cil2*1a/4.) SHEETNO.E343 0116:00 ses2f= abs (s2f*cl21*1a/4.) 7- *117:00 srf= set 3f+semif+sem2f+sesif+ses2f+stt3f ( '318:00 REM EAR SHEAR k ;119:00 tau 11f= abs (sif/(4*aear))+ abs (f11f/aear) 0120:00 tau 22f= abs (s2f/(4*aear))+ abs (f22f/aear) 0121:00 taurf=(tau 11f* tau 11f+ tau 22f* tau 22f)**.5 0122:00 taubf=taurf *aear/abi t 0123:00 REM EARBOLT TENSION 0124:00 btf=(se t3f +semif +sem2f)*aear/abi t n.m=.nn ..:..
U126 00 print *UFtkAl1Nb CYLINUhH BNU FNhbbUNE *;pDusnt 0127:00 print
- OPERATING UALUE EAR TENSILE STR "gerf 0128:00 print" OPERATING V/udE EAR SHEAR STRES *;taurf "0129:00 print" OPERATING EAR BOLT SHEAR STRESS ";taubf 0130:00 print" OPERATING EAR BOLT TENSILE STR ";btf 0131:00 print
'132:00 REM 13:00 REM CALCULATE VARIABLE COMPONENTS b.34:00 REM 0135:00 dsr=0.
0136:00 dtaur=0. 0137:00 dtaub=0. 0138:00 dbten=0. 0139:00 dsa=0. 0140:00 dsb=0. 0141:00 dpb=0. 0142:00 for J=1 to 3
-0143:01 f c o= 1 c go*wao*gi c ( 1, J )/1 rodo 0144:01 pbush=fco*(1dr+d>/(d*abush) 0145:01 ftr1=1br*wao*gic(1,J)/Irod 0146:01 s1=ftr1+wbr*gic(1,J) 0147:01 s2=wtot*gic(2,J) 0148:01 t3=wtot*gic(3,J) 0149:01 m1=-wtot*gic(2,J)*e5-wao*gic(3,J)*(e3+1cg)-wbr*gic(3,J)*e4 0150:01 m2=(ftr1+wbr*gic(1,J))*e5-(wao*e2+wbruel)*gic(3,J) 0151:01 tt3=ftr1*e3+wbr*gic(1,J)*e4+gic(2,j)*(wao*e2+wbr*el) 0152:01 fedr=1cg*wao*gic(1,J)/1 rod 0153:01 ma=fedr*(Irod-13.5) 0154:01 mb=fcdr*7.125 0155:01 siga=ma*ca/la '
0156:01 sigb=mb*cb/lb 0157:01 REM CALCULATE EAR TENSION 98:01 set 3= abs (t3/(4*aear>>
. .9:01 sem1= abs (ml/(2*d2*aear))
0160:01 sem2= abs (m2/(2*d1*aear>> l 0161:01 fcear=tt3/(2* dear) ! 0162:01 fr=x*fcear l 0163:01 f11=-(fcear* sin (phi)-fr*cos(phi)) l 0164:01 f22=fcear*cos(phi)+fr* sin (phi) i 0165:01 stt3= abs (f11*1a*ci12)+ abs (f22*1a*ci21) 0166:01 ses1= abs (s1*ci12*1a/4.) 0167:01 ses2= abs (s2*ci21*1a/4.) 0168:01 sr= set 3+sem1+sem2+sesl+ses2+stt3 0169:01 REM EAR SHEAR 0170:01 tau 11= abs (s1/(4.*aear>>+ abs (f11/aear) 0171:01 t au 22= abs ( s2/( 4.
- ae ar ) ) + abs ( f 22/ae ar )
0172:01 tauear=(tau 11* tau 11+ tau 22* tau 22)**.5 0173:01 taubit=tauear*aear/abit 0174:01 REM EAR 80LT TENSION 0175:01 btens=(set 3+sem1+sem2)*aear/abit 0176:01 dsa=dsa+siga*siga I g 0177:01 dsb=dsb+sigb*sigb {}9flhhg) M__ 0178:01 dpb=dpb+pbush*pbush 0179:01 dsr-dsr+sr*sr ATTACHMEM7_ 0180:01 dtaur=dtaur+tauear*tauear 0181:01 dtaub=dtaub+taubtt*taub1t -JOB HO. flout _ 0182:01 dbten=dbten+btens*btens FILE NO.- N C3:01 next J SHEETNO 11g,- 4:00 REM COM81NE STRESSES 0185:00 dsa=dsa**.5 0186:00 dsb=dsb**.5 0187:00 dpb=dpb**.5 0188:00 dsr=dsr**.5 0189:00 dtaur=dtaur**.5 0190:00 dtaub=dtaub**.5 a.a. ... sus.._w.... -
0192:00 print 0193 00 text 0,& DYNAMIC COMFONENTS & 0194:00 print 0195:00 print " DRIVE ROD TENSILE STRESS AT A";dsa 0196:00 print " DRIVE ROD TENSILE STRESS AT B";dsb 77:00 print " BUSHING PRESSURE ";dpb 98:00 print " VALVE EAR TENSILE STRESS ";dsr 99:00 print " VALVE EAR SHEAR STRESS ";dtaur um00:00 print " EAR BOLT SHEAR STRESS ";dtaub 0201:00 print " EAR BOLT TENSILE STRESS ";dbten 0202:00 dsa=dsa+ abs (sdraf) 0203:00 dsb=dsb+ abs (sd,rbf) 0204:00 dpb=dpb+ abs (pbushf) 0205:00 dsr=dsr+ abs (srf) 0206:00 dtaur=dtaur+ abs (taurf) 0207:00 d t au b=d t au b+ abs ( t au bf ) 0208:00 dbten=dbten+ abs (btf) 0209:00 print 0210:00 text 0,& FIXED PLUS DYNAMIC COMPONENTS & 0211:00 print 0212:00 print " DRIVE ROD TENSILE STRESS AT A";dsa 0213:00 print " DRIVE ROD TENSILE STRESS AT B";dsb 0214:00 print " PUSHING PRESSURE ";dpb 0215:00 print "UALVE EAR TENSILE STRESS ";dsr 0216:00 print " VALVE EAR SHEAR STRESS ";dtaur 0217:00 print " EAR BOLT SHEAR STRESS ";dtaub 0218:00 print " EAR BOLT TENSILE STRESS ";dbten 0219:00 end 0220:00 0221:00 0222:00 23:00 4:00 _5:00 ****** End of program ****** CYGNA ATTACHMENT JOB NO. f7044 FILE NO. 0s.01.f SHEET NO. 4.3 Af O) L_
espi INPUT GLOEAL ACCELERATIONS
? 2.26,3.62,2.3 INPUT DATA GLGEAL G-L8)ELS = 2.26 3.62 2.8 NORTH UECTOR ANGLES = 135 90 135 VERTICAL VECTOR ANGLES = 90 150 90 EAST VECTOR ANGLES = 45 90 135 WEIGHT VECTOR ANGLES = 90 0 90 LOCAL G-LEVELS -1.59807 -1.S8092E-5 1.97989 -8.62121E-6 -3.62 -1.06811E-5 -1.59807 -1.38092E-5 -1.97991 OPERATING DRIVE ROD STRESS AT A 766.432 OPERATING DRIVE ROD STRESS AT B 1319.35 OPERATING CYLINDER BRG PRESSURE -7.15824E-4 OPERATING VALVE EAR TENSILE STR 2111.01 OPERATING UALVE EAR SHEAR STRES 293.896 OPERATING EAR BOLT SHEAR STRESS 2460.85 OPERATING EAR BOLT TENSILE STR 1625.1 DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 28384.4 DRIVE ROD TENSILE STRESS AT B 43412.2 - U % d ; h ./c.'m tf ?r [ve..'
BUSHING PRESSURE 477.447 ',,h,',b b h kbfk k k hk hhh='.jj SEC SMECTJ 4.330- h s.4 8 EkR bOET SHNAN STRNbb hbb9 EAR BOLT TENSILE STRESS 10524.9 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 29150.9 DRIVE ROD TENSILE STRESS AT B 44731.6 -- PUSHING PRESSURE 477.448 =: := = e nE :T=Ee: -
- CYG h5A
-VAL-VE E: CHE^,R :TRCOC -tFS4.03 EAR BOLT SHEAR STRESS 9499.86 ATTACHMENT EAR BOLT TENSILE STRESS 12150 JOB NO. F2o44 FILE NO. os .01. F SHEET NO. " 3 M" O
c2 2 UT GLOBAL ACCELERATIONS 26,3.62,2.9 INPUT DATA GLOBAL G-LEVELS = 2.26 3.62 2.8 NORTH VECTOR ANGLES = 135 90 135 VERTICAL VECTOR ANGLES = 90 100 90 EAST VECTOR ANGLES = 45 90 135 - WEIGHT VECTOR ANGLES = 90 0 90 LOCAL G-LEVELS
-1.59807 -1.38092E-5 1.97989 -8.62121E-6 -3.62 -1.06811E-5 -1.59807 -1.38092E-5 -1.97991 OPERATING DRIVE ROD STRESS AT A 766.432 OPERATING DRIVE ROD STRESS AT B 1319.35 OPERATING CYLINDER BRG PRESSURE -7.15824E-4 OPERATING EAR WELD TENSILE STR 3090.43 OPERATING EAR WELD SHEAR STRES 735.124 OPERATING EAR BOLT SHEAR STRESS 2460.86 OPERATING EAR BOLT TENSILE STR 1625.1 -
(G v!'+11C COMPONENTS DRIVE ROD TENSILE STRESS AT A 28384.4 DRIVE ROD TENSILE STRESS AT B 43412.2 BUSHING PRESSURE 477.447 EAo WE'e O TEN 84 LE-STRESS EAR-WELD-SHEAR- 0TRC00 1-20 h ;2-21-02.74
-h SEE SM ?7C ,")- 3',J b EAR BOLT SHEAR STRESS 7039 EAR BOLT TENSILE STRESS 10524.9 FIXED PLUS DYNAMIC. COMPONENTS C'VGNA DRIVE ROD TENSILE STRESS AT A 29150.9 ATTACHMENT {.
JOBNO.jgg44, 4 DRIVE ROD TENSILE STRESS AT B 44731.6 PUSHING PRESSURE 477.448 yttg Ho 0 d' -]b-l -EA EWELD TENSILE STRESS 15152.i .1 -EAR WELT---SHEAR STRESC 29Gh06- i 3uer
'^-*' uC.4*A7 !
EAR BOLT SHEAR STRESS 9499.86 ~ ~ ~ ~ ~ EAR BOLT TENSILE STRESS 12150 L _.)
csph) INPUT GLOBAL ACCELERATIONS
? 1.44,3.54,1.9 INPUT DATA GLOBAL G-LEVELS = 1.44 3.54 1.9 NORTH UECTOR ANGLES = 135 90 135 VERTICAL VECTOR ANGLES = 90 180 90 EAST UECTOR ANGLES = 45 90 135 WEIGHT VECTOR ANGLES = 90 0 90 LOCAL G-LEVELS
-1.01824 -1.3504E-5 1.3435
-5.49316E-6 -3.54 -7.24792E-6
-1.01824 -1.3504E-5 -1.34351 OPERATING DRIVE ROD STRESS AT A 766.432 OPERATING DRIVE POD STRESS AT B 1319.35 OPERATING CYLINDER BRG PRESSURE -7.15824E-4 OPERATING VALVE EAR TENSILE STR 2111.01 OPERATING UALVE EAR SHEAR STRES 293.896 OPERATING EAR BOLT SHEAR STRESS 2460.85 OPERATING EAR BOLT TENSILE STR 1625.1 DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 18906 DRIVE ROD TENSILE STRESS AT B 28762.8 BUSHING PRESSURE 316.332 l ..-m
,'),,,h h.5 5,.dfk5 bI55
- m . mo sinuso E
60o. m TC6 STET 3 k 3.D 3-l EAR BOLT SHEAR STRESS 5077.94 l EAR BOLT TENSILE STRESS 7164.63 FIXED PLUS DYNAMIC COMPONENTS
~
DRIVE ROD TENSILE STRESS AT A 19572.5 DRIVE ROD TENSILE STRESS AT B 30082.1 PUSHING PRESSURE VALVE EAft-TENSttE-STRESS 316.333 78eo. 59 71 CYGMA
%%LVE-EAR-SHEAR-STRESS 900 4 48- ATTACHMENT l EAR BOLT SHEAR STRESS 7538.79 EAR BOLT TENSILE STRESS 8789.72 JOB NO. 31,44 FILE NO. OL ol F SHEET NO. 4 3 A8 O
l C nR1.2 ,
/ 3dT GLOBAL ACCELERATIONS-
#r d t4,3.54,1.9 INPUT DATA GLOBAL G-LEVELS = 1.44 3.54 1.9
' NORTH VECTOR ANGLES = 135 90 135 VERTICAL VECTOR ANGLES = 90 180 90
-EAST VECTOR ANGLES = 45 90 135 WEIGHT VECTOR ANGLES = 90 0 90 LOCAL G-LEVELS
-1.01824 -1.3504E-5 1.3435
-5.49316E-6 -3.54 -7.24792E-6
-1.01824 -1.3504E-5 -1.34351 OPERATING DRIVE ROD STRESS AT A 766.432 OPERATING DRIVE ROD STRESS AT B 1319.35
. OPERATING CYLINDER BRG PRESSURE -7.15824E-4 OPERATING EAR WELD TENSILE STR 3090.43 OPERATING EAR WELD SHEAR STRES 735.124 OPERATING EAR BOLT SHEAR STRESS 2460.86 OPERATING EAR-BOLT TENSILE STR 1625.1 ft!C COMPONENTS DRIVE ROD TENSILE STRESS AT A 18806 DRIVE ROD TENSILE STRESS AT B 28762.8
. BUSHING PRESSURE 316.332 EAR-WELD TEN 5iLE 5TRES5
-EAR-WELD-SHEAR- STRESS 6415 88 151+r92 g bg c 3 g 3 , /I g y
' ' , b EAR BOLT'SH84R-STRESS 5077.96
' EAR BOLT TENSILE STRESS 7164.63 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD, TENSILE STRESS AT A 19572.5 DRIVE ROD TENSILE STRESS AT B 30082.1 PUSHING' PRESSURE. 316.333
-EAR-WELD -TENSILE-STRESSr - 1506.3- 'y EAR-WELD SHEAR-STRESS 2252.01 V;
-84R BOLT SHEAR STRESS 7538.81 'J ' g'i8 g-
"f EAR BOLT TENSILE STRESS 8789.72 477gggggg7l JOB NO. 62 odd FIL2 NO. M 0 M SHEET MC.NN
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t 1 SECTION 5.0 APPENDICES 4 J CONTENTS 4
-5. 1 Respence Spectra EEM. kd**' 4 S Walkdown Sheets w . swr so-w)
-5.2
- j. 5 .' 3 Valve Local Coordinate Systems s .1. Say s w g m (AD N></'S744 7/Je 5.5 Revised Burns and Roe Piping Analysis Accelerations 5.6 Load Comparative.Sheees t
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.j r 4 BLDG A k MFR d/F -COMPONENT EL S06 DSCRP #6s; reepcyk MODEL# C657 SERIAL # ,x/27232-I MAT 'L S//S/rf (re 76 45 PSI @ .340 'F ASME CLASS ?. LBS SIZE 36
^ YOKE' ORIENTATION MOUNTING CONDITION [ TO AXIS OF PIPE ( ) NO OF BOLTS ,a ; ^
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N . GLOBA1 CO-ORDINATE VALVE STEM ORIENTATION l SYSTEM - l OPERATOR EPN D/A MANUFACTURER MODEL NO N/A SERIAL NO TYPE SIZE ORDER NO l MOTOR EPN 9/A PJmurACTURER l MODEL NO SERIAL NO ID NO INS CLASS 1-PHASE ( ) 3-PHASE ( ) AC DC_ h0MMENTS: 2. L a *\ S w A ct a C -- J t%da.m : P a.we. O shJs ( N 1 J .% : \ ~ro hoo EftJ s CE f-tms - 1A E : H o rote o PPIPARED BY b . el DATEYWN192 VIEWED BY (SIGNATURE)
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(LIGNATUE) A DATE A/ /A
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1 l O 5.3 Valve Local Coordinate Systems CSP-V-1 CSP-V-2 l l 1 l i O I O
"" - - - w-y- - -- - . .- - - - - , . . _ _ , . . _ _ , ,_ - ., _ . _ _ , _
an OpseAYOA 4. i V CS A- V- l, E C/C4C JCC _ OSh d-I,2. S5.,$.
= e 3 fkEFFLED By ,
hyfe 2 1j 3 n . [ EEvermsu> p : v)(( M J.e 4,,/73 CVGNA ~ g.3 9 ATTACHMENT
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JCS MC. 71044 , FILC NO. % 01 f l ' bMAUl 4 N SHEET NO. S 5 I Snwr 1 g 5L _ h bag
- l35' C OS 4$ , = - 0.107 . r e~s 3 Aiaz = 90
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SUMMARY
SHEETS O-O
O 5.5 REVISED BURNS & ROE l PIPING ANALYSIS ACCELERATIONS O i i" O
. .:. - . . - ('; y v ..-
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/.. ,.h MRf 111983 ,
4.d,pr. ...;,,J f - RECElVED Sub' ject: W. O. 3900/4000 Washington Public Power Supply Synter. -
'. WUP-2 Gil*Y , - , . Qualification of Mcchanical Pipe Inm ;< 1 1983 -
y.- . Mounted Equipment: Torwarding of *.. Information
;@'-. l-CYGNA-RlCHLAND *c .
April 29, 1993
'P.
,t
'C.,- DRUP-83-078 i
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O !'J. , ; ..i ' .
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\ 'Y , Mr. L. T. Harrold ,ly..
.j,, ,g, I_ ., ,; .
Assistant Director [y$!" -_ h,
' e ,L.91~ Washington Public Power Supply Systen 1l '. C;~ t,
@?-M 's .O ? i ? 3000 George Wachington Way
~
Ai : ACHMENT-Richland, Washington 99352 08 NO. $2.o+4 - Attention: Mr. E. A. trolcl c.rg l ... F!t.E NO.M.or . F-l . e, i ..
References:
(a) WPDR-G3-17, dated 3/16/03. SHEET NO.8 ' - " 9.MMlM :s (b) WPDR-S3-20, dated 4/12/83. E . . , ,. j l .VMC r;'- (c) WPDR-83-29, dated 4/12/83. (d) Telecopy, B. A. Holmberg to g
~
I 1 *
't J. J. Verderber, dated 4/4/83.
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= *;"
'D. I '
Gentieccns In response to the request of references (a), (b), (c)
..m,,.
and (d), this letter in fcruarding refined valve accelerations. AQ k$.' . '- represent The valve acceleration sheets for the five (5) CSP valves 4 the second iteration of the refinement task.. Valve
.+a b,.l * > '. . ' . .sheets '
for the other four (4) valves represent the first ~ ' ' P1 case inform the Woodbury:,, - Q~ ' <$'f,. - iteration of the refincuent task. Office if offerts should be rade to reluce 'i further. Very truly yours, i 6 . ORIG:NAL !.tGNED BY J. J.VERDERPER 4,x _&y. .. n. . John J. Verderber
'ihki.'N' .' JJV/ BPM /ec ~ Project Engineering Mannger " 7.ff.,9;)i. Att.
f CC: Mr. W. S. Chin - EPA - 3 v/l (Mr. J. E. Rhodes - WPPSS - 1 v/I P.r. P. Buck - WPPCS - I t/1 M:ll Prop 575
. 4' -w ) ; -n .
l 1
ATTAC!! met T Data forwarded with DRWP-83-078, dated April 29, 1983 Valve # Anchor Group calc. No. . IbSP-V-5) 125 8.14.129 GTcSP-V-2__3 125 8.14.129 CSP-V-3 125 8.14.129 CSP-V-4 125 8.14.129 CSP-V-5 125 8.14.129 RCIC-V-31 107 E.14.112A
' - 8.14.121 Ri!R-V-17 B 31 RifR-V-53A 29 -
8.14.62C RilR-V-53B 31 8.14.121B C) CYGNA ATTACHMENT JOS NO. Ib"Y FILE NO. 01ot.F SHEETlio. f51 r t l .kJ i
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nbii CE P V- 3 A Calculation INPUT GLOBAL ACCELERATICNS I ? 13.89,1.66,1.04 Sheet i INPUT ANGLES OF NORTH VECTOR O(,/ ? 90,90,0 INPUT ANGLES OF VERTICAL VECTOR
? 90,0,90 Preparea syl g' Date INPUT ANGLES OF EAST VECTOR ' "
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! GLOBAL G-LEVELS = 13.89 1.66 1.04 56 tiot,-C. -l NORTH VECTOR ANGLES = 90 90 0 VERTICAL VECTOR ANGLES = 90 0 90 EAST VECTOR ANGLES =0 90 90 INPUT ANGLES OF WEIGHT VECTOR s % q c cu e c,< c/) tc 's ,
? 90,180,90 EA L TsusstE 77U:5 LOCAL G-LEVELS '73p , (97.uT@ T.5 -37 75.:5
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- v. OPERATING VALVE EAR SHEAR STRES 89.1/06'- '5 of-m7.S.5* no- 25 h;o3*Mh* L27 e'T5 f
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i obten= 4.86604E+9 j gic(1,j)= j=-6.33239E-6 2 To7 A L Du)D EAT. 7E99Ls STLSL a= -3.1968 I'4+I~ '?I
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cf.' L Hounted Equipr.icnt; Forucrding of 8ll 3 ' Information L W i . CYGNA-RICHLAND y;
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. April 29, 1983 '
y;%y.; .... UnuP-83-078 el'.'.
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!1r. L. T. !!arrold Assistant Director e *
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% .4 4 'a - 3000 George Washington Way ATTACHMENT:,
Richland, WashinrJton 99352 JOB NO. '
- mENO.
Mr. B. A. liolmbcrg Attention: l ., SHEET NO. *
References:
(a) WPBR-83-17, dated 3/16/03. Ok.MNC.) (b) WPBR-83-20, dated 4/12/83. ,, . l
. ' r .t s - (c) WPDR-83-29, dated 4/12/83. .
', 8.4 ^ ' ' (d) Telecopy, B. A. Holmberg to -. - 9 .. ' 7., l M F~ J. J. Veracrber, dated 4/4/83. d
+
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4 14 (= Gentlemen:
. ...N .
In response to the request of references (a), (b) , (c) AAY and (d) , this letter is feruarding refined valve accelerations. -
.M*-@. m4 The valve acceleration sheets for the five (5) CSP valves
- Og J' Valve '
./'i 46 1'33 represent . sheets the forsecond iteration the other fourof(4) the refinement task.. valves represent the?"first .-W ^ ' '
g+ "..'; iteration of the refinement task. Picase inform the Woodbury<.;; Office if efforts should be t-ade to reluce accolorations f ~ further. 1 1 .,' Very truly yours, l . l l Jh: .. . ORIG:NAL StGHED BY J. J.VERDERBER ! w - m -s - .
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- f BPM /es' John J. Verderber
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.y n../f,Att.
ife, - Project Engineering Manager 'i. s - QY CC: Mr. W. S. Chin - EPA - 1 v/1 D!!r.
- r. J.F.E.Duck Rhodes - WPPSS - 1 v/l
- WPPCC - I s./l .'!all L$ rop ':75
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ATTAC!! MENT Data forwarded with BRWP-83-078, dated April 29, 1983 Valve # Anchor Grottp Culc. No. CSP-V-1 125 8.14.129 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 RCIC-V-31 107 8.14.ll2A Ri!R-V-17B 31 - 8.14.121 Ri!R-V-53A 29 8.14.62C RIIR-V-53B 31 8.14.121B E CVGNA g ATTACHMENT JO3 NO,_ bu FILE n o,3 x o, p SHEETNO,3 C : e l l 1 l l
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