ML17277B222
| ML17277B222 | |
| Person / Time | |
|---|---|
| Site: | Columbia  |
| Issue date: | 11/04/1983 |
| From: | Fernandez L, Khanachet F, Michael Scott CYGNA ENERGY SERVICES |
| To: | |
| Shared Package | |
| ML17277B221 | List: |
| References | |
| 361104, NUDOCS 8312300159 | |
| Download: ML17277B222 (374) | |
Text
Final Qualification Ressort.
IIIIIIIIIIIIIIIIIIIIIIIIIIIIII PROJECT: Equipment Seismic and Hydrodynamic Requalification GOB NO: 82044 CALC NO: OS.OleF CLIENT: Washington Public Power Supply System QID NO= 361104 TITLE: Equipment Seismic and Hydrodynamic Requalification of 30" Cylinder Operated Butterfly Valves:
CSP-V-1 and 2 CEP-V-1A and 2A
/Iz, .'k, ((/d/SS PREPARED BY: M.A. Scott 6/15/83 DATE
/
REVIVED BY: 'L.C. Feznandez PC+utoc 6/15/83 DATE APPROVED BY: F. Khanachet 6/15/83 DATE
//S REVISION:
J 8322300159 8312i 1 l PDR ADOCK 05000397 I
QXDN 361104 REVISION STATUS LOG prepared Approved by by Cygna Rev. Reviewed Energy No. Date by Services Description 2/16/83 'R. Hsieh H. Abolhoda Original Issue J. Rakowski
~ C" '
L; F rnandez Scott evised to 6/15/8 incorporate ddition of shear Fernanae Pi'8'.
lates D.Searle eview/comparison 11/4/83 f final piping p grtR~O>4 ccelerations
1.0 REQUALIFICATION CERTIFICATION
Revision+2 1. 1 WASHINGTON PUBLIC POWER SUPPLY SYSTEM REQUALIFICATIONCERTIFICATE WNP-QID 361104 COMPONCNT NO) -V- -V-2 COMPONENT DCSCRIPTIONc 1I
'nder 0 crated Butterfl Valves MANUPACTURERc BIF A-206763 ECIUIPMCNT CLASSIPICATIONi g] ACTIVC Q PASSIVE 5KISMIC CIUALIPICATIONRCPORT RKPERKNCCs C na Energy Services, "Equipment Seismic and Hydrodynamic Requalifica-tion of 30" Cylinder Operated Butterfly Valves," File No. OS.Ol.F, QID No. 361104I Revision 1, June, 1983.
RE U RED ACTION: 1 Re lace A-307 Ear Bolts with A-325 bolts.
2 Addition of shear plates, see sheets 4.3.30 to4.3.48 for additional details.
THK ABOVE SEISMIC 01UALIPICATION RCPORT5 HAVC BEEN REEVAI VATED IN ACCORDANCE WITH THC CUR RCNT NRC SC15MIC CRITERIA'
~ ICCC STANOARD5 244 IISTS) This equipment is qualified as 2 U5NRC RKOULATORYOVIDC5 1%2m I ~ 100 a assembly when the air cylinders are completely qualified addressed So 5TANOARD RKVICW PLANS QAAy 5 IOv ~ in QID f018001.
4 NVRCQASSB THC ABOVE COMPONCNT HAS SCEN POUND ACCEPTABLE POR PCRPORMINO IT5.INTCNOCD 5APKTY RCLATCQ PVNCTION W HCN 5U Bl ECTED TO THC PLANT SPKCIPIC VIBRATORY LOAO5 PREPARED BY OATK REVIEWED BY J.E. Rakowski 4 rg a .Jn n4k~ 3 25 83 Il OATK APPROVED BY Mk I'rtntlfr ~//rb 7 DATE t4$ l2074
2.0 SQRT FORM(S) AND REFERENCES 1
Revision 1 2.1 WASHINGTON PUBLIC POWER SUPPLY SYSTEM J'M ~F
- a. a a. J ~ 1 k 3 IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Qualification Summary of Equipment QlDg 361104 Ref. No.
I~ PLANT NAME: TYPE I~ NSSS: 7 A/E: Bur 1s Sr Roe 5 Mark XI CSP-V-1 6 2 I I~ COMPONENT NAME: y V.COMPONENT NO CEP-V-1A 6 2A I SCOPE:
Q NSSS 7 MODEL NlHBER A-206763 QUA NT I TY:
VENDOR: BZF 4~ IR THE CQ4%NENT IS A CABINET OR PANELS NAME AND MODEL Npe OF THE DEVICES INCLUDEO'/'A PHYs IOAL DEscRIPTIpN + APPEASE Butter f1 Valve with 10" C 1 0 erat b DIMENsloNs: 30" Nom'nal 1208 Valve Assy;914 Operator & Bracket 6 LocATI0N: BU I Lo I NG: Reactor ELEYAT(DN: 508 'csP) and 588 'cEP) 7 FIELD MOUNTING COHO I T IONS:
[g 80LT <No. SIZE Q IIELD <LENGTH )
B g $ 'YsTEM IN IIHIcH LpcATED, Containment Supply Purge Systems (CSP )
Containment Exhaust Purge Systems CEP)
FUNc'TIpNAL DEscRIPTIpN; Prim'ar Containment isolation revention o f of the release of radioactive material to the environment.
c IS THE EQUIFMENT REQUIRED FOR:
Q HOT STANCBY COLD SHUTDOWN Q BOTH Q NEITHER PERTINENT REFERENcE pEs IGN SPEc IF IcATI pN. WPPSS Spec . 28 0 8-6 8 I I I~ 'S E UIFMENT AVAILABLE FOR INSPECTION IN THE PLANT: QX YES Q Np PAGE I OF 5
Revision 1 2.2 Qualification Summary of Equipment (Continued)
QIDI 361104 Ref. No.
IV EQUIPMENT QUALIFICATION METHOD:
TEST QX ANALYSIS Equipment Seismic and Q CNBINATION OF TEST-Hydrodynamic Requalifica 4 ANALYSIS QUALIFIcATIDN REPDRT:. tion of 30" C linder 0 crated Butterfl Valve*
(No, TITLE & DATE). File No. OS.Ol.F, June, 1983 COMPANY THAT PREPARED REPORT:
coMPANY THAT REYI EwED REPDRT, Washin ton Public Power Su 1 S stems
- Plus original valve analysis V VIBRATION INPUT:
- t. ,LOADS CONSIOEREO: a. Q SEISMIC ONLY c QX C&BINATON OF (a) AND (b) 4 2 ETHOD OF COIIBI I G RRS:
Q ABSOLUTE SN g] SRSS Q OTHER (SPECIFY)
- 3. REQUIRED REsPDNSE sPEOTRA (ATTAcH THE GRAPHs): Section 5.1 of ID 361104 4 DAI44ING CORRESPONDING TO RSS:
Q CGE
[g SSE 5 REQUIRED AccELERATIDN IN EAGH DIREGTIDN:
Q zPA
[jj] DTHER (sPEGIFY) Section 5. 5 CBE S/S ss F/8 V ss F/B ss V ss 6 WERE FATIGUE EFFECTS OR OTHER VIBRATION LOADS CONSIDEREDT YES Q NO IF YES, DESCRIBE LOADS CONSIDERED ANO HOW THEY. WERE TREATED IN OVERALL QUALIFICATION FROGRAM!
The calculated stress ran es were com ared to the AISC allowables, as the structures analyzed were not part of the pressure boundary.
iNOTE: IF MORE THAN ONE REPORT, CCMPLETE ITEMS IV THROUGH VI I FOR EACH REPORT PAGE 2 OF 5
2.3, Qualification Summary of Equipment (Continued)
QXDN 361104 Ref. No.
II IF CALIF<CATION EY TEAT llfEN COIFLETE; N/A IN@ SINGLE FREQUENCY Q MULTI-FREQUE~ Q RANDY 2N Q SINGLE AXIS MULTI-AXIS QS E ET 3N NO OF QUAL IF ICATION TESTS: CBE SSE OTHER (SPECIFY) 4N FREQUENCY RANGE:
5N NATIRAL FREQUENCIES IN EACH DIRECTION (SIDE/S IDEE FRONT/BACKF VERTICAL)
'/S
% F/B %
6~ METHOD OF DETERMINING NATlRAL FREQUENCIES:
Q LAB TEST IN SITU TEST Q ANALYSIS
Q YES (ATTACH TRS a RRS GRAPHS)
Q NO BN INPUT g-LEVEL TEST: CBE S/S r F/B %
SSE S/S r F/B r V r 9N LABCRATORY MOUNTI NG:
EOU'NO.. Q CI EIZE I NELC <LENETN )
Cl a- a - -"--
I I~ TEST REULTS INCI.UOING MODIFICATIONS MADE:
12N OTHER TEST PERFORM'EO (SUCH AS AGING OR FRAGILITY TEST, INCLUDING RESULTS):
NOTE: IF QUALIFICATION BY A CQIBINTATION OF TEST.AND ANALYSIS, ALSO COH LETE ITEM Vl I PAGE 3 OF 5
Revision 1 2.4 Qualification Summary of Equipment (Continued)
QIDC 361104 Ref. No.
I~ IF QUALIFICATION BY ANALYSIS, THEN C(MPLETE:
I~ METHOD OF ANALYSIS:
STATIC ANALYSIS a----
EQUI VALENT STATIC ANALYSIS DYNAMIC ANALYSIS RESPONSE SPECTRlH 2 NATtRAL FREQUENCIES IN EACH DIRECTION (SIDE/SIDE, FRONT/BACK, VERTICAL):
13':.0 Hz F/B 11.45 Hz )'100 Hz 3
4o MODEL TYPE:
COH UTER CODES:
o ---'- a--"----
FREQUENCY RANGE AND NO OF MODES CONSIDERED:
Q HAND CALCULATIONS t
OTHER 5 METHOD OF C(MB I NING DYNAMIC RESPONSES: ASSOOLTE RIFI Q SRSS Qg ISFEOIFTI 6o DAMP ING: OBE SSE BASIS FOR THE DAMPING USED: N A*
7 sUPPQRT coNsIDERATIQNs IN THE MQDEI i e-mounted B. CRITICAL STRIXYlRAL ELEMENTS: GOVERNING LOAD OR RESPONSE SE I SMI C TOTAL STRESS A I DENT IF I CAT ION LOCATION C(HB I HAT I ON STRESS STRESS ALL(NABLE Operator Drive Cylinchr on Fatigue Rod CSP-V-1 Stress 86 i 826 90 F 000 CSP-V-2 Range 57,526 90,000 ,,
Ear Weld Support Ear Fatigue Zc CSP-V-1 Stress 28 F 000 26 I 554 Range --=-
MAKIMAM ALLOWABLE B . MAX CRITICAL DEFLECTION TO ASSURE DEFLECTION LOCATION FUNCTIONAL OPERABILITY Q 0.01" Va1ve disk radial approx 1/8" radial deflection clearance NOZE: Calculations based on accelerati:ons-.for CSP-V-1 and 2 will provide an envelope for CEP-V-1A and 2A. See Table 1.1 of Section 4.3 for relative re(tuired accelerations for CSP and CEP valve operators.
I
- Computed stresses are based on "as-analyzed" g-levels, stresses due to the "as-built accelerations will differ slightly. See discussion Section 4.0 Appendix D1.
PAGE 4 OF 5
Revision 1 2.5 Qualification Summary of Equipment (Continued)
QIDN 361104 Vill. REFERENCES
- 1) BIF Drawings Drawing I Revg Description A-206763 F General Arrangement CEP-625-10 From Reactor Nozzle X-3 to SGT-FU-1A, 1B c CEP-.625-11.12 From Reactor Nozzle X-3 to SGT-FU-lA, 1B C-26095 Model A-83B Cylinder A-206767 Valve Assembly DOC-D-220-0310-IR-66 0 Tube errection iso-metric D-207110 F Valve Data Sheet M-144 General Arrangment lan mis level CSP-807-3 4 Containment purge air su 1 s stem 1
References continued on page 2.6 J
~) ~,.>, /~ IIjÃ4>>
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Completed By 2 C~'pM&c~f ,//~/
ppgb>'tW~, //r!, 5 /& 89 Page 5 of 5
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII WPPSS Mechanical Equipment Qualification 0.E. Rakowski 3/25/83 Subject Checked By: Date 30" Butterfl Valves J-.c. F +~ /zz System Job No. File No.
CSP and CEP OS.01/F Analysis No. Rev. No. Sheet No, 361] 04 2.6 Reference cont'n
-"- --- =
-2) Formulas for Natural Frequency and Yiode Shapes, Robert D. Blevins-Van Nostrand Reinhold Company 1979 Edition
')
BIF Report TR-27234 and TR-27235, "Dynamic Torque Calculation of Butterfly Valve; Sizes 24 and 30 inch",
dated November 10, 1982.
- 4) Report TR-74-8 by McPherson Assoc., Inc., "Design &
Seismic Analysis 30" Cylinder operated Butterfly Valve".
(Rev. 1) 12/31/75.
- 5) WPPSS letter to Cygna Energy Services, GE-02-RWH-018, 12/17/82.
- 6) WPPSS, WNP-2 SEM"Ec[uipment List Summary-Sheets dated 2/10/83.
- 7) Cygna Energy Services, Equipment Qualification Walkdown Verification Form dated 7/14/82 and 7/19/82.
- 8) Cygna Energy Services, "Project Manual Design Criteria,"
DC-l, Rev. 1, 10/82.
- 9) Burns & Roe Revised Piping Analysis Loads for CSP-V-1 and 2 (received'/13/83) and CEP-V-lA and 1B (dated ll/15/82).
- 10) Communications Report, R. Ricappito of BIF and J. Rakowski of CES, "BIF Valve Dimensions", 2/11/83 Cygna Energy Services, "Equipment Seismic and Hydrodynamic Requalification Calculation No. OS.01.F", QID No. 361104, Revision 1, May, 1983.
'l 005 00 sL=,~meveaermmmeesam~wrm~msm~~aate2meamwPmaervWaw-s 62ex~< ~ePdWSS; ~2k
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII cct WPPSS < WNP-2 Seismic/Hydrodynatttic p L.C.F rnandez Subtect Cnectied Eiy Date 9
5yster.. Job No File No 82044 OS. 01 Analysis No Re@ Nc Sheet Nc 361104
,SW .a~les I/xyP3 UPSET CONDIT I Ofl 6-LEVELS EPIC CSP- V -1 0.76 1.36 0.88 CSP- V-2 0.66 1.33 0.79 FAULTED CONDITI ON G-LEVELS (RWIIIRE~)*
'R'/
8 AND 10 INCH AIR CYLINDER OPERATORS HYDR Q' EPN LDS ELEV V E CSP-V -1 Y 508. 00 2.26 3.62 2.80 CSP- V -2 Y 508.00 1.44 3.54 1.90 CEP- V -14, Y 588.00 1.93 2.23 1.85 CEP V -2A, Y 588. 00 0 96 2. 11 1. 16
- These accelerations represent the "as-analyzed" condition. 2 The required g-levels are tabulated in Section 5.5.
See Section 4 Appendix Dl for discussion oi itltIJaci on stress levels.
3.0 TABLE OF CONTENTS
)J TABLE Or CONTENTS QIDN 361104 SECTION TITLE NO OF PAGES 1.0 Requalification Certificate 2.0 SQRT Forms 3.0 Table of Contents 4.0 Requalification Analysis 4.1 Conclusions
- 4.2 Summary of Results 4.3 Analysis Pg. 4.3.1 Introduction Pg. 4.3.8 Calculations Pg. 4.3.53, References 5.0 Appendices 5.1 Response Spectra 5.2 Walkdown Sheets 5.3 Valve Local Coordinate Systems 5.4 SRN Sheets 5.5 Revised Burns a Roe Piping Analysis Accelerations 6.0 Drawings Revision 1
ballltlllllllllllllllllllllllll TABLE OF CONTENTS QIDI 361104 CON'T SECTION TITLE NO OF PAGES 7.0 Transmittals, Prior Calculations
-and Reports 7 ' Communication Reports 7.2 Original Requalification and SQRT Forms 7.3 BIF Report
- 7.4 McPherson Associates Analysis *
"Note: Excerpts from report included in specified section. For complete report see Cygna
,Energy Services File No. OS.01.F, QID 361104, "Equipment Seismic and Hydrodynamic Requalification of 30" Cylinder Operated Butterfly Valves," Revision 1, June, 1983'.
Revision 1
4.0 CALCULATIONS
'YGNA,.PgQUALZPICATION ANALYSIS
0 4f+0!
Calculation
-=- j~ f'i 't fz Cover jIIIIIIIIIIIIIIIIIIIIIIIjjjjjj Sheet Job No.
Equipment, Seismic and Hydrodynamic 82044 Requalification File No. 0S 01 F Client 'Cate. Set No.
1 Washington Public Power Supply System No. of Sheets 84 Subject BIF 30" Cylinder Operated Butterfly Valves, QIDN 361104 EPNS: CSP-V-1, 2 CEP-V-1A, 2A Statement of Problem Seismic and Hydrodynamic Requalification of CSP-V-l, CSP-V-2, CEP-V-1A, CEP-V-2A to Burns and Roe Piping Analysis Loads.
Sources of Oata See References pages 4.3.53 and 54.
Sources of Formulae 8 References
'ee II References pages 4.3.53 and 54.
The equipment requalification was performed based on calculations using Revised Burns and Roe Piping Analysis Accelerations, April, 1983. (See Section 5.5)
"As analyzed" loads are summarized in table form Sheet 2.7 For discussion of the effects of this discrepency refer to Sheet Appdx.
Dl Orlginators Checkers Distribution Revision No.
2 Supersedes Calculation Set No.
JE Bakowski LC Fernandez Supply System-2 Revision I 4 - fs=~
H. Abolhoda MA Scott Project File-1 Approved By: 0 t:
R. Hsieh DE Searle
(;~ (~
ll 1005.00
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Prolect Prepared By: Date Subject Checked By Date System Job No, File No.
Analysis No. Rev, No. Sheet No.
CONTENTS Calculation Cover Sheet.
4.1 Conclusions 4.2 Summary of Results 4.3 Analysis 4.3.1 Introduction 4.3.2 Calculations 4 4 References
'I 006 00 h t t t W, ~ \ )~
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII project Prepared By: Date
. Subject Checked By: Date System Job No. File No.
Analysis No, Rev, No. Sheet No, SECTION
4.1 CONCLUSION
S
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII WPPSS Mechanical Equipment Retpmlification. "'.C. Fexnand 6/13/83 Subject Checked 8y: Date 30 II ated Butterf1 Valves M.A. Scott 6/13/83 System Job No. File No.
CAC ij CEP 82044 OS. 01.F Rev. No. Sheet No.
4.1 Conclusions Four 30" BZF 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-l, CSP-V-2, CEP-V-1A and CEP-V-2A qualify with the following modifications:
- 1. Manufacturer supplied A-307 bolts must be replaced with A-325 bolts.
.2. Shear plates must be added to reduce the- ear weld stress (see sheets 4.3.30 through 4-3-48 ).
Valve operability was also demonstrated (see p. 4.3.20) while cylinder operability is addressed in QZD No. 018001.
I cee,00
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII pro'ject Prepared By: Date Subject Checked By: Date
$ ystem Job No. File No.
Analysis No. Rev, No, Sheet No.
SECTION 4.2
SUMMARY
OF RESULTS
f Calculation
~'aMVl4 CR a
5 tPi4 Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII
" WPPSS Mechanical Equipment. J.E. Rakpwski 3/25/83 Subject 30" Butterfly Valves Checked By: ""c za/~
System File No.
CSP 6 CEP 82044 OS.01.F Analysis No. Rev. No. Sheet No.
361104 1 4.2.1
~
SUMMARY
OF RESULTS Parametric data for the four subject'alves in this report is given in Table 1.1. Results of the requalification analyses, which include a comparison of calculated stresses to the allowables are given in Table 1.2. Allowable stresses for the various material types are given in Table 1.3.
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hS IASTAt I eo JOLTS AIIg COPP&<TI-cl'-3o7 REQvlPE. <HAP CDIRT To A 325 CIl Ch FA1I6uE EVAI uqTIOM OF A SIIEgg LOTTO PCSOI VES IdrO IDI TENSILE, SrLeSS RIII4CK AS Vl Vl CO CO FOLLOWC ', Qh,~ = 2 ZOAX 5'R = 2 ~+ax 4J 4J OIIPIIT c=4bh/ ri-IC T4( C-C~CI" CI<<
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Calculation jI Z
B a 4 s: i~ Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: .Date WPPSS Mechanical E ui ment Qualificatz.on J.E. Rakowski
" "'bP" butterfly Valves Checked
',C. F~
By: Oate Sl~ l~s System CSP and CEP 82044 OS.01/F Aoatyata No 361104 Rev. No Sheet No.
~
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+( c/r4/w b/is'imp THIS SHEZZ NOT USED 1005.00
Calculation T,
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'a L j Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII WPPSS EQ J.E..Rakowski 3/25/83 Subject checked By:
L 0 j t Date System Job No.
82044 OS'. 01/F Analysis No. Rev. No. Sheet No.
36110 4. ~ ~
SUMMARY
TABLE 1.3 ALLOWABLESTRESSES Since operability is required, the stresses'or the faulted condition will be kept below yield+. The table below is based on AISC criteria and the yield stresses at, temperature (340'F) from PG. 9 of REF. 4 for conservatism.
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SECTION 4'.3 ANALYSIS
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII NPPSS Mechanical Equipmt Requalification '.C. Feznande 6/13/83 Subject 30" linder ated Butter fl Valves Checked By:
M.A. Scott File No.
Date 6/13/83 System Job No.
82044 OS.01.F Rev. No. Sheet No.
QID 361104 EQUIPMENT REQUALIFICATION FOR QID NO. 361104 BIF 30uCYLXNDER 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'he highest- stress range.
The analysis method calculates stress from north, vertical and east components of operator response g-levels. These g-levels are the result of the Burns 6 Roe piping analyses.
(Ref . 9)
An SRSS analysis was set up in a computer program for each value assembly in its specific orientation.. The SRSS is taken at the maximum stress level due to seismic g-loading.
Operating loads due to seating torque force and dead weight are combined with the seismic stress by absolute sum. Valve ear bending stress components due to any one response g-level component are combined by absolute sum.
1000.00
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII
'@AS Mechanical Equipment QualificationPrepared Sy.'ate J.E.Rakowski o
1/10/83 Subject Checked Sy f' 90u Butterfl Valves L C 0/2 /
System Job No. File o.
CSP & CEP 82044 . OS.01 F Re.No. Sheet No.
4 3 "N'TPII4 i 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 QTD 361104'(30" valves/10" operators). Hand calculations which check selected por-tions of computer output is shown in Appendix C.
Appendix B of this section describes the air operator mass/stiffness model which was incorporated in the final piping analysis for calculation of operator re-sponse g-levels. The computer program includes an op-tion for using the valve ear forces and moments which are directly output from the piping 'analysis with the valve/operator model included. This was not finally however, to qualify the subject equipment. 'tilized, The equipment locations and elevations were taken from the P&ID's in s'ection 6.0. Natural frequency calcu-lations are given for the air operator assemblies in Section 4. 3.',2;1-.
Preliminary analyses were performed which showed that, for operator response g-levels greater than ap-proximately 3 g's, the air cylinder 'spring preload force would be exceeded and hence some disk flutter would occur when the valve is in the open position.
The calculation in section,4.3.2.2 shows that the mag-nitude of the valve disk flutter vibration angle due to- upper bound g-levels which occur in the hydro-dynamic frequency range is approximately 6 degrees.
This flutter was 'evaluated to have no detrimental effect'n system safety function as noted in Reference 5.
Valve operability was addressed in the following manner.
All valves have a Use Code of 1-3. It is noted that the g-levels pertaining to CSP-V-1 envelope CEP-V-1A and CEP-V-2A.
Calculation r~a'/c 't 2 a Sheet
~ 8 B. a c IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Date Proiect WPPSS Mechanical E ui ment ualification Prepared By; J.E.Rakowski 1 10 Date
'utterf Subject Checked By; Job No, L ~
~
File tstj.
System Cf.'N4'ev. No Sheet No, 4 3 3
'SJ33 LE For valves CSP-V-3. and 2, which must operate from open to fail closed during an event, the following additional evaluations were made:
'I
- 1) Dynamic flow torques were assessed pei Ref. 3 and found to be less than the seating torque which controlled the equipment stresses.
Furthermore these flow torques tend to move .
the valve disk toward the fail-closed position, as noted in the above report.
- 2) The details of BIF drawing 206 767> parts of which are shown in figures .1.1 and 1.2., allow the following conclusions to be made for valve operability:
A) Figure 1.1 shows that thrust bearings are part of the shaft bearing design. This design prevents lateral movement of the disk in the direction of the shaft to eli-minate interference with the valve body when closing. Further, it is noted on Page 26 of Ref. 3 that frictional~'torques in the shaft bearing system are=" igible.
B) Figures 1.1 and 1" cross section hav,
'~ g 4 ,alve within which the valve se Qsi-tion. The only me . > af-fect valve closing ~
ated is out-of-round di. t.on due to DBE piping ~ds on the valve.
These loads were accounted 1
(~
for in Ref. 4 in the overall valve sizing calculations, where analysis showed that the stress intensity in the 0.5 inch thick valve .body remained below 1.2 Sm, or approximately 0.8 of yield.
Stress contribution from dynamic loads on the valve and operator were relatively small. Further, as shown in the figures:
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'L C. F~~ "'/gg g.3 System Job No. File Na.
CSP and CEP 82044 OS.01 F Analysis No. Rev. No. Sheet No.
361104 4 3 The valve seat forms a heavily reinforced section made up of the valve body, internal hub and external flanges (including the mating flange of the piping). Hence the stress levels in this section are much lower than in the valve body and hence no distortion of the section could occur to affect seating of the valve. Valve flange dimensions are given below. Note the relatively large internal radial clearance of 1/8 inch.
- 2. Stress analysis of the valve extended structures are given in this report. Air operator operability is addressed in QID 018001.
The design data used in the analyses are given in Summary Table 1.1 (pipe-orientations and elevations are taken from the appropriate PAID's in Section 6.0).
Other pertinant data is given below.
- 1) Spring preload per communication report in Section 7.0 of QID 018001 are:
Fail Closed Preload = 2800 Final = 4800
- 2) Cylinder C.G.'s shown on the following sketches represent mta 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, ll/83 communication report Section 7)
Flange: width = 3.88",.thickness 2.625" Radial Clearance Disk/Seat 1/8"
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CSP and CEP OS.01/F Analysis No. Rev. No. Sheet No 361104 OPCWDS tTI08 10.5 5.3 b lb.ZG-cLosED F'osjTIOiY I Ocs.00
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Calculation t4- a':=t== mare's Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: H. AbOlhcda Date WPPSS Mechanicla Eaui ment uglification J.E. Rakowski 3/25/83 Subject Checked By: Date 30" Butterfly Valves L.C.F~m~ 0 ~< r5 System Job No. File o.
CSP and CEP 82044 OS.01/F Analysis No. Rev. No. Sheet No.
4 361104 4,3,5 CAL CUI ATION K
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared BQ. Abolhoda oete WPPSS Mechanical E ui ment ualification J.E. Rakowski .
3/25/83..
'0" Butterfly Valves ESP and CEP '82044 'OS.01/F Rev. No. Sheet No.
361104 4 3 9 I
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Subject 30" Butterfl Valves Checked By:
I..C. F~~~ ~ Date 9 6/D System Job No. FiteN .
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: Date WPPSS Mechanical E ui ment Qualification J.E. Rakowski Subject 30" Butterfl Valves System Job No. File No.
CSP and CEP Analysis No, Rev. No. Sheet No., 4 361104 (
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII QNSS Mechanical Equipment Qualification "'.E. Rakowski 1/10/83 Sub'ecI
.30'utterfl Valves Job No.
',0 F~.~
File No.
0/~r/rl System CSP and CEP 82044 O'-S. Ol F Analysis No. Rev. No Sheet No.
36110 4 l 4 3 ]
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4.3.2.3 STRESS ANALYSIS The procedures for the analysis of the subject valves are outlined below:
Recalculate the valve appurtenance stresses addressed in Ref. 4 using response g-levels from the Burns a Roe piping analysis. Incorporate the current seating torque given in Ref. 3.
Compare stresses to the lower yield strengths in Summary Table 1.3.
2.
~
If faulted condition stresses exceed the upset condition allowable stresses, repeat the analy-sis for the affected components using upset accelerations from the piping analysis.
- 3. Perform a fatigue analysis on significantly stressed components. Determine allowable alternating stress ranges from AISC 8th Edition, Appendix B, noting commentary.
The fatigue analysis is to be performed only for those EPN's subject to hydrodynamic loads. The number of respective load cycles is given below.
LOAD COMBINATIONS 5, STRESS CYCLES The following table lists the load combinations and
,the nubmer of expected stress cycles for each com-bination. (From tice design criteria)
Combination ~cclee
- 1. SRV Alone 3 (4500) =13500
- 2. OBE+S RV 50
- 3. OBE+SRV+Chugging 2000
- 4. SSE+SRV+Chugging/
SSE+AP- 10 Notes Load combination I4 with 15560 cycles can be used to conservatively bound all combinations.
Calculation L:
! ~= Ja ra: Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project WPPSS Mechanical E ui ment al'repared By: Date 3 25 83 Subject Checked By: r Date 30" Butte f Job No.
t-.o. F File N 0/z.
System CSP and CEP Analysis No.
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WPPSS Mechanical E ui ment Qualification J.E. R 3/25/83 Subject 30" Butterfl Valves
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Prepared By: Date Project WPPSS Mechanical Equipment Qualificatz.on J.E. Rakowski. 3/25/83 Subject 30" Butterfly Valves L.(. I~~f File No.
r./fr/I3 System Job No, CSP and CEP 82044 Analysis No. Re No Sheet No.
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Calculation
'i. ra=- Ji Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Date Project WPPSS Mechanical E ui~ment ualificationPrepared By J.E. Rakowski 1 10 83 Subject 3.0" Bu V lv System Job No. File No.
Rev. No. Sheet No
'5LVT84 i 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.
Ta er 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 Tab'1e 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.
Calculation arai Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: gate Mechanical .Equipment Qualification J.E. Rakowskz 1/10/83 Subject 30'utterfl Valves System Job No. File No P 82044 OS.Ol F Rev. No. Sheet No.
4
~
Method II: Use the north, east and vertical operator accelerations output from the piping analysis. Absolute sum for stresses wj.th each component then SRSS over re-sults for N,E and V.
Note): Analysis of the distrib'ution of stress on 4 valve ears to predict the maximum tensile stress cannot confirm a maximum value lower than the absolute sum of the elemental ten-sil stresses due to the six forces (from one acceleration direction, N,E or V). There-fore the absolute sum will be used at this level.
Note 2: Add stress due to the vector sum of deadweight plus seating torque force after above SRSS combinations are performed. (ABS)
Note 3: 10" A/0 parameters are. shown for use in QID 361104.
Anal sis of Seatin Tor ue Forces
A
- 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:
l g, LaCrLI MIS an clewsfva.Ivy shaA L.'tackMArQlvE
'.! cdxs setsmtc/gunpfyt jc.
th a.- cLk'/5 dll&SDhf F~ <ram c>per~r 1006 00
Calculation B 3 a Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Pro'ect . Prepared By: Date GPSS Mechanical E ui ment uglification
~
J.E. Rakowski 1/10/83 Checked By: r Date Suoject r'utt rfl Valves F File No.
.c, 9 /~f/~~
System Job No.
0$
Rev. No.
")57Ã4 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.
force will oppose operator weight when the brackets hangs downward from horizontal pipes.
0 erator Drive Rod Drive rod dyanmic stress is due only to g because g and g forces are taken out by trunnioA pins.
Aid seating torque stresses. 7.I25' F~ Lca, LP D TvUo FDtd tS AR.E cerrtr" qt. PT A I
TH < BvsHtv& h ys f'w B Aw Tq a Fgp~
REPUCF-lO t qZEPy PIP>ZZ~ WAc MA = F (.Lp p ls.s )
QA l-"A
~ +~Q IN o%7S lIJ
",l. (zS Fc, I3$ 3tH 5~
+qy gP = HgCI l.Posit'-
g Ql Z.41 IH Z. H <p4
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared 8y: Date WPPSS Mechanical E ui ment at J.E. Rakowski 3/25/83 Subject 30" Butterfl Valves System Job No. Fife o.
C P Analysis No, Rev, No. Sheet No.
361104 4 3 23 f(VA<LV:
I I
RPD AS hBS Ki(A APER- CtLS5
(-,
P V Qh(P(<< ~~togMTS SHIA(C t)')fQ A Wtt Fo(r'.('-FS 6'( UhLVE t-(((RS A 5A t'-<V f'E ~So /5a((-F>ESS PlOC@L (OAT PEFha.EE FOR, THE P(PIP)6 MopEL TO ChallLATE% RESPadSE C-LFV~ (SEE A TT.PIC'HIII EAJT ) THE SALVE- EP-R. Sys~SPn ~Wu0 h>u
'TOPS(oHAL fLSW ~(f',(t (7 9 M P IH CLUPED IA 7(kt:. fuOOGL AH 9 SfCSS FOR t'-E5 0 ~P Pbh'h BN'75 ~It-L /ttL SO BE.
OLtw Pgy FoP. Coutj&k&IO0 INTO tIALV(= EAk g>t ESMS, 7th E EquAafogg
'TS'WSIow d~e. 'ls HI, f'T~','%BE tccfc cccfcfs DEFjIP. ffaIc> Fr ) MZ 2PQ( =~t' est
~A to If
- S
(~ "prrpu c4arfa fA $g kZ $.5 rS)
+ WHE,(r T$ =+ IOS QP- F.T ys,= V z&~(4 sAP- MOQPL,:
(so~ A~VW<m)
TIDIIP'TENSIOII t+) wIfEN MI IS + fPIPPEPIDIrg) sT(tIttTttEA( As(A4 'trs(5 PMGkr(tf, -&6 it( ( ('chl0((t (I FoK 5 00 tl foAft L DE f fj PLZ.
n y ~
Calculation
/~la.f
~ S sE S 4 a~a Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII project Prepared By: Date WPPSS Mechanical Equi ment Qualification J.E. Rakowski 3/25/83 Subject Checked By: ~ Date 30" Butterfly Valves L ~ F y~+t~~
System Job No. File N CSP and CEP 82044 Analysis No. Rev. No, Sheet No.
4 3 24 361104 ~
cooRDINATE SYSTEM ( LOCAL)
I I~ !3 l~ II ay
>L t
0 1006 00
Calculation 4 al J e=t BB Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: Date WPPSS Mechanical E ui ment J.E. Rakowski 3/25/83 Subject Checked By: y Date 30" Butterfl Valves ~ ~ ~/ /e System Job No. Fite No.
Rev. No, Sheet No.
4 3 25 361104 l PoL TS Ht iViOS. 5L'ACUTE.Y5 ao EAWs:
$ 0t.T @Eh)VIOL/ IS PUE- Mt)
AEBA foLZ 5H&hg, 15 PU E.
) S7 ) V3 0
~
Qg. q p 0.3I ZM .+QIhl 4 Ap +
D T~Qc~
(Ass soM) qy)~, = tAi z +ALt, Fc yk AE(pahkyrdgs Facs5 g 3 the)..
p.. + hF-y F <cArh~c AG Coi JIVE. i)J SATE Ag Ag XAvpaa, 4> bP
~QduS PAC E S ~i~<) 3o R. Eaas 80T
'I hg Su8S~ITL TE A~P Fox 4W2 fs~-
4- Ag
'k 000 es
n ~ \
Calculation.
oa Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project WPPSS Mechanical E ui me t uglificationPrepared By:
J.E. Rakowski
'""""'" L.c. F~~~w."" <(Isl>>
Date 3/25/83, Subject 30" Butterfl Valves System Job No. File No.
CSP and CEP OS.O Analysis No. Rev. No. l,4 3 26 361104 l y F THo P ~ , TH E PJZBVI dU S'glf kT(ol 5 M 9 S~s>
MQ 'THo D Q blZ & ~LIC+gLE. HoM2& ~G Rg t') gXf'RESS ION S Fo 2 ~6'E St~ t=ol~&/P~~~P~S QtrE DERN Ep SELo~ lH tERlos op cj- lewa >
mM t2oNt"=Mls ~
>NNIVAL.Q-T E. Lc. C gt g~t> 5 y>VB.~
( 5QQ 5E Qlj&P'T t g QLEl:t(Ctrl CO S)JOL Q it'll~ t36, Tcs EAL'TIDP I/&o toR'5 l co T8 E p> E ft >
V peoG,L-IH tuRL/ l lN Loe4L p>tag).
QPc~ro U.g.g P t AE SE gqQA Tto P5 ALE Td 'L- QQ&D TO glivb THE FoEws As ov wa. gPRs hUE go DER.P lOHBH t A.HP 5FA tiNg ~QQQE Rt R-W 5 I FOR I ME USE Vcr R, lloaltH &R HIE Cft.CU~~ro iv OC OphPP TrH6 tHGD l j 2
~~/
QE E Fog cd f gEhc~(E.T c LlEhl z4 Ttog I H Lt,"+ t C'e oliIbIH Ale S> Na<> ppgE.
l 3 70RSl>rtr ttlPpoD T L.ogAL Awt5 g 3 P3 ZNlooO~t Q+' E R, 83 t FSR, e+ Filo L eL o FSR+e,
=.FtRle3 + HliR), Eq l'Oo]R<Z >WSR/Ze, lp Ft -~ + ='N>>~I ~8~ WAo~k F ~~ t- 4 Npg)CgqlVgpZ6]
Calculation J Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: Date WPPSS Mechanical Equipment Qualif ication J.E. Rakowski 3/25/83 Subject 30" Butterfl Valves System Job No File No. o CSP and CEP Analysis No. Re~ No Shee~No. 4 3 27 361104 )
FO ItC E, S OQ pppOVT ARS DU $ 'To LOCAL - AItlo /AC EWRATIO I"5 tr'&5 IIJ HE McAL Coo IM A tF T \
H I-I =
5:25'EYS Foat:e.s Ace lv TH-a LOCAt II2> 5 A/0 A.AS S VS~ 0 ~B FAo2,p = 4'lo W6 v~=28.S W pT'p ~ . I -h mt'otut pougpT waR(
A PYUAPt~ fagcf AT ~gNIOQ W
liter Fmi FSp I,Zp- I,ZpactS C'0+1'evt=eTS Or-5LAcK,F T I 9 EE-Tt A = 4~+ t~z + f Fee pe,z Fo~ AT 'TWPyto> IIJ 2, 5
VlA/p]3 AXIS ~ l o A/o uJEI@<I T UOE IGHT 0 F A/o I 0 6'xpQ )I 2 FsTa
+fir. IqZ)R ~ LU~bHT OF ~C<h 7 THE C 1,2(3-AXiS Pjtr'-ECTIOHQ F~ 2 = SEbXt iu 6 <~QL Fog.C.f ) I5 ALuAVS At.ops ?-- gWtS-Q+ LtQ, [
Itt03 ~ Ao>
- t. gl5 r'g
'l 006 00
(41 I'r . he. H > e Ah ',4 1 4ki ))4e Ee a ~ ". sc ~ ~ a w ~:c . *s v ~ v , >*su, ~
Calculation L 'v r s F I z Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project . Prepared By: Date WPPSS Mechanical E ui ~
ment Qualification J.E. Rakowski 3/25/83, Subject Checked By: . Date 30" Butterfl Valves I F System Job No. File No.
CSP and CEP Analysis No 3 ll Rev. No. Sheet No.
4 3 28 FOt;CQ OZ-LED Th <<OPS OAI ~~9 ". IF +'P F
(AN D)
Fct SI= "rr.i I. Fsn, = F~~i i >sufi
+
~IFIXEL
= ~a~> <~<x4 I-RDV P FORCE BPLji y C,F 4
Oe t HE. Oi~ERA-TO@ '.
FTr) = (L~o t4>)<wA,s o (+ Fo<cs sg spry) 0'p Fct.Evr S
~
<l~<- a C
~Lp ><<~~) W~~
LBHCTII L~e ~R I leg
~WA +)
oPEN
'S cL5 Sf'o ZS I0.94 ltI.9& Z I.5
Calculation L Sheet
~"=~~K,Ps'IIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By:
WPPSS Mechanical E ui ment Qualification . J.E 3/25/83 Subject 30" Butterfl Valves System Job No. File No, CSP and CEP 8204 Analysis No, Rev. No, Sheet No. 4 3 29 361104 5g = Fpoz + FsRE = Lwh~ yNBr
+gP p. 4~nctX + <STZ 0UT Ot- AQL
~cDct FgoZ <5'ORD ~ts t x, "4'3+3 '%F3+4 (i-.~-, ~ ws~)g~ e~ wp,)~/de ws.s )peg 4= T~P Mjp~
t" iA<<ay =(~A~a" sp>+~ss~)ea ~A>>( > ItJ TENDON 8F3 +
Mt =
~%
=
w~e( ~ <Fsri<s-r~n ez %ra~'
t (F~, <~s<>,)esgir~.e,~iw~ )~s.
4 =LEFT BES
~zFi<e> = <t wetl~ussi~es- eaose2 wst e, Itt
~eau'Tp
=
+g = (Wpg wW~)P~
q~tS 4> M g khan, 5>,Szgg 6 ~>r~F 10ss OC
h jul 'J 'P '1 1*I%ill c a,-4 I~ e I I Feel% t%% ~ f 'I,P ' 4 il
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII WPPSS ~hanical Equipment Reification . '.A. Scott ~ 6/15/83 By:~g+
Subject
, 30" linder ated Butter fl Valves Checked L.C. Fernandez Date 6/15/83 System Job No. File No, 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., Q stress range. The allowable fatigue stress range from AISC for fillet welds in shear with less than 20000 cycles of loading is:
SR = (1.5)(15000)=22500 PSI This includes the 50% increase due to fewer than 20000 cycles. The weld stresses are calculated using faulted loads. These loads than one percent of the total 15560 cycles of faulted/hydrodynamic produce'ess loading. Since the upset and emergency conditions are considerably lower in magnitude, small margins of overstress in fatigue will be tolerated for faulted stress levels. The following allowables will be adhered to in the ear weld stress calculations.
Allowable stress for welds for faulted conditions:
ll 1. 6 (0. 3) Fu = 28800 PSX Allowable stress for welds subject to fatigue. This is 4 the allowable stress range of, AISC Appendix B:
=1.25 (1.5) (15) = 14 KSX a owfat 2 1.25 = 25% increase due to previous comments
-1.5 = 50% increase due to AISC commentary 1000.00
Calculation
~ .a== 3Lfs) Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII NPPSS Mechanical t ification Prepared By:
M.A. Scott Date 6/15/83 Subject 30" linder ated Butter fl Valves Checked By: ~
L.C. Fernandez
~p Date 6 15 83 System Job No. File No.
CSP and CEP 82044 OS. 01.F Aeelys~ Rev. No. Sheet No.
QID 361104 4.3.31 (A s(c-r olR. &%< I'l)
Et/~xgx log ~O PtT WOl SR WAKI40 tCAI ~~ o~+o,-y~"
hJoTcH Ro~& c()ggGRS m CWAia- KX iav.iaaf, co
(
l t fl~ k4 tH ~+IlZeAW mx)v. cH~ ~~
Wg$ 'tCAt
+pic Mtg wHeocY CCS'"
A~ Id~ blent E7OI8 Ream~ e ZOO l= M rQ Wo 8t ~A FaM i UWM WAx all-I ET ~m~tOQ // Cr tJ / ~~I= IM~
~~ ~~ i ~ELM 8~K ZL Ale-&z2.'7.
0 d l 'III Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project WPPSS Mechanical ification Prepared By:
Checked By:
M.A. Scott ate 6 15 83 Subject Oate 30" Butterfl Valves-System Job No. File No.
'mHysis~. Rev. No. Sheet No.
361104 4.3.32 T 5s S
AP~lGlo Lo~~ K ~w oF ~t3T~tt' E'~c Q w~Vc o R- l 3'9Q I o Zz4'zC Vzwo I<Wzd [>z.~z0 l~g (~
CcshA5 l g~ ~94 &D'70 3Z70 l 7OyZZ. I +Z52'9 j 7~+3S I
.A
/4 zz'(i4 is) -z-a.>z.
f~.+
= rzv4+ 4!BG
Calculation Lm =="J '. F.t> Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII
' Prepared By: ate WPPSS Mechanical ication M.A. Scott 6 15 83 Subject 30" linder rated t. f V Checked By: ~ Date Job No. File No.
CSP and CEP 82044 OS. 01.F Rev. No. Sheet No.
~
4.3.33
0 I'. ~
" i~
Calculation a~ 3kfk Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII project Prepared By:
NPPSS Mechanical Ectuipnent Requalification M.A. Scott 6/15/83 pQ- Date Subject 30" linder ted Butter fl Valves Checked By:
L.C. Fexnandez 6 1 System Job No. File No.
CSP and CEP Rev. No. Sheet No, QID 361104 I ~ ~
ammo'moJt dS
////. FM M /yQ 6
%vs~/.s)
~~csW ~~ PmZ.m C- ~m ~~~~T ap t c, nJ
~r ~~a ~ad~ ~Z
~ ~~ caw~i mQ~o-W
> t=
c) f-/ ~t> uJtu
~m ~ C~~ac ~eN
~tc C O~c W D5,~ ~PS /Mni throe/~
~~F c~ r7~ ~cC c ~W W~c&L ~~M A~~~~~ +3~/./5)z = 9.5 +~
= s I.YS ~ .
I~6
Calculation L.~~f 3h.fs) Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII WPPSS Mechanical Byxipnent Regualification M.A. Scott 6/15/83 Subject Checked By: C~ate 30" Cylinder Operated Butterfly Valves L.C. Fernandez 6 15 83 System Job No. File No.
CSP and CEP 82044
~aiahh. Rev. No. Sheet No.
4 3 35 QID 361104
~HE ~W M~~c= 5 O~
/-/. ~a ] m ~o ~ ~~ a~a.~A.P VoM~7-. Q I
/Nil = /7d92-2 + <(eW54)(6) =a Assr g~-cs V, =
z(w~) - /oyoa ~a I eke ~~LB( ~Aw CJ~ '~AM
1 J 'l "- 1 r V E,w.; 4 g'it,%A t>1% ', .a taoaV' K[PP AO II& J e 4 \ ' v ) 3, ~ P elf sa, x r la..l ~ s 'JIC wl C 4 ~ 8 ')lt:e ), I,
Calculation
~j ~J k r'=t't 7
g I'
a p, Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: ate
. WPPSS Mechanical 'ication M.A. ScotM~ 6 15 83 Subject Checked By: t.+Date 30" linder ated Butte Job No. File No.
CSP and CEP 82044 QS.Ol.F Rev. No. Sheet No.
QQ8 361104 ~ ~
/ pJ gee'i ~r Jc ~~
ms- m~~rD~
~ized Ww~ad5'P'~ms~~>
~~~~am mr~~
ts nJ8rr /deca .IU coMwAess~
~~gc 77M'.. 8 ~pl~ ow c5~~g~4 C F'~
/@~i
~~ yA
~M~t wrk~t ~~8 "~~rM Co~&~/5o~
I 33 Q/Bc9 WJ .do&36 r(sd E')P~s' Mo~idc ~~ Igi M ~~ ~/Ar ~~s
~~B~ ~er'.=
-(.)(r') -7'7e-(-) I~>>. =
Z dH8 W.dj; dOOS'ed A E< g+,3<6 (/z~ )
t 7.88 ~ M~= W~~~s
~~ /cQ ~e.QlOr r T7M~~
~ p=t"- A-w. Jg
Calculation Jk jk Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII
"'"'ppSS Subject ical ~~t B~lification "'.A. Scott Checked By: Date 6/15/83 30" Cylinder Operated Butterfly Valves L.C. F z 6/15/83 System Job No. File No.
CSP and CEP 82044 OS.01.F RRBPjMA%t=. Rev. No. Sheet No.
m 361104 ~ ~
g(38
.v4 ~ >>e(~) c +@ I hg I
Calculation a r=t Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII
PPSS Mechanical Equipnent Requalification, "'.A. Scott~ 6/15/83 30" Cylinder Operated Butterfly Valves Checked By: ~~
L.C. Fernando Date 6/15/83 Job No. File No.
CSP and CEP 82044 OS.Ol. F Rev. No. Sheet No..-
~ ~
lf pg~p3~~> @At Eo ~~~K ~'~Jr A,>
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII
.project ' Prepared By: ate WPPSS 5Lchanical lification M.A. Scot 1 Subject Checked By: ate II System Job No. File No.
Rev. No. Sheet No, ID 361104 4.3.39 g~= SPI, i= S 58 (> <) z.rS rggt5,~ ~~
z.N z (y,q<y)
Q= -pg ~Q~ (=gz)(fisc,j(z o).~ /Bc/ls W~ ~t At c
~
~~
oe.'>A ~ A44 t &,gi l4\4%t"4%) t 6 ~ e 1 es*jy ~ ep ~ t C % ~ ~ Wl,f Q ~,
Calculation Sheet .
IIIIIIIIIIIIIIIIIIIIIIIIIIIIII
'.A. Scott / ~
WPPSS Mechanical Equipnent E~ualification 6/15/83 Subject Checked By: Date 30" Cylinder Operated Butter f1 Valves L.C. F ez 6/15/83 System Job No. File No.
CSP and CEP 82044 OS.01.F Cma~ Rev. No. Sheet No.
4 3 40 ID 361104 pt t~
~~Mac
~<@arnot-~ ~~~
~+As.
I Ha ~~~ co.~~ zM~ '
awzo eH ZV 5%LE5/j J
'E&ocrf W4 Lcj~
Calculation.
- h. ia s rat Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII rotect WPPSS Hpc~nical Eqgj.~t. Pgqua+. fiction " '" " IvI.g. Scag~ 6/15/83 Checked By: Date 30" Cylinder Operated Butterfly Valves L.C. Fern-tndez 6/15/83 System Job No. File No.
CSP and CEP 82044 OS.01.F Rev. No. Sheet No.
QID 361104 ~ ~
W Mm 6 wW CoWAC.
~$
I
~
MQE5b oY EXP'4 ~A~S I>
t 35~~t~ ~607 ~H~ /- / Mcs
-:9, = 5'~ ~ )-'5' l+; Ir za.s
'e+4 t8 zok 4/v
/G4 (p P t ovJC ~4Z ZQ hg~
t.1 p,
P! ' I 0 I. 1 ~ I ~ y X
Calculation I ~
L.M ~~3k fk't
%mr a "Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII WPPSS Mechanical- Equiprent Requalification M.A. Scott 6/15/83 Subject 30u ated Butterf1 Valves Checked By: ~
~
L.C. Fernandez Date 6 15 83 System Job No. File No.
CSP and CEP 82044 Rev. No. Sheet No.
QID 361104 1 ~ ~
I Hs AgIA.c g >Ra oA ~ A~ /s ~~
WB7 (<)
(+.~W)q~
. (,. '~. ~t,w
~ . ~
- I . *'
e 4 ~
A4 v '1<4'>,o 'f4E t 4 v< 4<>> ~ e C'oeeOS'o a ~ k ~ " 'r ~ en ~ e e.- q>> r)A s s ~
~
x s, < ~ s,a-K Ã w -aa asvl r, wa 4;- ~
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII
~~+,D&e
~
Prepared By:
NPPSS Mechanical Equi fication M.A. Scott Qi 6 15 83 Subject Checked By: Date 30ll ated Butter f1 Valves L.C. Fernanddz 6 15 System Job No. File No.
CSP and CEP Rev. No. Sheet No.
QID 361104 ~ ~
S c4 77M %7 / PRMl&C IOi ~ r(
~g Qa~'77~ /W
~&Go~. ~5~<~WVet-r' o~aj P6" cDd~W C~S'+~l ~
AG
~m N~oa ~e.S5.
427, Z
, ~v T
i
~ \ .= 4 y g E ' 0 I 0
Calculation
- h. a = J a fa 't Sheet ~
IIIIIIIIIIIIIIIIIIIIIIIIIIIIII.
Subject NPPSS Mechanical ~ t ification Prepared By:
Checked By:
M.A. Scott ~ ,
f Qate ate 6/15/83 30" linder ated Butter f1 Valves L.C. Fernandez 1 System Job No. ~
File No.
CSP and Rev. No.
QID 361104 4.3.44 M~ iWaMu W m~~z~e.
~ ~ cJ~/'~ Wc'.
u~r M~ ~catv~
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII
""""WPPSS Mechanical BPxiPaent Regualification "e'" '.A. Scott 4QP '/15/83 30" Cylinder Operated Butterfly Valves Checked By: ~ate L.C. Fernandez 6/15/83 System Job No. File No.
CSP and CEP 82044 OS.01.F Rev. No. Sheet No. ~
QID 361104 4 3 45
/ Wee WP~W ~W70 ~~ ~ndc ~ e S g/ oae/iW
sar: sea ~ vvromo, wx a.+el w ). w . ': e et a a s '%> s ~ 'r . w ss ~ s>wv': ~ ca+ ss Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII
~ /.bate NPPSS Mechanical t ification Prepared By:
M.A. Scott
~K 6 15/83 Subject Checked By: Qt. Date 30 It linder rated Butter fl Valves L.C. Fern d System Job No.: File No.
OS. Ol. F Rev. No. Sheet No.
(5) 361104 ~ ~
Q ~( Wd M ~f ~. CI'W
~+z-Wi Ut aF ~~ 'BY~~It I N MFy4=-Mw ~) ~~K:
~LA TK /S YSASICA-c.C-Y Mc c y~~ A ~g+~ D~WM
@~os.
I 475 I I
- g. $ 75 Cc lmS 4
+7
+Ra~ tt~ ~tz-v-i >A <- ~tzt~<M~ RM
~
~
Cu kn I ~ ~ks ~oM~~ ~c>~t ~
~Q/('3B7%) = 2&o's(c tu c'tt, M= dv (+) z.@7 1 IVI
Calculation cs h. 3 h. I s r Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject WPPSS Mechanical Bpupnent Requalification .A.
Checked By:
Scott ~ 5P Date 6/15/83 30" Cylinder Operated g
Butterfly Valves L.t . Fernandez 6/15/83 System Job No. File No..
CSP and CEP 82044 OS.01.F Rev. No. Sheet No. ~,
QID 361104 4.'3.47
~ut~W~ ~~ ~M ~W ~mph@ 9
>+o3c gg77 4/~p
,z (7
~CA ~Dw ~~ ~~~ ~d dl ~ 23K V NMI / cl~
C~~ l&~ ~~ WBd~ 79~
+~ = 9/77 ~l( IS = Q5I+
O hJ ~7~~ ~( Qp o%Q
+ l %35 LB/z4
~o >g u'
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Prepared By: te NPPSS Mechanical fication M.A. Scott 6 15 83 Subject Checked By: ~~ate 30" linder ated Butterf1 Valves L.. F System Job No. File No.
CSP, d
&irafysrs.Ra=. Rev. No. Sheet No.
ID 361104 4 3 48 3'0 4toM ~T ca3c 3~
r go; ( (y. s75+(I ~</~)I =(+sgcAo)t
=zqo7e'Efl
~~cc
~ odl
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: Date WPPSS Mechani J.E. Rakowski
'l.
Subject Checked By:
L 5//S/S3 System Job No. File No.
82044 Analysis No, Rev, No. Sheet No 361104 '4.3.49 Section. 4.3.5 -Fati e Anal sis t)iscussion The operator and bracket assembly are not part of the pressure boundary, therefore, the fatigue analysis will be performed in accordance with Appendix B of the AISC Manual for Steel Con-struction. The following assumptions apply'to the fatigue
~ analysis.
- 1) Faulted stresses (based on piping-analysis accelerations) will be used. This is'ecessary 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.
Calculation 3L fit Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: Date J.E.Rakowski Subject
" Butterf1 Valves .F P/- /;
Job Wo. File No.
System 820 4 0'01 F Rev. No Sheet No. -
NYf.b~4 4 3 5p
- 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 'he following page gives the calculated stress range, stress category, and al'lowable 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.
1005 tO
Calculation ca h. J a f k i Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Pr' Date 4V'SS Mechanical E ui ment ualificationPrepared By:
J.E. Rakowski 1/10/83 Srtbject
.30" Butterfl Valves Checked By:
',c. F~~
r r ~ Date
>/>~ (E>
System Job No. File No.
Rev. No. Sheet No,
'551M'4 4 3 51 Fati ue Anal sis (cont.)
STRESS STRESS'PSI)
STRFSS STRESS . 1.5 x ALLOW ITEM TYPE RANGE (PSI) CATEGORY (FROM AISC TRUNNION 410 PIN'RIVE ROD MAX SEE TA LE 1.2 SUPPORT F.ARS SEE TAB E 1.2 9127 18254 A 90000 MAIN SHAFT 7158 14316 NOTES:
(f} Assume shear stress on nominal area of a stud type shear connection.
Note. that this comparison includes all of the load combinations in one conservative comparison using the maximum stress -.and the total number of cycles ( 3 x 4500 + 2000 + 60 .=
15560)'00s 00
Prepared By Date Calculation. Sheet Date
'X.'8'ob ir/
Project t No. File No 3 Owx>Pr LM
>~Q94- Qr5'. Dl IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Subject Sheet No.
+~tl ~+ 4.3.52 Analysis No. Rev. No, 0>T; T HE T'RSL.E SEl om BEER ~H DE~Sr-2 F~>M
'H H8-S RPee~>zx 8 op THe HXSc Nt4xuxi aP STEEt CG'NsT'RMc 7 ?0 c C g LES W5EQ pj QE HHRKE2)
Ld ZY H aN HRRouJ.
Stress General Cate-Condi- Situation Kind of gory.
tion (See Stress'or Table B3)
Plain Base metal with rolled or cleaned sur- Rev. (go,~b material faceL Built-up Base metal and weld metal in mem- Tor Rev.
members be'rs, without attachments, built-up of plates or shapes connected by contin-uous full. or partial. penetration groove.
welds or continuous filletwelds parallel to the direction of applied stress.
Calculated flexural stress, fs, in base Tor Rev.
metal at toe of welds on girder webs or flanges adj ac'ent to welded transverse stiffeners.
Base metal at end of partial-length Tor Rev.
welded cover plates having square or tapered ends, with or without welds across the ends.
Mechani ~ Base metal at gross section of high- Tor Rev.
cally strength bolted friction.type connec-fastened tions, except connections subject to conn ec stress reversal and axially loaded joints tions which induce out~f-plane bending in connected material.
Base metal at net section of other me- Tor Rev.
chanically fastened joints.
Base metal at net section of high. T or Rev. B strength bolted bearing connections.
Attach- Shear stress on nominal area of stud- S ments type shear connectors..
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By:
NPPSS Mechanical E ui ment uglification 3/25/83 Subject 30" Butterfl Valve Checked By: "" etz~l~3 System Job No. File No.
CSP and CEP 82 Analysis No'6 1 104 Rev. No.
1 Sheet No.
4 3 53
4.4 REFERENCES
- 1) BIF Drawings Drawing I Revi Description A-206763 General Arrangement CEP-625-10 From Reactor Nozzle X-3 to SGT-FU-1A, 1B c CEP-625-11.12 H From Reactor Nozzle X-3 to SOT-FU-1A, 1B d C-26095 Model A-83B Cylinder A-206767 Valve Assembly DOC-D-220-0310-IR-66 0 Tube errection iso-metric D-207110 Valve Data Sheet M-144 General Arrangment, lan mis level CSP-807-3.4 Containment purge air su 1 s stem 1006.00
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII WPPSS Mechanical Equipment QualificatTon O'.E. Rakowski 3/25/83 Subject Checked By: r Date 30" Butterfl Valves I-.C. Fc /ZZ System Job No. File No.
CSP and CEP OS.01/F Aoaiys s o'6 j 1 04 Rev. No.
1 SheetNO 4 3 54 Reference cont'n
- 2) Formulas for Natural Frequency and Yiode Shapes, Robert D. Blevins Van Nostrand Reinhold Company 1979 Edition
- 3) BZF Report TR-27234 and TR-27235, "Dynamic Torque Calculation of Butterfly Valve; Sizes 24 and 30 inch",
dated November 10, 1982;
- 4) Report TR-74-8 by McPherson Assoc., Inc., "Design &
Seismic Analysis 30" Cylinder operated Butterfly Valve".
(Rev. 1) 12/31/75.
- 5) WPPSS letter to Cygna Energy Services,. GE-02-RWH-018, 12/17/82.
- 7) Cygna Energy Services, Equipment Qualification Walkdown Verification Form dated 7/14/82 and 7/19/82.
- 8) Cygna Energy Services, "Project Manual Design Criteria,"
DC-1, Rev. 1, 10/82.
- 9) Burns and Roe Revised Piping Analysis Loads for.
CSP-V-1 and 2 (dated 4/12/83) and CEP-V-1A and 1B (dated 11/15/82) .
- 10) Communications Report, R. Ricappito of BXF and J. Rakowski of CES, uBXF Valve Dimensions", 2/ll/83 1006.00
APPENDIX A COMPILED PROGRAMS AND RESULTS FOR CSP-V-1 CSP-V-2 CVGNA ATTACHMENT J08 MO.~BZag FILE NC ~OS. o(, P SHaa7 t(O.~4'
sbasi c esp 1 2 tm S-HAS I C Comp i 1 er Ve r s i on 5. 4b 001:00 REM+++++ BIF VALVE AND AIR OPERATOR SEISMIC STRESS 0002 i 00 REM+++++++++++++++ CSP-.V/AO-iz'2 0003:00 REM++w+++w++++++++ 10 INCH AO PARAMETERS 0004:00 REM 0005:00 var i,j,k = integer 0006:00 var lrod,lcg,x,phi,lave,ablt,l1,12,e1,e2,e3,e4,e5 = real 0007:00 var fst2, ca,ia,cb,ib,aa,ab,di,d2,ci,i1,c2,i2=real 0008:00 var lrodo,lcgo,ldr,d, abush, pbush=real 0009:00 var fcof, fco, ma,mb, siga, sigb, fcdr, fcdr f,maf, mbf=real 0010:00 var dear, fcear,fr, fii,f22,la, cii2,ci21,stt3,semi=real 0011:00 var sem2,set3,sesi,ses2,sr, tauii, tau22, tauear,aear=real 0012:00 var btens, taubl t, set3f,semif,sem2f,fcear f, frf,fiif=real 0013:00 var f22f,stt3f,sesif,sesZf,sr f, tauif, tau2f, taurf=real 0014 i 00 var taubf, bt f, dsr, dtaur, dtaub, dbten, dsa, dsb, dpb=real 0015:00 0016i00 var sdraf,sdrbf,pbushf, taui if, tau22f=real var wao,wbr, f tri,watri,s1,si f,s2,s2f,mi,m1f,m2=real 0017i00 var m2f, t3, t3f, t t3, t t3f, l br,wtot=.real 0018: 00 var bsi, bs2, b t3, bmi, bm2, bt t3=real 0019:00 dim real av(3) 0020:00 dim real wa<3) 0021i00 dim real wb(3>
0022:00 REM 0023:00 REM +++ BURNS 7 ROE EAR FORCES ARE bsi etc TURN ON WITH K=1+++
0024:00 REN "025:00 REM 326i00 dim real a<3,3) 027:00 dim real b(3>
0028:00 dim real glc(3,3) 0029:00 1 data 9 5, 10.5, .88, 3 94, 1.50,1.34 0030:00 2 data 25<21 50t ~ 488s48 ~ st 85t 627tl 75s3 ~ 0 0031:00 3 data 1847...875,.46,.648,.138,2.41,1.4 0032:00 4 data 593.,321.,5.25,8.5,28.5,15 ,7.75 0033:00 5 data 40.<16 25,26 ',43 >2 '75
~ A 0034:00 6 data 135.,90 ,135.,90.,180.,90.,
0035:00 7 data 45.,90.,135.,90.,0.,90.
0036:00 REM DATA 657 FOR VALVE/'GLOBAL-G ORIENTATIONS AND WEIGHT VECTOR 0037:00 r estor e 0038:00 read dl,d2,ci,ii,c2,i2 0039:00 restore 2 0040:00 read lrod,lcg,x,phi,lave,ablt,li,l2 0041 i 00 restore 3 0042: 00 read fst2;ca, i a,cb, ib,aa,ab CVGI~!A.
0043:00 restore 4 0044:00 read wao,wbr,ei,e2,e3,e4,e5 0045:00 restore 5 0046:00 read lrodo,lcgo,ldr,d,abush boa wo. 9~44 0047:00 restore 6 i-'iLEVO. 5.
'048i00 read a(1)1>,a<2)i)ra<3,1),a(1,2),a(2,2),a(3,2) No.
restore .7
'HEET 0049:00 0050:00 read a< 1,3),a(2,3),a(3,3),av( 1),av(2),av(3)
'>51:00 text O,h INPUT GLOBAL ACCELERATIONS 8c u52:00 input b<1),b<2),b(3) 053 i 00 print 0054: 00 text O,h INPUT DAT* h 0055: 00 print ='
0056: 00 print "GLOBAL, G-LEVELS ib( 1> sb(2) sb<3) 0057:00 print "NORTH VECTOR ANGLES = ";a(1,1),a(2,1),a<3,1) 0058:00 print "VERTICAL VECTOR ANGLES= ";a(1,2),a<2,2),a(3,2)
0 00:0 pr in ."EAST VECTOR NGLES = ";a(1,3),a<2,3),a(3, )
0060: 00 print "WEIGHT VECTOR ANGLES = ";av(i),av(2),av(3) 0061: 00 print 0062:00 for i=1 to 3 0063:01 for j~i to 3 0064:02 a(j,i)=a(j,i)+2 ~ +3 1416/360
~
0065:02 'lc<j,i>=b(i)icos(a(j,i))
')66: 02 next J
~067:01 next i oo68:oa for j~i to 3 0069:01 av ( j ) =av ( j ) +2. +3. 1416/360 .
oo7a:oi next 0071:00 print 0072:00 text o,h LOCAL G-LEVELS h 0073:00 print 0074:00 print glc(1,1),glc<1,2),glc(1,3) 0075:00 print glc(2,1>,glc(2,2),glc(2,3) 0076:00 print glc(3,1),glc(3,2),glc(3,3) 0077:00 REM WEIGHT COMPONENTS 0078:00 for j=i to 3 0079:01 wa(j)=wao+cos(av(j))
0080!01 wb(j)=wbi icos(av(j))
0081:01 next J 0082:00 phi=phi+Z.w3.1416/'360 0083:00 'a=lave/'2 0084:00 c i 12=el/i 2 0085:00 c i 21~cM i 1 0086:00 aear=ll+12 0087:00 REM CALCULATE EAR FORCES USE BhR LOADS AS OPTION LATER 0088:00 REM FIXED COMPONENTS ARE ALWAYS THERE 0089:00 lbr=lrod+lcg 0090:00 watr i=1 br~a(1) 11 rod
, n091:00 si f=wb( ) +wa tr 1 1
,)92: 00 w.t o t=wao+wbr 093:00 s2f=wb(2)+wa(2)+f st2 0094:00 t3f=wa(3)+wb(3>
0095:00 mi f~-(wa(2)+wb(2)+f st2) +e5~a(3) +(e3+ cg) -wb(3) +e4 1 0096:00 m2f=(wa tr 1+wb( 1) ) +e5~a(3> +eZ~b(3) +e 1 0097:00 t t3f=watri+e3+<wa<2)+f st2) we2+wb(1) +e4+wb(2) we i 0098:00 f cdr f=l cg+wa( 1 )r'1 rod 0099:00 maf =f cdr f w( rod-13. 5) 1 0100:00 mbf=f cdr f +7. 125 0101:00 sdr af = f s t Maa+ abs(ma f+c al i a) 0102:00 sdrbf=f st2t'ab+abs(mbf +cbt'i b) 0103:00 f cof=l cgo<wa(i )i'1 r odo 0104:00 pbushf=f cof +( dr'+d)f'(d+abush>
1 0105:00 REM STRESSES FROM FIXED COMPONENTS 0106:00. dear~<di+di+d2+d2)++.5 0107:00 set3f=abs(t3f/'(4+aear))
0108:00 semi f=abs<mi fi'(2+d2+aear) )
0109:00 0110:00 sem2f =abs(m2f 1(2+di +aear ) )
fcear f=t t3f/(2+dear) CVQMA 0111:00 fr f=x+fcearf ATTAl H~~AF.NT 0112:00 f 1 if=-<fcearf+sin<phi )-frficos/phi ))
0113:00 f22f=fcearf icos(phi )+fr f +sin(phi ) JOB NO.~S2o 0114:00 st t3f=abs(f11f+1 a+c i 12)+abs(f22f+1 a+c i 21) RLa No 0115:00 sesif=abs(sif+cii2+lat'4.) sHEsr No.M~
0116:00 ses2f=abs(s2f+ci21+la/4.)
~17:00 srf=se t3f+seml f+semZf+sesi f+ses'Zf+st t3f F18:00 REM EAR SHEAR 119:00 tau f=abs( s fr'(4+ac ar ) ) +abs( f 11 flac ar )
1 1 1 0120: 00 t au 22f =abs ( s2&'( 4+ac ar ) >+ abs ( f22f lac ar )
0121: 00 taur f=( taui f +taui if+ tau22f +tau22f ) ++.5 1
0122:00 taubf=taur f +aear/abl t 0123:00 REM EARBOLT TEllSION 0124:00 b t f=( se t 3f + semi f + sem2f ) wae ar/ab t n< sc.nn:
1 a
0126!VV pr nt urhKAl lNU CYLINDEK BKG PRESbUKh. ";pbusht 0127 t 00 print "OPERATING VALVE EAR TENSILE STR t sr f 0128:00 print"OPERATING VALVE EAR SHEAR STRES "; taurf,
'0129!00 print"OPERATING EAR BOLT SHEAR STRESS "; taubf 0130:00 print"OPERATING EAR BOLT TENSILE STR ";btf 0131!00 print 32:00 REM
'33! 00 REM CALCULATE VARIABLE COMPONENTS t .34!00 t REM 0135:00 dsr~O.
0136: 00 dtaur~O.
0137 t 00 dtaub=0.
0138!00 dbten~O.
0139:00 dsa~0, D140 $ 00 dsb=O.
0141: 00 dpb=0 ~
0142:00 for j~i to 3 0143:01 f co=i cgo+wao+gl q( 1, j )/1 r odo 0144:01 pbush=fco+(ldr+d)/(d+abush) 0145!01 ftrl=lbr+wao+glc(i,j)/lrod 0146!01 si=f tri+wbrwgl c(1, j) 0147:Oi s2=wtot+gl c(2, j) 0148:01 t3~totwgl c(3, J ) -
~
0149!01 mi=~tot+glc(2,J)+e5-wao+glc(3,j)+(e3 +1 cg)-wbr+gl c(3,J) 0150!01 m2=( f tr 1+wbr+gl c( 1, j ) ) +e5-(wao+e2+gbr c(3, j) +e4'el)wgl 0151 $ 01 tt3=ftr 1+e3+wbr+glc(l,j)+e4+glc(2,J)+ ( wao+e 2+ w br +e 1 )
0152!01 fcdr=lcg+wao+glc(i,j>/lrod 0153:01 ma=fcdr+(lrod-13.5) 0154!01 mb=fcdr+7.125 0155!01 siga=mawca/ia 0156!01 sigb=mbwcb/ib 0157!01 REM CALCULATE EAR TENSION
>8!01 set3=abs(t3/(4+aear)>
~9!01
$ semi=abs(ml/(2wd2waear))
0160: 01 sem2=abs(m2/(2+dl+aear))
01 61. t 01 f cear ~t t3/(2wdear )
0162!01 fr=,xwfcear 0163:01 f 1 1=-(fcear +sin(phi )-frescos(phi ) )
0164!01 f 22~f cear+cos(ph )+ fr+s n(ph i )
1 0165:01 st t3~abs( f 11 +1 a+c i 12) + abs( f 22%1 a+c i 21) 1 0166!01 se sl~abs( s 1 +c i 12+1 a/4 ..)
0167':01 ses2=abs(s2+ci21+la/4.)
0168!01 sr=set3+seml+sem2+sesl+ses2+stt3 0169!01. REM EAR SHEAR 0170!01 tau1 i~abs(sl/(4. +aear ) )+abs( f 11/aear )
0171'$01 tau22=abs( s2/(4. +aear ) )+abs( f 22/ae ar )
0172!01 tauear~( tau 1 1 +tau11+ tau22+tau22) ++.5 0173!01 taubl t=tauear+aear/abl t 0174! D 1 REM EARBOLT TENSION 0175!01 btens=(se t3+semi+sem2) +aear/abl t 0176:01 dsa~dsa+siga+siga 0177!01 dsb=dsb+sigb+sigb 0178:01 dpb~dpb+pbush+pbush 0179:01 dsr ~dsr+sr+sr cy g@
~
0180!01 dtaur=dtaur+tauear+tauear 0181 $ 01 dtaub=dtaub+taubltwtaublt JO ~0 g 2a'9 0182:Oi'i dbten~dbten+btens+btens a3,01 next J lsHgg+NO 4!00 REM. COMBINE STRESSES 85!00 dsa~dsa++.5 0186!00 dsb~dsb++.5 0187!00 dpb=dpbw+.5 0188!00 dsr=dsr++.5 0189!00 dtaur~dtaur++.5 0190!00 dtaub=dtaub++.5 hi h hh ~
0192t00 'p'r int 0173t 00 text O,h DYNAMIC COMPONENTS 5 0194: 00 print
'195:00 print "DRIVE ROD TENSILE STRESS AT A"idsa 0196 t 00 print "DRIVE ROD TENSILE STRESS AT B"Idsb 0197 t 00 print "BUSHING PRESSURE ")dpb "l 98: 00 print "VALVE EAR TENSILE STRESS "idsr 99t00 print "VALVE EAR SHEAR STRESS .";dtaur vc00t00 print "EAR BOLT SHEAR STRESS ";dtaub 0201: 00 print "EAR BOLT TENSILE STRESS ";dbten 0202 t 00 dsa~dsa+abs(sdraf) 0203t00 dsb=dsb+abs(sdF bf )
0204 t 00 dpb~dpb+abs(pbushf) 0205t00 dsr=dsr+abs(srf) dtaur=dtaur+abs( taur f )
0206t00 0207t00 dtaub=dtaub+abs(taubf) 0208t00 dbten=dbten+abs(btf) 0209t00 print 0210t00 text O,h FIXED PLUS DYNANIC COMPONE NTS h 0211t00 pr int 0212t00 pr int "DRIVE ROD TENSILE STRESS AT A";dsa 0213 t 00 print "DRIVE ROD TENSILE STRESS AT 8" I dsb 0214t00 print "PUSHING PRESSURE "; dpb 0215 t 00 pr i n t "VALVE EAR TENS I LE 'STRESS ")dsl 0216 t 00 print "VALVE EAR SHEAR STRESS ";dtaur 0217 t 00 pr int "EAR BOLT SHEAR STRESS ";dtaub 0218 t 00 print "EAR BOLT TENSILE STRESS ";dbten 0219 t 00 end 0220 t 00 0221 t 00 0222t00 0223t00
~4t00
- 5!OO w+w+++ End of program +++++w ATTACHMENT
cspQ1,.
INPUT GLOBAL ACCELERATIONS 2 '6s3 ~ 62,2 '
INPUT DATA GLOBAL G-LEVELS NORTH VECTOR ANGLES 2 '6 135 3
90
'2 '2 8
~
135 VERTICAL VECTOR ANGLES= 90 180 90 EAST VECTOR ANGLES 45 90 135 4IEIGHT 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 '7991
,OPERATING DRIVE ROD STRESS AT "A 766.432 OPERATING DRIVE ROD STRESS AT B 1319.35 OPERATING CYLINDER BRG PRESSURE -7.15824E-4 OPERATING OPERATING VALVE EAR TENSILE STR VALVE EAR SHEAR STRES
'111 '1 293.896 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 ~ ~
~e/MPH'~,Ma~ A~Yrf &g~p~g gW C~dwfar.
BUSHING PRESSURE 477.447
+S<c s~T> 1,3 3o - $ E V'a.
EAR BOLT SHEAR STRESS 7039 EAR BOLT TENSILE STRESS 10524 "9 FIXED PLUS DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 29150.9 DRIVE ROD TENSILE STRESS *T B 44731 '
PUSHING PRESSURE 477.448 5
EAR BOLT SHEAR STRESS 9499.86 ArrACH@ENT EAR BOLT TENSILE STRESS 12150 sos xo.U~~~~
FILE NO. os Ol.
SHarr WO.~~.~~
cs 2 INPUT GLOBAL ACCELERATIONS 26~3 62s2 8
~ ~
INPUT DATA 3LOBAL G-LEVELS 2.26 3.62 2' lORTH VECTOR ANGLES 135 90 135 VERTICAL VECTOR ANGLES= 90 180 90
-1 59807 -1 38092E-5 97989
~
-8 '2121E-6
-1 '9807
-3 '2
~
-1 '8092E-5 1 ~
-1.06811E-5 1.97991
)PERATING DRIVE ROD STRESS AT A 766.432 3PERATING
)PERATING DRIVE ROD STRESS AT B CYLINDER BRG PRESSURE 1319 '5
-7 '5824E-4 3PERATING EAR WELD TENSILE STR 3090 '3
)PERATING EAR WELD SHEAR.STRES 735.124 3PERATING EAR BOLT SHEAR STRESS 2460 '6 3PERATING EAR BOLT TENSILE STR 1625 ~ 1
'NI C COMPONENTS
)RIVE ROD TENSILE STRESS AT A 28384.4
)RIVE ROD TENSILE STRESS AT B 43412.2 3USHIf lG PRESSURE 477.447
=AR-W
=AR BOLT SHEAR STRESS 7039
- .AR BOLT TENSILE STRESS 10524.9
~
FIXED PLUS DYNAMIC COMPONENTS
)RIVE ROD TENSILE STRESS AT A 29150 '
)RIVE ROD TENSILE STRESS AT B 44731 6 OENO ~ZEA4
'48 F
'USHING PRESSURE 477 FILE IIO
..AR-W EIiEET MO. 4.sA7 R BOLT SHEAR STRESS 9499.86
- AR BOLT TENSILE STRESS 12150
g~p Q INPUT GLOBAL ACCELERATIONS
'P 1 ~ 44,3 '4<i.9 INPUT DATA GLOBAL G-LEVELS NORTH VECTOR ANGLES =
1.44 135 3
90
'4 1.9 135 VERTICAL VECTOR ANGLES= 90 180 90 EAST VECTOR ANGLES = 45 90 135 4lEIGHT VECTOR ANGLES = 90 0 90 LOCAL G-LEVELS
-1 '1824 -1.3504E-5 1 ~ 3435
-5 '9316E-6 -3.54 -7.24792E-6
-1.01824, -1.3504E-5 -1.34351 OPERATING DRIVE 'ROD STRESS AT A 766.432 OPERATIVES DRIVE ROD STRESS AT B 1319 35
~
OPERATING CYLINDER BRG PRESSURE -7.15824E-4 OPERATING VALVE EAR TENSILE STR 2111.01 OPERATING VALVE EAR SHEAR STRES 293.896 OPERATING EAR BOLT SHEAR STRESS 2460.85
'OPERATING EAR BOLT TENSILE STR 1625. 1 DYNAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT.A 18806 DRIVE ROD TENSILE STRESS AT B 28762 '
BUSHING PRESSURE 316.332 'l
$ Gag, S~ET5 'f.3%+ +5 &
EAR BOLT SHEAR STRESS EAR BOLT TENSILE STRESS 5077 '4 7164.63 FIXED PLUS DYhlAMIC COMPONENTS DRIVE ROD TENSILE STRESS AT A 19572.5 DRIVE ROD TENSILE STRESS AT B 30082.1 PUSHING PRESSURE 316.333 QVQNA EAR BOLT SHEAR STRESS 900 .,~
7538.79 P'fTACHMEÃT EAR BOLT TENSILE STRESS 8789.72 JOB NO. ~~
FiLKNO. ~~
SHEET NO
esp 1Q INPUT GLOBAL ACCELERATIONS
"<4,3.54,1.9 INPUT OAT*
3LOBAL G-LEVELS 1.44 3.54 1 ~
WORTH VECTOR ANGLES = 135 90 9'35 VERTICAL VECTOR ANGLES= 90 180 90
- -AST 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 3PERATING DRIVE, ROD STRESS AT A 766.432 3PERATING DRIVE ROD STRESS AT B 1319.35 3PERATING CYLINDER BRG,. PRESSURE -7 '5824E-4 3PERATING EAR WELD TENSILE STR 3090.43 3PERATING EAR WELD SHEAR STRES 735 '24 3PERATING EAR BOLT SHEAR STRESS 2460.86 3PERATING EAR BOLT TENSILE STR 1625. 1
)MI C COMPONENTS
)RIVE ROD TENSILE STRESS AT A 18806
)RIVE ROD TENSILE STRESS AT B 28762.8 3USHING PRESSURE 316.332 a'-rR-blE tO ~'ENSTt~TR SCC. S <C R BOLT SHEAR STRESS 5077. 96
.AR BOLT TENSILE STRESS 7164 63
~
FIXED PLUS DYNAMIC COMPONENTS
)RIVE ROD TENSILE STRESS AT A 19572.5
)RIVE ROD TENSILE STRESS AT B 30082 1 F
'USHING PRESSURE 316 '33 94R-WELD TENSI-LE-STR i"-tR-WELD SHEA~ .
~
=AR BOLT SHEAR STRESS 7538.81
- AR BOLT TENSILE STRESS 8789.72 JOB NO 82 FII.B NO SHErr Wo.~<~~
APPENDIX B VALVE/AIR OPERATOR MODEL FOR FINAL PIPING RESPONSE G-LEVEL CALCULATION.
CVGMA VOS NO.
~E~+"
FILE NO. OS 0 SHEET NO.
I P
I
Calculation Sheet Illlllllllllllllllllllllllllll Project Prepared By: v f0 Date S J= l 3 Subject Bz r I/Au/E Ac ATa p. ~I/ . 8. z4/l>3 System Job No. File No.
C S and CEP P0 q.q 0 T.ol P .OZ/r Analysis No. Rev. No. Sheet No, 34tjo,4 4IO& I 4
g) 070 L Co> Ft PW CoNOEaroal y
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! ~ >>r'&4 Jk th)!7 Sheet 4
llllllllllllllllllllllllllllll Project Prepared By: Date wP s )ZAN Checked By:
87 F VAlv C. ATI" Job No. File No.
CgP and CEP o7:o< lw r os.o!.rv Analysis No. Rev. No. Sheet No.
' 4 3 p3 3G(lo ++ %ttoG VAioE. EARS tt 8 ex!. (24HLvE) lG .
AiR c FRAT A)( =Ay= 4p = IS lH Z.t Z~~= t04 lP Cs"7
.Dye = II.Z " Z.(, +
Sl. Z g3 Cy = S.~
C.~ S.'lS 4'.7 5 E- Z8 y in+, FS,
~ I].L<IO P 2 = S.i!a" +gg Qz ~F<<
(p~ < =o A.
$ o8a z'1 lr! ~5
=W~= A~ =.4.S4 lu
~j '32(tr 4
Xyq ~ lb( IH
+
255 lmrO lH, tgdg IAI Z,~~ = 2.Il'. lu 4.22- tu C.< -- .ES l~ . 3l'5 C~ = S.94 le 'E.5 6
=ZS <<o rSr e, = ll.S ~ lO PSr.
I, =zg.W I lg" docw ~ e&J Qsg EVu<r~ oars'Z Ls tt s L< = (..S>S
$ .o" Q8 vnssLrss, reise uoK.! E.tt Lode t'I s'
(. ECS"<<(.
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<ll)'~b
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII tv f'II'55 E 6} of-'repared By:
Checked By:
e Date Date
/ A~.G. Acritg t AE.X System File No.
C.SP and cEp dTOI a Analysis No, Rev. No. Sheet No. OS.01/F guilt G4H 34IIO ~ ~
~5 sw 4 F'w OFF sET II Raio LiN< iV,+8 uoC (tg..ao )
A T 5'Z .t' ~S SHow/tj Qa x- +Rl
~~~ = Z.,SZI~~ $ 0+
g)y = 5;qS I ~ Z0 I 't2.
Cy = I . Ii 6 g,zr
). I L5
).z+
P ~ 2 I 6)OPSY = Ilhg )b i+ In. 'l2.'gS
'a Wive. goo 4 ~-2.4I 0, >-- Z.fi P~= Z.gt>V I~ a 4'AJ E yy = i'7< l~ seed
= Cg = . 6(5'rJ Ht& g
>VZSD. g e. = BD&io P9z Es= lr<(o e
I =
C I35 yLlN Dzk PtlT Q=D + hDD z99rr Aq rdD.~s'9S, I ~.s L(g = t+p lg Qy'y = '?Q. IH lPo v S2 II I 2-7 IN+
A~= PZ -- A~ =tr SC Ia 7% IP
~=4= +
iooe oo
t 8~
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII By: Date v Ps& E I Subject Checked By: Date RAP AOOa &IF VALVE 0 ~ ~
System GS P and CEp /isfr~'repared om.d ol g Sheet No.
4.3.S5 OS.01/F Kii04 <'KGII06 ED r
PK,Scg LP T&4 at= AO Ph o DEI IQCt. Q b(Q& 4 UAL~f'AR'5:
o.
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k.'pz = 0+
= 4+ fa,)~
Q~ Rod.<, aa) ~ lb..
4 .Wt-h5 comic P~K Pp
< ~<<~.Qi 3 ,~ I
~c) +.3-49 oj= rt'(lo4 'Fav I ~as" r 005 00
Calculation BFa J- iai Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: , Date I 5 3 Subject System LVE. L- 3 M Checked By:
A File No.
Date s&e and CEP 82044 OT.01 F 6 OS.01/F Analysis No.
IO"I 8 I Iz0 Rev. No.
i I Sheet No.
~ ~
%+a& chic w z g A
~r/r cjig
>W LZ-~) g~ <<C7jest. I~ c~~
y.>-po +.e W~
zQ 3 Po.
(R-o.) (it% za 'f -u) g f p, = NJ I2. FX I ~ A 8
~F J F-~= ZlX IO P~E (L)> (a.=o) = 7.I Z.S (O.tS )
6 Iz+ z'I%lb s 0.'1 - t9$ >> l0 j go~ +8~)J.3+ 0.70
- '3.nS I
un g
~
lZ, gl.lK'b)" = ~<<1
~
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>>L3 4->> r-~ z.c,ee.>>io L)t b,rz 3.1%/I ~ c QP 4+ Q = +12 E.wt~, Kazp l.95'- 't.<o ->>
~ 7
/ '
Lulls Wy.
I /
.gi
<>~St@ << YHG EAR- RY5TEhh 57lI=FPlF Sy I)U ~I8.5~
MDOEs vEP Y LARc F, . Egc gggE cpz~~<g
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/ ~
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Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Subject System Analysis No.
3 V
and CEp Tu AT Rev. No.
Prepared By:
Checked By:
Job No.
gg 82044 Sheet No.. 4 3 p7
~ "
File No.
, Date Deke S/ ~ a g
t
/
J TJ4 WBMM 9 hku. D'~ . VLO
~ 'I
/y 4F it, = T' g .- 1'B.'lC e KB) =
-1.~8 C.ZS'.75
+s.zs =
a.e8 s T 4F~Q m) rh &g e
F~ ~ 0 -Fg~4' ot ~~(~
F,'c jghScB SLA ~P
+FPB P
~m8:
A~ Yyke.~ KB Fp (~
(Fc CBD.'diet F rd W~ djy )
2 Bgyhckkk g=,l.D/c.--4 a2 = -(F, ~dt rp ~t- ) t~> < 3 j .'I yu ~ :. 5Mb'-
t'Q.%LPk= t'+
1006 00
I i
- i' ql 4 4
Calculation B. m == J k f a 4 Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Prepared By: Date PP Qg$ 3 A 'Ex4A Subject V v 1- Fso MooE UP 8 E4ss System File No.
'82044 OT.01/F & OS.01/F Analysis No. Rev. No. Sheet No.
4 ~ 3. BS I tNrBrc Fc ~ceelp -F eoec l - l.3Z7 (F ~q iFRs w ~ ~ 9'
.'lO Z.'1 Z'"+
err Cree ri: = . roZ
. 7+2
, 4't l I >'f
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'l,3Z."l r .1qq .CBZ F z.1'S, z.'l+,4,7t lroZ.Fc. +.199
.74 2 FP. . '514
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,qkf..s~i S, =, 'tax Fg .PSO
~ I t P~~~'
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~. g' e'.
zc = Eel l( cicdetc+ y"R~t"3 P R4na) r~4 P~ ~ .Szi Pc fo R R
> .s+o l. lo5
),'to 4- s'I,'fez. Fc IDEE'~ R E.X lre~
2 T
)( g pg 5)3 z L L W=F.~oi~
r 005 00 g)
Calculation Jkfi Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII P'ePa'ed By:
WPPSS EQ J. E. Rakowski 1 Subject Checked By: Date /
BZF Valve/Actuator Model Summary System Job No. File No.
CSP and CEP 82044 OT.01/F & OS.01/F Analysis No. Rev,. No, Sheet No. p 3 B9 361104 & 361106 Z
,os(<..zs) (~9)(io) (t ts) = i>z.(io) r ~/m~
(7.os) (s 9't) l5&S i.7 Z (io)
(.Sa s (<o)
So Pf'0 C.T BLACkt=T Ft ATE BEUDlhl &
S.>6 fb Io.G 2
C Lt5SE'i 4a.5 Z'S.ZSgg.g 37 (beiou J
I 3~ cAQat.~E.E cating, i PX.C tl> Cyl .
i 0 c+cqL A
tl, f'tH j- m I5.$
R7" PQ f: Ch t. CLC Lh ltd 0 bl- ElACt< I= T I=LE X> SILI7 YJ ~H.E.
Ou3 Id& ME.AS Ulz BA QuW~ ~~l~ 'T4 JC,G M Otu C'P - $ 0- 5 4 8 . Pblq IS e,.go) (MR~E..
OEiL,& (~i(/ A3 FnlO aF (.)I. LIP ):,g.~ 1z.G *,ls Foie cE AT EAl'. OF t=yL (I E': EK (So (~
1006 00
~
!l 3 '.,N1 r ~, s < mp + r ~ ' > 4 " ~
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Prepared By; Date WPPSS EQ J.E. Rakowski 1 3 83 Subject Checked By; Date BZF Valve/Actuator Model Summar ~ C ~
System File No.
CSP and CEP 82044 OT.01 F Analysis No, Rev. No. 3 B]0 Pv ERAL,F FLEgtGir-t T 7 l,2 7 (t o) ~/ Jt&
CQ LC,t>t P=t+ P t-6'CC. I jYQ PhoMF 47 Ot= ( 9 FJ->'1 0(
C Auatt.au ER. @Farm GSG.C T'o g,G.PRF S&N T THE C RRclcET., Us& ~He F t-Lou <ac Plmavs togs b, + '58> = ISO + .WI2'7 w 0 I'lo
~ t~~=F)iso 2,
3
- 5) - Fk ~ ~BR 2 - FL r ply FX R.~+Iq EST. z RZ E~ 3 H.
=t IScs q I ~'5.53 +.z (.io) 4o)
,a ~z. q ( res +,~)
,I?O q QQ
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'4 E-~ 'I C'5 ~ 4L ~ 4~ \ 14 ~ ll jl
j Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Prepared By: Date WPPSS EQ J.E. R Subject Checked By: Date BXF Valve/Actuator. Model Summar System Job No. File No, CSP and CEP 82044 OT.01 F & OS.01 F Analysis No. Rev No. Sheet No 361104 & 361106 4-3-Bil p,- 9,8 4. F. + G', ~ AH=@I-Fk + (%F) < k <~V Z.SS F-X F~
-7 j,g(io) + I'0 - 7,v(ic) 2 e 7Ltc) 3P.&) -, E'T3
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4 SPY Q.'l The(orJ A< &St STA>C E 'E-T Tc 0 H t6g IJyt-DE.. 5/N<
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Calculation L ~~ Jkfkt Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII By.'~
Prepared By: Date .
PRE- E I D caked Date /y VALvE i"T A%ok (+
System Job No File No.
and CEP 82044 /F Analysis No. Rev. No. S"eet No. g I IIO~ 4 tOu I
~ 3. B12
~
r ggAF'T gN r DRI Yg. POD I
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e LII Y-
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a~Bit>~ ride C'ate. 2 P yy To P'5 ID't 5 7 I FFQE~S
/ I hc(c ZA + A~ fA ei~ 5-tt F F IU B B 5 E 5 gp Co oTMC>~-
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: Date I 3 Sub't Che l) d By:
0)- UMMA System File No.
C. and CEP 82044 OT.01/F 6 OS.01/F Analysis No. Rev. No. Sheet No.
54IlO 10t 4 ~ 3 +13
~AR s:
Zl 2 2.5 '. S X Z. S X 4 = I 5 IW K
Ay 4p = IS = I IH cZ~ yg.g>>
RUE--TIA S T!) <
G X<
[. Q,S (.to) 8 l.a 2 (.<o) L W T ~
(,q z((o)~
X J.Ws'Qo)
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r I.O ID + lO Z
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Calculation s si', r=~) Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By: Date 3
v Lv7 uA 0 Mo EL ~ma System Job No. File No.
and P 82044 Analysis No. Rev. No. Sheet No.
4 3 B14 Dl.llo io4
/ SZ gC~~ r/is(s>, (
.I A'0 l~.l> IO
'.'39
{o ~o)
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(iil 8 i wA 9 Do r5
~ c. Id ANAL-'ssis
~So art ~O~P~8$ ~
v~rz Kg() c~R pz'~ 5w ~~+ Q.3~0
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Calculation f~s i-= Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project System Analysis No.
P p
and CEP Rev. No.
KL Prepared By:
Checked By:
Job No.
82044 4 3 g ~
915 File No, Date Bete II I gCKE.T yg5
- l. (25 zSs 8.8
( QB pk9. pg'SLESS1 @6th LIQ~
+l.l>5 g.dy 2,.5'> ( zo")
PIA = 7.M QcP4e(-SoW, W M~
g = I IZS' 4
. ZC Xe =
TZZ Vf I ~~,
].7 $ ip Z. I2.
A-~t, - z.qg m) 4.'It su q,45 I0'0 II,S'., = 7,IzS 58(tIF T
< t,>75'= I+
~o O'E. MFT 7,(W~
r
'yl- DBFcBevtDl/
9-~EC~tgU f BytBF retd Z$ ,5 (L judy IOQ~~~~T.)
qO (.l D ~V~=S)
TH$ EE FoM> slNcE sp J(F7 I>
p 0 p ~ t'g) p-gg L 6 F Gg~'T~
p,t'-YUAN MMGP(, IJSE:
7$ (p 2';~s Z~- i.Z~>>" ta2.
1006 to
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Sub)ect System Analysis No, WPPSS EQ BIF Valve/Actuator Model Summar CSP and CEP Rev. No.
Prepared By; Checked By:
Job No.
Sheet No.
2 e
g ~
J.E. Rakowski File No.
Date Dele 1 3 01/F 4 3 Fo k 'TH e LhcVQT ELE-~ ~
r.fykkfCE Q = D p rl! f 2'f7/ fs fkykkkf ) (Saf~)
g Dffc ~ef = 2'2.s' fs +k3:6 ) vZgg WE.tf" H T = Kl7 gg 34+
Z Ag = 4 y = Aq = 4 ~Y- Iu (o.S iieet I.v ft-AWE 8PQ & tH t" (M t="~i trI c F g@t'-I~ f W fLAH5:
3 1kckk
= S)2k = f (Ck.s)i I3 S ) = f02. fkk IL I ~ .( <5 Z55 f006 00
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Prepared By Date B,TF AivE'/ Yu System File No.
82044 OT.01/F 6 OS.01/F Aoalysis No. Rev. No. Stteet No.
Il 104 4 3 p] 7 AISLE PRIVY. RoC C LI E.
gNt P c gq P P I P tg yg 5 AE 2
~Bi~: GLcVtS lLS 0>
'(
f4 l1
~'t~
593 tr"~)
<<o Q'. pr.NB gob:
L= u..~
Z.
= Z.+
A - W/< 9 Z.kl<<d C. = .'<<I'1S ~
4 - ~x~-
>yy = '~+'W< = ~< IN l0 Oz,x" cyL: l, =o hNc pup 0> Xyy =
l@= l>.~~
14o tl A 5'
APPENDIX C SAMPLE HAND CALCULATIONS TO CHECK PROGRAM
'EP-V-3'A p~ Alp, FZOQ.~
~><R hip, OS. g ( p
-3.cZ
nb i f C E P- tJ - 3 A Calculation INPUT GLOBAL ACCELERATIONS
? 13 '9<i ~ 66<1.04 Sheet
.INPUT ANGLES OF NORTH VECTOR
? 90,90,0 INPUT ANGLES OF VERTICAL VECTOR Date
? 90,0,90 Prepared By:
J.E. Rakowski 1 0 INPUT ANGLES OF EAST VECTOR Date Checked By,'
0,90,90 Job No. File No.
NPUT DATA 82044 Shee+ b4 GLOBAL G-LEVELS 13.89 1 ~ 66 1 ~ 04 4.3.C2 NORTH VECTOR ANGLES = 90 90 0 VERTICAL VECTOR ANGLES= 90 0 90 EAST VECTOR ANGLES = 0 90 90 INPUT ANGLES OF WEIGHT VECTOR '5'PLE DECI( CALC 90 s 180 r 90 WRF55 E.A R >t=wSt<E LOCAL G-LEVELS T>F (Fe>)<vs-mv ~s.~
'-5 '9861E-5 -6.33239E-6 1.04 - (h5o -Wq)+ bS-27)4S Lb
-5.29861-E-5 13 '9 1 '6
-6.33239E-6
~
-3.96728E-6
-3.96728E-6 TyP 4938 )
I.c,=~~~
t.s OPERATING DRIVE ROD STRESS AT A 477.198 F, ='-,cg~ T~F = -'7$
OPERATING DRIVE ROD STRESS AT 8 821 . 458 3 75613E 4 Fat- = t-i.03+T~F = '245 OPERATING CYLINDER BRG PRESSURE OPERATING OPERATING VALVE EAR TENSILE STR VALVE EAR SHEAR STRES 89 1706 s~ =l
~ ' ~
esx(-(<sg >sl J.\@3>>'(L>&(w 7c(i i ~ gS i I
QC(~ ~Pl.oM-
~
OPERATING EAR'OLT SHEAR STRESS 1078. 68 OPERATING EAR BOLT TENSILE STR 525i.@95 . = $ Z RI gl c < 1, j ) = j=-5. 29861E-5 ~ dAe gn clw'd ((wIw(~g~'.
fc dr=,
siga~ .267492 1 .'22282E-2 1
(((
I
= ~~"
tw((okgg('gyk)05'(/we~((((~
Z.+to 0 l.58 2-o sigb= -.409114 Fc du e t o T3=-5. 71 1 81 E fs~e ~ dm shoon =~w(w'~ ~<~)*~~a~
f 1 1= 2. 73638E-2 Z f22=-5.85968E-2 dsa=
dsr~ 3.3257E+7
~ 071552 G'chic g<<~ ~ gk ~ ~>O ~t.tS +7.<<a-29l PSX dbten= 4.86604E+9 glc( l,j)= j=-6 '3239E-6 2 TaqgL DID she, ~aOSiLC +ASS.
fcdl =
siga= -3.19681E-2
-1.4614E-3 f2'++l- z'l( = l(4( vs~((37 QZ)
,sigb= -4.88934E-2 Fc due to T3= 321.752 f 1 1 ~ 43 'ggtt'f p4Q g) CN i.c '.
(KS( 1((.46) (( $ '('( 4 (.O<y,= ( 55 f22= 3 .082 Q dsa~ .072574 dsr= 3.7607E+7 ($
dbten= 4.86759E+9 I~ (L5B ( H.r+ z((w( o+a(r)/zs.='(1'(zK~~
glc(i,j)= j=-1.04 3 fcdr= 240 013 siga=
si gb=
5250.28
'029.99
~
I
~~ s5 ~t cvL,~dtj to T3= 919.516 Cw~e~~
Fc due f 1=-440 516 1
f 22= 943.322
~
Q,p-w(a Q( ~ d/>4/ss
~rJ /D' Rc.a= 2 O'R (r'R4i=+7
'I 00((
Ot(
/ . j 1 Calculation 2
B r a k Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project Sublect Sys<<rnCSP WPPSS 30" Analysis No, Mechanical Butterfly and CEP 361104 Va'ives E ui Rev. No.
ment ualification Prepared By:
Checked By:
No.82044 Sheet No.
g 4
~
~
J E. Rakowski 3 =C3 Date Deke'ob File No.OS 1 10 83 plop CH SCK TSVSit E. S>RESS CAt.c S:
4'c( I54 -,LQ < y~o WI 0> OK 4c 3ZX 5z'2 5t 6QQ (00)
's = ~t> Fc z.w lies + zz.z tlat QOQO tr g QH Ect<:
F~~I yI ZE 2 'lkdgIZ eh) k l+
ld5 Nlyck ek)Z yk'$.5 +kCgLecf edc5.25 (IC BIZCBCJ +>'t9+I<>h X5 + Z1/ IIIBLklg (J J tt Q
$ 04$ yp QQ5 0 O tc Choct-usto~s e F coact casE c&p -V-yh-I, WigRtt r'TFES5 s5 OH Ph a~ CHe c((
Z. g C+ VAa <Sa.,t~v~ptjtj 6 S~k-sS ccAp~gauVS ~p'aC.
BE A 4t N r- PWm g LE, ~BOWS l.Vo~ adown )
GgtVQ Qb 5YLt=5S t=HE.t=KS (H0't 54lttmi~t )
. 5'. BOi-t <SHS<Og CSeCWS (POZ gH ttJy) 2000 00
I" 1
~ '
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIII$
"'"'bH39-lJ P "z.
Prepared Byf Checked By g . J~ Date Date j
Sub jec iP,i "c-'iiicI i.doZw giE System Job No.
~ GZ Analysis No Rev. No.
~ @ +
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5.0 APPENDICES TO REQUALIFICATION ANALYSES
SECTION 5.0 APPENDICES CONTENTS 5.1 ""'Response Spectra 5.2 Walkdown Sheets 5.3 Valve Local Coordinate Systems 5.4 SRM Sheets 5.5 Revised Aurns and .Ro'e:
~ Pipina Analysis. Accelerations 5.6 Load Comparative Sheets
5.1 RESPONSE SPECTRA I
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Mf'PSS RERCTI3R BLOG. SRSS QF SRV SSE FIP/CHUG.!
Hfhss, NCl. 182 EL. 500 CCiNT Hr NtlENT VESSEt .. FT. HClRIZ. TRRNSLATIGN DnVP I NG= . OOS, . OS, . OZ, . OV
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5.2 WALKDOh& SHEETS h
EQUIPMENT UALIFICATION VALEDOWN VERIFICATION FORYi c
i \ ZPNg'St'-K- l llllli!!lllitlllll!!!!'!l!llll QIDf ( ll 0 {
BLDG FLOOR ZL QO) COORDS W.~ . (o MFR QZ F COMiPONENT ZL 5 O ~ DSCRP 04 FLY MOD ~r.
2.0 tD t~~ SERIALS PS I 8 oF LBS SIZE
'Br ASME CLASS YOKE ORIENTATION MOUNTING CONDITION TO AXIS OF PIPE ( ) NO OF BOLTS
// TO AXIS OF PIPE ( )
BOLT TYPE WELD TYPE 6 SIZE BOLT YOKE LENGTH (FLANGE TO FLANGE)
PIPE MOUNTED YES( ) NO ( )
PER?~ENT OBSTRUCTION (WITHIN 2") YES( ) NO( )
FULL(6WAY) ANCHOR BETWEEN COMPONENT 6'RI CONT YES( ) NO( )
ATTACHMENT JOB NO.~S~
F)i.S NO.~5D( F SHSSINO. < I' GLOBAL CO-ORDINATE VALVE .STEYi. ORIENTATION SYSTEM PERATOR EPN MANUFACTURER ODEL NO SERIAL NO'RDER YPE SIZE r NO OTOR ZPN MANUFACTURER ODEL NO SERIAL NO D NO INS CLASS I-PHASE ( ) 3-PHASE ( ) AC DC COMMENTS: Definition '(N/F = Not Found)
G'~rcccr (" ceo( I~ Si Ifcci cc5 of gcl l c( F~ ~
g(Sc g )/ls7an(.zdsaefrlb4 f)E)QP()~E)3 ~hkElhz)'ixAPI ~~ m J~CUs gdsA~":.
PREPARED BY cP DATE~VI)1(1REVIE)c)ED BY DATE~
( SI NATURE) (SIGNATURE)
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Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project 1'z Prepared By Checked By Date Date EQUrk OAL.i System Job No. File No.
~r ~
AsslysisNs, Rsv.Ns. Sheet No.
g~Q~r .r~~ '20 fA BI sy'," ](
I I ~g'. fr or] ro "ry"J I ~
~~'!
QSP- 1-i )Z. ~gp gi fYJ)
(
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ri L rsj Jlr:V(9-9)
ATYACHViEM7 JOB NO.~~<~
RLENO.~<.F SHEET NO. ~<~
~= 7' esP- v'-~
C5P- v'-2 Beer yorg /igirJ A-A PIED SKErsrJ(FDS yrJ< FrrysFosE oF bsysreririo oFErJ4yoz ogrorJys lorJ o~cyJ
'l 005 OO
E UIPMENT UALIFICATION mow ~ a VA r~
WALKDOWN VERIFICATION FORM ch b'C=( 'F
'IIIIIIIIIIIILIIIIIIIIIIIIIIIII OIDg SC, Lt 0 t BLDG FLOOR EL SD( COORDS ~. < l 7 '(
MFR g3. f- COMPONENT EL 5Og DSCRP 0 'F(-Y MODf Q - Zcb(o+~3 SERIALS MAT'L PSI 6 oF LBS SIZE ASME CLASS YOKE ORIENTATION MOUNTING CONDITION J TO AXIS OF PIPE ( ) NO OF BOLTS
// TO AXIS OF PIPE ( )
BOLT TYPE WELD TYPE 6 SIZE BOLT qI YOKE LENGTH (FLANGE TO FLANGE)
PIPE MOUNTED YES( ) NO ( )
PERMANENT OBSTRUCTION (WITHIN 2") YES( ) NO( )
FULL(6WAY) ANCHOR BETWEEN COMPONENT 6 PRI CONT YES( ) NO( )
ATTACHMEÃ7 JOB NO.
Raa VO. >>'<.<
SHEET NO.
GLOBAL CO-ORDINATE VALVE STEM ORIENTATION SYSTEM PERATOR EPN MANUFACTURER ODEL NO SERIAL NO YPE SIZE e ORDER NO OTOR EPN MANUFACTURER ODEL NO SERIAL NO D NO INS CLASS I-PHASE ( ) 3-PHASE ( ) AC DC CPI(RENTS: Deiinitiori '(N/F = Not Found) )-)
@ 4WCT'IO4 ~0M'<lZ~IM,WLT %45, f g~ f4ggg Igg~4~~
~
)O PREPARED BY g: gA cK i
(SI
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v(.8 J NATURE) e.i p/(pter DATE%(1))LREVIEHED BY J'ATE~/g (SIGNAT RE) /
gT uC z/g (6bh.
Calculation Sheet IIIIIIIIIIIIIIIIIIIIIIIIIIIIII Project
/ 'fz Prepared By: Date Checked By: Date EQUiP. gAL.r System Job No. r File No.
~ ~
y AoetyoeMo. Rev.No. Sheet No.
grQ+r g~y s
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ATTACHMENT JOB NO.~tJo File J40 ~o.r SHEEVNO. E e 7' CSEE. v'-/
.est-d-z BKL J JOy J VyeyJ A-A f JE 6 SEE7deriy.oz 7eJE DJJ2DoSE oy= JJEDyE7yyJ& oD&47oE oEyEyJnq,yo J ooyoeJ Jooe oo
1 PAGE I OF -I E UI PMENT QUALIFI CATI ON WALKDOKN VERIFICATION FORM IlllllllltllllAllllllllllllll EPNk CE, V' 8 1 QID f 3 (.ll O BLDG FLOOR EL cooaDs ~(
MFR COMiPONENT EL oscar 30" 6 6 MODE 4 -2.O(oWE SERIAL4 +72 39 5 MAT'L5 A - 5 ~{- - 6<
( 5 PSI 6 h'(O aF LBS Nr ( . BI ZE StD ASME CLASS YOKE ORIENTATION MOUNTING CONDITION J TO AXIS OF PIPE ( ) NO OF BOLTS I A TO AXIS OF PIPE ( )
BOLT TYPE V(t & BOLT 0 ~f5 WELD TYPE 6 SI ZE +I YOKE LENGTH +~A (FLANGE TO FLANGE) MOUNTED YES (vf NO (
6'IPE
) 4 AC Q~
PERlY&ANENT OBSTRUCTION IS COMP BETWEEN CONT &
(WITHIN 2" ) YES (
IST ANC. (FULL 6
) NO ( K WAY ANC) YES ((rs. &(0 ( )
DO MULTIPLE SUPPORTS EXIST BETWEEN CONT & COMP YES ( ) NO (
CVGV LjJ ATTACHMENT 9oa'r JOB NO. ~
FLENo. o~'l-F SHEH NO.~ ~
X GLOBAL CO-ORDINATE VALVE .STEM ORI-Ebl TARPON SYSTEM PERATOR EPN MANUFACTURER ODEL NO SERIAL NO YPE SIZE ORDER NO t
iOTOR EPN Y~UFACTURER ODEL NO SERIAL NO D NO 1-PHASE ( ) 3-PHASE ( ) AC DC COMMENTS: g Ll~i7 ~~'44$ R) DFAS- gPg~s - a0 t~v~
(4 8d: fed 3loo Q aaufa t @at': '0 as aa Ctt rrl )S E: Q R j of/5'loD PFKPARED BY DATE +/(<((LREVIEWED BY DATE ~/
(S GNATURE ) {S NATU E)
TM tta Pv I C LIAM
I PAGE 3 OF E UI PMiEN T VALIFI CATI ON ViALKDOhN VERI F I CATZ ON F Oui IIIIIIIIIIIIIIIIIIIIIIIIIIIIII EPO CE I'-V- 2 0 I
aIOg 3(' i'0 BLDG g- FLOOR EL ~ )F cooaos S 'l 5';f MFR P)g F COMPONENT EL SSF oscar 3o ' 8wfl MODE C)G5 +
PSI 6 7 IO 'F SERIALS +>Q ( ) MAT'L Q -5'I(-
I) I=
I.BS SIZE ASME CLASS YOKE ORIENTATION MOUNTING CONDZ TION J TO AXIS OF PIPE ( ) NO OF BOLTS o/p BOLT TYPE H A 'OLT ~/"
TO AXIS OF PZPE ( )
q)
WELD TYPE 6 SIZE YOKE LENGTH QI 6 (FLANGE TO FLANGE) PIPE MOUNTED YES ( +) hO ( ) L(W- (l s g
PERMANENT OBSTRUCTION (WITHIN 2" ) YES ( ) NO ( )
IS COMP BETWEEN CONT & IST ANC. (FULL 6 WAY ANC) YES
( L) NO ( )
DO MJULTZPLE SUPPORTS EXIST BETWEEN CONT 6 COMP YES (W
( ; NO ATTACHMENT JOS NO. qDoV FILE NO.
SNEEVNO. </ILREVIEWED BY DATE (SIGNATURE ( QNAT )
5.3 Valve Local Coordinate Systems CSP-V-l CSP-V-2
Aim Qpz@voa CSP'-V-~ 2.
/ ~
decsge~~<
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!- =
ufw~i fp.sPA-RED g r FEUDS~ lb px gf/PS N
CV~'N4 ATt ACHViE~JT
/ 'Og;,io. ~lr'ioe FILE Ã0.
SHEET MO. ~ ~ ~
Sudan.
>,.=..its Cos 4~~ = ,41Q7.
>r~z-= gO sos -- -IJa-=-
~ >> F
~ &jgg = /8h 8b5 4~~ = - d,.7Q7,,.
&~- .<g. 805 4~g = 5.7d7 4~~= y9S'. M5 4~ C),70'7
~v~ =.W~'vz Qg5 4gg 0
= >a~
4s Qd5 Bing,.- 4 V
5.4
SUMMARY
SHEETS uses numbers 43 date/time 02/i0/83 09: 06 function ~N -SRM MASTER EQUIPMENT LIST-EPN COMPOSITE EPN
~SP-V-1 SP-V-i+
C CONTRACT MFQ SERIAL NUMBER
-20 7h DESCRIPTION 30" B Y CONTAXNMEN ISOL VALVE LEVEL EC SAFETY FUNCTION ACCURACY iiF d.
R A 4320 5
A/E DRAWING D5 ELEV DETAIL ZONE R43 ROOM S KIS. QUAL ENV. QUAL QUAL STATUS TM QID TEST ANL F/0 C 'GING DBE C SEIS ENV Q1 0 E. 07 ghfi04 MES AQE c
TITLE pREPAPkO BYC g.c.
nATE c:sgp DATE ci%<
~os ~O.
o5'.ol. P piiE VO.
p.):St SO. ~~".
user number 43 date/time 02/i0/83 09: 07 function ~X -SRN RASTER EQUIPMENT LIST-CONPOSITE EPN
-CSP-V-2 SP-V- +
CONTRACT NFC SERIAL ICFfBER h8 pygmy -2 6T63 DESCRIPTION 30" BFLY CONTAI NT ISO VALVE
~ St 55 a-LEVEL EC HOURS SAFETY FUNCTION ACCURACY R 4SZO Ba, V l 5 A/E DRAMING E BLDG ELEV DETAIL ZONE ROON Db R ~O N. 5/7. 4 f43 SEIS. QUAL ENV. QUAL QUAL STATUS TN FREQ QID HL TEST ANL F/0 C AGING DBE C SEIS ENV ox o ov a~a,am CVf3ÃA PRO,~e"V TLTlE 5+me~r Q 4.c4 PRCPe"mfa.0
+r~Mea GV'.Z ATE Z%
H~'ÃED 7:
DATE 40B NO
~u.a so.
8!IEET .NO 5
user number 43 date/time 02/10/83 09: 13 function FIN -SRN MASTER EGUIPNENT LIST-EPN CONPOSITE EPN 2MEP-V-1A+
CONTRACT NFQ MODEL SERIAL NUMBER 2 B250 DM0 6-206Y63 27234-3 DESCRIPTION
~ ~ ' ~
user number 43 date/time 02/10/83 09: 13
%unction FIN -SRM MASTER EGUIPMENT LIST-EPN COMPOSITE EPN 2~EP-V-2A 2-CEP-V-2A+
CONTRACT MFQ MODEL SERIAL NUMBER 2 B250 DWQ A-206T63 27234-4 DESCRIPTION 30" AO BLFY DRYi4E L EXHAUST LEVEL EC USE HOURS SAFETY FUNCTION ACCURACY 2 i 3 4320 Bii F A/E DRAWING AE ZONE ELEV DETAIL ZONE ROOM M543 Si3 55S J. 4/5. 4 R62 SEIS. QUAL ENV. QUAL QUAL STATUS TM FREG GID HL TEST ANL F/0 C AGING DBE C SEIS ENV Y P 36ii04 MESSAGE
5.5 REVISED BURNS 6 ROE PIPING ANALYSIS ACCELERATIONS
1 "I
Sub)ecto M. O. 3900 /4000 Washington Public Power Supply Syster..
RECE)g<ED HHP-2 Qualificat ion of Mechanical Pipe I'r of zc )gg3 I
?.'ounte8 Eq uipnent; Forwarding of Informatio n
's ~
CYGNA-RICHLANj3'-:.;
~ i April 29'9'I3 DWn 070 C
I
.; /i 5$ r. L. T. Harrold t Assistant D irector ~
g>
Washington Public Pome r Supply System ~ ~ V~
3000 Georg e Washington Way A~P,CHtv]FNY Pichland, Washington 9 9352 e .".t tention z her. B. A. Holmhc:rcpt
'g.ot.
F!iS N0.~NO.~
F g.5, I
- '!".",. .. Referencess (a) tqPBR-G3-17, Gated 3/16/03. SHRIFT (b) WPBR-83-20, dated 4/12/83.
(c) WPDR-83-29, dated 4/12/83. ~
It
'3 i
'(1) Telecopy, B. A. Holmberg to
~
J. 8. Verderber, dated 4/4/83 A GentlerLeni Zn response to the request of references (a) > (b) < (c) and (d), this letter is for:rarding refined valveCSPaccelerations.
~ tv The valve acceleration sheets for the five (5) valves Valve,'", ~,,'
~p~ -g p( e..'~.',
represent the second iteration of the refinement task..
~
first w
sheets for the other four (4) valves represent the iteration of the refinement task. Please inform the Rmdhury~.",:.: 't
~4 Office further.
if efforts should be r."~de to reduce accelerations hl very truly yours,
, ORIGIN;L ~IG~Ico ov ). 3.x rsDER>EIr
~
~
PM/es Zohn Z. Verderber Pro)crt Engineering Manager CC: Mr. W. S. Chin - BPA 1 ~r/1 QHr. V. E. Rhodes - tH'PSG 1 >:/1 lg P. Buck - t'PP"S - l ~./1 .'lail Drop ."r75.
ATTACHMENT Data forwarded with DRWP-83-078, dated April 29 > 1983 Valve Kale. No.
P-V- 125 8.14.129 SP-V-2 '~ 125 8.14.129 CSP-V-3 125 8.14.129 CSP-V-4 125 8.14.129 CSP-V-5 125 8.14.129 RCIC-V-31 107'1 8.14.112A RHR-V-17B 8. 14...121 RHR-V-53A 29 8. 14. 62C RFI R-V- 5 3 B 31 8. 14.121B ATYACHPAEi~.'7 JOB NO.
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t 6.0 DRAWINGS USED FOR REQUALIFICATION
6.0 Drawings QIDO 361104 DRAWINGS SUBMITTED TO SUPPLY SYSTEM IN ORIGINAL PACKAGE A-206763 Rev F A-206767 " C D-220-0310-IR-66 Rev 0 C-26095 D-207110-F CEP-625-10 '
2 Rev 5
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7.0 PRIOR CALCULATIONS USED FOR REQUALIFICATION
7.0 TRANSMITTAL, PRIOR CALCULATIONS AND REPORTS CONTENTS 7.1 Communj.cation Reports 7.2 Original Requalification and SQRT Forms 7.3 BIF Report: Dynamic Torque Calculations of Butterfly Valve
- 7.4 McPherson Associates Report:
Design and Seismic Analysis of 24" Cylinder-Operated Butterfly Valve *
- Note: Excerpts from report included in specified section. For complete report, see Cygna Energy Services File No. OS.01.F, QID 361104, "Equipment Seismic and Hydrodynamic Requalification of 30" Cylinder Operated Butterfly Valves," Revision 1, June, 1983.
7.1 COMMUNICATION REPORTS Memorandum LM'j Q Project Memo No. 14B IIIIIIIIIIIIIIIIIIIIIIIIIIIIII W. Schlafer oete: November 1S, 1982 R El VED P. Guglielmino/J. M. Foley Job No: 83015 NOV 1'I 158?
Subject:
c opies: T. Wit tig
~CYGNA-RICHLAND The above QID's have been revised to include the effects of the following:
- 1) Dynamic Torque due to Containment Backpressure Effect (TCB)
- 2) Dynamic Loads Sg, Sg and 3'g, two horizonta 1 and vertical.
- 3) Seismic Loads.
results and recommendations are outlined below. A~ACHMENT The A. QID No. 361106 - 24" Primary Containment Butterfly JOB NO.~
Q.o/4 NO.~
oS.ol F Isolation Valves. PILE
'7.(.l EPN's: CSP-V-3, 4. Fail Close SHEET NO.
CEP-V-3A, 4A Fail Close, CSP-V-S, 6, 9 Fail Open ')
Maximum Dynamic Torque result from BIF Report No.
TR-27234 is 11,691 in-lbs. for the air flow analysis
~
and 11,379 in-lbs. for the steam flow analysis.
These valves are lower than the design seating torque value of 17,000 in-lbs used in the original McPherson Associates analysis report No. TR-74-7.
- 2) Stresses due to Seismic and Dynamic Loads are within the material allowables and satisfy the requirements of the AISC Code, Appendix B, for fatigue evaluation.
(Fatigue evaluation applies only to EPN CSP-V-9 which i s subjected to Hydrodynamic loads.)
- 3) Results of the stability analysis for both the
'close and fail open valves are as follows:
fail a) Fail Open Valves (CSP-V-5; 6; and 9).
The current fail open design using a 100'/in spring with 3508 preload will not be stable in the open position. The spring preload should be increased to provide stability for the open position.
However, if theopenpreload stabilize the is increased enough to position when subjected to seismic and dynamic torque conditions, the corresponding final spring load will be too great to allow proper seating with the 70 PSI air supplied to the operator. It is recommended that the spring preload be increased to approxi-mately 16508 and that the supplied air pressure be increasecf to 95 PSI.
b) Fail Close Valves (CSP-V-3; 4 and CEP-V-3A, 4A)
The current fail closed design using a 1008/in spring with a 15008 preload will not be stable in the open position. This occurs because almost all of the load exerted by the 70 PSI cylinder operating pressure is required to com-press the spring t'o its-.final load of 30008.
PEPSI The additional axial load of 1244 lbs. due to seismic and dynamic torque will cause the valve disc to flutter. However, the full 15008 pre-load is required to seat the valve closed, the spring load cannot be reduced. Therefore, we recommend the air pressure be increased to 85 to stabilize the disc in the open position when subjected to seismic and dynamic torque loads.
QID No. 361104 30" Primary Containment Butterfly Isolation Valves (Fail Close)
EPN's CSP-V-1; 2 CEP-V-1A; 2A
TR-27234 is 23,099 in-lbs. for the air flow analysis and 23,171 in-lbs. for the steam flow analysis.
These valves are lower than the design seating torque valve of 27,800 in-lbs. used in the original Dynatech analysis report No. 1351, Rev. 1.
- 2) Seismic Stresses were found to be acceptable.
Fatigue analysis was not required since the valves are not subjected to hydrodynamic loads.
- 3) Stability analysis for the fail close position showed that theses valves experienced the same stability problems as the 24" fail close vali (See discussion above)
ATTACHhl Ebf 7 JOE NO ~fio FILE NO Otto.s ENEET NO. ~l-t
The above results and recommendations are based on the assumption that stability is defined as no motion of the disc in either the open or closed position due to seismic, hydro and dynamic torque loads.
ATTACHMENT JOB NO.
FILE NO.
SHEET NO.
Washington Public Power Supply System P.Q Box 968 3000George Washington Way Richland, Washington 99352 '(509) 372-5000 December 17, 1982 GE-02-RWH-82-018 Cygna Energy Services 141 Battery Street Suite 400 San Francisco, CA 94111 Attention: Mr. T. Wittig, Project Manager
Subject:
NUCLEAR PROJECT 2 CONTRACT C-0892 Investigation of the CSB and CEB systems shows that during a dynamic event the systems are not degraded in any way by the butterfly valves fluttering. Therefore, all work on Work Release Nos. 14 and 17 which address valve stability should be terminated.
R. W. Hickman - 575 Senior Engineer, Equipment qualification RWH/sms cc: F. Khanachet, Cygna Richland JOB NO Fil.E NO ~~~
R ECEl VED SHErr No.~~ ~
Ltr-C r-2 1982 C YG!~A-RICHLAND
Communications
~'j 3b. rid Report llllllllllllllllllllllllllllll Company: Telecon 0 Conference Report C5S )0 Project: Job No.
Date:
N PPo~
Subject:
Time:
Place:
l t- t.V K I QC, Stab) 5
Participants:
Cf>- 54<
StfC-of Item Comments Req'd Action By 2./ (ol s's F~ f SIP .YAGA6 FLAVORS plMFN Sioux, u
4'5 l.~S l .d. '5t
- o. > 8.1S NO.~
F08 r>LN No.~
SNSSr N0 ~
Q.o l DI. ~
1.(.C'igned:
f Page of Distribution:
1020.00
Communications Report lllllllllllllllllllllllllllllr Comoany., Telecon o Conference Report CE S Protect' Job No. 82044 WNP-2 Eauittment ualification Date:
4
Subject:
Time:
Weld size at Valve Flange/Ear Interface Richland Participants'on CES /RBO
.Searle Rick Rica oito BIF 401-885-1000 of Item Comments Req'd Action By Requested and received information concerning t e attachment of the rectangular shaped "ears" to the valve body flanges'.
Rick informed me that all of these items were af-fixed to,the valve flange by means of welding.
a) 0.31".fillet weld three sides b) 0.31" "J"/Groove weld on side flush with flange face
Reference:
BIF Order No: PN27234, PN27235 BIF Assembly Drawing,: A-206767 VOE NO.~>~
FILE No.
IIO.
ds.or.e'HEET
'I (.s SIgnec'age SC& OL T.
Project Wittie. F. Khanachet, D; Armstrong, K. Scott R. Hickman, Fi1.e PP)'"Beax3L,. Or ice Fz e of ]
7.2 Original Requalification and SQRT Forms NUCLEAR PLANT VfPPSS Eb I 0't I
UNlT 2 SEISMIC ANO HYOROOYNAMIC LOAOS RE(UALIFICATION CERTIFICATION JOB NO. 2808 E(UIPMENT NAME: 30" Cylinder Operated
'Butterfly Valve
'PFC. NO: 68 EQUIPMENT. NO: CSP-V-l, 2; CEP-V-1A, 2A .
LOCATION: Reactor Bldg. Elevs. 508'0" 508'0" 562'0" ~ 558'0" EQUIPMENT CLASSIFICATION: Q ACTIVE 'C1 PASSIVE
~
SEISMIC QUALIFICATION REPORT
REFERENCE:
- 1. Seismic analysis of 30", cylinder operated butterfly valve.
Report No. TR-74-8 (Rev. 1) dated 12/31/75 by McPherson Assoc./BXF
- 2. Dynatech project No. BlF-14 deflection analysis of butterfly valves by Dynatech R/D Co. 4/12/76 Trans.13B THE ABOVE SEISMIC QUALIFICATION REPORT(S) HAVE BEEN REEVALUATEO ANO RE(UALIFIEO WHERE NECESSARY.TO SHOW THAT THE ABOVE-MENTIONEO COMPONENT
'S CAPABLE OF PERFORMING ITS INTENOEO SAFETY FUNCTION UNOER ALL THE APPLICABLE LOAOING COMBINATIONS INCLUDING THE POOL OYNAMIC'OAOS.-
PREPAREO:
APPROVEO:
OATE:
~ ~
nutech San Jose, California p t WNP-2 File No Washington public power Supply System Washin ton Public Power Su 1 S stem Tag No. CSP-V-l, CSP-V-'
CEP-V-1A
. CEP-V-2A Class I, Active 30" C linder 0 crated Butterfl Valve A~1 ACHPAFNy Original qualification'ethod 'OB NO.~o~
A. Equivalent static. analyis rff.fNQ. OS.of.f'HEET ffP. f.Z. 2 Reevaluation A. The natural frequencies were not calculated.
B. Valve operability was 'frerified by'eflection calculation.
C. Calculated stress margins are within allowables.
RRS not used, but seismic coefficients used in the analysis envelops the interim SQRT criteria.
E. Loads combined by SRSS method.
III. Conclusion A. The 30" cylindeq operated butterfly valve does not comply with interim SQRT requirements.
l
- 1. The natural frequencies were not calculated IV. Recommendations A. Analyze valve to SQRT requirements.
I V. Comments on original analysis A. The horizontal acceleratipn used were for SSE 3g in orthogonal direction and vertical, combined using SRSS.
'shr'af B. The natural frequencies were not calculated.
C. Maximum critical deflection was 0.104 in. vs.
0.50 in. allowable.
Revision 0 o 1 Prepared By/Date of 1.
Checked By/Date
t ~ Tag no . CSP V 1 CSP-V-2
'CEP-V-1A CEP-V-2A ualification Sugar of E ui ment I. Plant Name: ~T)e:
1'. Utility: Washin ton Public Power PWR Supply System ~~
2 NSSS: GE A/E: Burns & Roe BtlR 5, Nark XI
- 3. Vendor: HcPherson BIF
- 4. If the component is a..cabinet or'panel, name and model No. of the devices included: N/A 5.. Physical Description a. Appearance 'alve
- b. Dimensions
- c. Weigh>> 321 lbs.
- 6. Location: Building: R evation: 508'0", 508'0", 562'0", 558'0"
- 7. .Field Mount'ing Conditions [ J Bolt (Mo. , Size . )
Containment Supply Purge System
- 8. a. SyStem in WhiCh lOCated: Containment Exhaus Pu v Drywell Exhaust,
- b. =
Functional
Description:
Containment Isolation c., Is the equipment required for f g Hot Standby f 3 Cold Shutdovi.".
f3 Both '
3 Neither
- 9. Pertinent Reference Design Specifications: 2808-68 Prepared by:
3/81 Checked by:
~ton%
O FlLBNO ~05 BNBBTNO ~t
I v ~
~ ~
III. Is Equipment Available for Inspection in the Plant: P.g Yes f3 No IV; Equipment /uglification Nethod:
[ 3 Test QQ Analysis f3 Combination of Test and Analysis 8aallfitation Report>>: contract 68, Transmittal 24 Report No. TR-74-8 (Rev. 1) 12/31/75, Seismic
~~~5 ~38" C+~ex.J3geraLad Butterfly Valve Company that Prepared Report: NcPherson Assoc/BIF Corpany that Reviewed Report: Burns a Roe/NUTECH V. Vibration Inpu-:
- 1. Loads considered: a. fQ Seismic only
- b. 5 3 Hydrodynamic only c- [ 3 Combination of (a) and (b) 2~ Nethod of CorMning RRS: f. 3 Absolute Sum fg SRSS /XI N/A
- 3. Required Response Spectra (attach the graphs): Attached
. 4. Oar>>ping Corresponding to RRS: 08= SSE
- 5. Required Acceleration in Each Direction: f. g ZPA F3 OtherAttachmentl .
. 08E SSE S/S ~
5/5 E-N
~ 36g F/B ~~ww&wHw~&&~>>>>w'ww& Y=
F/8 ~A~&&
N-S
~ ~~%& os
- NOTE: . If more than one each report.
report complete items XV thru VII for gyp,4A CHgEQT goB gO.
n( ~0 ping NO.
sHa~ No
I I
~ IW
\
3 If gualification by Test,'hen Complete Nods}
f 3 random
- l. f. $ .Single Frequency [ ) Multi-Frequency: [ 3'sine beat
[3
S~~
Frequency Range:
- 5. Natural Frequencies in Each Girection (Side/Side, Front'/Back, Yertical)-
S/S K
- 6. Method of Oetermining Natural Frequencies f 3 Lab Test . f. g In-Situ Test 5 3 Ana1ysis
., S. Input g-level Test: OBE S/S =
SS~ S/S Labora ory Po"nting:
- l. [ ] Bolt (Mo. ~ Size '
[ ] Meld (Length } [J
- 10. Functional operability verified: [ 3 Yes [ 3 No f 3 Not App1icable
-ll. -
Test Results including modifications made:
- 12. Other test, performled (such as aging or fragility test, including resu1ts):
1
<<Note: If qualif',ca-'.on by a combination of test and analysis also complete Iten' I I.
CVGMA 12/8Q ATTACHMENT doe No.~zoo RLS NO.~S'HEST NO.
If gualification \&&&'<<<<&~\WW'W'W&W<<W~W YII. ~W<<<<W~W<<WW~%& by Analysis, then complete: <<<<~~
- 1. Method of Analysis:
5 ) Static Analysis f: 5 Equivalent Static Analysis 9I =39' =.29 j 3 Dynamic Analysis: @me-His&ry v'..3 5 3 Response Spectrum
- 2. Natural Frequencies in Each Direction (Side/Side, Front/Back, Yer".ical)'/S
~ F/B ~
%&A&%%%WA<<<<~&&&&<<
- 3. Model Type: C 3 3D I: g 20 531D I. ) Finite Element 5 3 Beam (zan Closed Form Solution
- 4. I g Computer CodeS: ~ 0% &~ &~ &&~ <<None W ~ I<<W ~ ~ <<W W Frequency Range,and No. of modes considered:
I." 3 Hand Calculations
- 5. Method of Combining Dynamic Responses-' 3 Absolute Sum [, ) SRSS
[ l Other:
Qs p Qc17y]
- 7. Support Considerations in the model:
- 8. Criti cal Structural Elements:
A. Identification Location Governing Load or R s ponse Combination
'ei smi c Stress T otal-Stress Allowa"le tzas s Valve Body 17,796 18,000 psi psi Maxirum Allowable Deflection B. Max. Critical to Assure Functional Opera-Deflection Location bility O.l04 in. Disk 0<<500 in.
cyoggL, g TTp,CHI)lf.'HT 3/&l
~ ~
I 1
~
~
~
Attachment L Stat'c Seismic "6" calculations (Stick .'towel)
OBE Level, L/2% C=i"ical Caapina, "" quenc.r cue-o and above SSE Value ~ " v OBE Va ue Suildir.a Area Eleve tion (= t. )
Horizontal CSE, e Ho SSEi i ontal Ve ticaL C3K, Vertic GS=.
Reactor 653+* 1.25 1.00 Huildinq 567 547 58
+57 l2.50Lo L.00 2.00 Z.QO 8 z~
~
52l 500
.57 68 l.'4
~L +3
.a7
<<6>>
- l. 74
- l.36-47a'43 ~ 80 l,.60 60 L.Zd
~ 87 74 60 L.ZO 434k+ . 1.00 "
2.00 .40 .80 Diesel Cen. 414*4 1.00 2.00 40 .80 "LO Hz/L9 Hc 472 3.5/.60 7 0/l 2. Z 6/L.6 5. 2/3'-
454 3 2/.70 64/L4 1 5/0 0 0 /'0 437 2 2/ 90 44/LZ 2 4/L.L 4.S/2-Radvas e
+8 Hc/LO H 54L 524
- l. 5/l. 5 L l/L.L 3 0/3.0 202/%42 2
L 0/L 7/.3 4.0/2.:
3.4/1.<
500'66 lL.l/
0/65 60 2.0/L.3 2 '/l.3 S/.65 L.7/.50 3.'6/L-
- 3. 4/L
.'t]S
'7 R=c~ar 492'-LL 5/8" 3 2 3 2 3ui,lding 80'-4" 3-2 3.0 L.3
+~macy 467'-S" 3.0 .IZ.3 ~
l,.3 Con~e
<<8 Hz 455'" 4-0 3.0 L.3
<<*From eleva 'sat additional S
(by NuTech)
ATTACHMENT JOB NO. ~~'<<
FlLE NO. 09 n( F sHEEv N0.~7~
7.3 BIF REPORT: DYNAMIC TORQUE CALCULATIONS OF BUTTERFLY VALVE
B IF A UNIT OF GEl'lERAL SIGNAL 1600 DIVISION ROAD WEST WARWICK'. I 02893 QUALIFICATION OF PRIMARY CONTAINMENT BUTTERFLY ISOLATION VALVES.
UNDER LOCA CONDITION DYNAMIC TORQUE CALCULATION OF BUTTERFLY VALVE r
PREPARED FOR:
WASHINGTON PUBLIC POWER SUPPLY SYSTEM VALVE SIZES 30", and 24" WPPSS CONTRACT NO. 68 -- -*-
BZF ORDER NO.: PN27234 & PN27235 WPPSS IDENTIFICATION NO. CSP-V-1 & 2, and CSP-V-3 & 4 Prepared by: Debendra K. Das Date: He v ~ l0 l 'I 6 2.
Checked by: Dezso Szila vi Date. ~u', /o. l9Q.
REPORT NO. TR-27234 And TR-27235 o~q RLE Na. OS. Oi.T SHEET HQ.
TM3LE OF CONTENTS SECTION PAGE
- 1. Summary
- 2. Dynamic torque tables 2
- 3. Ref erences
- 4. Analytical Procedure and Flow Data
- 5. Analysis for 30 inch valve (I) a. Hand Computation of several test cases for air flow 25
- b. Computer results and comparision with hand computation 28 (II) c. Hand computation of several test cases for steam flow 40
- d. Computer results and comparision with hand computation 42
- 6. Analysis for 24 inch valve (III) e. Hand computation of several test cases for air flow 53
- f. Computer results and comparision with hand 'computation 55 (IV) g. Hand computation of several test cases for steam flow 67
- h. Computer results and comparision with hand computation 69
- 7. Appendix 80
- a. WPPSS Calc.No. ME-02-83-08-0, Sheets 1 thru 9
- b. LOCA Temp. Curve
- c. LOCA Pressure Curve
- d. MPPSS Letter dated 10/22/82
- e. BIF Flow Loss Coefficient K plot .
IHKE7 t40.
This report contains the dynamic torque analysis of two butterfly valves of sizes 30, and 24 inch. The analysis is performed for LOCA (loss of Coolant Accident) per WPPSS Specification, reference 1 on page six of this report. The analytical procedure and the assumptions are outlined in the section beginning on page seven.
Dynamic torque calculations have been performed for two media, namely; air and saturated steam for various angles of opening of these valves.
The results of the analysis tabulated on page two through five I
of the report indicate that the dynamic torques developed under the specified flow conditions are less than the.design torques used in the. original Seismic and Stress analysis of these valves. Therefore 8I I
the valves are safe against the action of dynamic torque in the event'f a LOCA.
~ = ~
SUMMARY
OF RESULTS Table 1 30 Inch Valve, airflow degas TDJQe Angle W Dynamic 8 Torque in-lb 1.0 90 (Full open) 11020 1.5 78.75 23098 2.0 67.50 18138 2.5 56.25 14747 3.0 45.00 12428 3.5 33.75 10780 4.0 22.50 8014 4.5 11.25 3972 5.0 9. 0 (Full closed) 0.0
- TNet= 22174 in-lb
NOTE: The design torque used in the Seismic analysis report No. TR-74-8 by McPherson Associates for this valve is 27800 in-lb. Therefore the design is safe.
SUMMARY
OF RESULTS Table - 2, 30 Xrch Valve Steam flow
=
Time Angle W Dynamic S degas Torque in-1b 1.0 90(Full open) 11032 1.5 78.75 23175 2 ' 67 50 18142 2.5 56.25 14668 3.0 45.00 12424 3 5 33.75 10580 4.0 22'. 50 7809 11.25. 3867 5.0 9. 0 (Pull closed) 0.0 * ~
TNev= 22174 in-lb
Al i ACHQKSY 405 m ~>o~q RLE NO.
SHEET 40.
SU~y OF RESUI TS
- Table - 3i 24 Xnch Ual ve; Air flow Time Angle c4 Dynamic 8 degas Torque
'n-lb 1.0 90(Full open} 5525 1.5 78.75 11692 2' 67.50 9095 56.25 7428 3 0 45.00 6239 3.5 33.75 5430 4.0 22.50 4043 11.25 2020 5.0 9. 0 (Full cloyed) 0 0-* TNet= 13808 in-lb At full closed position the dynamic torque is zero and the net torque is due to seating and bearing fric ion.
Note: The design torque, used in the Seismic analysis report No. TR-74-7 by McPherson Associate for this valve is 170(gin-lb. Therefore the deisgn is safe.
h
~ [6 I 1:) ~
~ ' . 4 Ok i 40 't
SUMMARY
OF RESULTS Table 4 24 I'nch Valve, Steam flow degas Time Angle c4 Dynamic Torque in>>lb 1.0 90(Full open) 1.5 78.75 11394 2.0 67 50 8921 2.5 56. 25 7213 3.0 45. 00 6109 3.5 33.75 5202 4.0 22.50 3842 4.5 11.25 1902 5.0 9. 0 (Full closed) O.0
CYGNA AlÃACHMEST
~ tto ~209q RLC ttO.
SHEET ttO T.
REFERENCES WPPSS Specification 2808-68, Calc. No. ME-02-83-08-0, Sheets 1 thru 9, dated 10/8/82.
LOCA Temperature Curve Fig. 6.2-2.
LOCA Pressure Curve Fig. 6.2-3.
- 2. ANSI/AWWA C504-80, AWWA Standard for Rubber-Seated Butterfly Valves. American Water Works ASsociation, Colo.
- 3. Beard,C., Final Control Elements, Valves and Actuators, First Edition, Rzmbach Publications, 1969.
- 4. Hutchison, J. W., ISA Handbook of Control Valves, 2nd Edition.
'5. 'orque and Sizing Calculation for BIF Butterfly Valves, No. D-214590, dated 1/9/75 for WPPSS Contract 468.
- 7. B I F Test Report iTR-0650-43, Hydrodynamic and Headloss Test of 12" 150 Lb. Butterfly Valve with directIy connected short radius elbow upstream, dated 2/24/82.
B IF Drawings: 30 inch Valve General Arrangement Drawing A-206763 24 inch Valve General Arrangement Drawing A-206764
7.4 McPHERSON ASSOCIATES REPORT:
DESIGN AND SEISMIC ANALYSIS OF 24" CYLINDER-OPERATED BUTTERFLY VALVE
CYGNA ATTACHMENT BIF A UNZT OF GUTTERAL SIGiNAL 1600 DIVISION FILE NO.
HEST HARNZCZ, R IROAD 02893 ..NEEr NO.~7.
DESIGN AND SEISMIC ANALYSIS OF 30" CYLINDER OPERATED BUTTEFZ'LY VALVE r OR-HASHZNGTON PUBLIC POWER SUPPLY SYSTEM --. --*--
AND BURNS AND ROE CUSTOMER P.O, CONT CT'.6 BZF SHOP ORDER 50 PN2 34(U+QSOB BZF g. 34-1 nehru 4.
PPR O. TR-74-S RER8RKQ B~Y McPHERSON ASSOCZATES, ZNC APPROVED i7 79-
~4 hQin~ ~ App~i3 (I sir(;
mq'- ~oPC E(8 00 00<
DESIGN AND SEISMIC ANALYSIS OF 30" CYLINDER OPE A D BUTTERFLY MVE A- 06 66 2 eb a 74 ATTACHMENT Prepared For". JOB NO.
OS.al. F FiLE NO.
BIF SHEET NO.M A Unit or" General Signal Corporation Prepared By:
Thomas M. Riley John R. Henry BIF A Unit of General Signal Corporation Purchase Order No. 84908-63 McPherson Associates, Report No. TR-74-8 ~ L>>~>~)"+
Inc.
McPherson Associates, Inc.
400 Totten, Pond Road Maltham, Massachusetts 02l54 n &~c iMam 400 TOTTEIV PONO RQAO e 'WAt.THAM,MASSACHUSETTS 02l54
SEXSi~fIC A'fALYSIS OF 30" CYLINDER OPERATFD BUTTERFLY VALVE A-206763 4TT~C H MBQ'P Joe OO.~2~
A
'r'j;~
Unit of General Signal Corporation saaNg. >~ ot ~
SHEET NO. >'f >
Purchase Orfer No. 84908-63 McPherson Associates, Inc.
Report No. TR-74-8 mls~<
FOR 30" VALVES.
BIF Contract No. BXF S.O. No. Valve Tag Ho's N 27234-F CSP-V" 1 CSP-V-2 CEP-V-lA CEP"V-ZA
0 REVI SION RECORD NUS REPORT NO. TR-74-8 REYISION 12/31/75 CVGNA Page 3 . a) Haterial was ASTM A-126 5 A-48 ATTACHMENT b) Allowable stress values corrected JOBNO. gee'f I RI.EVO 0 ." F Page 5 a) b)
Drive lever was 8-208217-17 Clevis was D-146578-1 o.2'~
Page 9 a) Hat'I was ASTH A-126, Class C b) . Corrected yield stress allowable.
c) Deleted ASTH A"48 Pages 28 5 30
~
a) Hat'1 was ASTH A-48 b) Corrected al lowable stress (. (
Page 32 Pages 33, 35, 36 a)
Ref. Dwgs. ware b) Corrected I gyV B-20+F7, D-14@78-1 owableg>
TABLE OF COiiTE!G'S Section No. ~Pa e Table of Contents L3. Certification 1.0 Introduction 2.0 Summary of Results 3.0 Conclusions 4,0 References .
{,0 Design Data e 6.0 Analysis lo 6.1 Cylinder Operator Assembly Cylinder Support Bracket 6.3 Clevis Ass emb~
Wd',Drive Lever',
V,$ 'i'~<~ '~ 31 6e4 Valve Body Support ",Ea~rs" an Associated. 38 Hardware Q~
6.5 Shaft and Dis,c Assembly and Associated Hardware 6.6 Valise Si-ing and Stress Analysxs Cons " r ..g Combined Operat'ng and Seismic Conditions
<TTACHhgegy sos No.~eel Fa.a No.
>>aar
<< or No.~4.5 r.
44 ~ ot Certi fication Hctherson Associates, Enc certxfxes that the 30" Butterfly 0 4 Valve, A-206763, as shown on the'ustomer drawings was analyzed in accordance with Nashington Public Power Supply System Specification No. 2808-68 and, to the best of our
')knowledge and belief, meets the requirements of Paragraphs
- 3. 2 3- 3, and 3. 5. 2. 4 of this document and Re fer nce 3 of
> I I
Section 4.0 of this report.
t John R;Henry'.'egistered Pro essi'anal Engineer Hass. egistration No. 25929 ATTACHESPNT voB No.¹~W FlLE NO. ~<+
SHEET NO.Z~~<
1 ~ ~ ~ ~
~
I l~~>>v rs ~
Section 1-0 ENTRODUCTEON
'he purpose of this report is to determine the structural uacy oof a 30" Butterfly Valve Assembly vhen subjected aadeequacy to seismic accelerations as described in Reference 1 an+
to insure the valve design is in accordance with Reference 3
'f th s report.
The seismic plus operating analysis is perfor d in accor-ance with 1fashington Public Power Supply System Specifica-tion Ho. 2808-68, Reference 1, and all applicable informa-t
( tion as described in Section 4.0 of dais report.
CVGM~
ATTACHMENT JOB NO ~S2o I
. FILENO.~I.oI.F
- HEaT No.~~8 Section 2.0 SUMfARY OF RESULTS.
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3.0 CONCLUSION
S McPherson Associates, Inc. concludes that all components for the 30" Butterfly Valve, as analyzed in this report, meet the requirements. of all governing specifications for seismic plus operating considerations as defined in References 1, and 3 of. this report.
l Section 4. 0 REFERE.'ICE S ATTACHMENT gag go ~LDVC FILE NO, 0~ ~<
washington Public Power Supply System Specification No. SHaaVaO. ~~ <<
- 2. BEF Drawings Drawinr No. Revis'n Description A-206763 30" Butterfly Valve-General Arrangement A-900501 Body, F A-900502 hfachining abricated'ody,
'-900499 Disc, Fabricated A-900500 Disc, hlachined A-208l95 Cylinder Support Bracket
~ B-900514, B-900515 Q 2.l>4XQ Operator Sha Drive Lever ts-p a,>i832-~ Clevis D-184100 Hill'er Cylinder Section XIE, Nuclear Power Plan- Components, and Pressure Vessel Code, 1971'ith Addenda.
AS'oiler
- 4. Virgil hforing Faires, Design of Machine Elements Edition, The hiac'fi11an Co., N.Y., 1965.
Raymond J. Roark, Formulas for Stress and Strain, 4th Editionp hfcGraw Hill Book Co.1 1965
- 6. Laddish Catalog No. 5'5-Grinnel, Piping and Engineerin gr'd Edition, 1971.
X ~
~
S. 1963 S pl =en .o Sc. w Thread St ".Bards for Fed .al Services.
- 9. Baumeiste. 5 i~farks, Standard Handbook for hfechanical Engineers, 7th Edition, hfcGraw Hill Book Co.
- d. Ment, Hechanica1 Engineers Handbook.
- 11. A.S.T.i~i. Standards - Part 2
- 12. A.S.ff. ~fetals Handbook
- 13. Timoshenko and Goodier, Theory of Elasticity, 3rd Edition, NcGrav Hill Book Co., 1970.
- 14. Seely and Smi&, Advanced hfechanics of tfaterials, 2nd Edition, John Niley 4 Son, Inc., 1966.
- 15. MacHinery's Handbook, 17th Edition, The Industrial Press, 1964.
\
- 16.Section VIII, Pressu.e Vessels, Division 2, Alternat.ve Rules, AeS.bi.E. 3oiler and Pressure Vessel Code, 1971.
'hemic"'ubber ~ blishing Co., Qt~daru fathematics
~ Tables, 'l'@elf D Zciitione g
) .
Qg e
v',~>CEMENT Joe <Q p[LK NO S~EE~<<
~/LAN of.ot
~~
f9
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7.3 BIF REPORT: DYNAMIC TORQUE CALCULATIONS OF BUTTERFLY VALVE
1 B IF A UNIT OF GENERAL SIGNAL 1600 DIVISION ROAD e WEST WARWICK, R.Z. 0289'3 QUALIFICATION OF PRIMARY CONTAINMENT BUTTERFLY ISOLATION VALVES UNDER LOCA CONDITXON DYNAMIC TORQUE CALCULATION OF BUTTERFLY VALVE PREPARED FOR:
WASHINGTON PUBLIC POWER SUPPLY SYSTEM VALVE SIZES 30", and 24" WPPSS CONTRACT NO. 68 BZF ORDER NO.: PN27234 & PN27235 WPPSS IDENTIFICATION NO. CSP-V-1 & 2, and CSP-V-o e.
Prepared by: Debendra K. Das Date: h3ov ~ 10 '.l 'I 82 Checked by: Dezso Szila i Date:
REPORT NO. TR-27234 And TR-27235 AMiACHMESY
V 4
p, ~
TABLE OF CONTENTS SECTION PAGE
- 1. Summary
- 2. Dynamic torque tables
- 3. Ref erences
- 4. Analytical Procedure and Flow Data
- 5. Analysis for 30 inch valve (I) a. Hand Computation of several test cases for air flow 25
- b. Computer results and comparision with hand computation 28 Hand computation of several test cases for steam flow 40 Computer results and comparision with hand computation 42
- 6. Analysis for 24 inch valve (III) e. Hand computation of several test cases for air flow 53
- f. Computer results and comparision with hand computation 55 Hand computation of several test cases for steam flow 67 Computer results and comparision with hand computation 69
- 7. Appendix 80
- a. GPSS Calc.No. ME-02-83-08-0, Sheets 1 thru 9 b.. LOCA Temp. Curve
- c. LOCA Pressure Curve
- d. WPPSS Letter dated 10/22/82
- e. BIF Flow Loss Coefficient K plot .
SUMMARY
This report contains the dynamic torque analysis of two butterfly valves of sizes 30, and 24 inch. The analysis is performed for LOCA Boss of Coolant Accident) per WPPSS Specification, reference 1 on page six of this report. The analytical procedure and the assumptions are outlined in the section beginning on page seven.
Dynamic torque calculations have been performed for two media, I
namely, axr a nd saturated steam for various angles of opening of these valves.
The results of the analysis tabulated on page two through five of the report indicate that the dynamic torques developed under the t
r specified flow conditions are less than the design torques us'ed in the. original Seismic and Stress analysis of 'these valves. Therefore the valves are safe against the action of dynamic torque in the event of a LOCA.
~)~ ~20O>>.-tV SLED; OS SHEET 40. T
1tttt, ~ P, a ~ t,gt tt N It I
SUMMARY
OP RESULTS Table 1 30 Inch Valve, airflov Time Angle d Dynamic s deg Torque in-lb 1.0 90 (Pull open) 11020 1.5 78.75 23098 2.0 67.50 18138 2.5 56.25 14747 3.0 45.00 12428 3.5 33.75 10780 4.0 22.50 8014 4.5 11.25 3972 5.0 9. 0 (Pull closed) 0.0
- TNet= 22174 in-lb
NOTE: The design torque used in the Seismic analysis report No. TR-74-8 by McPherson Associates for this valve is 27800 in-lb. Therefore the design is safe.
CY.GMA ATI ACHNEf
i p ~ -s ~- ~
t I
~ -L I
SUMMARY
OF RESULTS Table - 2. 30 Xnch Valve Steam flow Time Anglect Dynamic S degas Torque in-lb 1.0 90lFull open) 11032 1 5 78.75 23175 2 ' 67 50 18142 .
2 5 56.25 14668 3.0 45. 00 12424 3 5 33.75 10580 4 ' 22.50 7809 4.5 11.25 3867 5 0 9. 0 (Pull closed) 00* TNet- 22174 in- b
ATiACHMESY 408~ ~2o~
FILE NO.
SHEET 40. ~
SUMMARY
OF RESULTS Table 3~ 24 Inch Valve; Air flow Time Angle W Dynamic S degas Torque in-lb 1.0 90 (Full open) 5525 78.75 11692 2.0 67.50 9095 2.5 56.25 7428 3 0 45.00 6239 3.5 33.75 5430 4 0 22.50 4043 11.25 2020A N
5.0 9. 0 {Full
- J closed) O 0 TNe't= 13808 in-lb I
At full closed position the'ynamic torque is zero and the net torque is due to seating and bearing friction.
Note: The design torque used in the Seismic analysis report No. TR-74-7 by McPherson Associate for this valve is 170(gin-lb. Therefore the deisgn is safe.
4
f' *,t Il n
SUMMARY
OF RESULTS Table 4 24 Xnch Valve, Steam flow degas Time Angle e4 Dynamic 8 Torque in-lb 1.0 90(Pull open) 5425 1.5 78.75 11394 2 ' . 67 '0 8921 2.5 56.25 7213 3 ' 45 F 00 6109 3.5 ~
33.75 5202 4.0 22.50 3842 11.25 1902 5.0 9. 0 (Pull closed) O-0 *- TNet= l3808 in-lb
~ II ~
I '
,~
REFERENCES WPPSS Specification 2808-68, Calc. No. ME-02-83-08-0, Sheets 1 thru 9, dated 10/8/82.
LOCA Temperature Curve Fig. 6.2-2.
LOCA Pressure Curve Fig. 6.2-3.
- 2. ANSI/AWWA C504-80, AWWA Standard for. Rubber-Seated Butterfly Valves. American Water Works ASsociation, Colo.
3~ Beard,C., Final Control Elements, Valves and Actuators, First Edition, Rmbach Publications, 1969.
4~ Hutchison, J. W., ISA Handbook of Control Valves, 2nd Edition.
'5. Torque and Sizing Calculation for BIF Butterfly Valves, No. D-214590, dated 1/9/75 for WPPSS Contract 468.
7~ B I F Test Report frTR-0650-43, Hydrodynamic and Headloss Test of 12" - 150 Lb. Butterfly Valve with directly connected short radius elbow upstream, dated 2/24/82.
- 8. B IF Drawings: 30 inch Valve General Arrangement Drawing A-206763 24 inch. Valve General Arrangement Drawing A-206764
SEE QID 361106 FOR BODY OF REPORT CVGHA P ~PQH~ASNY SOS WO.~ES'"
FlLE NO. OS.o(.F SHEET No.
7.4 McPHERSON ASSOCIATES REPORT:
DESIGN AND SEISMIC ANALYSIS OF 24" CYLINDER-OPERATED BUTTERFLY VALVE
BZF A UNIT OF GENERAL SXGNiAL X600 DXVZSXON ROAD FILE NO.
HEST HARNZCKP R I 02893 SHEET NO.~>.
DESXGN AND SEISMIC ANALYSZS OF 30", CYLINDER OPERATED BUTTEFZLY VALVE FOR HASHZNGTON PUBLXC POHER SUPPLY SYSTEM AND BURNS AND ROE CUSTOMER P.O CONT C 6 BEP EEOP ORDER EEL PN2 34~U+OEO&
RE Q B~Y McpHERSON ASSOCXATESP INC APPROVED
) <co~ ~
g App%aQ I) St7C mv,'. ~<PC 00 00
DESIGN AND SEISMIC ANALYSIS OF 30" CYLINDER OPE. A D Q BUTTERFLY ABYE A- 06 66 2 eb a 74 ATTACHNlBNT Prepared For: JOB NO.
05.tBt. F FILE NO.
BIF sHaav NQ.M'~
A Unit of General Signal Corporation Prepared By:
Thomas M. Riley John R. Henry
~ ~
BIF A Unit of General Signal Corporation Purchase Order No. 84908-63 McPherson Associates, Report No. VR-74-8 ~
Inc.
h 1>l>~('T+
McPherson Associates, Inc.
400 Totten Pond Massachusetts Road'altham, 02154 c:P4a~wn m~c=i~~m 4$ TOTTEN PONO ROAD ~ 'LYAt.THAM,MASSACHUSETTS 02154
~ C s ' ~ ~ ~
S k 0
e'EXS~iIIC ANALYSIS OF 30" CYLINDER OPERATED BUTTERFLY VALVE A-206763
~os oo.~~~
+~
RLR NO. ~< ~
~x~ ~~<'m SHaarN0. 7+>
A Unit of General Sign'al..Corporation Purchase Or6er No. 84908-63 McPherson Associates, Inc.
Report No. TR-74-8
~l>A,a<
FOR 30" VALVES BIF Cont.ac No. BIF S.O. No. Valve Tag No's N 27234-F CSP-V-1 CSP-V-Z CEP-V-lA CEP-V-ZA
REVl SlON RECORD NUS REPORT NO. TR-74-8 REViSiON 1 12/31/75 Page 3 . a)'aterial w'as ASTM A-126 s A-48 ATTACHMENT b) Allowable stress values corrected JOHNO. Stall FILENO Os ol.F Page 5 a) Drive lever was B-208217-17 SHEET NO.2'~
b) Clevis was D-146578-1 Page g a) Mat'1 was ASTM A-126, Class C b) Corrected yield stress al lowabl'e Deleted ASTM A-48
')
Pages 28 s 30 a) Hat'1 was ASTM A-48 b) Corrected allowable stress ( (
Page 32 a) Ref. Dwgs. were 8-20M-Q),D- @18-1 Pages 33, 35, 36 a) b) Corrected 1 owab 1 eg>
TABLE OF COiNTE.'tTS Section No. ~Pa e L Table of Contents Certification 1.0 introduction 2~0 Summary of Results.',0 Conclusions 4.0 References .
'esi~ Data.
~ '.0 Analysis 6.1 Cylinder Operator Assembly 6.2 Cylinder Support Bracket i 6.3 Clevis Assernb t &O'.Drive Lever'., 31 6.4 Valve Body Support ".Ea~rs" an Associated 38 Hardware 6.5 Shaft and, Disc Assembly and Associated Hardware 6.6 Valve Sizing and Stress Analysis Cons'ing Combined Operating and Seismic Conditions SOS No.~eqq Foie uo e'E. ei. p.
aHEET No.~4. S
A, h
'1
<<<<<<<<<<<<<<4'+<<<<<<
Certification HcPherson Associates, Inc. certifies that the 30" 3utterfly Yalve, A-206763, as shown on the customer drawings was analyzed in accordance with Washington Public Power Supply System Specification No. 2808-68 and to the best of our Knowledge and belief, meets the requirements of Paragraphs 3.2, 3.3, d 3.5.2;-4 of this document and Reference 3 of Section 4.0 of this report.
t John R ~Henr'y'
'Professiona<<l Engineer
'egis~~ered
~
Mass. egistration No. 25929 g ~
0
Section .1. 0 INTRODUCTION The purpose of this report is to determine the structural adequacy of a 30" Butterfly Valve Assembly when subjected to seismic accelerations as described in Reference 1 anu to insure the valve design is in accordance with Reference 3
'f this "eport.
The seismic plus operating analysis is performed in accord-ance with I')ashington Public Power Supply System Specifica-tion No. 2808-68, Reference 1, and all applicable informa-
~t ATTACHMENT vosNO. >><<<
- nENO ~oo.i F "H=v No.2< ~
JOE NO.~E5:oO FILE Np.g}f.oI. F
~
-"HABET ND.~~8 Section 2.0 SUMIARY OF RESULTS
I
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3.0 CONCLUSION
S McPherson Associates, Inc. concludes that all components for the 30" Butterfly VaLve, as analyzed in this report, meet the requirements 'of'll governing specifications for seismic plus operating considerations as defined in References 1, and 3 of. this report.
CVGMA ATTACHMENT JOB NO.~+
at.EW~O. <<4~ ~ ~
SHEET MO.M~~~
4 4'
- 1. <fashington Public Power Supply System 2&0&-68.
Section 4.0 REFERENC"S Specification No..
Vaa ND ~
ATTACHMENT RLg NP, 0'S.ol (F sHaavN0.7~ ((
- 2. 3IF Drawings
\
Revision Description A-206763 3 30" Butterfly Valve-General Arrang ement
'-900501 Body, A-900502 Machining Fabricated'ody, A-900499 Disc,'abricated A-900500 Disc, hfachined A-20&195 Cylinder Support Brachet-
~ B-9005l4, g Z)LWKq 3-900515 Operator Sha Drive Lever ts-p p.isa'hZ-m Clevis
'-1&4100 A Miller Cylinder I
Section III, Nuclear Power Plant Components, AShfE Boiler and Pressure Vessel Code,. 1971 with Addenda.
- 4. Virgil Moring Faires, Design of Machine Elements; 4 Edition, The hfac.'fillan Co., N.Y., 1965.
5o Raymond J. Roar%, Formulas for Stress and Strain, 4th Edition, hfcGraw Hill Book Co., 1965.
- 6. Laddish Catalog No. 5'5.
- 7. Grinnel, Piping and Engineerin Pr'd Edition, 1971.
I
&. 1963 S(emp1 aveee~t ia ccwow Thread ctenderds coz Z~Aawal Services.
L(
9 Baumeister 4 hfarks, Standard Handbook for hlechanical Engineers, 7th 'Edi.tion, hfcGraw Hill Book Co.
XQ..~ent, Mechanical Engineers Handbook.
- 11. A.S.T.)i. Standards - Part 2
- 12. A.S.M. Metals Handbook
- 13. Timoshen3co and Goodier, Theory of Z1asticity, 3rd Edition, NcGraw Hill Book Co., 1970.
- 14. Seely and Smi&, Advanced Mechanics of kfaterials,
. 2nd Edit on, John 1Viley 4 Son, inc., 1966.
1S. MacHinery's Handbook, 17th Edition, The Xndustrial Press 1964.
- 16. Section VXlX, Pressure Vessels, Division 2, Alternative Rules, A.S.M.Z. Boiler and Pressure Vessel Code, 1971.
~ Ctlemxcal Rubber Pub lishing Tables, Twelfth Edition.
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