ML19268C082
| ML19268C082 | |
| Person / Time | |
|---|---|
| Site: | Cook  |
| Issue date: | 11/19/1979 |
| From: | Fowler B WYLE LABORATORIES |
| To: | |
| Shared Package | |
| ML17318A508 | List: |
| References | |
| NUDOCS 7912200512 | |
| Download: ML19268C082 (117) | |
Text
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** SCIENTIFC SERYCES AND SYSTEMS GROUP
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C~ _ . . _ . _ . . . Q, ~~. DYNAMIC LVALUATICN TIST PROGRAM CN A SAFL"! DCICTICN SYS*T.M PANEL, AN AUX LIARY RELAY PAh?L, d AhT A HCT SHU'"OCWN PA T.1, i t' r M'_
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DYNAMIC EVALUATICN TEST PROGRAM CN A SAFETY D10ECTICN SYSTTM PMC, AN AUXII.*ARY TJt!.AY FMC, AND A HCT SHt.7%WN PME FCR AMERICAN C.ECTRIC PCWER SERV!CE CORPCRATICN TAC BRCACWAY NEW YCRK, NEW YCRK 10004 84 4
SEISMIC SIMULATION Test Report ~
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i REPORT NO. 44560-1 h WYLE JOB NO. 44560 02064-250-DN, Ref. 06 M I l PAGE1 OF 117 PAGE REPORT M" M i November 19, 1979 1 [7 gn p ; p, i ri DATe SPECIFICATION (S) See References e .h .L4 ., --j. in Section 7.0 1.0 CUSTOMER American Electric Power Service Corperation ADDRESS Two Broadway, New York, New York 10t Q 2.0 TEST SPECIMEN A Safety Injection System Panel, an Auxiliarf Relay Panel, and a Het shutdcwn Panel 3.0 MANUFACTURER Harl concration 4.0
SUMMARY
A Safety injection System Panel, an Auxiliary Relay Panel, and a Het Shutdcwn Panel, desekibed in Paragraph 5.1, hereinafter called the specimens, were subjected to a dynamic evaluatien test as required by the American Electric Power Service Corporatier (AEPSC) Purchase Order Nurter 02064-250-9N, Ref. 06, and Wyle !.aboratories' Test Plan 541/1735-1/DK, dated April 21, 1979, Revision C. The dynamic characteristics were determined by providing c force input to the specimens with a small exciter specifically designed for modal-type testing. The testing was performed at the Donald C. Cook Nuclear Power Plant, Unit No. 2, located in Bridgman, Michigan. The specimens were tested in their actual in-service configurations over the period of October 31, 1979, through November 4, 1979. Ala. Profasslonal Eng. **"*"**'******'***"*****"""""*"'"*"'**'"'"""**
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STATE OF ALASAMA Re
- No* 6363 COUNTY OF MADISON PREPARED BY Mf#A ^ d James W. Forsman , o.,no ausy swom.
AP ED BY - ceooses and says: The information containec in tnis report is tne result of complete , f f and caretudy.c nituct tests and is to the oest o his unowiecge true and correct in
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WYLE O. A. , # - 4 . IM"c-M , j y y;]pyy,11 SUBSC BE # # % 19N - w &D'swoArn to ofore me tnisef.22 day of wy(E UWBWATOMES Notary PActic in anc for the State of Aisca . SCIENTIFIC SERVICES AND SYSTEMS GROUP My Commiseson expires 19 HUNTSVILLE. ALA8AMA i
2 PAGE NO. REPORT NO. 44560-1 WYt2 LABWtAM sammnc anvcts Am sysmes snoup 4.0 St20(ARY (Continued) Figures 1, 2 and 3 show the node points, excitation points, and acceleremeter locations. Photograph 1 shows the typical test setup. Photegraphs 2 thrcugh 4 shcw the acceleremeter 10catiens fer a typical test. i Appendix : contains the Inertance Plots frem,the resonance searches. ' Appendix II centains the mode shape data, mcde shapes, and damping decay picts. Appendix ::: centains the Instrumentation Log Sheets and the Instru-mentation Equipment List. Appendix ri centains Wyle 'aborateries' Test Plan 541/1735-1/0K, dated April 21, 1979, Kevision C. a.
3 PAJE NO. MM scume satymas AM SYSME GROUP REPORT NO. 44560-1 5.0 TEST TJQUIPIMCCS 5.1 Specimen Description and Mounting The felicwing specimens shall be subjected to a dynamic evaluatien test: Specimen Apprcximate Sice No. Oescricticn L x W x H 1 Safety Injection System Panel 138" x 96" x 96" 2 Auxiliary Relay Panel 122" x 24" x 96" ,, 3 Hot Shutdewn Panel 144" x 72" x 96" The specimens shall be mounted in their actual in-serrice configuratiens. 5.2 Excitatien 5.2.1 Ferce Input A force input shall be provided by a small, lightweight, armature exciter specifically designed fer medal-type testing. A feree trans-ducer shall be used at the attachment reint to measure feree input. The force input shall be applied to the specimens in each of the two (2) horizontal axes. The feree input shall be applied at twe (2) 1ccations as felicws: F10er-mounted cabinets - The feree input shall be applied near the top of the cabinet and aise apprcximately 24" frem the ficer. . Flocr- and ceiling-mcunted cabinets - The force input shall be applied approximately 60" from the ficer and also reprcxi-mately 24" from the ficer. 5.3 Resonance Search A sine sweep from approxir.ately 1 He to 35 H: using apprcximately 5 pounds force input shall be performed to identify major resenances for each test configuratica. The sweep rate shall be no greater than ene cetave per minute. Inertance (g/lb input) picts frem the resonance search tests shall be provided. In addition to the sweeps, resonant frequencies shall be verified by cbserring feree and acceleremeter output 11ssajens figures en an oscilicacope. The frequencies where feree and acceleratien are 90 degrees cut-of-phase, indicating a resenant condition, shall be recorded in the test icg.
PAGE NO, 4 44560-1 MMM REPORT NO, scamps saavsts ANO Iffmd8 BROUP 5.0 TEST REQUIREMDf!S (Continued 5.4 Mode Shapes and Campino for each test configuratien, mode shapes omd damping values shall be determined at the primarf resonant frequencies. Mode shap.,a shall be determined by tuning in the resonant frequency and using accelerometer probing methods at predetermined locatiens to describe the relative motion. The mapping shall be performed using two (2) accelerometers (ene biaxial) . Phase shall be determined free an oscillcycope Liseajous display. , Camping values shall be calculated frem escillograph decay recordings of acceleremeter signals taken by quickly turning off the exciter while exciting the unit at the resonant frequency. A decay curve shall be develeped from the escillegraph recordings and the damping shall be detemined by the felicwing formula:
, X C/C c
= ,' icg 2
.in eX n
where C/C = camping n = Number of Cycles X, = Amplitude of Cycle "o" X = Amplitude of Cycle "n" Additionally, the bandwidth method shall be used to determine the specimen damping. 5.5 Instr :mentatien 5.5.1 Excitatien Centrol Exciter force input shall be measured and controlled by a feree trans-ducer at the exciter attachment to the specimens.
PAGE NO, WTII. M 44560-1 scarmt savulEl Me sYs7mu ameUP REPORT NO. 5.0 TEST PM UIREMntTS (continued) 5.5.2 Specimen Response Six (6) response accelerometers (three biaxial locations) shall be located on each specimen under test. The biaxial locatiens shall be (1) the driving point, (2) the center of the cabinet face, and (3) approximately 18" from the floor. Frequency respcnse test accelsrometer and force data shall be recorded on FM tape. Inertance plots from the resonance search tests shall be presented in the test repert.
6 PAGE NO. 44560-1 WYLE N REPORT NO. manym seavets a sy:Tras snow 6.0 TEST PROCEDURES AND RESULTS 6.1 Specimen Mounting The specimens were mounted in their actual in-service configuratiens. 6.2 Excitation 6.2.1 Ferce Input A force input was provided by a small, lightveight, amature exciter specifically designed for modal-type testing. A force transducer was - used at the attachment point to measure force input. The force input
- was applied to the specimens in each of the two (2) hericental axes.
The feree input was applied at two (2) locatiens as follows: Ficor-mounted cabinets (Specimens 2 and 3) - The feree input was applied near the tcp of the catihet and also apprcximately 24" frem the flocr. Floor- and ceiling-mounted cabinets (Specimen 1) - The force input was applied approximately 60" from the flect and also apprcximately 24" frem the ficer.
'"he excitatien points are shown in Figures 1, 2 and 3.
E.3 .Casonance Search Precedures A sine sweep from approximately 1 H: to 35 He using approximately 5 pounds force input was performed to identify majer resonan-es for each test configuration. S.e sweep rate was one octave per min ca. In addition to the sweeps, resonant frequencies were verified by observing force and accelerometer output Lissajous figures on an oscilloscope. The frequencies where force and accolaration were 90 deerees out-of-phase, indicating a resonant condition, were recorded in the test log. 6.3.1 Resonance Search Results Inertance (acceleration divided by for:e versus frequency) picts are contained in Appendix I. No resonant frequencies were found belcw 35 H2 during the tes*dng of ^ the Safety Injection System Panel (Specimen 1) . i
7 PAGE NO. WYLE N 44560-1 scamMc sumcas ase :Tsfuus ensur REPORT NO. 6.0 TIST PROCIDUPIS A!C RESULTS (Continued) 6.3.1 Resonance Search Results (Continued) Resonant frequencies found during the testing of the Auxiliarf Relay Panel (Specimen 2) and the Hot Shutdewn Panel (Specimen 3) were Specimen Axis Frecuency (H2) 2 Frent-to-Back 11.2, la.2, 33.3 2 Side-to-Side None below 33 Hs .. 3 Frent-to-Back 16.1, 22.9, 24.4 3 Side-to-Side 22.3 6.4 Mode Shane and tamoine Precedures Fer each test cenfiguratien, mcde shapes and damping values were determined at the primar/ resenant frequencies. Mede shapes were determined by tuning in the resonant frequency and using acceleremeter prebing methods at predetermined locatiens to describe the relative metien. The mapping was perdermed using twe (2) acceleremeters (one biaxial) . Phase was determined frem an escillesecpe Lissajeus display. Oa= ping values were calculated from escillegraph decay recordings of acceleremeter signals taken by quickly turning off the exciter while exciting the unit at the resonant frequency. A decay e.zve was devoleped frem the oscillegraph reccrdings and the damping was deter nined by the fc11cwing formulas 4
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8 PAGE NO' WM N REPORT NO. 44560-1 scamps sunncts ame gramas snour 6.0 TEST PROCEDURES AND RESULTS (Continued) 6.4 Mode Shape and Camping Procedules (Continued) C/C =
,nn log e . eX n
where C/C, = Camping n = Number of Cycles X, = A=plitude cf Cycle "o" X = Amplitude of Cycle "n" Additionally, the bandwidth methed was used te determine the specimen damping using the fellcwing formula e . 'o Camping Facter = ~2 l 2f n where: f, and f, are. frequencies at which
= Q Q o_
h and Q, = Resonant Magnification Facter at f f = Resonant Frequencaf.
9 PAGE NO. MN scsutet samts: Am sysima ensur 44560-1 REPORT NO. 6.0 TEST PRCCEDURES AND FJ:SULTS (Continued)
. 6.4.1 Mode Shape and Oamping Results Appendix II contains the mode shape data, mode shapes v.d damping decay curves for Specimens 2 and 3.
The dam =ing values for Specimens 2 and 3, as determined from the damping decay curves and bandwidth method, are: Specimen Frequency Camping (% critical) No. Axis (Rz) Log Decay Bandwidth 2 T-B 11.2 1.9 2.6 2 T-B 13.2 4.7 6.5 2 F-B 33.3 3.2 4.4 3 F-B 16.1 3.2 3.8 3 F-B 22.9 3.0 3.3 3 F-B 24.4 3.3 3.2 3 5-5 22.3 3.3 5.6 6.5 Instr,:mentatien Procedures 6.5.1 Excitatien Centrol Precedures Exciter force input was measured and centrolled by a force transducer at the exciter attachment to the specimens. 6.5.2 Specimen Response Precedures Six (6) response acceleremators (three biaxial locations) were located on each specimen under test. The baxial locatiens were (1) the driving point, (2) the center of the cabinet face, and (3) approximately 18" from the flocr. Acceleremeter locations are shown in Figures 1, 2 and 3. Frequency response test accelercester and ferce data were reccrded en FM tape. 6.5.2.1 Specimen Restonse Results Appendix 2 contains the Inertance Plots obtained frem the specimen respense accelerometars. 6
10 PAGE NO. 44560-1 scasst stavets a systass saeur REPORT NO. 7.0 PJTERENCES 7.1 American Electric Power Service Corporation Purchase Crder Number 02064-250-9N, Ref. 06. 7.2 Wyle Laboratori4s' Test Plan 541/1735-1/OK, dated April 21, 1979, Revision C. e
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0 9 e Page No. 18 Report No. 44560-1 This page intentionally left blank. e PAGE NO. 19 WYLE e- *t * ~1 snuffys sumet! Aus sYsmes Gasur REPCRT NO. APPC::: : OTEATA:30 : 71,0TS RL'!! O R.**7E 10 . SPEC:2EN AXIS PCINT . 3afety Inle: :.:n 2ystem Fanel 7: nt-to-Eack i
- Safety In:ection System Panel Trent-t:-Back 2 3afety injection System Panel side-to-Side 3 5 Aux 111 arf .telay Panel Trent-se-Eack 1 9 Auxiliary Relay Panel Front-to-Back 2 1 Auxiliar/ Relay Paa.el 3ide-to-Side 3 11 Het Shutdown Panel T::nt-t -Back i 15 Ect 3hutdewn Panel Trent-t -Back 17 Hot Shutdown Panel Side-to-Side 3 w
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- FCACEINPUT TEST RUN NO.
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'i TEST AUN.NO. . Page No. $9 Report No. 44560-1 9~ PULL SCALI INERTANCE 0.001 0 0.01 jd .01 0 1.0 C t $ S' 9' 4 6 i i . - . . . ~ . . 6 i 8 i 3 I 1 I ( l i 6 J l i e # I , e i 9 8 16 S_.~ 4 4 _s ..~ ^ "mlll N It ? I 3 em) ' s i i i i i , 4 , 1 =,, __ 1 , i a. ., , , , , 8 8 W i ,' 6 , aa 4 *a : - u 2 4 8 7 3 . g , n aw i I 4F W W hM I i & 19 A , .'.M.-M A . . r ,'IIT o ., W Ri f 1 nah i e e i ;J s i i i T o 'ns nm 6 . .w v .. , ,' , 4 . 4 ie r q m ,i " . a i e 4=lp'a a . . . r . io a 4 . . . r . s. 1 'I '. I 1C0 1CCC \ ; Frecuency (H ) - ':t AXIS - <.c ACCEL NO. e'
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CF SYSTEM NAWRAL TPJ:QUENCIES TCR IN0IANA AND MICHIGAN POWER COMPANY TCR T!E OC1;ALD C. COCK !;CC:.,IAR 70WER P!.R.'T, ":! 0 :!O. 2 APPROVED BY: APPROVED BY .,( FOR: PROJEC' MANAGER: h APPROVEDeT: _ _, APPROVED BY FOR: , _ QUAUTY ENGINEER- ! ' APDROVED BY: - P#EPARED BY -- A% FOR: PROJECT ENGINEER: ~ REVISIONS ,c., ,, ,, fA Rev.No, t oAft i pact $ Ap tcito i sv i AP3;t. I otscRipricN cr enAmst$ A l8-8-79l All bF l M / k l Revised entire test plan per l l l l , , Customer request. B lB-30-79l 3 'AK M /[ Para. 3.3 - Added ". . . in the three! l l l I l l coordinate directions." I C l10-12-79l All lBCT gg( Revised entire test plan per l l- l l l \ Customer request. -l i I I l I I l 1 I I i i l I I I I I I COPvRtGHf 3Y WYLt i,ABQRATCAIES. ?wt tlGHf 70 REPRODUCt. COPY, EXHIBIT. OR OTHtRW!$t uf1LIZE ANY OF fME WArtRIAL CONTAINED ddRE:N #1THOUT ?HE IMpet$$ DR!CR 7t AM11${0N 3P WYLE LA80AA70R!a$ !$ #40H18! TID. THE AC !PTANCE 3F A SyRCHA$t ORDER ;N 00NNtlTICM WlTH THC MAf TRIAL 'QNIAINED MERtlN 1esAG 48 (QUlv& LINT TO EXPRESS PRIOR PERMl!$10N. Page No. 111 .- - Report No. 44560-1 541/1735-1/K TEST MOC!Dutt NO. 2 PA CI N O. MME SCSNilFIC $49VIC15 AND SYSTEMS Gmoup ReviCion 0 1.0 SCOPE In-situ vibration testing of centrol panels containing electremec'wical eq';.ipment for the purpose cf determining the natural frequencies within the frequency range of 1 to 35 H: shall be the scope of this test. A total cf three (3) Panels shall be tested. The Panels are located at the Oenald O. T,ak Nuclear Pcwer Plant, Unit No. 2, Fridgman, Michigan. 2.0 SPEC: MEN MOUNTING The specimens, consisting of a Safety Injection System, a Het Shutdown Panel and an Auxiliary Relay Panel, shall be mounted in their actual in-use configuratiens. 3.0 IX0 TATICM 3.1 Ter:c neut A for:e input shall be provided by a small, lightweight, armae re exciter specifically designed fer modal-type testing. A feres rans-tucer shall be used at the attachment point := measure f:res input. The force i.put shall be applied to the specimens in each of the two (2) heri: ental axes to excite the specimens. A typical test setup is shewn in Figure 1. The force input shall be applied at two (:) iccations as f 11cws: Ficor-mounted cabinets - The f:rce input shall be applied near the top of the cabinet and also approximately 24" frem the flocr. Flocr- and ceiling-mounted cabinets - The feree input shall be applied approximately 60" from the ficer and also appr=xi-mately 24" from the floor. 3.2 Resenance Search A sine swetit from approximately i H: to 35 H: using appr ximately 5 pcunds force input shall be performed to identify major resenances for each t(st configuratien. The sweep rate shall be no greater than one octave per minute. Inertance (g/lb input) plots frem the resonance search tests shall be provided. A~ typical inertance plot is shewn in Figure 2. In addition to the sweeps, resonant frequencies shall be verified by observing force and accelerometer cutput I.issajous figures en an escilloscepe. The frequencies where f:::e and acceleration are 90 degrees out-of-phase, indicating a resenant conditien, shall be recorded in the test icq. an, 32 m.,. un eg. i Page No. 111 Report No. 44560-1 + , 541/1735-1/tK ft37 PROCEDutt NO. PAGE NO. 3 N sc:ENTWIC simvicts AND SYSTEMS GROUP AeVISiOR C 3.3 Mode Shapes and Oamping For each test configuration, mode shapes an'd damping values shall be determined at the primary resonant frequencies. Mode shares shall be determined by tuning in the resonant frequency and using accelerometer prebing methods at predetermined locations to describe the relative motier.. Che mapping shall be perfo med using two (2) accelerometers (one biaxial) . Phase shall be determined from an escilicecope Lissajous display. A typical mode shape is shown in ' rigure 3. Camping values shall be csleulated from escillograph decay recordings cf acceler: meter signals taken by quickly turning eff the exciter while exciting the unit at the resenant frequency. A decay cuz re shall be developed from the oscillograph recordings and the dar. ping shall be determined by the follcwing formulas , X. 0/0 e = O an icg eX 4 n where C/C = Oamping n = Number of Cycles X, = Amplitude Of Cycle "c" x = Amplitude of Cycle "r." A typical decay curte is shown in rigure 4. Additionally, the bandwidth method shall be used to determine the specimen damping. 4.0 :MSTR*JMEM'"AT:CN 4.1 Excitatien Centrol Exciter force input shall be measured and controlled by a force trans- 'ducer at the excitar attachment to the specimens. g ,e n Page No. 113 Report No. 44560-1 541/1735-1/CK ft$7 PROCEDURE NO. PAGE NO. 4 scisNDFC SERWCES AND SYSMMS GAoup Revision C 4.2 Specimen Response Six (6) response accelerometers (three biaxial locatiens) shall be located en each spec 1. men under test. '"he biaxial locatiens shall be 1) the driving point, 2) the center of the cabinet face, and
- 3) appr:xtr.ately 18" from the ficer.
Frequency response test accelerometer and force data shall be racerded on FM tape. Inertance plots frem the resonance search tests shall be presented in the test reper . 5.0 REPCRT Six (6) :: pies of a :ertificatien-type report shall be tasued su:se-quant :s ::=pletion f testing. This report sna11 be ngned by a Registered Professi nal Engineer and shall include inertance p10;s, natural frequencies, mede shapes, damping, and acceler: meter locations. the repert shall also include a list of the test equipment and its calihratien. 6,. i '( e n 2' Pa*je No. 114 . Ra, port No. 44560-1 Test Procedura No. 541/1735-1/DK Page No. 5 Revision C 3 Y ~ S N sf D D ~D) a e lu o . .a '--'"'"'"#^' --^r--wPh*---'M-'--e'-'-e-'-, ,-..,_.,w.,..,s - .s.-,,:,e - .,.,%A,.,,,,u,-, ,,, , - m , - . + , ,- t ){ , , . ',? gy ,",,,s. u ,w . J ,,4 4s y pa , j' " ^ *Y ~ n , .h , ;te,, ... z',-k?d b' R .l, , . & ? ;: v_ , *g Q.- ;. k r[Ny;l; . u. n$ ;% y( ; *p. .. .i' - ' " e y v <,.. < f1.; hm , .- kl ,m. f ,c f - .h . } ; ?h u .. . R[.hs' l' lJ it , - ..L.eA. * ; l h ' 2 &_11_p/ "' 9+ ,,, e ea v /* / eum qw <v . f - h ) ~FlChL' *~~ [ T , . ~ #. sm,9 , =~ m ;g- h .a sn y;eQ { l[I T-1 _ a - - % r.m ac a m m ra , . TIG*.'.RE 1. TYPIC.% TEST SE*UP e 9 Page No. 115 I ' I ' F4 Port No. 44560-1 Test Procedure No. FULL SCALI INERTANCE $41/1735 1/gg i Pace No. 6 C.C01 C C.01 2 C.1 0 1.0 C Pavision C 4 i. t Ii I I I. p i I I. __ 3 N .=> 3 R s .m
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- 2. Drawines E7012 Series Timing Relay Class IE '
E7014 Series Timing Relay Class IE '
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