ML20062J354
| ML20062J354 | |
| Person / Time | |
|---|---|
| Site: | Hatch  |
| Issue date: | 04/30/1975 |
| From: | Sinwell J, Sucevic J WESTINGHOUSE ELECTRIC COMPANY, DIV OF CBS CORP. |
| To: | |
| Shared Package | |
| ML20062J352 | List: |
| References | |
| EL:486, NUDOCS 8010150540 | |
| Download: ML20062J354 (113) | |
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Astronuclear
- Laboratory EL:486 April 1975 r
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, ii i
SEISMIC TEST OF DIESEL GENERATOR CONTROL CONSOLE XAL 71696 SD 3025 i t WESTINGHOUSE ELECTRIC CORPORATION Astronuclear Laboratory l
. Post Office Box 10864 3 Pittsburgh, Pennsylvania 15236 i
Prepared and Tested by: D 1.J F. Sinwell l .
, Engineering Laboratories Approved by:
l 0 h. ,5== =S l vJ. M. Sucevic, Manager - i Engineering Laboratories 4 4 w
, Astronuclear
.- - Laboratory EL:486 April 1975 i TABLE OF CONTENTS Page Section
- 1 1 INTRODUCTION 2
2 TEST ARRANGEMENT 3 3 TEST DESCRIPTION 4-4 DATA ACQUISITION 5 5 TEST SEQUENCE l 7 6 TEST RESULTS l LIST OF ILLUSTRATIONS Page Figure 9 Seismic Test +45 Degree Position 1 10
'- 2 Seismic Test -45 Degree Position 11 3 '
Accelerometer Location Al 12 4 Accelerometer location A2 and A3 13
' 5 Accelerometer Location A4 and A5 14 i 6 Accelerometer Location A6 15 7 Accelerometer Al Control (Calibration Run) 16 8 Accelerometer Al Control (Colibration Run) 17 9 Operating Basis Earthquake - Accelerometer Al Control 18 10 Operating Bcsis Earthquake - Accelerometer Al Control 19
.' 11 Operating Basis Earthquake - Accelerometer Al Control Operating Basis Earthquake - Accelerometer Al Control 20 12 21 13 Operating Basis Earthquake - Accelerometer Al Control 22 14 Operating Basis Earthquake - Accelerometer Al Control 23 15 Accelerometer Al Control (Colibration Run) 24 16 Safe Shutdown Earthquake Accelerometer Al Control 25 17 Operating Basis Earthquake Accelerometer Al Control 26 18 Operating Basis Earthquake Accelerometer Al Control 27 19 Operating Basis Earthquake Accelerometer Al Control 28 20 Operating Basis Earthquake Accelerometer Al Control 29 21 Operating Basis Earthquake Accelerometer Al Control 30 22 Safe Shutdown Earthquake Accelerometer Al Control
, 31 23 Data Acquisition System 32 24 Seismic Test Control Room l
i i 1 1
f s t EL:486 April 1975 LIST OF TABLES i Table Page 1 Control Console Resonont Search Prior to Seismic Testing 33 i 35
-2 OBE and SSE Peak Acceleration Levels APPENDIX A Test Record Los Book Sheets K3320586 through K3320594 1 - 10
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i , my Astronuclear
- Laboratory EL:486 , l April 1975 6
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1.0 INTRODUCTION
The generator control unit was subjected to seismic testing using a random input applied by a bioxial test machine. The simulation was a shock spectrum input with a duration of at j least 30 seconds containing 10 cycles of strong motion acceleration. The input is to envelop the required operating basic of earthquake and safe shutdown earthquake spectrum os [ required, t. r l
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1 i EL:486 . April 1975 , 2.0 TEST ARRANGEMENT 2.1 The unit was mounted on the bioxial test table and located 45 degrees to the input driving force. This test setup is shown in Figure 1. 2.2 . The second test setup is shown in Figure 2 and was rotated 90 degrees from the first setup. 2.3 Six occelerometers were used to record the unit accelerot'ons. 2.4 The unit was powered during all of the testing. / 0 4 2 4
, , Astronuclear I -
L300faf0fy EL:486 i April 1975 i 3.0 TEST DESCRIPTION e 3.1 The unit was tested as per the test program from H. E. Lehman dated . l February 14,1975. (Copy attached at back of this report.) ,a 3.2 The unit was powered and the functional contact monitoring was conducted i during the te;t. 3.3 The resonant search and the shock spectrum test were conducted on a bioxial test stand. 3.4 The tests were performed with the following test equipment and all of the
- equipment had been calibrated:
, , 3.4.1 6 Accelerometers (Endevco 2262) 3.4.2 6 Conditioners (B&F 1-211 A2) 3.4.3 6 DC Amplifiers (Dynamics 6050) 3.4.4 MTS Vibration System 3.4.5 1 Brush Recorder (Mark 200) 3.4.6 1 Exact Oscillator (Model 7060) 3.4.7 B&K Exciter (Type 1018) 3.4.8 1 Techni-Rite Electronics Event Recorder 3.4.9 1 M/ RAD Corporation Synthesizer (N981) 3.4.10 1 Electro Instruments X-Y Recorder (Model 500) 3.4.11 Spectral Dynamics Sh :k Spectrum Analyzer SD320-2
?
3.5 The input wave was made up of decaying sinusoids covering the frequency rance of 1.25 H: to 35.0 H: and two sine beats were added to satisfy the two peaks en the required response spectrum. I 3 iJ C . _ _ _ _ _ _ _ _ . _
EL:486 April 1975 4.0 DATA ACQUISITION 4.1 The data was recorded on a Brush Mark 200 ink-type recorder. 4.2 The acceleration signals were conditioned by the dato acquisition system shown in Figure 23. 4.3 Transducer locations: 4.3.1 Bioxial Test I, Series l Al Horizontal Side to Side Control, Figure 3 A2 Horizontal Front to Beck inside Middle Door, Figure 4. A3 Horizontal Side to Side Inside Middle Door, Figure 4. A4 Horizontal Side to Side inside Middle Panel, Figure 5. A5 Horizontal Front to Back inside Middle Panel, Figure 5. A6 Horizontal Side to Side Top of Relay Penel, Figure 6. 4.3.2 Series I, Test 11 Bioxial Test - Unit Rotated 90 Degrees Clockwise From First Direction Some os 4.3.1 above. , 4.4 Input acceleration was analyzed on a Spectral Dynamics Shock Spectrum Analyzer. Analyzotion was performed at 1/6 octave intervals. These X-Y plots are shown in Figures 7 through 22. 4.5 The field output voltage was monitored and recorded during testing. 4.6 Six sets of contacts were monitored during the testing. 4 4
4
.y Astronuclear l Laboratory EL:486
[ April 1975 i 5.0 TEST SEQUENCE f 5.1 Series I, Test I, Run 1 The generator control unit was mounted on the drive plate at 45 degrees to the input motion of the test table. This setup is shown in Figure 1. i 5.1.1 The control console was electrical tested for correct operation.
, $ 5.1.2 A bioxial sinusoidal resonant frequency search was performed to determine natural frequencies of the unit.
5.1.3 A series of Operating Basis Earthquakes (OBE) and one Safe Shutdown Earthquake (SSE) simulations were input to the unit as follows:
, . Run 2 Calibration Run i
Run 3 Calibration Run Run 4 Calibration Run Run5 Calibration Run Run 6 Operating Basis Earthquake
. Run 7 Operating Basis Earthquake Run 8 Operating Basis Earthquake 1
i Run 9 Operating Basis Earthquake
, Run 10 Operating Basis Earthquake Run 11 Calibration Run Run 12 Safe Shutdown Earthquake 5.2 Series I, Test il The unit was relocated on the bioxial test table and rotated 90 degrees clockwise rotation from the first test setup. The setup is shown in Figure 2.
l i 4
. i 5
EL:486 April 1975 5.2.1 A series of Operating Basis Earthquakes (OBE) and one Safe Shutdown Earthquake (SSE) simulations were input in the unit as follows: Run1 Operating Basis Earthquake Run 2 Operating Basis Earthquake Run 3 Operating Basis Earthquake Run 4 Operating Basis Earthquake Run 5 Operating Basis Earthquake Run 6 Safe Shutdown Earthquake ) 1
- 6
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I W Astranuclear Laboratory EL:486 April 1975 l 6.0 TEST RESULTS 6.1 Series I, Test i The generator control unit was subjected to a seismic simulation consisting of a shock spectrum input with a duration of 30 sec. containing at least 10 cycles of A strong motion acceleration. Prior to testing the unit was electrical tested for correct optration. The testing consisted of five inpets at the required OBE l level cnd one input of the SSE level. Shock spectrum analysis plots are con-toined on Figures 7 through 14. Data summaries of resenant secrches are contained in Table 1. Data summaries of the OBE cnd SSE peak cceeleretion levels are contained in Tcble 2. 6.1.1 The following indications were observed during the sweep test:
- 1. Alarm indication, w bL% /-9 S
- 2. Contact bounce indication of the generator bearing overtemperature ct 14.5 Hz.
- 3. One annuncictor lamp inoperative.
6.1.2 The following indication was observed during Series I, Test I, Run 6: f
! 1. Generator bearing alarm indication.
6.1.3 The following indications were observed during Series I, Test I, Run 12:
- 1. All ennunciator lamps indicated.
6.2 Series I; Test ll
; The generator control unit was subjected to a seismic simulation consisting of a shock spectrum input with a duration of 30 sec. containing at least 10 cycles of strong motion acceleration. The testing consisted of five inputs at the required l l i
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4 EL:486 April 1975 + OBE level and one input at the SSE level. Shock spectrum analysis plots are contained on Figures 17 through 22. Data summaries of the OBE and SSE peck accelerotion levels are contained in Table 2. All other test setup information and test results are contained on Test Record Bock Sheets K3320585 through K3320594. k 4 4 e 8
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l l 1 TITLE SEISMIC TEST OF DIESEL GENERATOR CONTROL CONSOLE CUSTOMER BELOIT POWER SYSTEMS SERIES I TEST I RUN 7 OPERATOR Bertolomeo, Zummo, Sinwell l CONTRACT NO. XAL 71697 ANALYSIS METHOD 1% 1-100 . . . . . . _ ,
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CBE TITLE DIESEL GENERATOR CONTROL CONSOLE CUSTOMER BELOli POWER SYSTEMS SERIES I TEST I RUN 8 OPERATOR Bertolomeo, Zummo, Sinwell CONTRACT NO. XAL 71697 ANALYSIS METHOD 1% 100 . . . . _ . . , , . . . . , , ,
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OBE i TITLE SEISMIC TEST OF DIESEL GENERATOR CONTROL CONSOLE CUSTOMER BELOIT POWER SYSTEMS [~ SERIES I TEST l RUN 9 OPERATOR Bertolomeo, Zummo, Sinwell CONTRACT NO. XAL 71697 ANALYSIS METHOD lo, {- 100 .. = _ _ _ . .. e
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TITLE SEISMIC TEST OF DIESEL GENERATOR CONTROL CONSOLE CUSTOMER BELOIT POWER SYSTEMS SERIES I TEST I RUN 10 OPERATOR Bertolomeo, Zummo, Sinwell CONTRACT NO. XAL 71697 ANALYSIS METHOD 1% 100 v. ._ . . _ . . . . . . . . . .
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22 1
TITLE SEISMIC TEST OF DIESEL GENERATOR CONTROL CONSOLE CUSTOMER BELOIT PO'NER SYSTEMS l ( SERIES I TEST I RUN 11 l OPERATOR Bertolemeo, Zummo, Sinwell l CONTRACT NO. XAL 71697 ANALYSIS METHOD 1'o j 100ie ___- .. i , ; ; i + . ~ . . . . . , 7 l l i l , . t t }-t t 1 e e _ _ _ . . . _ . .. _ _x: _- l:.__ __ - :.; _._ _ y . ,_.
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TITLE SEISMIC TEST OF DIESEL GENERATOR CONTROL CONSOLE CUSTOMER BELOIT POWER SYSTEMS SERIES I TEST l RUN 12 OPERATOR Bertolomeo, Zummo, Sinwell CONTRACT NO. XAL 71697 ANALYSIS METHOD 1% 100 ., . _ . . ._ ;-.._ . _ _ . . . . . _ . . . . _ . . . t i 1 t 9i I, Y*--*--] l ; a e f* -b- f-* l f- l l L~-5 5 $ I'f'~A~ t 1, *
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OPERATOR Bartolomeo, Zummo, Sinwell CONTRACT NO. X AL 71697 ANALYSIS METHOD 1% i 100 . . 4 i . e ee e
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TITLE SEISMIC TEST OF DIESEL GENERATOR CONTROL CONSOLE CUSTOMER BELOIT POWER SYSTEMS SERIES I TEST ll RUN 2 OPERATOR Bertolomeo, Zummo, Sinwell CONTRACT NO. XAL 71697 ANALYSIS METHOD 1% 100..
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! TITLE SEISMIC TEST OF DIESEL GENERATOR CONTROL CONSOLE CUSTOMER BELOIT POWER SYSTFMS j' SERIES I TEST 11 RUN 3 OPERATOR Bortoicmeo, Zummo, Sinwell CONTRACT NO. XAL 71697 ANALYSIS METHOD 100 v. _. . _ _ _ . . , ,
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TITLE SEISMIC TEST OF DIESEL GENERATOR CONTROL CONSOLE . CUSTOMER BELOIT POWER SYSTEMS . I TEST II RUN 4 SERIES OPERATOR Bartolomeo, Zummo, Sinwell CONTRACT NO. XAL 71697 ANALYSIS METHOD 100 v. . ._._. s -
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, TITLE SEISMIC TEST OF DIESEL GENERATOR CONTROL CONSOLE CUSTOMER BELOIT POWER SYSTEMS
[ SERIES I TEST 11 RUN 5 OPERATOR Bertolomeo, Zummo, Sinwell CONTRACT NO. XAL 71697 ANALYSIS METHOD 100ie - . . . . . .. .
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SUMMARY
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. Horiz. Horiz. Horiz. Horiz. Side to Front Side to Side to Front to Side Horiz. to Back Side Side Back Top of j Side to inside Inside inside Inside Panel Side Middle Middle Middle Middle Above Controi Door Door Penel Panel C/E Relay Field
.g Hz Al A2 A3 A4 A5 A6 VDC 1.00 .100 .150 .150 .150 .150 .150 83 ,
i 1.50 .250 .350 .250 .300 .350 .300 83 l 2.00 .200 .350 .250 .250 .300 .250 83 2.50 .250 .350 .300 .300 .350 .300 83 3.00 .250 .400 .250 .250 .350 .300 83 3.50 .300 .650 .350 .300 .400 .350 83 4.00 .250 .250 .300
.250 .450 .350 83 1
4.50 .250 .500 .250 .250 .450 .300 83 5.00 .250 .700 .250 .300 400 .300 83 5.50 .250 .400 .250 .300 .400 .300 83
$ 6.00 .250 .400 .250 .300 .400 .300 83 6.50 .250 400 .300 .300 .450 .350 83 7.00 .225 400 .250 .300 .400 .300 83
,I 7.50 .225 .600 .300 .350 .450 .350 83 4.00 .200 .500 .250 .300 .400 .350 83 8.50 .200 .600 .300 .325 .500 .350 83
.I 9.00 .200 .700 .300 .350 .700 .400 83 9.50 .200 .900 .300 .350 .700 425 83 10.00 .200 1.20- .350 .400 .800 .500 83 I
10.50 .200 1.50 .500 400 1.00 . .550 83 11.00 .200 1.20 .450 .450 .800 .550 83 11.50 .200 .750 .350 .450 .950 .600 83 12.00 .225 1.10 .450 .500 1.30 .750 83 12.30 .250 1.60 450 .500 1.60 .700 83 12.50 .250 2.00 400 .450 1.50 .550 83 13.00 .200 1.50 .500 .500 1.00 .500 83
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.; 33
TABLE 1 (CONTINUED) Field Hz Al A2 A3 A4 A5 A6 VDC 14.00 .150 (340] .550 .900 - {2.50 1.50 83 14.45 .250 3.80 .800 1.20- 3.00 1.60 83 15.00 .225 3.00 .550 1.00 2.25 1.25 83 16.00 .250 1.50 .250 .550 .750 .800 83 17.00 .225 .600 .150 .500 .600 .500 83 18.00 .250 .800 .150 .250 .800 .300 83 19.00 .250 1.30 .250 400 .500 400 83 20.00 .225 1.00 .100 .250 .650 .350 83 22.00 .200 .550 .125 .150 .200 .200 83 24.00 .200 .400 .100 .125 .200 .200 83 26.00 .200 .350 .100 .125 .200 .200 83 26.75 .200 .400 .150 .100 .300 .200 83 28.00 .175 .200 .150 .150 .300 .400 83 29.00 .175 .050 .050 .250 400 .350 83 31.00
.175 .300 .200 .225 .225 .400 83 32.00 .175 .100 .200 .200 .400 .400 83 34.00 .175 .400 .350 .200 .150 .300 83 35.0 .175 .250 .350 .150 .100 450 83 l
34
(
@ Astronuclear Laboratory 7
TABLE 2 OBE AND SSE PEAK ACCELERATION LEVELS
SUMMARY
7-Horiz. Horiz. Horiz. Horiz. Horiz. Side to Front Side to Side to Front to Side Horiz. to Back Side Side Back Top of Side to inside inside Inside Inside Panel Side Middle Middle Middle Middle Above Field Control Door Door Panel Panel C/E Relay VDC g Al A2 A3 A4 AS A6 Series I, Test I, f Run 6, OBE 1 .350 .750 .375 .425 .600 400 83 Series I, Test I, Run 7, OBE 2 .350 .800 400 .450 .650 .575 83 Series I, Test I, Run 8, OBE 3 .350 .800 .450 .475 .750 .600 83 ( Series I, Test I, Run 9, OBE 4 .350 .750 .400 .450 .650 .550 83 1 Series I, Test I, Run 10, OBE 5 .350 .850 .450 .450 .700 .500 83 4 Series I, Test I, Run 12, SSE 1 .400 1.80 .500 .650 1.20 .800 83 Series I, Test II, Run 1, OBE 1 .300 .800 .350 .400 .600 .450 83 Series I, Test II, Run 2, OBE 2 .300 .850 .350 .450 .650 .500 83 j Series I, Test 11, Run 3, OBE 3 .350 .900 400 .550 .800 .600 83 Series I, Test 11 Run 4, OBE 4 .250 .800 .400 .500 .650 .550 83 Series I, Test 11 Run 5, OBE 5 .350 .900 400 .525 .650 .600 83 Series I, Test 11, Run 6, SSE 1 .400 1.75 .550 .800 1.20 .900 83 i l 3 - 1 35
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l SEISMIC TEST PROCEDURE l l EMERGEflCY DIESEL GEt1ERATOR CO:lTROL DETROIT EDIS0tl CO. EtlRICO FERMI NO. 2 I i i i l A. Annunciator
, 1. Connect temporary jumper between teminals TB1-2, TB1-5, TB1-8, TB2-1, TB2-4, TB2-7, TB2-10, TB3-3, TB3-6, TB3-9, TB4-2, TB4-5, TB4-8, TB5-4, TB6-6, TAl-1, TA2-3 and TAl-10.
- 2. Remove all fuses except FU3, FU4, FU7 and FU8
- 3. Use 125 V DC 10 ampere power supply. Connect plus lead to TC5-11 h of panel, negative lead to TCS-12.
4 Put local-remote switch in REMOTE position. I 5. Energize power supply.
- 6. Silence and reset any alams.
- 7. . Push and release lamp test button to insure that all alarm windows are lit.
8 Simulate generator bearing temperature high by moving set point needle of meter relay to coincide with meter reading. Alarm 16 l will flash and horn will sound. Depress and release silence button. Lights go steady on and horn is silent. Move set point needle away from trip point. Light remains on. Depress and re-lease RESET. Light goes off. Annunciator is ready for test. De-energize O.C. supply. I B. Exciter Regulator (SER) i 1. Disconnect and tape wires connected to SER terminals X1, X2 and X3.
- 2. Connect ATl (0-180 V, 20 amp 3 9 power supply), 5 SL resistors, I voltmeter and ameter to SER terminals XI, X2 and X3 as shown on drawing SK012975.
l 3. Connect AT2 (0-208 V, 5 amp 3 0 power supply) to panel terminals TC3-10. TC3-ll and TC3-12 as shown on SK012975, i 4 Disconnect and tape wires going to EGA from panel teminals TC-1, TC-2 and TC-3.
- 5. Replace fuses Ful, FU2, FUS and FU6
- 6. Energi:e D.C. supply. (Reset annunciator).
- 7. Put voltage control MAti-AUTO switch in AUTO position. !
- 8. Put LOCAL-REMOTE switch in REMOTE position.
SEISMIC TEST - DETROIT E0! SON
- 9. Ensure that ATl and AT2 controls are set for zero voltage output when ATl and AT2 are energized.
- 10. Energize autotransformer. Slowly increase output of ATl while observing dc voltmeter on panel, ac voltmeter connected to SER and line ammeter. Do not allow readings to exceed.
240 volts dc 180 volts ac 20 amperes ac Adjust control until dc voltage is approximately 200 volts.
- 11. Slowly raise voltage of AT2 observing panel voltmeter (120 V =
4160 V reading). Do not allow it to go higher than 4160. As the voltage is increased, some point will be reached (between j 3000 and 4000 volt reading) at which the line current delivered I by ATI begins to increase. This is due to the beginning of
. regulator SCR conduction. When connected to a generator the
- SER would now be causing generator cutput voltage to be slightly -
{. higher than the command voltage. When this point is reached increase output of AT2 until panel Ir meter reads 4200 volts. ATl current will decrease. Again raise ATl voltage (without exceeding the limits of paragraph 10, above) until line current begins to increase. Slightly back off ATl output voltage from this point. Record all readings at this point (for later use) including approxi-
,, mate settings of AT1 and AT2.
Y
- Reduce AT1 and AT2 voltage to zero and de-energize ac and dc supplies.
C. Contact Sensino (See drawing SK012875)
- 1. Disconnect and tape wires on left side of terminals TK-5, TK-6, TK-7,TK-8, TL-1 and TL-3. -
3 2 Connect jumpers in any order convenient to complete circuits A and
)" B shown on drawing. Use any suitable contact monitor to detect and record 3 millisecond closures of circuit A and 3 millisecond opening of circuit B. The use of 125 V DC and a high impedance i recorder is only suggested.
I 3 Make temporary connection between teminals TE5-9 and TM-1 and t, atween TES-10 and TM2-5. g 4 Energize dc supply to ensure that HFA relay 2PK6 energizes (contact
,. closure between TE6-3 and TE6-4).
5 Check that circuit A and B are functioning by operating recorder and manually opening and closing appropriate contacts in the line-up. E i . 6 De-energize de supply. 3 4 . , 4
SElSMIC TEST - DETROIT EDIS0l1 D. Accelerometer Instrumentation (Sketch SK012975) Mount five accelerometers in approximate locations shown. Mount table accelerometer to suit standard practice at the laboratory. XY motions will be detected for one test series; ZY motions will be detected when the control cabinet is turned and mounted at 90 degrees to the XY position for a second test series. E. Seismic Tests Make a resonant frequency search from 0 to 35 HZ with a 0.2 g peak horizontal input and a 0.133 g peak vertical input. The search sweep rate will be approximately two octaves per minute (maximum rate). Af ter resonances have been detected perforn a biaxial sine beat test at the five resonant frequencies of greatest amplitude. If less than five resonant frequencies are found, make mid-octave tests between the. resonant points so that tests total five. If no resonances are found , perform the sine beat test at 1.5, 3, 6,12 and 24 HZ. In all five sine beat tests the maximum amplitude of the beat and the cycles per beat will be appropriate to give full output response at the test frequency. A sufficient number of beats will be made to correspond to thirty seconds of strong earthquake motion. When the above tests are completed, the cabinet will be remounted at 90* to the position it had above. Thereafter,the above procedure will be followed a second time. During the sine beat testing the test circuits of paragraoh A, B and C will be energized. Voltage to the field simulating resistor will be (asset to read in described approximately)240 voltsrecordings paragraph B . Chart with the SCR's non-conducting of this voltage and of the contact monitors will be made at approximately one inch per second. If contacts change state, the approximate duration will be determined with a triggered sweep oscilloscope. A test report will be written containing acceleration data, typical recorder charts and any recorder charts showing malfunctions. Photo-graphs of the test set up will be included. All temporary connections will be removed and all disconnected wires will be replaced when the tests are complete. Thereaf ter , the unit will be returned to Beloit Power Systems for a final touch-uo and inspection (including a repeat of the continuity test made before shipment to the testing laboratory). H. E. Lehman 2/14/75
~
APPEiiDIX D r* l~ SCIENilFIC SERVICES AND SYSTEMS GRCUP EASTERN OPERATIONS FACILITIES L0uTEL IN 1 HUNTSVILLE, ALA. AND HAMPTON, VA.
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- m. 4 Test Report 43615-1 sb
[, f. REPORT NO.
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p gyg % p WYLE JOB NO. hB! *ghc.M.'pgf58 M.M jj#j CUSTOMER 1-1473-8 14 gggggg[.g - P. O. NO.
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PAGE 1 0F 113 PAGE REPORT I ' De c e.-ter 13, 1977
' l MMg 't DATE ll N *' "'
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See References SPECIFICATION (S) in Section 7.0 1.0 CUSTOMER sasler Electric Ccmpany i ADDRESS Foute 143, Hichland, Illinois 62249
' Exciter Cabinet, Part #9115700100, Serial #125 2.0 TEST SPECIMEN Basler Electric Company 3.0 MANUFACTURER 4.0
SUMMARY
I The Exciter Cabinet, hereinafter called the specimen, was subjected to a Seismic Simulation Test Program as required by the Basler Electric Company Purchase Order Nu-ter 1-1473-8, and Wyle I.aboratories' Seismic Test Plan 541/6089/ES, dated April 19, 1977, Revision A. It was demonstrated that the specimen possessed sufficient integrity to withstand, without compromise of electrical function, the prescribed simulated seismic environment after the high voltage contact fingers were adjusted prior to Test 11
- . (see Paragraph 6.3.1) except during Test 19 (SSE, FB/V). During Test 19, Electrical l Monitoring Channels 5 and 6 displayed deviations as described in Paragraph 6.7.1.
'- Structural problems were experienced during the test program as described in Paragraph 6.3.1.
STATE oF ALABAMA C .
; 3 PREPARED BY o couNTv oF MAOlSoN M V-Gr h William W. Holbrcok ,,,,,y,,,,,,,
APPROVED BY ;l/ . v a..,s... .e4 . .. . r . . n o. m .. .o o <an... .o .a m.. ..co,i . m . .. . a t J .
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SCIENTIFIC SERVICES AND SYSTEMS GROUP REPCRT NO. 43615-1 l
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4.0 S'JMMARY (Continued) Table I contains a descriptien of the tests. F Figures 1 and 2 shew the Cperating Basis Earthquake Requir2d Response IL Spectra. I' r igeras 3 and 4 show the Safe Shutdown Earthquake Required Response Spectra. Photograph 1 shows the damage to the speci=en, observed during the pre-test inspection. Photograph 2 shows one of the ten aluminu= spacer biccks used for specimen mounting.
;- Photograph 3 shows the specimen mounted on the Wyle Multiaxis Seismic Si=ulator for testing in the fr:nt-to-back/ vertical crientati:n.
j Photograph 4 shows the screw-down terminal lug which replaced the broken
! terminal lug on the cable that connected to Transfer =er PPT 4 (H3). The i broken terminal lug was dis cvered during post-Run 10 inspectien.
Photograph 4 also shows the bent stud on Transfer =er PPT 4 (H3) which was observed during post-Run 16 ins =ection. Photograph 5 shews one of the two cracks (nut, belt, and washers rs=cved) in the cross support menber for the current transformer dis vered during post-test 10 inspection. Phot: graph 6 shows the high voltage mating finger :entacts for the draw-out drawer 1ccated in the cabinet which were adjusted prier to Test 11 by the f i 3asier Technical Representative. Photograph 7 shcws the high voltage contact plates en the back of the
! draw-cut drawer. ,
Photographs 8, 9, and 10 shew the damage to the specimen dise vered during post-test progra= inspecticn. 1 Photographs 11 thrcugh is shew the locations of the speci=en response , ac:eler==etars. Appendix I centains transmissibility plots fr:= the resenant search tests. Appendix II contains selected ac:elerati:n versus frequency picts fre= 1 Resonant Search Test ?. l 1 L r .
3
- PAGE NO M M ENO 43615-1 SCIEt4TIFIC SERVICES AND SYSTEMS GRCUP REPORT NO.
l
.i 4.0 SU:'24ARY (Continued)
Appendix !!! contains the Test Response Spectra picts for the Safe Shutdown Ear.hquake tests. 1(I- Appendix IV contains the Instrumentation Log Sheets and the Instru=enta-tion Equip =ent Sheets. l Appendix v centains the Wyle Laborateries' Seismic Test Plan 541/6C89/ES, dated Apr:,1 19,1977, Revision A. I
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1 PAGEHO. 3CIENUFIC SERVICES AND SYSTEMS GaCUP 43612-1 REPORT NO. i j' 5.0 TEST REQUIREME:.7S I't 5.1 Specimen Mountine and crientation The =ounting hole pattern in the specimen shall be transferred to the i il surface =ounting fixture and the fixture, in turn, shall be welded to the Wyle Seismic Simulator Test Table. The holes in the fixture shall be drilled and tapped and the specimen attached using ce==ercially-available bolts and washers. The =ounting of the specimen shall si=ulate the actual in-service configuration as closely as practical.
>1 The specimen shall be initially oriented such that its longitudinal axis shall be colinear with the longitudinal axis of the test table.
f For the second axis of tests, the specimen shall be rotated 90 degrees in the horicental plane. 5.2 Low-Lavel Resonant Search A low-level (approxi=ately 0.2 g horicontally and 0.1 g vertically) biaxial sine sweep shall be perfor=ed on the specimen frc= 1 He to 35 Ht to establish natural frequencies. The sweep rate shall be one octave per minute. 5.3 Rande= Multifrecuenev Tests The specimen shall be subjected to 30-second duration simultaneous heri-
, contal and vertical phase-inccherent inputs of rande= =otion censisting of frequency handwidths spaced one-thrd octave apart over the frequency range of 1 He to 40 He. The a=plitude of each ene-third cetave frequency I
' shall be independently adjusted in each axis until the Test Response Spectra (TRS) envelcpe the Required Response Spectra (RSS) . The resulting table motion shall be analyced by a spectrum analycer at a damping cf five l- percent (5%), and plotted at one-third octave frequency intervals ever the frequency range of interest.
)
I Five (5) Cperating 3 asis Earthquake (CSE) tests, f'olicwed by a Saf'e Shut-down Earthquake (SSE) test, shall be perfor=ed in both the side-te-side / vertical and the front-to-back/ vertical orientations of the speci=en. j The CBE and SSE RRS are shown in Figures 1 through 4. i 5.4 Scecimen Resconse l Twelve (12) speci=en-=ounted uniaxial pieco-electric acceler==eters chal' be located en the test specimen during the tast progra=. FM tape and osciliegraph recorders shall previde a reccrd of each acceler==eter - 1 response. Transmissibility picts of the specimen respense accelercesters I! frc= the resonant search tests shall be providad. TRS picts of the control snd specimen-=cunted accelerc=eters shall be previded frc= the SSE test in each test orientatten. . 1: o Li
. _ _ _ _ . _-_m__
1 I 5 gg PAGEWO. SCIENTIFIC SERVICES AND SYSTEMS GROUP qgpggy 3g, 43615-1 f 5.0 TEST REQU!?S. MET!S (Continued) I, 5.5 Electrical Powering Electrical powering of 400 VAC, 60 Hz, 3-phase at approxiastely 20 a= peres, 1,' shall he furnished for the test speci=en. In addition, 125 Vr,C at 10 amperes or loss shall be connected to the specimen control circuitry. 5.6 Electrical Loads A 10 ohmeter resistive load at 1000 watts shall he connected to the specimen during the simulated seismic tests. l 5.7 Electrical Monitoring l Six (6) channels of electrical monitoring shall he recorded en an oscillo-graph recorder during the test program. These channels may be used to j ascertain electrical continuity, spurious or improper operatien, contact ( chatter, etc. before, during and after the seismic excitation. l l E
- r
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. I t
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I- 6 PAGE NO.
'M MMO 43615-1
,- SCIENTIFIC SERVICES AND SYSTEMS GROUP REPORT NO.
~
6.0 TEST PRCCIOURES ANO RESULTS l- 6.1 Scecimen Mountine and Criantation Precedures It was discovered during the pre-test inspection that the specimen
, Ib. . . cross member and floor had been damaged as shown in Photograph 1.
The specimen was bolted to the mounting fixture using nine (9) SAE
- Grade 5 1/2"-13 bolts and one (1) SAE Grade 8 1/2"-13 cap screw (the Grade 8 cap screw was used in place of a hexhead bolt, to allow
- tightening with available tools). The bolts secured the speci=en with the ten (10) aluminum spacers to the fixture (see Photegraph 2) .
f The mounting fixtura was welded to the Seismic Simulator Table. The specimen mounting simulated the in-service mounting configuration as closely as practical. The specimen was initially criented in the
- side-to-side and vertical (SS/v) orientation. For the second axis of tests, the specimen was rotated 90 degrees in the hori: ental plane to the front-te-back and vertical (FB/V) orientation shown in Photograph 3.
6.2 Resonant Search Precedures A low-level (approximately 0.0 g horizontally and 0.1 g vertically) biaxial sine sweep was perfor=ed en the specimen frem i H: to 35 H: to establish natural frequencies. The sweep rate was one octave per minute. 6.2.1 Resonant Search Results The resonant search tests are described in Table including test nu=bers, axes, and input accelerations. Transmissibility plots of the specimen response accelerometers (divided by the control acceleremeters) frem the resonant search tests are presented in Appendix I. Selected acceleration versus frequency plots fren Rescnant Search Tes: 9 are presented in Appendix II. h k. 6 18 .
-w l ~
I e i
7 PAGE No. ggg
. SCIENTIFIC SERVICES AND SYSTEMS GACUP REPCRT NO. 43615-1 e
/
gp 6.0 TEST PRCCEOURES AND RESULTS (Continued) iI L 6.3 Randem Multifrecuency Test Procedures
;f The specimen was subjected to 30-second duration simultaneous horicontal
- and vertical inputs of randem motion consisting of frequency bandwidths spaced one-third octave apart over the frequency range of 1 H: to 40 H:.
,' The amplitude of each one-third octave bandwidth was independently
?I adjusted in each axis until the TRS enveloped the RRS. The horizontal and vertical control acceleremeters were recorded on~oscillegraph and
. . FM tape recorders. The resulting table motion was analy:ed by a spectrum ll
- analycer at a damping of 5% and plotted at one-third octave frequency intervals over the frequency range of interest.
e Five (5) CBE tests, folicwed by an SSE test, were performed in both the
.I . side-to-side / vertical and the front-to-back/ vertical orientations of the specimen. The CBE and SSE RRS are shcwn in Figures 1 through 4. , t 41 6.3.1 Randem Multifrecuency Test Results 1 t .i The following structural problems were noted during the si=ulated ,l b seismic test program.
The post-Run 2 (CBE, SS/V) inspection revealed a broken nylon cable clamp
.t w
holding lead H3 (Transfor er PPT 4). The cable was not repaired or replaced, , ) The post-Run 8 (SSE, SS/V) inspection revealed one of the four draw-cut drawer securing bolts had damaged threads. The bolt was replaced and nc
?; further problems were enceuntered with the belt.
s{ Y The post-Run 10 (CBE, FB/V) inspection revealed a broken ter=inal lug
; (PPT 4-E3 lead) which was replaced with a screw-dewn tMr=inal lug (see h- Photograph 4). Further damage was found in the hori: ental cross suppcrt "I" beam for the current transfor=ers (CT1, CT2, and CT3) ; cracks gj appeared on either side of the top at the "I" beam mounting holes J( (see Photograph 5).
t gj Prior to Run 11, the high voltage centact fingers (see Phetograph 6) el were adjusted by the Basler Technical Representative to make better O' contact with the high voltage contact plates (see Photegraph 7) . Li The post-Run 16 inspection revealed a bent stud on Transformer PPT 4 (H3) Ei where the screw-down ter=1.al lug was installed after Run 10 (see Photograph 4).
.t
- f. Post-test pregram inspection revealed two cracks in opposite locations en the bettem of the ":" beam cross support me=ber fer the current trans-
.. for=ers (see Photograph 3). The ficer under the PPT 4 transfer =er was
- g'i bulged in the area of the mounting belts as shewn in Photograph 9 and s the cen:er longitudinal support member under the ficer of the transfer:er revealed six crac.<ed welds. Two of these cracked welds are shewn in j Phetegraph 10. 4 h\b
--__---__w _ _ --- ~ . - - ----n - w
PAGE NO. 0
,, SCIENTIFIC SERVICES AND SYSTEMS GROUP REPORT NO. 43615-1 i
, 6.0 TEST PRCCEDURES A:D PISCI.TS (Continued) 6.4 Specimen Restonse Precedures l Twelve (12) accelerometers were located on the specimen to =enitor response to the si=ulated seismic testing. FM tape and oscillegraph recorders provided a record of each accelerc=eter response. Photographs 11 through 16 shew the locations of the specimen-=ounted accelerc=eters.
j l The horicontal accelerometers (lH, 3H, etc.) were oriented in the front-to-back direction for front-to-back/ vertical testing and re- l
, oriented to the side-to-side direction for side-to-side / vertical testing. l 6.4.1 Specimen Res=onse Results I l
Transmissibility plots of the speci=en response accelerc=eters from the I resonant search tests are presented in Appendix I. 1 I
)
C Selected acceleratien versus frequency plots frc= Resonant Search Test 9 ) f, are presented in Appendix II. l The trans=issibility plots frc= Accelerometers ;V, 6V, 8V, and ICV j (Test 9) show an unusual high peak at 7.5 He. Evidently this phenc=ena was caused when the PPT 4 transformer resonated at 7 He in the front-to-
, back direction (Accelerc=eter 9FB, as shown en Page 60 of Appendix II) and l
caused the vertical input to decrease drastically as shown on the vertical centrol acceleratien versus frequency plot in Appendix II (Page 59). Since the vertical respense of the transfor=er (Accelerc=eter 1CV, as shown en Page 61 of Appendix II) was excited by the front-to-back resonance e
"' of the transfor=er and since the vertical input decreased drastically as described above, an unusual high peak resulted at 7.5 He. The "Q" & shown en Trans=issibility Plots 2V, 6V, SV, and 1CV (see Appendix ) is ,y not a true vertical resonance but is a result of the vertical input &' decreasing to approxi1=tely 0.007 g at 7.5 He.
- y. TRS plots of the specimen response acceler==eters at 5% damping for the y SSE test in each test orientation ara contained in Appendix III.
6.5 Electrical Pcwerinc Precedures
,"*=
Electrical powering of 400 VAC, 60 He, 3-phase at approxia=tely 10 amperes
, was furnished for the test specimen. In additien, 125 VOC at 10 amperes or less was cennected to the specimen centrol circuitry.
Q 6.6 Electrical I.cadine Procedures A 10 oh=eter resistive load at 1000 watts was connected to the field output of the specimen during the simulated seismic tests. 1
}
h.m-9
O
~
PAGE NO. a SCIENTIFIC SERvlCES AND SYSTEMS GROUP REPORT NO. *tg1-l 6.0 '"EST PROCE "RES AND FISULTS (Continued) 6.7 Electrical Monitorine Procedures Six (6) channels of electrical =cnitoring as described below were
,l i recorded on an oscillograph recorder during the test program. These
~
channels were used to ascertain electrical continuity, spurious or improper cperation, contact chatter, etc. before, during and after the simulated seismic excitation.
, ,3 1. Field output voltage, ncminally 100 volts, i} across 12.AL load (F+ to F-)
- 2. T32-P to T31-N (4 NO contacts of K2) 4 1
- 3. T32-FL to T31-NC (2 NO contacts of K3)
, 4. T32-13 and 14 parallel with T32-15 and 16
{, (NO contacts of K16) gl 5. Filtered sensing voltage between T32 (PC Card 4i #911:007100) and TP1 (PC card #91120061C0) c
- 6. Unfiltered sensing voltage between L1-1 (PC s
- card #9112007100) and TP1 (PC card 3l :
49112006100). 6.7.1 Electrical Monitorine Results
\
It was demonstrated that the specimen possessed sufficient integrity ,; to withstand, without comprcmise of electrical function, the prescribed
!i i' simulated seismic environment after the high voltage contact fingers a'
were adjusted prior to Test 11 (see Paragraph 6.3.1) except during Test 19 (SSE, F3/V). During Test 19, Electrical Monitoring Channel 5
;j.
displayed three (3) spikes, the largest of which reduced the 3.9 VOC filtered sensing voltage to approxi=ately 3.3 VCC. Electrical Meni-toring Channel 6 also displayed three (3) spikes, the largest of which gi reduced the 56 VCC unfiltered sensing voltage to 39 VOC. 9 The rpecimen was exposed to two (2) < SSE tests (Tests 17 and 13, r3/V, 9 He icw horicentally) without any electrical deviations (see Table 2). n' The specimen was rotested in the side-to-side / vertical orientation after the high voltage contacts were adjusted as described above without any
;! electrical deviations '(see Table 2, Tests 20 thrcugh 25) .
Y I }N I e 1 4 1 40 I .. =8 e . 1
PAGE No. gg _
. SCIENTIFIC SERVICES AND SYSTEMS GRCUP REPCRT NO. 43615-1 1'
7.0 REFEP22:CI3 [ 7.1 Basler Electric Cc=pany Purchase Order !!u=her 1-1473-S. If ,, 7.2 Wyle Laboratories' Seismic Test Plan 541/6CS9/ES, dated April 19, 1977, Revision A. 7.3 IIII Standard 344-1975 Specification entitled "Rece== ended Practices for Seis=ic Quslification of Class 1 Electrical Equipment for !!uclear j- ! Power Cenerating Stations" . i 7.4 Basler Electric Cc=pany Cocument 91157C0002, Revisien 3, entitled
" Test Precedure for seisrJ.c Qualification of Static Enciter, Part I
tiu=ber 91157001C0" 7.5 Basler Electric Cc=pany Crawings: Sche =atic Diagram, Power Chassis 9115701910 Rev. 3 Sche =atic Diagra=, Centrol Chassis 9115702910 Rev. 3 Outline Crawing 91157CC920 Rev. D Interconnection Oiagra= 9115700960 Rev. L h i l l i l l l l I 1 b
Ptqs !!o. 11 P1 port 230. 43615-1 e TM3 :
!$T RCI OESCRIP*:0:13 1
- P' T .WC:* EFATIC:3 l \- ~IST
- c. YPT 7s*
~!STl uit i 1."!!! 6 wPA
'O 8 1:?A ?I!'AFXS 1 Sine Sweep ss/V --- 3.20 0.10 specimen not ;cwored.
Il,
- 2 PM S3r/ CSE 1.30 0.60 Cable clamo on H3 lead broke (did not repair). *1gatened
'~
moun-ing bolts. Ouring run, S!5 (T.:*.) 'raried era-ically. 3 M Ssr/ (CBE 1.50 0.43 C35 (E.M.) varying. 4 3:7 SSN CBE 1.40 0.43 C35 it.M.) varying. 5 PM SSN CBE 1.45 0.45 CH5 (E.M.) varying. 6 PM SSN CBE 1.45 0.40 CH5 (E.M.) varfing.
? R:e ssW CBE 1.70 0.32 ct5 (E.M.) varfing.
9 FM 3SN SSE 2.35 0.65 One of the four draw-cut drawers' securing bolts was replaced after Run 3. 9 Sine Sweep nn - 0.20 0.10 specimen not pcwered. r 10 ?M F3r/ OBE 1.40 0.75 CM5 (E.M.) experienced large deviaticas becaure the ter a- .
.at lug en M3 lead trone duri..g test (see Photo. 41.
Post-test inspectica re-vealed t.m ::acks in :ross
, marJ:er for the :urrent .rans-for:er f see Photo. 5) . Cus-to ter acjusted M.V. :entacts (see Photos. 6 and *1 price j to Test 11. Added E.M. CH6 j
. prior to Test 11. j 11 ?M T3/V <OBE 1.15 0.65 l
. \
.. FM T3/V CSE 1.15 0.65 )
( 11 FM T3N CSE 1.19 0.67 14 PM Ft V CBE 1.20 0.65 15 ?S rsev 05: 1.;2 0.67 16 Pn r3N CSE 1.33 0.66 Caste =er signtened trans-fer-er (FP 4) counting bcits. 17 Pn ra/V < 35E 2.15 c.35 <3SE % $ M: hori:Ontally. 13 FM T3/V < 35E :.27 1.05 <35E 3 3 M: her::entally. 17 P:7 T3N SSE 2.40 1.08 Three spurious responses on E.M. C35 and 0H6 (see
! Para. 6.7.1).
20 72 7 53/V CSE 1.40 0.39 21 *N $3/V CSE 1.40 0.33 i I
- 7;T 35N 03E 1. Q 3.37
! 22 ?;T 33e*/ C3E 1.40 0.35 24 MT 33eV CBE 1.55 0.43
;$ F27 S te*r 23E 2.15 0.52 1
* --* ::: 33
- Oade-et-lade T3 * .::ce-t -lack
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- Ft.n:3= 'ulta ret;et. 7 I*
- Elastrt:al :.onat:r t
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' Page No. 14 Report No. 43615-1
( EULL SCALE SHOCK SPEC TRUM (g Peak)
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' Report No. 43615-1
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