ML20054E217
| ML20054E217 | |
| Person / Time | |
|---|---|
| Site: | Grand Gulf  |
| Issue date: | 04/14/1982 |
| From: | Klepper I, Sheel A, Stramback G GENERAL ELECTRIC CO. |
| To: | |
| Shared Package | |
| ML20054E213 | List: |
| References | |
| NUDOCS 8204260266 | |
| Download: ML20054E217 (47) | |
Text
{{#Wiki_filter:E Enclosure 2 to AECM-82/152 TEST REPORT GRAND GULF NUCLEAR STATION HPCS POWER SUPPLY UNIT I. Klepper A. Sheel Approved: d. 7/ . . rg G. B. Stramback, Manager Reactor Instrumentation and Protection Design Nuclear Control & Instrumentation Department General Electric Company San Jose, California l 820426024G
TABLE OF CONTENTS
- 1. Introduction . . . . . .. . . . .. . . . . . . . . . . . . . . 2
- 2. Test Plan . . . . . . . . . . . . . . . . . . . .. . . . . . . 3
- 3. Tests . . . . . . . . . . . . . . . . . . . . . .. . . . . . . 4
- 4. Test Results . . . . . . . . . . . . . . . . . . . . . . . . . . 8
- 5. Design Margin . . . . . . . . . . . . . . . . . . . . . . . . . 15
- 6. Acceptability . . . . . . . . . . . . . . . . . . . . . . . . . 17
- 7. Conclusion . . . . . . . . . . . .. . . . . . . . . . . . . . 20
- 8. References . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
- 9. Figures and Tables . . . . . .. . . . . . . . . . . . . . . . . 22 Appendix . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23 1
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- 1. INTRODUCTION The HPCS Power Supply was developed to power the high pressure core spray (HPCS) system for BWR/S and BWR/6 plants.
The HPCS Power Supply concept was originally provided in a licensing topical report, NED0-10905, May 1973. The NRC staff reviewed the topical report and Amendments 1 and 2, NED0-10905-1, August 1974, and NED0-10905-2, April 1976, respectively, and concluded that "the analysis and simulated tests provide reasonable assurance that the concept, though unique for diesel generator loading is workable, however, due to the marginal nature of the design concept, and partial testing performed, the staff will require that an actual test be performed which simulates as close as practicable the actual HPCS system configuration."I The staff also reviewed and accepted Amendment 3, NEDO-10905-3, August 1979, and concludert that the acceptance is only for a particular design diesel generator unit (Diesel Engine GM-EMD Model 20-645E4; Generator Ideal Electric Company, Type-SAB, Frame-M636PB) and "Each of the other diesel generators listed in NED0-10905 (Table 3-1) must undergo similar prototype qualification testing to be acceptable."4 The remainder of this report presents results of prototype qualification testing on a particular design diesel generator unit depicted in NED0-10905 Table 3-1 as Diesel Engine GM-EMD Model 12-645E4-Tandem. l 2 1 5
- 2. TEST PLAN In accordance with the staff's requirement,I a test program was 2
arranged. The test program was presented for the staff's review and the staff provided comments on the test program.3 NED0-10905-3 presented a revised test procedure, incorporating the staff's comments, to be used as guidance for additional testing in accordance with the staff's requirement. I Based on the staff's acceptance and requirement for additional testing,4 a prototype qualification test for a second engine type, tandem-12 cylinder, (as referenced in Table 3-1, NED0-10905) was arranged. 3
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- 3. TESTS ,
3.1 TEST SITE The test was conducted during preoperational tests on the HPCS equipment at the Grand Gulf Nuclear Station, Unit 1, presently under construction , t by Mississippi Power & Light Company. l t 3.2 TEST REQUIREMENT ! A test program specific to Grand Gulf was prepared and discussed with the staff in a meeting on July 23, 1981. Based on the July 1981 meeting discussion and the NRC's question 40.29, detailed Grand Gulf test instructions were prepared and incorporated into preoperational test procedures IP81PT01, IP81PT04, and IE22-PT01. The test instructions i were reviewed by the NRC site representative. " i 3.3 DOCUMENTATION , All the test data were logged and signed off by.the preoperational test , supervisor. The completed test instruction containing all test results is filed in the General Electric Document Control System, San Jose, California, at Grand Gulf under the control of the GGNS Records Coordinator, and is available for review. I P 4 4
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3.4 TEST ARRANGEMENT 3.4.1 Process Arrangement The piping and instrumentation diagrra is shown in Figure 3-1 and the process diagram for the HPCS system is presented in Figure 3-2. In a loss of coolant accident (LOCA) mode of operation, the HPCS pump (E22-C001-C) operates with suction from either the condensate storage tank with suction valve (E22-F001-C) open, or the suppression pool with suction valve (E22-F015-C) open. The injection valve (E22-F004-C) is automatically opened during this mode. However, because of lack of reactor pressure, in this prototype test, mode H of operation (see Figure 3-2) was selected. By opening the motor operated valves E22-F010-C and E22-F011-C, a flow path from condensate storage tank to condensate storage tank was established. In this way the HPCS system operation was checked over the entire flow range and respective pump discharge pressures. 3.4.2 Power Supply Arrangement The main one line diagram, Figure 3-3, shows the electrical distribution network for Grand Gulf Units 1 & 2. The HPCS one line diagram, Figure 3-4a through 3-4c shows the electrical configuration of the HPCS power supply system (bus 4.16KV-17AC, bus 480VAC, and bus 125VDC). 5 L
In the normal condition, the system is operated from one of the offsite sources, and the DG is not running (breaker #1 open). Extra heaters were added for test purposes to load the system to some margin in excess of the normal design load. Loss of offsite power (LOP) was simulated by tripping breaker #5 (152-1705 Figure 3-3). 3.4.3 Equipment Descrption 3.4.3.1 Diesel Engine The test was conducted on a tandem 12 cylinder, turbocharged GM EMD engine Model R12-654E4. The governor is Woodward EG series, electric type hydraulic actuator. 3.4.3.2 Generator The AC synchronous generator, manufactured by Portec, Inc., Electric Products Division is rated at 4125 KVA (3300 KW) continuously, 900 RPM, 60 Hz, 4160/2400 V, WYE connected. The generator is equipped with a static exciter and static voltage regulator, type SVS. The generator data are tabulated in Table 4-3. 3.4.3.3 Motor The motor is an induction type K manufactured by General Electric Company rated 3500 HP, 4000 V, 60 Hz, 1800 RPM, and 436A. 6
The motor characteristics may be found in NEDO-10905, May 1973, Table 3-4. 3.4.3.4 Pump The HPCS pump (Figure 3-6) manufactured by Borg Warner Corporation, Byron Jackson Pump Division is rated 3500 HP, 7275 GPM. The pump calculated performance and factory test curves are shown in Figure 3-5 and 3-Sa. 3.4.3.5 Test Setup and Instrumentation An additional forced cooling system was added to the engine labe oil and jacket water cooling system to cool the engine after shutdown. The cooling system was used only to cool the engine when required after a test run to bring the temperature down to the prewarmed condition. Before each test run, the engine was brought back to normal configuration by valving off the additional forced cooling system. Normal system instrumentation was used during the test. Additional Brush oscillographic recorders were used for recording all major parameters, such as speed, voltage, KW, KVAR, frequency, flow, and pressure. All instruments were calibrated. A detailed instrument list and calibration records are available for review from GE's Document Control System and are maintained at Grand Gulf under the control of the GGNS Records Coordinator. 7 l 1 l
- 4. TEST RESULTS 4.1 FUNCTIONAL TEST Prior to actual test, all control and protection circuits and systems including excitation systems, voltage regulator, and governor were checked for operability.
The alarms and protective relays were set and tested to meet the' design requirements, preparing the entire system for the actual test. No adjustment except that recommended by the normal maintenance procedure, were allowed during test runs. 4.2 DIESEL GENERATOR STARTING TIME This is an exclusive start test without loading of DG to determine the starting time for the DG. The DG start signal was manually initiated from the local panel and the transient events were recorded on an oscillographic chart. Five (5) such consecutive starting tests'were performed: three from the engine at cold, prewarmed standby condition (lube oil temperature at 85 F-140*F or 29.4*C-60 F and jacket water temperature at 95*F-155*F or 35*C-68.3*C) and two from the engine at hot equilibrium condition 8
(Jacket water temperature at 165*F-175*F or 74*C-79.5*C and lube oil temperature at 170*F-190*F or 76.7*C-87.8*C). The following results were obtained: Rated Speed (90015% RPM) in 7.1-7.6 secs. Rated Frequency (601.3 liz) in 7.4-7.8 secs. Rated Voltage (416011% VAC) in 7.9-8.3 secs. The test data from start no. 3 (cold) are tebulated in Tables 4-la and 4-Ib. The oscillographic chart recordings are shown in Figure 4-1, 4.3 IIPCS SYSTEM OPERATION FROM NORMAL POWER SOURCE This test was performed to determine the performance of the HPCS system. This test was performed with the IIPCS bus (17AC) being powered from the of fsite (normal) power source. An automatic IIPCS start signal was initiated with automatic opening of the injection valve F004-C and water suction from the suppression pool with valve F015-C open; an injection in the reactor vessel was achieved in 4.0 secs. at rated flow of 7115 GPM. This result was well within the design requirement of 27 secs. maximum. Note: This above test was performed with the actual injection valve used for llPCS; a fast opening valve with 12 secs. maximum
- apening time.
4.4 IIPCS SYSTEM OPERATION FROM DIESEL GENERATOR SOURCE 4.4.1 Rated Flow ! This test was run to determine the performance of the llPCS system 9 l l
operating at rated flow (7115 GPM) with the diesel generator as the only source of power. The system was aligned to inject water into the reactor vessel with an automatic opening of the injection valve E22-F004-C and suction from the suppression pool with valve E22-F015-C open. The IIPCS power supply (bus 17AC) was in its normal condition, i.e. , DG in standby condition with bus 17AC (4.16 KV) being fed from normal offsite source. A loss of offsite power (LOP) and a LOCA were simultaneously initiated by manually tripping the offsite wer breaker (to provide for DG start) and manaally initiating the IIPCS system (to provide HPCS pump start as soon as the llPCS DG is available for loading). This test was repeated five times following the same test sequence. [ A rated flow of 7115 GPM was achieved in 14.6-17.8 secs from the time initiation signal was applied. This is well within the design requirement of 27 secs. maximum. At rated flow the IIPCS pump motor drew 1800 KW (2413 IIP) which is less than the nominal 3500 IIP and DG load was 2000 KW. The DG satisfactorily started and accepted all system loads and none of the low voltage notor starters dropped out af ter bus 17AC was reenergized during IIPCS pump start. 10
4.4.2 Maximum BHP Flow This test was run to determine the performance of HPCS system at maximum BHP of HPCS pump motor, with only DG supplying the 4.16 KV bus, without being paralleled to offsite power. All the normal HPCS loads were operational and the HPCS pump was manually started. The test valves E22-F010C and E22-F011C were manually positioned to obtain the maximum load on HPCS pump motor, f.e. , maximum BHP of HPCS pump motor. Therefore, the system was set in condensate storage tank to condensate l storage tank (CST) mode, and operated for one hour. 1 i The total water flow was.3700 GPM. The initial voltage dip at the start of the pump went to 60%.and recovered to 70% within 3.3 secs. In the first 2.5 secs. after start, the frequency dropped to 98.3% of its rated value and recovered to the rated value in another 1.7 secs. The same test was run with the system set in suppression pool to suppression pool mode; valve E22-F023-C open to obtain the flow corresponding to the maximum BHP on HPCS pump motor. The voltage dip at start of the pump was 63.63% and recovered after approximately 3.6 secs. to 72.72%. i In the first 3.6 secs, the frequency dropped to 95.6% and recovered to its rated value after another 2.5 secs. i No equipment failed to operate due't'o low voltage during pump motor l start,-in both tests. . s 9
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The transient events'for test 4.3 and 4.4 were recorded and the charts I are available for review-fron GE document-Control System and are maintcined at' Grand Gulf under the control of the GGNS Records Coordinator. 4.5' STARTING AND LOAD RELIABILITY TEST The HPCS System was aligned for a flowpath from CST to CST, by positioning the test valves E22-F010C and E22-F011C'to load the HPCS-pump motor at its maximum BHP. The bus 17AC (4.16KV) was fed from the offsite power transformer 21; breaker 152-1705 (Figure 3-3) closed. The DG was ready for auto start. Extra heaters (480 V) were connected to the HPCS 480V MCC to load the DG in excess of the design ' load of HPCS System (HPCS pump motor at BHP and HPCS MCC loads of 270 KWiiO%).
- A signal from undervoltage relay of bus 17AC (4.16KV) provided a DG start signal after the offsite breaker (152-1705) was tripped. The HPCS I
} system was manually initiated to provide a start signal for the HPCS pump. The test was run for one hour, during which time the lube oil and jacket water temperature reached their equilibrium point (jacket water temperature 165*F-175*F or 74*C-79.5 C and lube oil temperature 1' . 170*F-190*F or 76.7*C-87.8 C). The load was maintained at maximum design load of HPCS system.
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- v _ 'At the end of one hour run the DG was shutdown. An external forced cooling system was employed to cool the engine to its standby condition 2 ) 12
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(lube oil temperature 85 F-140*F or 29.4*C-60*C'and jacket water temperature 95*F-155*F or-35*C-68.3*C). The test was repeated 69 times, of which 63 times were from engine in
. warm standby condition and 6 times were from the hot equilibrium condition of engine.
.For hot equilibrium condition the test was immediately initiated after.
the shutdown of DG without using the forced cooling system. All variable readings were taken at 15 minute intervals and chart recordings monitored the transient events for each of 69 starts. There was no failure (as defined by Reg. Guide 1.108) in starting or carrying the HPCS design load (HPCS pump motor at BHP and normal and resistive 480V MCC loads). The resulte of the 69 tests are as follows: Time from the start signal till 8.46-9.2 sec. DG tied to bus Time till HPCS system attained 21-26,25 sec. the rated flow (7115 GPM) Minimum voltage on Bus 17AC (4.16KV) 2800-2975V or 67.3%-71.5% of rated 4160V Time for Bus 17AC voltage to return 4.1-4.6 sec. to 80% of rated voltage Time for Bus 17AC voltage to return 4.23-5 sec. to 90% of rated voltage Minimum frequency on Bus 17AC (after 59-59.6 Hz or DG on Bus) 98.33%-99.33% of rated Hz 13
During the one . hour test of each of 69 starts, the DG load was maintained at the maximum design load of HPCS system 2700-2850 KW and water flow at 4650-6000 GPM to attain the BHP of pump motor. Due to similarity of the tests, one typical group of strip charts (Figures 4-2a through 4-2d) and data sheets (Tables 4-2a through 4-2d) , for the test #23 are included in this report. All-other test run data and charts are available from GE Document Control System and are maintained at Grand Gulf under the control of the GGNS Records Coordinator. 1 3 4 1 i t I i E 4 I 14
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- 5. DESIGN MARGIN
.This test was performed for the .first time to the largest. combination of
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DG (4610 HP Tandem type 3300 KW) and pump (3500 HP) ever used in HPCS
- system of a BWR plant (see NEDO-10905, May 1973, Table 3-1). The results of the test demonstrated the following margins.
5.1 STARTING TIME MARGIN t d The HPCS system attained a rated flow-(7115 GPM) in a maximum time of 17.8 seconds (test 4.4.1). When compared to the design requirement of 27 seconds the system demonstrated a starting time margin of 9.2 seconds. 3 The starting time achieved during the CST to CST test configuration (test 4.5) was somewhat longer due to test conditions which required operator actions to manually position the two slower operating (much
. slower than tiie HPCS injection valve F004-C) test valves F010-C and F011-C to a position that yielded the maximum BHP of the HPCS pump motor.
Further margin in starting time is anticipated in case of an actual LOCA condition because of high reactor pressure which requires a very low initial HPCS flow. l 15 4
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5.2 LONG TERM LOAD CARRYING CAPABILITY The DG supplied successfully the maximum design load of HPCS system (maximum' BHP of HPCS pump motor and HPCS-MCC). This condition t represented the maximum load to be'ever supplied by DG in an accident. condition. The load margin was 13.64%. At all other points, the power demand by the pump is much less, i.e., at rated flow and especially during an accident condition when reactor pressure is high. On a long term basis, the DG would be loaded to less than 70% of its continuous rating. The DG also successfully passed the 24 hour full load carrying capability test (R.G.1.108 requirement) of which for 22 hours, it was loaded at 100% of its continuous rating (3300 KW) and for 2 hours it was loaded to 110% of its continuous rating (3630 KW). I a 16 i
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- 6. ACCEPTABILITY 6.1 PERFORMANCE The performance of the DG was satisfactorily demonstrated. It fully demonstrated the capability of the DG to perform its intended function for HPCS application. The following performance was particularly verified during the test.
- a. Fast and reliable starting of the engine in 8.3 seconds or less was demonstrated repeatedly from both cold and hot engine conditions.
- b. The DG could successfully start and accelerate a large motor almost equal to its size (3300 KW generator and 3500 HP motor) well within the required time.
- c. During the loading sequence of the DG, the frequency and voltage decreased to 98.33% and 67.3% of nominal, respectively. The voltage returned to 80% in 4.1 secs and 90% in 4.23 secs of rated value. Regulatory Guide 1.9, position C.4 requires that the DG unit design should be such that at no time during the loading sequence, should the frequency and voltage decrease to less than 95% of nominal and 75% of nominal, respectively. The test met this requirement for frequency but not for voltage. However, the DG carries a single large load (HPCS pump motor) which represents more than 90% of the design load on the HPCS bus 17AC, and therefore a larger decrease in voltage is acceptable. The HPCS system 17
F operation was entirely successful in meeting the design requirement of establishing rated flow condition in far less than 27 secs. The voltage recovery and the speed of DG during transient events also l meet the Regulatory Guide 1.9 requirement.
- d. Because of the excellent performance in terms of volts / cycle-, which is a true measure in determining the performance of an electrical system, the voltage and frequency variation did not have any adverse effect on the design load. The system fully utilized the benefit of low voltage starting.
- e. No adverse effect of load sequencing was encountered during the test, which simulated as close as possible the actual load of HPCS system.
1 f. The DG successfully carried additional 480V loads in order to assure a maximum design load of HPCS. This will satisfy minor variation of load without jeopardizing the performance of the system. _The voltage and frequency variation had no adverse effect-on the battery charger and its load. 1
- g. The voltage and frequency overshoot during 100% rated-load rejection had no adverse effect on the diesel engine's operation.
f
- h. The DG carried 100% and 110% rated load without exceeding the diesel eng; ,e manufacturer's design limits.
i l 18 l 1
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- i. .The reliability of starting and-accepting design load in the required time was fully demonstrated by starting and carrying .
design load 69 times without. failure from both hot and cold' engine starting conditions. This met the objective of establishing a 0.99 reliability for the particular DG design. j . Long-term load carrying capability was demonstrated by running the < system for a period of almost 70 hours during starting and load reliability test.
- k. .The system has adequate margin in all respects, such as starting time, accelerating time, and long-term carrying capability.
- 1. The pump performance proved that it closely corresponds to manufacturer's data (see Figure 3-5).
e 1 J 19 l
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- 7. CONCLUSION The. test fully demonstrated that the HPCS power supply can fully meet Its design intent. This series of actual pump loop tests provided full assurance of the workability of the HPCS power supply concept and confirmed that the analytical studies and factory prototype tests could
$ conservatively predict the engine generator performance. It also further confirmed the results of LaSalle test. Even though the DG size and configuration were different at Grand Gulf, compared to LaSalle, the results of both tests are remarkably similar. 4 i l-s i 4 1
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-20 L_
-8. REFERENCES The below listed references are presented in Appendix A:
- 1. Letter from Olan D..Parr tu G. G. Sherwood, December 17, 1976, on General Electric topical report NED0-10905.
- 2. General Electric letter No. 781-106-77, November 17, 1977, from J. F.. Quirk to Olan D. Parr on GE HPCS Power Supply Unit,
-Qualification Testing.
- 3. Letter from Olan D. Parr to G. G. Sherwood, March 31, 1978, on GE HPCS Power Supply Unit, Qualification Testing.
- 4. Letter from Olan D. Parr to G. G. Sherwood, April 7,1980, accepting results of GE prototype testing of a specific DG ' unit -
(2600 KW) identified in NED0-10905 (Table 3-1). 21
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TABLE 4-la D/G STARTING TIME TEST, COLD, DATA SHEET
IPS1PT04 F p JqJ. yt W m dawahr.v-,.a a u o.,
,? DAIA sne.r.t 4,
i1 Diesel Cenerator Starting Test-Start No. 3 (Cold) SHEET 2 0F 2 - Part 2: Recorded data -
. Field flashing initiation ti=e 47 (, see Field flashing cocpletion time (, , 9 see Engine cranking initiation time o sec Engine cranking completion time z. . f er sec Acceleration time to atta(n rated ,y)/ p e) speed (900 + 4.5 rpo or 60.0 + .3 Itz)(-r.3 / 7 5 sec.
- ~ " .
],,' " and rated v 1tage (4160 + 41 VAC) 5,'/ sec. ,
~~ ~~"
Part 3: Ac'cep'tanc'e criteria' ,, , , , , , , , , , ,
~
All dat'a "ta' ken' on this data sheet is baseline except ~ for the following: , , , _
*k-g :: ' Air pressure (PI-F107A, B; PI-R108A, B) > 160 psig ff9f*C< Luce oil teeperature (TI-R010A,B) < 115'c - ~ ~
75 p*C[ Jacket water temperature (TI-R004 {,B) , t < 90*C-druster# /r ere_(f.TrsatNAvwi,B) g {rp,",*(1 g Acceleration time to rated speed and voltage (< 10 seconds DATA SHEET 8.7 COMPLETED BY: lTESf SUPERVLSOR SLG:iAfURb l DATE
~
..l~^-~
I ~ h r 3/ 30 /f 2.1 "' i TABLE 4-lb D/G STARTING TIME TEST, COLD, DATA SilEET h}
i h ' A A SHEET 8.33 h fb '~ hg HPCS Diesel Gehe' rator Operating Parameter's For ! i %7 L1 w. D/G.. Load And: Reliability Test No. 23 i
~j .
DATE: hM,82. SHEET 1 0F 4 i i ;- - k,. , , i L'.l l l Step i Step I i l 0 i ~l 17.3.23.21<---------7.3.23.10-------->l
$ l Instrument, l C l Service DescriptionlEng I . l l t 1 jl . MPL 1. A .l l Units l 115 min l 30minl45 minl60 min l !
t humber it T l- , I 'l' I I l l 1 l lll~
~
. I I .I l l l l l l 1 !
Il *
, . .l 0 l l .,IInitial l<----After Enr,ine Start---->l ;
11 1N l l -l Data l l l 1, [ flE22-J1-R609 l 1 l Wattmeter i KW l cd i S ee **l' eve o d 300 o 'l 2 9c O l i ; 4 lE22-JI-R608 l 1 1 Varmeter i KVAR l 6 l/Eco'l12oo .4 s cC*lI ?('/' l j
.lE22-El-RblO I 1 i Bus Voltmeter i KV 14,/6 I N, 2 0 ts'l M J u d e+ z c G *l d .'r ^ ^ l .
i j ?lE22-11-R607 l 1 l D/G Ammeter i AMP l O l +2Ovl'.'20 .442o 'lA*tO I4 ,
*lE22-SI-Rel2 l 1 l D/G Freqpency l HZ l (* t$ i 6o *i 60 64 's e *I i- 0 l
'lE22-SI-R615 f 1 1 l Bus Freguercy I HZ l pC l (O 'l 40 si s. o 'l /. ' .' ! [
l l l / l l l l l 1 l ! i .. l LIS-U600 l 4 l FO St'orare Tk l IN l (. b' ' I s. 5l N 6, F ' 81 /,f' " l /,C l f
.Il LIS-H602 1 4 i EO Day Ik i IN 1 / 3,5 " l '3 u *l Si " vi / C" #6 ro" I (
plL1-R600 1 5 -i F0 Stor Tk i IN I (3 $' l (,,5 ' 51 (, t ' s i 4.F' / l (.F lj jlL1-R601* l-5 l FO Day Tk i IN l / 'I s ' 5 l 3 # ' "I S f " ,/ l ,t d " *' l 7A i ,I f
;l i 4 l l 1 I i i 11 1
) {lJ1-R031 . ~ -l - 6 l Wattmeter i KW l O I Q ') 9 D l .2 7 t,6 1a790 l/7pC l [ l ilJI-R032 1 6 l Varmeter l KVAR l O l //ob 1//00 l //d o l II M ll [ lEl-RO34 1 6 i Bus VM 91-02 i KV i M ,10 0 1400 0 I o]oo lup co i 4 PN l' ; glEI-R034 l 6 l Bus VM 02-03 l KV l t/. /40 l u ;) o o I (,eJ oo I (pg oc i 4Pcc. ! [ EI-R034 i 6 i Bus VM 93-01 i KV l 6. 2 0 o lt40 6 & l In ob i uf o o i 4 2fC l -[
;.; l LEI-R033 1 6 i D/G VM 01-02 i KV i o lugoo itraoo loaooi 4 Fco I , l
[lEl-R033 1 6 l D/G VM 92-03 l KV l 0 l (fa r>o l(/3 0 0 14,/a 00 i fL'CO i , j glEI-R033 1 6 l D/G VM 93-01 l KV l O lud oo 1U2 00 l ua oD l 42601 (
'lII-R051 1 6 i D/G AM 01 i AMP l e l y ss luss i t/ /s i A er I ;
- flII-R051 1 6 l D/G AM $2 l AMP l o I se r.5 l // / 5 i 4/ S I 4 18" l l
! hlII-K051 1 6 i D/G AM 93 l AMP l C l 4/ p c; i4/5 i et/ 5 l 4 /5 l l [ISI-kO24 1 6 i D/G Freauency i HZ l c I t. O I60 160 t /. r7 l t
'lSI-ROSO l 6 i Bus Frequency l HZ l6O I (. O I6O I6o i r- U l f i El-R046 -
l 6 l Exciter VM l VOLT l C l69 i $9 l 90 1 OF I l II-RO47 I 6 i Exciter AM i AMP ! 6 I99 i/00 i /o o i Ao l l l 'lEl-R029 l 6 i DC Supply VM l VOLT l 19l 1f 3 1 1131 l /3/ l 138 l j l l11-R030 l 6 i DC Supply AM l AMP l ff- l // l // l // l II l t esI-R000 6 6 i Running Time i HR I 14 1, 0 119 3. 3 i /fr3. 5 i /BM i S M.n l !
- ,lSI-R002 l 6 l D/G Tachometer l RPM l n lSoo l 960 1900 1 DN l i [
I il l l l l i r/l I l !l [ ! lE22-FI-R603 ! I i hPCS Pump Flow I GPM i C i 5/e c) t l S Tfv > r1 5 3 r O v. c,300 i t IE22-PI-R601 1 1 lHPCS Pump Dis Pressi Psig i O l 14.5'l 5 50 # 1 F50 l MO ( l
. lE22-PIS-N652
.,' 1 2 iHPCS Pumo Sue Press Psiz 1 1.0 1 2 0 l ; O '< i 2 0 *' 8 2n ij( !
pgenec 3 rt & jntr- mie Mw GIS
- q. ..-.
4' Eag 3.is.u s-s es 3-ef 11 3 14 -S~4 [ DATA SilEET 8.33 COMPLETED BY:
,fgy f.,t e_ f l
l TEST SUPERVISOR SIGNATURE I D,sTE i l 3,6. I
~3[hh__I m, l TABLE 4-2a -
HPCS D/G LOAD AND RELIABILITY TEST DATA _
.,,,-r-,--g--, --
-----,-w.-- .y . . . - _ ,
icoAcav4
.- REV. 1
'{"[
d 3}, - Q. p p DAtt SHEET 8.33 ' . ~ Ii 'J1PCS Dicsal"CeM.r'ct.ci'Optreting Perrmsters For 's
.kd $ [j 'Ohd3 -
.D/G: Load And Reliability Test No. 23 l .
S ,; ,r.^ . ('.i e y O e s SHEET '2 ,'OF 4 -
._.,,' * * - ,g_ ** ,
i .l . t . ,
...l.L i . ;; - .; +
1- ' i Step i Step I
,l
.u 33 4.- . l TO -l ~ ~ " -
'l 17 . 3. 2 3 . 21 <--------7. 3. 2 3 .10--------> l 5 9l . Jins trtident ' Pl C l l Service"D uriptionlEng 'l - - 1 l l l l
$l e MPLL',y g,.l A ..},.,.3,77.,.lUnits ';.y: 1115 min! 30minl45 minl60 min l pts,f,utumber r . rl :;.T ',.! r...;..l.. ,.:
- pe er .I l l . ;l . . . I I I
- I -
~.I'. I l . ' 'c'- t.' O ~ El- l *% . . Initial
- l1 ;-x.:l <---Af I I ;4 .c - . il- ; I l
! ldh.v l; .. .;g,~~.. @! E : lO ter Engine Start---> l
,g m,..b,..
7' ' l N l 1 l Data l i' ' l l l I LITI-R049-1A l 3 i A CYL 1 EXH l *C i 54 1470 lu 7 2 l 470 i F- 7cp i ITI-R049-2A i 3 i A CYL 2 EXH l *C l4o i fle d 1 4 9 "> l YS6 1990 l lTI-R049-3A i 3 i A CYL 3 EXh 1 'C l Sg i c.7 'l i /J 7 9 i 4 79 i e -J l
'lTI-R049-4A I 3 l A CYL 4 EXH l *C i 5/ l t- 5 5 i y e; g i 4 6 o 1 4:.6 c/ l ITI-R049-5A i 3 l A CYL 5 EXH I *C -l 59 i V.3 3 l /2 3 4 1 43(o i f,. -' 5 l
,lTI-R049-oA i 3 i A CYL 6 EXH I 'C i f( l (4 / r.( i 4/9 i 4:23 I u-2.0 l lTI-R049-7A i 3 l A CYL 7 EXH I *C iSp l 4 63 l9A3 l '/ 6 3 la 65 l lTI-R049-8A l 3 i A CYL 8 EXH l *C I S e' l 479 l 479 l u 8'o 19- 7d l
'lTI-du49-9A 1 3 1 A CYL 9 EXH I 'C i 5 (, Im iu90 i 4YoI#fC l l~TI-R049-10A i 3 1 A CYL 10 EXH l *C l 6R I44;2 i '/ O 5 l yy '7 i @ p l lTI-R049-llA l 3 i A CYL 11 EXH l *C l 30 l --
l I - I- l lTI-RO49-12A - 1 3 i A CYL 12 EXR l 'C i 55 l u39 l440 i cy o I u ?c l lTI-R049-CEA i 3 l ENG A EXHAUST l *C i Sg -1 c.7 4 l c ;7 5 i 42 # i a 5- l lTI-R049-1B l 3 i B CYL 1 EXH l *C l 5') l45b l t/-4 D l t,tt,o l 94.e; J l lTI-kO49-2B i 3 i B CYL 2 EXH i "C i 5J i U (, 3 l445 I c 6 */ i _Je d _5 I lTI-R049-3B I 3 i B CYL 3 EXH I 'C i g/ i 447 1461 Iu70ie7o i TI-R049-4B i 3 i B CYL 4 EXH I *C l 64 i 4 /,6 I u h D. I O />,.1 i#/5 i
.TI-RO49-ab i J i B GYL 3 EXn i 'G i 44 14u 3 1446 6 uu <t e.
o l lTI-R049-6B i 3 i B CYL 6 EXH l 'C l fo; l437 i 4 t/. / I u u l I W_.; !
. lT I-R049-7B l 3 i B CYL 7 EXH l *C l 63 1452 I(#55 1 y s ') i @ /,~ c i lTI-hug 9-oB i 3 i B CYL o EXH i 'C i /., 0 I u b ci i46W l '/69 I 5 'ro l lTI-R049-9B i 3 I B CYL 9 EXH I *C i SA l t/ s 0 146 o i y 5 0 I ?'j 5 l lTI-R049-103 1 3 i B CYL 10 EXH l *C l $/ l c e; V lG54 iun&I P160 l lTI-x049-llb i 3 i B CYL 11 EXH i ~C i 5/ Iu;5 4 9 3 fo I u 3 8 i N/ l lTI-F049-12B i 3 i B CYL 12 EXH l *C 1 g9 iu35 143fa l u 3 'i l 6 * '
l T I-R049-C EB i 3 1 Ene B EXHAUST I 'C i f6 1427 i 'f 3 0 1 4 3 / i MU i l I i i l i I I I l l TIS-N045 1 3 l Stator Temo PT 1 1 *F l lai i/70 I/73 I/76' I/$C ! l TIS-N045 1 3 l Stator Temo PT 2 i *F l /7 /, I # a ') l / 9 Ce ! / 9 /p i 2 er o l T IS-iius 5 1 3 1 Stator Temo Pl' 3 i "F i /q o I / /. 4 i /1 '> t s'76 i/fO : l TIS-NU45 1 3 i Stator Temo PT 4 l *F i/M i / g 5- I/70 i/7/ I / 7S : lT IS-!!045 1 3 i Stator Temo PT 5 l *F 1/2 A I n. 4 l/72 I/79 I / .- O ! [ T IS -hoe.5 1 3 i Stator Iema PT o i 'E i //9 i f (. ? I//3 i/74 i/N i m givt a za Nt" m c '; 24.
- 3. vt .cj ). 3./19 ) 3./G. D 3 -' '/S ~/ ,;./.2.
DATA SHEET 8.33 CCMPLITID BY: I nst SUPERVISOR SIGNA!URE I DATE. l l 3lJ'WW l TAELE 4-2b HPCS D/G LOAD AND RELIABILITY TEST DATA
.. i,- REV. 1 ,
eus pfgp%DA3A SHEET 8.33 -
- *d Jg. t PCS Diesel:Centrat 3r Oparating Parameters For
{t 9ggg
~
% 4.y
-g ,D/G Load And.Relir.bility Test No. 23 l
i 3.,,
.. , SHEET 23 'OF 4 m ,-
.r , 3:-
j,. : W'.
- y.
._ _ ; , , .;;x , . *7 ,
, + i . 'g, .: *2 '.,l al. .... s
... L
- I %.. . . . .
i .7 .,1 Step .i Step I TRs5l %,.;g' l7.3.23.2l<' ,...,. -7. 3. 2 3.10-------> l
~
"l; M- N,. .. w,si. ;, . 15l30 u-l4A **. 'g, G .;,
~ '
; l. ; Instrument ';lf[,CidlSersive Descriptionlbig ~ .'-l .
,1 /Al a < l l l tli 0 ,HPL. 43 l* # . '
. .. ,, Qy., l Units l s ., .. ,115 minl 30 min l45 minl 60 min ! ,
.El ' ME[NumbeW;fd ' l".A% .
MY:,# . .!!. l * . I I l
@lD@&T';'[gi:ljiflb.fh Pj pg , p.
l4
@W p
t-55l a; 0 i.: l@b 3r,,,eg :,N ' . l E-' *22
..s'
'W'N'.Q;~bW 1'.
- P l
Initial I ~ Data 'l AI
. l.Wi'9'#2~ ',
C---Af ter Engine Statt----> l
..:.. l l
J ll . +l I l I l PlTI-R003A ** l -3 l J4 CLR SSW INL l 'C 1 /S I15 i /6 i /6 I / 5' l I
'clTI-R004A l 3 l J4 OUTLET .- -l *C l f33 1 63 i GT l 6? I 67 I (
ITI-xOO5A i 3 i JJ INL TO OIL CLR i 'C i M i ~7 a i -7 R - I ~1 1 1 72 l ! LlTI-R006A i 3 l JJ OUT FM OIL CLR l 'C l J '.A i '70 1 70 .I 7 0 i 70 l L 1 t i I el 1 l i i I
.III-R009A i 3 i LO FLTR INL i "C l 55 i 9 'k i W I 94 i T u- I
.lTI-R010A .
I 3 i LO CLR OUTL l "C 1 4- y I hi I 70 l 70 I 70 I
' lPI-R016A l 3 i LO PRESSURE '- lPsig l ' - () l 47 l 9(, - l 9/, l 94 l l 4
lPI-R017A - i 3 i LO FILTER INL IPsig i O I- O l d i O I D I "lPI-R018A l 3 i LO FILTER OUTL IPsig l O i O I o l O i O I
.l -l i l l -
l l l i l
,IPL-RU65A . 1 3 FO INL PRESS iPsig i O I '5 </ i qq l 38 i 3Y l L li l - -
l 1 l l l l si l ITI-R003B i 3 l J4 CLR SSW INL i "C l /O l /O i /O l /O l /0 l lT1-ROU43 i 3 l JJ OUILET l 'C i t/-A I-74 I 70i 7d 1 7d l ITI-ROO5B i 3 I JJ INL TO OIL CLR I 'C l 70 l -7 6 l 70I 70 - l 70 l
.lTI-R006b i 3 l JJ OUT FM OIL CLR l *C l ~7 0 l 70 1 -70 l ~/o I 70 I l I i i l i i i 1 l I .lTI-R009B l 3 i LO FLTR INL i "C l 5 'l i QO i 9 .3 ' I T .$ I 93 l lTI-R010B l 3 i LO CLR OUTL i *C l S 6, l l v i TA. l G. I %l lPl-Kuleb i 3 i LO PRESSURE iPsig i O IQS IQ6 i% i G (. l lPI-R017B l 3 i LO FILTER INL lPsig i D i O l O l O l O I lPI-R018B l 3 i LO FILTER OUTL iPsig i O l # l O I O i n I f l l l l l i i i i l lPI-R065B l 3 i FO INL PRESS iPsig i U i 37 i '2, 7 i 2, 4 i a ci l l l l l l l s, <* 4.Lh o l I l ITest Inst, i 3 i CRANKCASE PRESS A lin H201 ,3 4 A--tr I 2-P i V. O 1 4, r- 1 ITest Inst. l 3 i CRAMCASE PRESS B lin H201 ,3 i 'l -f e i f.1-:t i3,6 I 3.6 l l [ l i i l J'6'*t- % 6 l l l lTest inst. 17 i e 7 luutside Amat. Temo I 'F l ~7I , i 7 '/ . 6 1 YO, / I 74 i ~/ % 8 l Test Inst, l'31 % ID/G Room Temo l *F l '3 ~/. 5 l 9 0, d 19 5. '/ 198J . V I Q d. (- I l I l Clock Time iHR-MINI % '2 '3 0 l C F 512D O IM X !3?09 i ;
I i i l I I i i l I i 3.u-SL sCHw c el ! Cnw 'y'. 7-A 3_ g,, . g 2, .y s'2- ).9;,79 , ,
, ~~ Jx. t v.~ L-4' Cr - xla <w "W 3"u'c - },jf 'fia!g , *
,_ i DATA SHEET 8.33 COMPLETD BY:
i t l IESI SUPdRVISOR SIGNAIURE i DATE I . 1 I I l M- .-- i 3//Wft i - I TABLE 4-2c HPCS D/G LOAD AND RELIABILITY TEST DATA L . . . . _ . _ _ . _ __ _ - . _ _ _ . _ _ _. . - ._ .
~
-- j . . 'i1P81PT04
., , ,. ,.c .4. . yn . . .
REV. 1
. .kJ ~- y'
% k-
- +
4 % , ,
- *2 -DATA SHEET 8.33 h.'b; 1
J. 0yt Y
- d. '{
h5)Cselbenerator Operating Parameters For D/r 'm d!And Reliability Test No. 23 i SHEET ,, 4 0F.;4
. . .' l .u. r. .??.; &a.z l m- . -.
fLocation v1._ -11H13-P601-16B" .
'. Location :21 1H13-P625 '. ., ,
. Location 3- . '1E22-S001 Engine" Skid-
~~ *
$ Location '4 '
1H13-P877
' Location (-5? '1H13-P870 Lc, cation 6 .. ,; 1H22-P118 .
?-
., ., 'q-.,.s : - .. .
p ). i . u,.. . , , . . ,
- Data From Recordings: -
. ', . ;.:. . l:. c*
- y.~-
t ~
- ]'
Time 'from undervoltage signal 'till D/G tied' to bus'-I. b sec
' Time till HPCS at rated flow (from U.V. signal) 7,3, '1 sec .
Tir.: till ;;1.e 222 r00'. O full cpu (fs; ".". rign21) -ce-Ddt"Ttf Stetcu = 3 : D/G steady-state load 1106 KW 450 KVAR Minimum Voltage on. Bus 17AC AS70 Volt (after D/G on Bus) k nimum Freq on Bus 17AC 59,3 HZ (af ter D/G on Bus) Srd TcGM7 fiiie af ter D/G,fie 'for frequency to return to'9$8% (58.8 HZ) O see
//; f see Time after y/G). tie for Bus 17AC voltage to return to 80% (3326 VAG) e.6 see Time af ter D/G tie for Bus 17AC voltage< to return to 90% (3744 VAC) ..
. . , 7. ,f t.w,,; .. - ...--- .. .+. .
" Comments: Tyb.' n.m, New - 59, 3 - .
g ,
. ~c ~
Test Equipmer.t used: M//efb/I6 cy h 4:er/t.p2(cf /6 pf
& C '1 L d '2 6 0 0 /{,12* - ~5dW&& AKl .-^ 'L *3 6 n a fSL G o d s. d 'r Z D O# R7[
6-O t)L D 116 e
- T '7 5 Acceptance Criteria: A11' data is baseline 'ex' cept for the following: D/G load (E22-R609) is maintained at .,
d.esign loads for at least one hour. .;r ' *
. c < y.- c . . ' ~;... .y;,; ?
DATA SHEET 8.33 COMPLETED BY: ,
- p. .
ITEST SUPERVISOR SIGN TURE , i DATE l I
~
m I 7//dB / / 2!
'm ' - .,. .l l
t TABLE 4-2d HPCS D/G LOAD AND RELIABILTY TEST DATA l t l l i
A. C. SYNCHRONOUS SALES ORDER NO. DATE REV.
- SERIAL NO. 3/7/74 2 200- GENERATOR DATA 17312216/217
! 17312216/217 , VOLTS / A.9PS PHASE HERTZ TYPE KVA 3(6 Wire) 60 j L-11022 4125 4160/2400 ( 572.5f992.3 , 1 P.F. OLES DtHY RPM FRAME INSUL CLASS Continuous 900 150 F .8 - 8 Direct Axis Synchronous Reactance (Ifns atura t edi Yd -
.732 P.U.!
f 1
.386 P.U.'
" Yo 2 Ouadratur. Akie svnehrnnnue panct w , f 7 X'd .135 P.U.
! 3 Direct Axis Transient Reactance (Rated Voltage) (" ") X" d .072 P.U. l 4 ' Direct Axis Subtransient Reactance
") X"q L .088 P.U. f f
5 Ouadrature Axis Subtransient Reactance (" f" "l Xo .058 P.U.! l 6 Zero Secuence Reactance l (" ") X2 .080 P.U.! Negative Secuence Reactance 7 T' doi 5.291 Sec. l 8' Direct Axis Transient Ouen Circuit Time Constant T'd .977 Sec. l ! 9 Direct Axis Short Circuit Transient Time Constant
~
T"d .04 Sec. l 10 . Direct Axis Short Circuit Subtransient Time Const 4.192 Ohms l 11 Synchronous Incedance Unit on Rated KVA Base SCR' 1.436 P.U. Short Circui.c Ratio l 12
.722 Ohms 13 IField Resistance at 25 Dee; C
( Amos l 14 Field Current at Full Load. Rated Voltace and Power Factor 109.6 69.2 Amps 15 ' Field Current at No Load, Rated Voltage Amos 60% Volts .- 40.2 16 Field Current at No. Load. 105.1 Volts 17 Continuous Duty Field Voltage 27.5 % 18 Inherent Regulation
- 2. Ohms 50. Amns l Recommended Field Discharge Resistor:-
i 19 PrNL 10680 Kh'/5. Rad s l ! 20 ' Synchronizing Power Coefficient at No Load PrFL 13990 KW/E. Rad l [ 21 Synchronizing Power coefficient at Fu11' Load PdQAO 6280 lb s . 22 Unbalanced Macnetic Pull with Rotor Displaced: Curve No. 2503 Magnetization Characteristics 23 l
- Rating - above P.U. values are based upon 4125 KVA, 3300 KW base rating. I Generator 2000 Hr. (continuous) rating at 50 degrees C:3474 KW at 0.8 P.F. i capable of 10 percent O.L. for: 2 hr. in any 24 hr. period.1/2 hr. rating: -
3688 KW at 0.8 P.F. . , , STATIC EXCITER N.A. . TYPE SATURATION CURVE ' L- NO: Q CITER DATA VOLTS A5P ' "ML
, INSUL. CLASS ,
i 1 KW _ t i
^
w chms ; 2 Field Resistance at 25 Dec. C Ohms 9"A 3 Recommended Rheostar: Plate (s) TABLE 4-3 HPCS POWER SUPPLY GENERATOR , DATA
9 i APPENDIX CORRESPONDENCE RELATED TO HPCS POWER SUPPLY PROTOTYPE TESTING 4 'l 23}}