ML20064A646
| ML20064A646 | |
| Person / Time | |
|---|---|
| Site: | Fort Calhoun  |
| Issue date: | 09/11/1990 |
| From: | OMAHA PUBLIC POWER DISTRICT |
| To: | |
| Shared Package | |
| ML20064A645 | List: |
| References | |
| EA-FC-90-062, EA-FC-90-062-R00, EA-FC-90-62, EA-FC-90-62-R, NUDOCS 9009170172 | |
| Download: ML20064A646 (342) | |
Text
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I FORT CALHOUN STATION DIESEL GENERATOR UPPER TEMPERAT4RE OPERATING LIMITS I EXECUTIVE SU % RY l The as built configuration of the Fort Calhoun Station Diesel Generators results j in radiator air cooling flow reduction -due to the size restricted radiator 1 exhaust duct and turbocharger air inlet tem >eratures greater than the.outside i 8 ambient air temperature due to the room conf Lguration. This room configuration-L and reduced radiator air exhaust flow result in a reduction in the output capacity beyond the normal engine temperature derating requirement.
'This derating is determined first by load testing the' diesel. generators at the a expected worst case emergency loss of coolant accident loads to determine the g ' jacket water outlet temperature rise above outside ambient air and turbocharger inlet air. temperature rise above outside ambient air. The jacket water outlet temperatureisthenadjustedto208'F(theenginelimit). The amount by which
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i I the jacket water outlet temperature is adjusted is added to the test measured outside ambient temperature to obtain the maximum outside ambient air temperature limit. The measured jacket water outlet and turbo intake temperatures are scaled iS up by the difference between the maximum outside ambient limit determined above (3 L and the measured outside ambient temperature. T: engine is derated based on these adjusted values using the curves in attachment 8.2 of this analysis. The graphs, depicting engine derated capacity output with time, are produced using the above methodology based on a cool engine and room temperature initially
- at the outside ambient temperature upper limit. Engine output decreases as the i room and jacket water outlet upper temperatures increase.
The results indicate that the Diesel Generator LOCA load for outside ambient air ' i3 ' temperatures of 107'F for DG-1 and 103'F for DG-2 would remain below the 2000 I g hour engine rating of the engine as it heats up. The 2000 hour rating corresponds to loading which assures a high degree of reliability from the engine. when operated at or below this rating. Operation of the engine above the 2000 hour rating would occur only af ter on-line testing in which the tagine would be hot when responding to the accident. The I engines are expected to perform reliably above the 2000 hour rating for this case, as stated by the engine manufacturer, EMD (Electro Hotive Divis< on of GM). After the run above the 2000 hour rating, the engine would be inspected for any y - abnormal. wear. .- The. static exciter and generator must also operate at this elevated ambient , temperature. Using the same testing method and air temperature rise above l$ l 1- 5 outside ambient air, the differential temperatures of the static exciter air
. inlet temperature and generator air inlet temperature are determined. The t
E different< a1 temperatures of the exciter and generator are then subtracted from their respective temperature limits to determine an upper operating temperature , r I'
3 limit. Both the exciters and the generators have ambient air temperature limits.
'above the engine limits. The exciter limits require that the cabinet doors be removed. This is a temporary configuration until a modification is made to reinstall some-type of door. This analysis is also based on the diesel room 8 ventilation fans being'off.
' The results are considered conservative. Test instrument uncertainties were I . conservatively applied. Based on the results of the analysis, the Fort Calhoun Lemergency diesel generators are considered operable.
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h Ea0ineering' Analysis Preparation-Review end val . Engineering Analysis No.: EA.FCo.,tA.,Gia, Rev. No. Fore PED.QP. 1 Page 1 ef 8 EA Page No. t Ea0ineering Analysis Cover Sheet File me. m/A Total Pages n a l EA TITLE: DIESEL GENERRToa UPPER TEMPERRTURE OPERATING LIMITS. I II QACATE80RY: [x3CQE [ )LimitedCQE REPORT TYPE: [ x) Analytical Report g [ ]FireProtection ( )Special [ INonCet l [ ) Revision INITIATION: 3l Respor.sible PED Department Elmetrical/Isc Responsible Department Head .5 . T . o'connor 1 Preparer n.r. f.h.erev P I. oate Vendor / PED Department No. 356 Vender / Dept. Code N/A Due Date 9/12/90 ENSINEERING ANALYS!$ TYPE: Oft;ER: cIn eo0617/c4(x ) I Electrical Equipment Qualification l'EEQ) Seismic E 1 nt alification(SEQj Core Re1 al ter Code Error alysis NuclearMat('
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] Engineering Analysis Preparation Review and preval Engineering Analysis Noot EA-FCo 90-063 Rev. Noo 0 Form PED-QP. 1 Pa 2 of 2 EA Pa No. i Engineering Analysis Cover heet File o. w/A Total Pages 338 ] PREPARATION / REVIEW: ($1GNATURE($)/DATE) Preparer (s) n. F. Mehaffev N/2 4 cv /of / 9b Reviewer (s) IFbD Independent Reviewer (s) 1 --t 8e// -v MLm sh//fe /I2Rh1 g- , , - AFFECTED DOCUMENTS: Responsible 1 Title Revision Division / Dept USAR Section 8.4.1.1 2 PED /356 SDBD-DG-112 Section S.I.3.1 3 PED /356 I I AFFECTED SYSTEM /EQU1 PENT: l System DG DG-1, DG-2, Al-133A, AI-133B, Tag No. VA-52A, VA-52B. l PED-QP 5.24 Rev. 0 7/8g
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' Engineering Analysis Preparation, EA No. EA-FCr e n-o n s .
. Review and Approval Rev. No, n Fern PED-QP 5.2 Page 1 of 4 EA Page No. a EA Review Checklist
- 1. Does the PURPOSE section adequately m o m' and correctly state the reasons or v i the need to prepare the EAT A
- 2. Does.the EA adequately and ce rectly address-the concerns as stated i.7 y the PURPOSE section?
- 3. Are the RESULT 5 and CONCLU$10NS .
stated and reasonable and supportive -l of the PURPOSE and SCOPET 1
- 4. Were the methods used in the performance of the Analysis appropriately applied? E I 5. Haveadjustmentfactors, uncertainties and empirical correlations used in the analysis _been correctly applied? X l
- 6. Were the INPUTS correct 1 selected and 1 incorporated into the EA I 7. Are all INPUTS"to the ANALYSIS correctly numbered and referenced such that the source document can be readily retrieved? X
- 8. Were the ASSUMPTIONS used to prepare the EA adequately documented? X
- 9. Is the information presented.in the ANALYSIS I accurate and clearly stated in a logical mannerf. 5 PED-QP-5.25 Rev. 0 7/89
I Engineering Analysis preparation, Review and A preval-EA Noo EA-FC. a n _ n n Rev. No.- 0 l
'I Form PEO-QP .2- Page 2 of 4 EA Page No. 4 :
EA Review Checklist' 1 i
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- 10. Have-the appropriate REFERENCE and the -
1 latest revisions been identified? $ l i
'I 11.. Have the REFERENCES been app wpriately i
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- 12. If manual calculations are presented in I X
the ANALYSIS are they:
- a. free from mathematical errorf X a
- b. appropriately documented consensarate v with the scope of the analysis? A I o 13. Have all documents that are 1 acted b the EA been correctly identifi and t e el effect of the impact clearly stated? Y , _ , , _ _
- 14. Are the EA and all references free of I J,. unconfirmed inputs? N l
- 15. .Have all crossouts or overstrikes been
[ initialed and dated by the Preparerf X I ! I V E
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Engineering Analysis Preparation, EA No. EA-FC. en-no Rev1W and Approval- Rev. No. n l Form PED-QP-5.2 Page 3 of 4 EA Page No. s EA Review Checklist I 16. Is the EA legible and suitable for m a m
- . reproduction and microf11 ming 7 X '
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, 17. Mas the EA been prepared and assembled in accordance with g pc soraph 4.9 of this proceduref y a <l
- 18. Mas the El. Cover Sheet been appropriately completed? y q
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- 19. For tw siens only, is ths change 1 E ident<"<ed and the reason for the i u5 change provided on the Record of )
L. Revision Sheet? N J
- 20. - Does the c uter run have page I number and phanumeric j program number on every sheet? N -]
'I 21. Is the listing of the final computer I input and output provided? N
- 22. Is the e uter code title and version /Selproperlydocument,ed .
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.t E 24. Is the computer program validated j and verified in accordance with N00-QP 57 2 q
- 25. If the computer program was developed 1
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E Re1inseringAnalysisPreparati:n, EA No. EA-FC. 9 0- 0 6 2 1ew and Rev. No. O Fore PED-@.2preval .Page 4 of 4 I EA Computer Analysis Review Checklist-EA Page No. 6 ~ ~ - I -26. If a vendor time share program was used has the program been qualified J.81 BR 1/A v under a QA Program approved by 0 PPD 7 4
- 27. Is the modeling correct in terms a
l efgtg input and initial I Note: For all "No" responses a written comment shall be documented on 'I CommentFormPED-QP-5.$brieflyexplainingthedeficiency and, as appropriate, providing a suggested resolution. I - i i I Comments: t b o Comment Resolution: I 1
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wy .___ _ ____- i it I EA-FC-90-062 Rev. 0-Page No. 10-eas TABLE OF CONTENTS 1.0 PURPOSE 12
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2.0 SCOPE 12 3.0 INPUTS TO THE ANALYSIS 12
4.0 REFERENCES
13 5.0 ASSUMPTIONS 13 6.0 ANALYSIS 13 7.0 RESULT $ AND CONCLUSIONS 29 8.0 ATTACHMENTS 30 s I l' I
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'; En EA Noot CA FC- ' 90-062
.c Re!insering'AnalysisPreparation iew and Approval Form PED-QP-5.4 Page 1 of 1 EA Page No. Il Record of Revision
'Rev. No. , Description / Reason for Change I 0 INITIAL ISSUE I
I I-I I' . I I I I I
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I I I PED-QP-5.31 Rev. 0 7/89: ;
':l4 g , EA-FC 90-062 W Rev. O Page No. 12 l3 eas l~g 1.0 PURPOSE The purpose of this Engineering Analysis is to establish with justification 'a the maximum outdoor am)ient air temperature at which diesel generators DG-1 and DG-2 can be expected to provide po.er to the Engineered Safety reatures 5 (ESF) loads and to identify those auxiliary systems required for the ESF loads to assure safe reactor shutdown should a Design Basis Event requiring p'E diesel generator response occur. This maximum limit also assures that '5 single failure criteria are met. t 2.0 itQ[1 The scope of this Engineering Analysis is to: l, 2.1 Define the worst case load and load profile. 2.2~ Establish the engine / generator outputs based on the ambient 4 i temperature and (Desel generator room effects. 2.3 Establish the capability of the generator / exciter to operate.in the diesel generator room environment. 2.4 Establish the margin available to allow operator restart of . equipment to enhance shutdown, i.e. an air compressor. l l I .2.5 Determine maximum ambient temperatures for which the DG's are - operable. 3.0 INPUTS TO THE ANALYSIS 3.1 Calculation number FC03382 Rev. 1, Diesel Generator LOCA Loads 3.2 EA-FC-89-026 Rev. O. FCS Diesel Generator Ambient Temperature Upper Operating Limits l'
- 1. J 3.3 DG-1 Testing Performed, 6/25/90 g 3.4 DG-1 Testing Performed, 6/26/90 8 3.5 DG-2 Testing Performed, 7/16/90 ,
q 3.6' DG-2 Testing Performed, 7/17/90 l 3.7 Power Systems Analysis of FCS Generator Capabilities 3.8 EMD Specification Sheet for the Generator i 3.9 Diesel Generator Nameplate data I 1 L i
+ -- . . , . . . . - - , . , , , -v . . - . ~
b l :l i y 3 m i f' EA-FC-90-062 .l l Rev. O i l Page No. 13 l k eas j
, I 3.10 ' Tables from the
- Standard Handbook for Electrical Engineers
I 3.11 E$-87-12, FCS Weather Tower Uncertainty Calculation #FC01381, Rev. J
4.0 REFERENCES
4.1 Letter ' dated 7/2/90 from M. . J. Fleckens'tein of EMD to - R. F. [ Mehaffey OPPD Engine Loads Above the 2000 HR Rating 1 4.2 Letter dated 7/20/90 from Roland Royal of G.E. to G. P. Schwartz - G. E Static Exciter , 4.3 Calculation ffC05487, Rev. O, DG-1 Ambient Temperature Operating I Limit. 4.4 Calculation #FC05486, Rev. O, DG-2 Ambient Temperature Operating l Limit I 4.5 " Data Reduction and Error Anal sis for- the Physical Sciences", Philip R. Bevington, McGraw-Hil ,1969, p. 71-72. i 4.6 Temporary Modification 90-019. I 5.0 ASSUMPTIONS 5.1: The sequential loading of"the diesel generator has only a 1 1
- j. secondary effect on long term engine / generator performance because j L loading is com)1ete within approximately 60 seconds and will not a be considered Tere.
I 5.2 Station Blackout analysis requires that the loss of offsite power and diesel generator onsite power must_be assumed. BasisEvent(DBE)'isoutsidetheboundsofthisEA. This Design . 5.3 Limitorque motor operated valves are not considered long term-loads. Cycling time is insignificant compared to long term loads. 6.0' ANALYSIS This analysis will' establish the temperature limits at which the ; l; engine / generator can operate the worst case safety-related loads in response i
- i. to a Design Basis Accident with a loss of offsite power. To accomplish '
L this, accident loading will be compared to elevated ambient air temperature ; engine performance based on test data taken during load operating runs of ; DG-1 and DG-2. The analysis also insures the static exciter and generator J can operate at the analyzed higher temperatures. L I ! I o
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EA-FC-90-062 ! W Rev. O I Page No. 14 ! u
- t L The analysis is organized to i
- 1. Determine the worst case accident load on the diesel generators. )
- 2. Model the worst case load based on time into the accident, p 3. Assemble the test data into a useable form.
l 4. 5. Establish the engine / generator output capability. Establish the engine / generator and exciter derating methodology. L
- j
- 6. Establish how the test instrument uncertainty affects derating (from no. j 5).
- 7. Define the derating equations using 5, 6.
n . . < l 8. -Analyze the derating of DG-1 using information from 2,3,4,7. l
- 9. Analyze the derating of DG-2 using information from 2,3,4,7.
L 10. Establish generator temperature limits using 7. 11'. Establish static exciter temperature 1imits using 7. h 6.1 Worst Case load and load Profile The Fort Calhoun Station is required to have sufficient.onsite I electrical generation capacity to safely shutdown the reactor and maintain it in a safe shutdown condition under all Design Basis Events- (DBE) which could result in a loss of offsite. power or He, require the assumption of a loss of offsite power (except station i 1: 5 blackout)- la addition. Sin 91 e failure criteria aust be met- The following discussions review the expected electrical /DG system requirements under specific DBEs to define the worst case load and lo d profile. 6.1.1 Worst Case Load - ? A rocess of elimination is used to determine the worst case load by looking at the equipment required to respond to a DBE. This is , discussed below. 1 pI 6.1.1.1 Reactor Trip and Coincident Loss of Offsite Power
]
E ~ I' A reactor trip and coincident loss of offsite power where the Reactor Coolant System (RCS) and the Steam Generator secondary system remain intact require a minimal amount of equipment for i LI !
.______._________________._______._i_____._________._____________s_. -
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w EA FC-90-062 LI Rev. O Page No. 15 eas safe shutdown. The basic systems required are raw water, component cooling water, auxiliary feedwater, charging, containmentcooling,andlowpressuresafetyinjection(shutdown cooling). In addition the operators would be expected to have the
^
instrument air system in operation. 6.1.1.2 bncontrolled Heat Extraction The most limiting Uncontrolled Heat Extraction case would'be a main steam line break in containment which would require automatic initiation of Engineered Safety Features. In this case the Raw' Water (RW), Component Cooling, (CCW), Charging (CH), Auxiliary I' Feedwater (AFW sequential start of FW-6 Containment Filtering and. Cooling'( ) Containment Spray (CS),, High Pressure Safety Injection (HPSI , and Low Pressure Safety Injection (LPSI) systems I'> will be automatically aligned and sequentially loaded on the diesel generator. The initial loading is expected to be nearly the same as a large break LOCA, however, once the RCS-inventory I has been restored, the HPSI and LPSI pumps will operate on minimum recirculation resulting generators. in a reduced load to the diesel 6.1.1.3 LOCA The ESF response to a LOCA automatically aligns and loads the ESF I and auxiliary systems on the diesel generator. In the small break LOCA case, the LPSI pumps- are ex)ected to be on minimum recirculation and not running at full 'oad. In the case of a tube rupture, containment spray is not required resulting in a smaller I. load on the diesel generator. In the large break LOCA scenario, the LPSI and HPSI pumps are expected to run at full flow until the SIRW Tank is. emptied. This represents the largest load for the
. longest time. The large break- LOCA loads will be used in all further discussions.
6.2 DG Peak Load The expected peak load based on a large break LOCA for DG-1 is I 2509.1 kW and for DG-2 is 2457.7 kW (calculation #FC03382 Rev.1, Attachment 8.1). The peak loads are expected to occur after the final loads have automatically sequenced on the diesel and accelerated to full speed. I 6.3 Worst case Load Profile I The large break LOCA load profile is based an loads which either reduce over time as a result of accident mitigation or receive automatic trip signals some time into the event. I .
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u j ' EA-FC-90-062 Rev. O Page No. 16~ . eas 6.3.1 ' Load Reduction Due to Containment Depressurization The reduced load over time criteria is met by the . containment
' filtering and cooling f ans (VA-7C, VA-7D, V?. 3A and VA-3B). These
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loaded to 100% power when the containment I>< fans are initiall
' air /steammixture s near 60 PSIG. As the steam in containment is condensed by the containment spray system -and containment filtering and cooling units, the fans unload-(due to a reduced air /steamdensity)toapproximately50% load. Using USAR figures I' 6.2-5 and t 6.2-6, the containment pressure;begins to reduce in pressure at approximately 100 seconds and 15 reduced to near pre DBA pressure approximately 2000 seconds' into the LOCA event.
I' Thgse curves are based on 3 s:) ray pumps, one spray header - 280 x 10 BTV/HR heat-removal. This is equivalent to one_ spray pump 6 I and one'large fan cooler with a heat removal rate of 280 x 10 BTV/HR as descriged in the USAR Chapter 6. One spray pump is' equaj to 140 x 10 BTV/HR and one large fan cooler is equal to 140 x ,10 BTV/HR.
- 6. 3. 2. Automatic Trip I The LPSI pumps meet the automatic trip criteria (no operator action required). These pumps are tripped on RAS which at minimuta safety injection occurs at a) proximately 3740 seconds (USAR Section6.2.5). This is approx mately equal to the flow based on I the safety injection pumps and charging pumps on JG-1.
6.3.3 Load Profile The load profile is graphed in Attachments 8.6 and 8.10 for each diesel. This load profile is based on;the~large break LOCA.
'6.4 Test Data Reduction Due to the room specific configuration for each ent,ine, testing was used to establish the relation between outdoor ambient air and N the critical diesel generator air temperature dependant functions.
I 6.4.1 The test- data used in this analysis was compiled using a thermocouple datalogger, engine panel mounted temperature gauges, and readings from the Fort Calhoun Station weather tower I thermistors. The critical parameters used in this analysis are outside ambient air temperature, combustion inlet air temperature (turbocharger intake air temperature) and jacket water outlet temperature. The analysis is based on the following:
- a. Thermocouple average temperature for ambient air inlet temperature.
I . .
.)! ! 4 ! 3-) :
'EA-FC-90-062 Rev. 0 Page No. 17-L, eas Thermocouple average temperature for turbocharger inlet iI" E -
b. c. temperature. . Engine panel mounted temperature gauge for. Jacket water outlet temperature, I d. e. Thermocouple for generator inlet air-temperature. . Thermocouples for exciter control cabinet temperatures.
- f. ' Weather tower 10 meter temperature reading..
Data reduction was accomplished in two steps. First, it.was determined that the data required could be compiled at 15 minute intervals.versus the datalogger 5 minute interval printout. This I was done due to the relatively slow rate of change of the observed temperatures. ,Second, averages were taken at each time interval where more than one thermocouple was used to measure the same . temperature area. 6.5 Enoine/ Generator Power Outout Criteria 6.5.1 Engine Capability The criteria used to verify that the ESF loads are acceptable are I based on insuring that the loads do not result in demands on the engine which would result in increased wear and decreased reliability. To quantify the engine reliability, Electro-Motive -, Division, General Motors Corporation (EMD) has established output j I' ratings. for its engines based on engine wear over a specified period of time. The time intervals specified are 30 minutes, 4 l i hours, and 2000 hours. The. time ratings provide a measure of: l I stress on the engine. Operation at these high loads should be_ minimized, however, the e ines are expected to provide reliable performance even with brie excursions into the 30 minute and four
' j]
d I+ , hour rating range. EMD has developed these ratings 4 based on i detailed knowledge of the temperature effects of elevated loads,. and experience with the engines (refer to Attachmat 8.32).
'i Following an engine ren that exceeds the interval rating it should I. be inspected for abnormal wear and refurbished as required to -
achieve the highest possible reliability for future use. I The 2000 hour rating is a guide to schedule maintenance frequency. Operation at the 2000 hour rating for 2000 hours would indicate that an inspection be performed at the end of the run. J I
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The. acceptance criterion used here is to minimize the time above
.the 2000 hour rating, q
The published engine ratings are based on turbo charger intake temperatures of 90'F. For intake temperatures above 90'F, EMD has provided de-rating curves (Attachment 8.2). These are straight I L ! I;
+ . . .
( EA-FC-90-062 Rev. O ! Page No. 18 l eas j I line curves showing intake air temperatures versus percent of full lead rating. The curve used- is based on jacket water outlet temperature (JWOT) of either 190'F or less, or 200'F to 210'F. ! For the purposes of this analysis where test data shows JWOT absve j 190'F,-the 200'F to 210*F curve will be used. j When jacket water outlet temperature and turbocharger inlet i I temperatures are known while the engine is heating up during the i initial stages of operation, a time versus engine / generator output l limit can be plotted for the 2000 hour en This is a ' more detailed view of engine performance.gine rating. 'I L In the highly unlikely event that a large break LOCA were to occur shortly after the engine has completed its monthly surveillance,
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the'30 minute rating curve would be applied to the initial LOCA 1 loads. in excess 'of the 2000 hour rating. - This would assure. 1 operation of the ESF loads based on EMD's expectations for engine performance. L Actual 90'F. rating of the engines is given in Attachment 8.26. l
'6.6 Deratino Methodoloov 6.6.1 Engine Derating 1 The limitin arameters for engine / generator power (in kilowatts)-
output are jacket water temperature.and turbo charger air inlet temperature. The jacket water outlet temperature (JWOT) LI i determines what turbocharger air intake temperature de-rating i curve is applicable. The percent of standard rating versus j elevated inlet ' temperature curves- (based. on jacket water 4 I i temperatures) are shown in Attachment 8.2. The graph shows two ' deratings, the upper ri ht curve is based on a JWOT of = 190'F, the lower curve on a JWOT n the range of 200*F to 210'F. -In this. i analysis, engine / generator power output is based on the 190*F L curve when JWOT is 190'F or less, and the curve of 200'F to 210'F-when'JWOT is above 190*F. For purposes of this analysis, 208'F will 'be used as the maximum JWOT, based on cylinder head life (refertoAttachment8.2).
]
The differential temperatures (temperature rise) from ambient l 4 outside air temperature to radiator inlet and turbocharger inlet L are based on-test data taken with an engine / generator output of i L 2500kW. The 2500kW is representative of the peak LOCA loads the L additional 9.1kW on DG-1 "s not considered to be significant DG-1 i peakloadis2509.1kW). The 9.1kW is 0.36% of the 2500kW load, i therefore, the heat contribution from 9.1kW of load to overall engine heating is minimal. 5'
l L3 EA-FC-90-062 l f5 Rev. O ! Page No. 19 ! eas j '. 6.6.2 Exciter and Generator Derating i
'{
L Temperature limits . for the generator and static exciter are l determined by taking the known upper limit of the exciter and L3 generator and reducing it by the rise between ambient outside and l l3 the respective exciter and generator- inlet . temperatures. ; Instrument uncertainty will be included in a conservative manner. j 6.7 Instrument Uncertaintv This ~ section discusses the expected uncertainties of the instrumentation used to measure the critical sarameters of ambient , I air into the diesel generator- rooms, ;acket water outlet i i temperatures, turbocharger inlet temperatures, generator air , cooling temperatures, and exciter cabinet air temperatures. L 6.7.1 Outside Ambient Air Temperature Uncertainty. : l Ambient Air entering.the room was measured using 6 thermocouples i mounted ' at the room air ' intake and recorded on a data logger. L Each of these type J thermocouples has an uncertainty of 2.2 C or 4 i3 3.96'F. .The data logger has a .72*F uncertainty, however, post- ; celibration testing indicated an uncertainty of .22*F. Using the '5 ; r .re root of the sum of the squares method, the loop uncertainty ive each thermocouple is
- 3.97'F. . ;
The use of six thermocouples to measure the ambient air E temperature will result in a more accurate reading. Using the- 1 lj error analysis method for multiple inputs of equal uncertainty as i e defined in Chapter 5 of " Data Reduction and Error Analysis for-the -1 Physical Sciences", reference 4.5 (Attachment 8.3), the overall ' uncertainty of the average temperature is reduced to the individual loop uncertainty divided by the square root of the .i total number of channels. For the ambient airLcase, the uncertainty would be
- 3.97'F# 6 =
- 1.62'F. The actual outdoor I ambient air temperature will be the average reading minus 1.62*F, which is conservative. The outdoor ambient air temperature calculated in this manner is conservative because this tem >erature l is used to calculate 6 elta Ts between the outdoor amb'ent and j other temperatures greater than : ambieht- (jacket water outlet, turbo intake air, exciter cabinet intake air, and generator intake air temperatures) which produces larger delta Ts. A larger delta Iw~ T will give a larger temperature rise above ambient for the system being analyzed yielding a conservatively lower upper temperature >
limit for that system. I I
iE EA-FC-90-062 5 Rev. O Page No._20 eas 6.7.2 Turbocharger Intake Air Temperature Uncertainty The turbocharger intake air (combustion air) temperature uncertainty was determined using the same method and equipment as I the outside ambient air temperature. In the case of the turbocharger air' intake, nine thermocouples were used. expected uncertainty is _t 3.97'F/(9 = a 1.32*F. For the purposes The
~o f engine derating due to turbocharger intake temperature, any I terperature rise of the turbocharger intake over ambient will be increased by 1.32*F, resulting in a conservative derating.
6.7.3 - Exciter Cabinet Inlet. Air Tamperature Uncertainty The exciter cabinet inlet air temperature was measured using one 4 e thermocouple at 6 height of 3' at the front of the panel which was g monitored by the same datalogger as ambient air. Using the same methodology as used for the ambient air temperature uncertainty the exciter air inlet temperature uncertainty would be t 3.97'F I since only one thermocouple is measuring the temperature. 3.97'r will be added to the exciter air inlet temperature when determining ~the upper limit. The This is considered a conservative application of uncertainty. 6.7.4 Generator Cooling Air Inlet Temperature Uncertainty The generator cooling air inlet temperature was measured using one thermocouple and the same datalogger as outside ambient air. The expected uncertainty is
- 3.97'F. The 3.97*F uncertainty.will be I subtracted from the upper generator operating temperature limit, which is a conservative application.
6.7.5 Jacket Water Outlet Temperature Uncertainty Jacket water outlet temperature was determined using an engine panel mounted gauge with an uncertainty. of a 2.0'F. The gauge I readings were compared to a calibrated thermometer with an uncertainty of
- l'F.
folicwing table: The results are shown below in the Calibration Gauge Thermometer D,nji Da.tg a Rg.dj.nq Readina Delta T DG-1 7/27/89 161'F 160.5'F 0.5'F 180'F 180.1*F 3.9'F 185F 182.0*F 3.0*F 188 " 184.3*F 3.7'F 189'F 186.0*F 3.0*F 191*F 187.3'F 3.7'F I I .
Y__ I , EA FC-90-062-Rev. 0
, Page No. 21' eas 192'F 188.2'F 3.8'F 'I 193'F 190.0*F 3.0'F Calibration Gauge Thermometer gn,i.t.
n pgg Readino Readino Delta T DG-2 7/16/90 170'F 170.0'F 0.0*F 180.0'F 0.0'F I 180*F 192*F 203'F 214*F 190.0'F
'200.0*F 210.0*F 2.0'F 3.0'F 4.0'F The specific area of interest for DG-1 is 188'F and for DG-2'is 195'F because these arc the steady state . jacket, water outlet 'E temperatures-used to determine the ambient temperature limits'.
W Looking at the data in the area of interest the gauge reading for DG-1is3.7'FtoohighandforDG-2is2.5'Ftoohigh-(derivedby. interpolation of the DG-2 190'F and 200'F data points). Based ~on this testing a
- 1.0'F uncertainty will be used based on-the ther::ometer uncertainty. This will result in a correction-factor being applied to each gauge reading. DG-1 readings will be I- reduced by 2.7'F and DG-2 readings, will be reduced by 1.5'F,
- maintaining the + '1.0'F uncertainty for ' jacket water outlet
-temperature, which is conservative.
6.7.6: Weather Tower Outside Ambient Temperature Uncertainty The weather tower 10 meter air temperature can be used to determine the margin available to manually load additional equipment' on the ' diesel generators. ES-87-12, Weather Tower
^
I Instrument Uncertainty Calculation FC01381 (Attachment 8.4), established a temperature uncertainty for the ERF' computer readout of'* .71*F. .This uncertainty is not considered significant, the reading alone without correction can- be applied. Data taken I during the;6/25/90-testing cor. firms the adequacy of the weather tower as shown below: ling lengr Therms.pmd.u. Delta T 14:38 87'F 86*F l'F I 15:30 17:40 90'F 89'F 89'F 88'F l'F l'F
'6.8 Basic Engine Limit and Rating Calculation Including Uncertainty I with a Jacket Water.0utlet Temperature Based Operating Limit I
I
0
~B ,
EA-FC 90-0C 3 , Rev. O Page No. 22
. eas The. basis for the following equations is that the < limits of concern vary linearly with outside ambient temperature.
A.. DG-1 Operating Limit = Tat - ((Tm - 2.7) - (Tg - 1.62)) B. DG-2 Operating Limit = Tm - ((T m - 1.5) - (Ty - 1.62)) C. DG-1 1.32)-(Tg Turbo Derating)Tanp., = DG-1 Operating Limit +- ((Tri +
- 1.62)
D. DGi2 1.32) -Turbo Derating) Temp. = DG-2 Operating Limit + ((Tri + (Tg - 1.62) E. Exciter Temp. Limit DG-1 = Ttt-((TE + 3.97) - (Tg - 1.62))
- F. Exciter Temp. Limit DG-2 = T tt - ((T + 3.97) - (Tg - 1.62))
E G. Generator Temperature Limit DG-1 = Tg - ((Tci + 3.97) - (fg - I ' H. 1.62)) Generator Temperature Limit DG-2 Tot - ((Tai + 3.97) - (T, y 1.62)) All-variables.are in 'F. T at - engine jacket water outlet limit Tm - engine, jacket water outlet measured in the test Ty - outside ambient air measured during the test T; - turbocharger inlet temperature measured during the test
.I. Tct . - exciter temperature limit g TE - exciter temperature measured in the test
- generator temperature limit
,I '
Tat Tai ierator inlet temperature measured in the test 6 '. 9 DG-1 E wine Deratina Analysis 6.9.1- Description of DG-1 Test I, tested on 6/25/90 .to determine room specific DG-1 was temperatures. . The test was conducted using water as the engine coolant. Readings were taken every five minutes from thermocouples and every 10 minutes of the engine jacket. water I, : outlet panel temperature indicator. Near the end of the test, the voltage regulator for the exciter f ailed. After repa*:r, DG-1 was tested on. 6/26/90 for operability and to obtain- test data on I . temperature behavior with the static exciter cabinet doors removed. This test will be used only to help establish exciter cabinet temperature limits, due to the rapid decline of outside I I .
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i m 1 ambient-ttmperature during the test. The test data-'istused to ' calculate;the maximum ambient temperature at'which DG-1 will be
< 4 considered operable based on jacket water outlet and turbocharger '
inlet. temperatures.- 63.2' DG-l'AmbientiAiriTemperature Limit Based on Jacket Water Outlet- r rTemperature-E ( Using Equation:A given in Section 6.8-and thc steady state testi y 4 data, the DG-1Loperating temperature limit can be' determined by: 'i J j E m. DG-1 Operating Limit = 208'f ((T3 - 2.7'F) - (Tg - 1.62*F))- , ? g = 109'F -l I .. . k M L 2Where Tg = 188'F and ' Tu - = 88'FL o It~ is believed that DG-1 would perform its design function during y a LOCA at1 109'F ambient, however 107'F will be used as the upper' E"< ambient-temperature limit since it is supported by-the present q 107'F limit from Calculation # FC05487, Rev. 0 (Attachment'8.5). ' s :6.9.34 LDG-1:Derating Based on , Turbocharger Air Intake Temperature Over ' y LTime
-If c the- diest ; vaerator output is modeled ~ based ion xtime andi L,
associated tert.:., atures, starting.with an assumed room ' inlet air 1 at 107'F and the engine at the jacket water preheated temperature,- -
",,'" -a plot of power output versus time can.be made. Using Equation C , 1 L
of :Section 6.8, ?DG-1 Turbo Intakr Temp. = 107'F.'+ ((Ty + 1.32) - d i (Tg - 1.62)) to calculate engine output during heating, a capacity. 9 versus time profile can'be developed., The-graph in-Attachment ,M I T *- , 8.6-1 is based on the data tabulated in Attachment'8.6-2 and shows " the. output capability versus time capability. y
' Also plotted on the graph in Attachment 8.6-1 is the expected 11oad
. . profile. As can be seen, the load profile exceeds the 2000 hour- ' limit by ap)roximately 0.94% maximum'at 780 seconds into the LOCA- i 'I M' and insign ficantly exceeds the 2000 hour rating for a brief.
-period before the Low Pressure Safety Injection pump trips. The t
~
load profile-is well below the 2000 hour limit for the remainder ' ' ,I of the accident. Since this graph is based;on actual test data
, with the engine having an approximate ~12 minute (4 minutes at idle
- from'14:14 to 14:18, 9 minutes from 14:39 to 14:47) period _of no load. operation before being fully loaded, this graph is "
s lI' conservative since. heating occurred during the first 12 minutes
-with no load on the engine. If the test data for turbo intake is
+ . corrected 3*F lowe ' .a negate the affect of no-load engine warming '
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EW , Ca nD wL + Page No. 24 , , eas b ' ? m' [h,n - that occurred in the test which wouldinot take place:in an auto: load 1 situation, tbn the! engine capcity 2000 hour kW r. ting
- 6 4
exceeds the load profile.(see Attachments 8.6-3 and--4). inis'is
#GF still i:onservative in that the jacket water outlet temperature was ig' i "> not adjusted. This is supported by the DG-2 data in section 6.10, F gg the-plots of DG-2 show the load profile below the 2000 hour limit forithe entire accident.- Since DG-P. is more temperature limited' <
b than DG-1, it is--judged that DG-1 would ' maintain 4the 2000: hour .
~ limit above the load profile for the entireTaccident since the
- t. . E*. diesel would be loaded =almost immediately upon being started and-
$@3 , -would carry the peak load with much cooler jacket water: and air-4 ~. temperatures. It is OPPD's,' judgement that the- increased 1 ti.mperature sensitivity of DG-2 outweighs the effects ofiani Me approximate-50 kW lower load'on DG-2 than,DG-1.
&1 b# ~
~ 6._9. 4 DG-1 Derating Based on a Hot. Engine
? t .Therelis expected to be a-period of some three hours perimonth-i P when DG-1 would be : at? elevated temperatures af teria' monthly -
'%j, surveillance test. In the event of a LOCA under these conditions,
- the engine would still be expected to perform its safety function.
"3 Attachment 8.7-1 shows the 30 minute, 4 hour, and > 2000 hour wg ratings based on a1107'F! ambient and a hot engine. The engine manufacturer, EMDf has indicated that the engine can successfully k, aw? carry the' load profile shown.
g3 , . 3 0,' Attachment 8.8' represents ;the' engine 2000 hourccapacity versus 73 outside embient temperature! with a maximum jack'et; water y' ' temperature of 208'F. Thistgnph shows the capacity of DG-l it-f2 ambient temperatures from: below 90*F to ~ the: maximumL limit of; 107'F. This graph can be used in conjunction-with-the weather tower temperature to determine the margin available to start other B'gla"! v loads,
'f , 4 6.10L DG-2 Enoine Deratino Analysis dc i
- 6.10.1 Description.of-DG-2 Test 'l
<!E4 i .DG22 was tested on 7/16/90 and 7/17/90 to determine room s)ecific ]
temperatures. The test on 7/16/90 was conducted using et1ylene- E
. E '..5 glycol (glycol) as the engine coolant and the test on 7/17/90 used l F c
* ' water as the engine coolant. Readings were taken every five
.s - minutes 'of the- thermocou ples and every 15 minutes of the engine s JWO panel temperature indicator for the test on 7/16/90 and every
- 10 minutes of the engine JWO panel temperature indicator for the test on 7/17/90. For both of these tests, the static exciter ,
cabinet doors were removed. The test data will be used to " calculate the maxie m ambient temperature based on jacket water a i 3, ll g , ;
~ ~ ~
n . A g; , m i; ' , 1 (-
' ~
i s , 5 gL , ' EA-FC-90-062 eg' Rev.~0= cPage No.=25
; eas.
. ' outlet-and turbocharger inlet temperatures.
) ,r 5 6.10.2 DG-2 Ambient Air Temperature Limit Based on .lacket Water Outlet Temperature ,
~ Using Equation' B given in Section 6.8 and- the steady state test dah , the DG-2 operating temperature limit can be determinedLby:
DG-2 Operating Linit = 208'F - ((Tx -- 1.5*F) - (Tg - 1.62*F))
. = 102*F where T fu == '195'F 89'F for the and test on 7/16/90-
= 103'F where T fg>==90*F 195'F andtest on 7/17/90:
for the w . The 103'F value ,s supported by Calculation # FC05486, Rev. O', .
? '
, ; which was based on data - taken 6/13/90 using glycol coolant (Attachment 8.9).
530.3: DG-2 Derating Based on Turbocharger: Air Intake Temperature Over.
~If thei diesel generator output -is < modeled - based on time and k,an c '
associated-temperatures,' starting with room inlet air at 103*F and lgj ~ i thetengine at the' jacket water preheated temperature, a plot.of
- power output versus time can be made. Using Equation D-of Section 6.8:--
E: e .DG-2 Turbo Intake--Temp. =:103'F + ((T u +.1.32)L- (Tg - 1.62)) Tocalculatkengineoutputduringheating,acapacity.versustime .,: f g. a' C' ' ' profile can-be developed. The graphs in Attachments 8.10-1 and 8.11-1 are based on the data. tabulated in Attachments B'.10-2 and
- c. 7
'8.11-2 and show the output versus time capability.
r; : .,.
,' Also plotted on the graphs in Attachments-8.10-1 and 8.11-1.is the expected load profile for DG-2. The plots of' Attachment 8.10-1 j,E ; and 8.11-1 represent the 2000 hour limit.of the' engine:at:103'F X. ambient- temperature with 15 minute -and 12 minute periods.
44 respectively from:enoine start unt4 'ully loaded. 'As can be seen,;the lead is below the ?000 nour limit. 6.10.4 DG-2 Derating Based on a Hot Engine <-
' Ep ' there is expected to be a period of s >me three hours per month W' . when' DG-2 would be at elevated temperatures after a monthly surveillance-test. In the event of a LOCA under these conditions, w + .
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'Page No.'26
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tn , a _ 4 p i DM the - engine would: be expected to perform its safetyLfunction. /sh-i p Attachment 8.12 snows the 30 minute. 4 hour,' and 2000 hour ratings based on~ a '93'F . ambient and a hot. engine.
. manufacturer, ~ 3, has indicated that the engineican successfully-The- engine-t t
carrytheloudprofile,shcen"(refertoAttachment8.32).
~
N Attachment 8.13 represents the engine 2000 hour L rating, versus 1 outside ambient = temperature .witho a maximum. jacket water: j b *f .L temperature of.'208'F. This graph.shows the capacity of:DG-2 at' 1 ambient temperatures from = below 90'F to the maximum limit L of-g . 103*F. :This, graph'can be used in conjunction with the weather- ;
,rc . tower temperature.to determine the margin available to start other '
loads. j y . 6.11: :DG-l'and DG-2 Generator Temperature Limits' > E 6.11.1' . Generator Peaking Duty Temperature Rating h -in " Gg The, generators' Np9er. temperature limits can be derived from the nameplate -data of the generators which specify the rotor and E .statorainsulation temperature rise limits. .See Attachment ~8.14 E -and the- EMD Generator Characteristic Data, Attachment' 8;15. The-- -t ,5 o . peaking stator rise limit rating is.105'C and the rotor rise limit-is:70*Cabove40*C(acommondesignnumber).-'Fromthegenerator 1 data sheet, the load based rise 'at 2500 kW (wh kh represents the - peak DG-loading by 0 PPD)-is:56*Ccfor the stator and 50*C for.the:
~
+ 3 rotor ' ,above ' 40*C, ' This equates to a - limit of 60'C. maximum- '
? temperature! (40'C ambient, plus a 20*C margin ~ ino the stator R between ' the 70*C limit and the 50*C ' load ~. induced temperature.
- g rise).. l ist Theoperating
- temperaturelimitswoul'dbe'60*C(140*F)minusthe- l
,J5 room inlet to the. generator inlet temperature rise and correcting ! h for uncertainty as shown in. Equation'6.8 G and'H. Attachments A 8.~16 through 8.18 provide plots of the' generator inlet temperature. : ig P rise. Using the data in Attachment 8.21-1 to determine generator-air inlet' temperature rise, a limit of '121'F 'can be calculated for j DG-1. Using the data from Attachment 8.18-1 to determine : H lE h _ generator! inlet air temperature rise, a limit of 114*F can. be' ' l; E calculated for.DG-2.
- .n ;
E 3, Please note that when using the data, or graphs in Attachments } 4; 3 8.16 through 8.18 the data taken when the room fan is.off should " lE be used, since fans VA-52A and VA-528 are not to be in operation. l 6.11.2 This judgement is supported by the ratings of the Class H insulated stator and Class F insulated rotor. Looking at motor
~
insulation ratings (which can provide information on the ! [f r ' i T .. _ _ __ ___._________-___.____.-----.._---__---m--_ - - - - - - - - - - - - - -
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[4 g<m ' EA-FC-90-062 1 Rev. 0- , am " n , Page No. 27 - g
.M eas sy.- + ,
j> insulation. systems),. Class F insulation is.ca)able of 105'C rise
,&^ W i '
above a 40*C ambient and Class H' insulation s capable of 125*C- , trise above a 40'C ambient. Refer to the tables in Attachment'8.19-: 1 taken from the " Standard Handbook for Electrical Engineers". 3
, '6.12 Exciter Temperature Limits-l j _6.12.1 Exciter Limit ,
a " , . Each Emergency Diesel Generator (EDG) receives field: excitation- ^3 via a General Flectric Model 357930SA212A11' Static Exciter. These E exciters were part of the original EDG installation andL are - ,
-approximately.20 years old. G.E. (Letter dated' July 20, 1990,
,in: Attachment-8.20-1) has stated that the open exciter panel will y' ! at- 50*C. . Since both doors- to each *
, exciter have no problem operating (Temporary Modification TM-90-019 ref.
panel were removed 4.6), the. exciter < panels are now considered to be in open air. In-
- E 1
this configuration,'the ambient air reaching the exciter panels , 1 5 has not reached 50'C-(122'F). , 6.12.2i Exciter Test Data IA EDG tests performed 6-25, 7-16, and 7-17-90 show that the exciter o can safely be operated at the- present DG .'outside ambient M j' , temperature limits and=will'be used as the basis for the.following discussions. Based on-the test data,.the running of the VA-52:
.N i fans:during engine ope ation causes elevated temperatures at the-
-exciter cabinet. TNs > data will not be used in the: analysis.
I>> 1 LTherefore, the faas shall be off. m 6.12.2.1 DG-1 Test performed on 6-25-90 1 Thi test measured exciter panel temperatures near the exciter
'4 (panel! doors on) at'3and 8' heights above the floor with-one
~
m Es type J thermocouple at'each height. Since only one thermocouple u~- was'used for the 3' measurement (the ambient air intake-to the
-exciter panel if:it were ventilated), the full 3.97'F thermocouple-13; Luncert'intya will be used for the air:near.the exciter cabinet.
l3; There were 6 thermocouples measuring intake air to the room,
;, therefore l'. 62
- F uncertainty will be used for ambient-air ,
temperature. 1 Attachment 8.21-1 shows the relationship between the intake air to J the room and the ' air near the exciter cabinet at 3 and 8 feet ; above the floor, uncorrected for instrument uncertainties. The j
~I~ air near the exciter cabinet very closely follows the intake air i to the room until about 17:00 hours when the VA-52A fan is turned f ; on in the supply mode. The exciter air near the cabinet starts y.
f
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.h 4 p '
s EA-FC-90-062 Rev. 0 ~
,m '
Page No. 28 s eas on in'the supply mode. The exciter air.near-the cabinet starts increasing and no longer follows the intake air >to the room. At-I 17:41'the fan is' switched to the exhaust modo. At this time the-air near the cabinet makes a considerable juma in temperature and- ,
, I then appears to level off at 18:15 hours while the fan is in the ,
JW exhaust mode, o4 ,
- ' O The delta T-is (90.8'FL Using
+ 3.97 -:)ne values=at7.3'F; (89.1-1.62) 17:00 hours The (fan outdoor maximum off) ambient could 8' , reach 122*F , 7.3*F = 114.7'F.
6.12.2.2 OG-2 test performed 7-16-90 4 This test measured ambient temperatures using type J thermocouples>
- F^ at 3' and 8' heights above the floor.at each side of the-exciter J cabinet.- Also,.nine th,ermocouples were placed inside the exciter cabinet to measure ambient air temperatures near components in the-cabinet. This test was' performed with the doors to the exciter-I cabinet removed. Refer to Attachment 8.22 for. sketches of thermocouple locations. The 3' thermocouple reading will be used
-as the basis for determining the maximum allowable outdoor ambient .
I-temperature.'
~calculations thermocouple, Since this reading:.was taken with. a<, single-(the refer to full uncertainty
'section. 6;6.1- ofof 3.97'F must be used this analysis).- .The-in the =
outside^ ambient temperature .was measured with.six thermocouples.
<I' :.
with a combined average uncertainty of~1.62*F (refer to section
. 6. 7.1 )l. .
Attachment 8.17 shows that the exciter; intake air tracks' the-intake air to the room while the VA-52B fan is off (up to 17:17 . i! . hours).' For purposes of deter;nining' the. delta' T between outside-4 ambient air and exciter cabinet intake air the values at 17:00--
?I:- hours will.be used. At 17:00 the air intake to the room is 88'Fr '
and ithe. 3' cabinet air ~ intake 99'F. Therefore, the delta T-is (99+3.97) - (88-1,62) ='16.59'F. This: indicates that to maintain I the exciter intake air at 122'F max., the outside ambient air can - be 122'F - 16.6'F = 105.4'F max.
-6.12.2.3 DG-2 test performed 7-17-90 This test was performed and temperatures calculated as in the DG-2
;m; test performed 7-16-90 above.
g. Attachment 8.18 shows that the exciter intake air temperature rose until it-reached a constant value and then held that value for the The VA-528 fan was off'for the whole test.
- f: :
rest of the test. Therefore, the delta T between outside ambient and the 3' exciter 1 cabinet intake air temperature will be taken at 19:00 hours. This
.I.
r
;s. ,
+ <
tw% g%,lW E '
^
f['g* , EA-FC-90-062-Rev. 0
"' Page No.-29 A ; eas- !! ,m E ,' , delta T,is:(101+3.97) - (90-1.62) =116.6*F. .The maximum outdoor e -ambient temperature based on this-test can reach I?2*F -'16.6*F =
a q;i 105.4'F to keep the exciter intake air from exceeding 122*F and-
"' confirms;the: data'taken 7-16-90 for DG-2.
6.12.3- Exciter-Panel Internal Temperatures f Table 1 of- Attachment 8.22 contains- approximations: of - average temperatures inside the exciter' cabinet with-the doors removed;- J The temperatures listed are measurements of ambient air inside the y', cabinet which is heated by components in the exciter such as SCRs J ; and power 1 resistors. As shown in Table 1, the upper portion of
'- - i the cabinet is warmer, while the bottoiarea is cooler.= This:is-.
% what-is to be expected since the air entering the bottom is heated-by exciter components as it travels. upwards.' Points C, F,.and-J
, from Table 1 are graphed'with the 3' outside cabinet front readingM
'in. Attachments 8.23, 8.24, and 8.25. . The 3' points (datalogger-channel 42. from 6-26, _7-16, and 7-17-90 . tests) is used to .
I represent the ambient air intake to the exciter cabinet throughout this analysis. As shown in the graphs, L the 3' point- is, an - accurate representation.of cabinet intake ambient air temperature. I4 7.0 RESULTS AND'CONCLUSIOF1 7.1L , Results
-Max. Out. Ambient 1 Max. Oit. Cooling Max. Out.- Ambient Based.0n iy Amb. Litjl Liauid Amb. Exciter Generator Fan' Status-DG-1 107'F- Water 114*F 121*F .VA-52A off DG-2 103*F Water 105'F 114*F VA-52B off-7.2 Conclusions Based on the results of this analysis, the maximum outdoor ambient'
- I air temperature for each diesel generator to carry the loads as stated in the purpose are as follows:-
Maximum Outdoor Ambient Temoerature DG-1 107'F 1 ? DG-2 103*F L ~ These limits are based on the diesel generator's anticipated jacket water outlet and turbocharger air intake temperatures based f
~r,, _ E' " ' ' y' , s 4 :, s y. L [ ' is , EA-FC-90-062-
.Rev. O!
Page. No._' 30 - eas 3 temperatures allow each dieel neerator to operate within its-i 1 2000 hour rating for-the'LOCA1 analyzed here.. Additionally, the generator and exciter cabinet (with..the doors removed) are not expected to see temperatures which would exceed their limits.o The > VA-52A and B f ans shall be "0FF" when the respective diesel -is' ' aim a
, 4 run.
R Through the course. of the accident (LOCA) the diesel generator will: unload to a point below the 2000 hour rating of:the engine. The kW margin between the actual load and the 2000 hour rating is available for addition equipment stcrts, for the large break 1LOCA l- - analyzed here. ' Actual margin 11s dependant on the pump loads and-ambient air-temperature.
. USAR Section 8.4.1.1 -and SDBD-DG-112 - Section- 5.1.3.1 must < be-Ir4 ~
' updated as a result of this analysis.
8.0LLIST OF ATTACHMENTS
-Attachment Descriotion Calculation number FC03382 Rev.1 Diesel Generator LOCA:
?I , '
8.' l -
- Loads c8.2 Derating)
(2 pages curves for EMD diesel at elevated temperatures
; )
i 8' 3. " Data Reduction - and Error. Analysis for the: Physical-
- Sciences", Philip,R..Bevington, McGraw-Hill, 1969, p.
S' .71-72. U .' 8. 4 - -FCS Weather Tower Uncertainty Calculations
.8.5 Calculation #FC05487, Rev..0, DG-l' Ambient Temperature.
n Operating Limit
# .8.6 DG-1 Load profile (6-25-90).and 2000: hour derating-(4' pages) 18.7: Graph of DG-1 Derating at 107'F' Ambient (2 pages) i 8.8 -Graph of DG-1 Output Power vs. Ambient Temperature ~'(2
.pages)
M 8.9 Calculation #FC05486, Rev. O, DG-2 Ambient Temperature r Operating Limit
- 8.10 DG-2 Load profile (7-16-90) and 2000 hour derating (3 Kh m pages)
W y '8.11 DG-2 Load profile-(7-17-90) and 2000 hour derating (2 pages)
~~
- 4 u 8.12 Graph of DG-r Derating at 103*F Ambient (2 pages) 8.13 Graph of DG-2 Output Power vs. Ambient Temperature (2 pages) 8.14 Diesel Generator Nameplate Data
+I ,
8.15 Attachment EMD Specification Sheet for the Generator DescriDtion y,
y I EA-FC-90-062 Rev. O Page No. 31 eas Attachment Description 8.16 Graph of air temperatures for DG-1 on 6-26-90 2 pages 8.17 Graph of air temperatures for DG-2 on 7-16-90 2 pages 8.18 Graph of air temperatures for DG-2 on 7-17-90 (2 pages) I 8.19 Tables from the " Standard Handbook for Electrical Engineers" G. E. letter dated July 20, 1990 (2 pages) 8.20 8.21 Graph of air temperatures for DG-1 on 6-25-90 (2 pages) l 8.22 Sketch of exciter cabinet front thermocouple locations 8.23 Graph of inside and outside cabinet temperatures for DG-1 on 6-26-90 (2 pages) 8 8.24 Graph of inside and outside cabinet temperatures for DG-2 on 7-16-90 (2 pages) Graph of inside and outside cabinet temperatures for DG-t 8.25 8.26 2 on 7-17-90 (2 pages) Letter from Ted Fryar of Morrison-Knudsen to Randy Mueller, dated 2/21/80. 8.27 EA-FC-89-026 Rev. O, FCS Diesel Generator Ambient I. Temperature Upper Operating Limits Data from DG-1 Testing Performed, 6/25/90 8.28 8.29 Data from DG-1 Testing Performed, 6/26/90 8 8.30 Data from DG-2 Testing Performed, 7/16/90 8.31 Data from DG-2 Testing Performed, 7/17/90 8.32 Letter dated 7/2/90 from M. J. Fleckenstein of EMD to R. I 8.33 F. Mehaffey 0 PPD Engine Loads Above the 2000 HR Rating (2 pages) Telecon dated 8/16/90 between EMD and R. F. Mehaffey 8.34 Temporary modification 90-019 8 8.35 Test Instrumentation i I I I I I I _. _
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.. enst Approvel.
- FC /B 9 0 % *10TAL PAGES & 48- (7-Form PED-OP-3.11 Form Page No. 1 of 2 0A Cogogpery: _ lt0E O LIMITED COE C FIRE PROT.
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CE CULATION TITLE vel 830R CALC.ND. N / A s AM3e/ Genenl0v LOC & D MR NO. u O f:
- O ENOR. AN EYSIS
!" e ":- 0 000 NO.
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+Q 9; cAPPROVALS - SIONATum & DATE C0pgrI9tATION O'E' SUPERSEDES .=0urmo(<>
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" EA-FC-90-062, Rev.0 ATTACHMENT 8.1-2 J Celculeuen Preparacon., Review CE M ATION N l Cale.Page No. E cnd Appeoval Form PED-OP-3.1 Form Page No. 2 of 2 pg gJ Jgg ,
Celouleuon Cover' Sheet. FACILITY / SYSTEM ff% l M g xtwono. O ~ Or < achs% r .. [ cALcuLAT!ous ueED AS INPUT IN T E ANALYSIS EQUIPMNT TAGS g - c. . . ,.... ,, A.,,, _ 77F2 502, L L JFG D4 I ,a bl v2
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EA-FC-90-062, Rev.0 m;, e ATTACHMENT 8.1-3 [ aunaE R 3' E 'MLCULATION PREPARATION, REVIEW AND APPROVAL
; FORM PED-4P-3.2 Form Pass No.1 of1 CALCULATION NO*
PRODUCTION < ENGINEERING DMSION FC03382 CALCULA110N . REVISION - SHEET REV* NO. DESCRIPTION / REASON FOR CHANGE
- 0. ' INITIAL ISSUE 1
Added~VA-63A, VA-63B, VA-64A, VA-64B, and deleted VA-63 ner MR-FC-87-20. CH-1A CH-1B, CH-1C: Changed load from 62.2KW to 50.0KW due to section 6.4.1 of EA-PC-90-76. EE-dRt chanced' load from 10KW to OKW due to Tnvertar el in ammumaa +n ha powered'from the battery charger which is already assumed at full load in this calculation. VA-BOAR chanced load from 4.36KW to OKW. van in manually e+mv+=A ann + hydrocen removal - not recuired for initial stace of accident. l I i l. t yf PED-QP-3.29 m
. o-ngo 4' i . ,T' EAFC-90-062,Revod--
~5 L ATTACHMENT:8.1- ,
- .,. o -cas,rna a c
CALCULATION PREPARATION, REMEWi AND APPROVAL CALCULATION NO. (FORM PED-QP-3.3 - FORM Page No. l'of 5
, ;o .
pc en .-:.' 1
- i ;g' PRODUCTION - ENGINEERING c CALCULATION
SUMMARY
SHEET Rev.No. N-
^
0 ELECTIVE t f In . WT ROTRICAL inaEING MODEL FOR- DIESEL GENERATORS i The . objective iof this: calculation,is to provide a model-of'the 4
- expected ; l ' loading- ofL each _of the emergency' diesel' generators.
DG-2 .w hich; load in response to:a. Loss of Coolant DG-11 and (LOCA) coincident with a loss-of-.offsite power. This
-Accident
~ model -will. begin with.-_the point in time.in which.the final' sequenced., load '. group.has accelerated to full speed'and running-at;.its! expected- accident load and will and at the point RAS '-
occurs.- 4-IIh 4 II
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l, ' EA-FC-90-062,'Revc 0 p< i. p ATTACHMENT g 8.1.
! CALCULATION' PREPARATION, REVIEW - AND APPROVAL 4 < FORM PED-QP-3.3 FORM fogo No.2 of 5 CALCULATION NO.
U PRODUCTION ENGINEERING CALCUdTION FC FC D'l3R2 s :
SUMMARY
SHEET Rev.No. f . METHODS = ni The load information for equipment loaded on the diesel generators will be calculated and summarized using the ELMS printout and othe ELDL database (See' Inputs). The Load Shed-Infornation- Summary will include the load shed status and r'd electrical load in KW for each item listed. The load (in KW) for each motor can be determined by: [ Rated HP)-x 0.746 KW/HP P (in KW) = ----------------------------
% efficiency The . load (in KW) for each load given in KVA can be determined by:
P (in KW) = (load (in KVA)) x (power factor) The Load Shed Information Summary for DG-1 includes 4.16KV Bus 1A3 and all~ 480V .Busas ied from 1A3i These 480V. Buses are 1B3A, 1B3A-4A, 1B3B, 1B3C and 1B3C-4C. Also included in the summary is any 480V MCC that is fed from one of the aforementioned 480V Buses and is not load-shed. These MCC's I i are MCC-3A1, MCC-3A2, MCC-3B1, MCC-3C1 and MCC-3C2. Load Shed.Information Summary for DG-2 includes.4.16KV Bus I The 1A4 L1B4A,' and~ all-'480V Buses' fed from 1A4. These 480V Buses'are-184B, 1B3B-4B and 1B4C. Also included in the summary is any 480V MCC that is fed from one of the aforementioned 480V Buses and is not load shed. These MCC's are MCC-4A1, MCC-4A2, MCC-4B1, MCC-4B2, MCC-4C1, MCC-4C2, MCC-4C3 and MCC-4C4. note that load shed means 4.16KV load shed, 480V under I iPlease voltage breaker trip, ESF 480V load shed, OPLS load'shed and those control circuits which drop out as a result of loss of offsite power and require manual starting. The value (in KW)_ of the load for each device which is load shed or is sequentially loaded will be placed in the " LOAD (KW)" of the Load Shed Information Summary. Each device which I column is not- load shed needs to be examined to determine whether it is a continuous or intermittent load (such as valve cycling). 91 m aus I- _ . _ _ . _ . . . . . _ . . _ . . _ _ . . . _ - . . . _ . . . . _ . . . _ _ . . _ _ _ _ _ . . . _ . . _ _ _ . _ _ _ . _ . -
EA-FC-90-062, Rev.0 4 ATTACHMENT caraam a 8.1b i l CALCULATION PREPARATION, REVIEW- AND s APPROVAL FORM PED-4P-3.3 FORM Page No.2 of 5 CALCULATION NO. FC 'l '
. PRODUCTION ENGINEERING CALCULATION
SUMMARY
SHEET Rev.No. .M
' METHODS g The :value (in KW) of a continuous load will be placed in the g " LOAD (KW)" -column while the value of a' intermittent load will be placed in the " INT LOAD" column of the Load Shed Infornation Summary.
_Also included _in the summary will be the cycle time (in seconds)-for any applicable valve '.isted.
~
, once. the Load Shed Information Summary is completed, a total.
will be determined for non-load shed continuous loads, non-load , and sequential loads. As noted in the.
- .shed -intermittent the- .intermittent loads loads are not. considered part of' I, assumptions, the total long time. running load on the diesel generators. The total. load on each diesel _ generator is equal to the sum of the total not- load- shed continuous load (dead load) and the total I : sequential load.
;The expected containment cooling fan load will be estimated on 100% load at maximum containment pressure and 50% load I based during~ " normal" condition - no steam / air atmosphere. It will
-be -limited 'for the purpose of this cal ulation to a minimum long term load 1of 75% of motor name plate rh 'ng I
I . t. t - t
. iES l 4
EA-FC-90-062, Rev.0 ATTACHMENT 801- 7 CBRNE ak 7
'MTION PREPARATION, REVIEW AND - APPROVAL FORM PED 4P-3.3 CALCULATION NO.-
FORM Page No.3 of 5 l
- PRODUCTION DeGINEERING.CALEULATION MN N Rev.No. 1 ASSUMPTIONS
- 1. Non-load. shed -loads which are used intermittently are not considered- to be part of.the total longer term load on the diesel generators.
- 2. Equipment which is used _ infrequently, such as , welding receptacles .-and stress gallery disconnect switch, are assumed to have noLload.
3...When % efficiency or power factor. information is. not available, a power factor = 0._80 and a % efficiency = 0.95 I will be'used as typical values for electrical equipment. 4.- The . diesel generator model assumes that the-sequenced load I group has accelerated to full speed and is running at expected load.-
- 5. is . assumed to occur with minimum safeguard actuation-I RAS maintaining: the highest diesel loading for the maximum expected time on each diesel generator.
I 6. This-. model assumes that no manual' restart of. equipment such-as' air compressors, turbine- plant- cooling Auxiliary Building ventilation-fans occurs. pump, and 7 The : charging. pumps-are assumed to operate mt full load for-the duration of time covered in this calculation. N I 8.- The-. calculation represents the worst case in that equipment
.which could be running (not- intermittent) is running on
.each safeguard train at the time of the-loss of offsite power and'DBA.
- 9. For. conservatism >.the battery chargers are-assumed at-full =
I load. s PED-QP-3.32
+
+n bc ,
'EA-FC-90-062, Revc0
, ATTACHMENT!801-O j;
+ ans fea m 8-i %LCULADON PREPARATION, REVIEW AND APPROVAL M N-3.3: PORM Page No.4 of 5 M D O N N O.L a/ PRODUCTION ENGINEERING CALCULATION 8 Rev.No. 1 INPUTS / REFERENCES
- REF.
- 1. -Sargent' &, Lundy Electrical Load Monitoring System (ELMS) NO.
I Printout. I ;2. ' Electrical Load Distribution Listing-(ELDL), Vol. 3, 4.16KV1 and 480V Buses and MCCs.
- 3. =GHD&R Drawings 11405-E-3, 4.16KV One Line Diagram I 11405-E-4, 480V One Line Diagram, Sh. l' 11405-E-5, 480V One Line Diagram, Sh. 2 11405-E-6, 480V MCC One Line Diag., Sh. 11
~11405-E-7, 480V MCC One Line Diag., Sh. 2
'4. GE Drawings-177B2371, 480V MCCs Elementary Drawings.
'5. EEQ Manual, Section 2, Containment LOCA Response Curves.
- 6. . :USAR, Figure 14-6-6, Containment Response
- 7. USAR, Section 6.2.5, Time to RAS
'8. . USAR, Section 8.4, Emergency Power Sources 9.- Stone- & . Webster Calculationo(16472.19), Confirmation of D1 a and D2 Loading.
"g i(,
- 10. EA-FC-90-76:
Cable Tray, Loading Calc / Justification I >
' 11. MR-FC-87-20:
Replacement. Control Room Outside Air Filter Unit Q
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EA-FC-90-062lRev.0L
's ATTACHMENT 8.1-S ;I m a,a n m 9 !
g ?'.ALCUMTION- PREPARADON, REVIEW AND APPROVAL ! E FORM N 3.3 FORM Pass No.5 of 5 DM NO. i I g PRODUCDON ENGINEERING CALCUMTION g
SUMMARY
SHEET gey, No. 1 W , CONCLUSIONS.. I Attached ~ are DG-2. the L Load'Shed Information Summaeies for DG-1 and These = summaries note the'-- load shed status for each
. device, .the -load in KW, the intermittent load (if applicable),
and the cycle time (in seconds) for appropriate valves. l To- determine the. loading .on each diesel generator, the total , l sequential- load and^the total non-load shed continuous' load are needed. The total' non-load shed intermittent load will also- be p found, ml5 , Reference the attached: Load Shed Information Summary for DG-1 for. load -information~ on individual equipment loaded on DG-1. l The load totals for DG-1 are a*Lfollows: j Total-Non-Load Shed Intermittent Load : 61.3 KW l Total Non-Load Shed Continuous Load : 296.5 KW Total sequentialfLoad : 2212.6 KW- $ Therefore, the total load which would be loaded on DG-1 as A result of LOCA coincident-with a. loss of:offsite power is i 296.5 KW . + 2212.6 KW = 2509.1 KW y After i '.approximately 2000 seconds the ventilation fans VA-3A and , VA-7C i teculd be- expected : to: unload by approximately 25% of . rated j l KW or -73.6 KW. This would reduce the load'to approximately 93 2435.5- KW. At RAS 3740 seconds into the event (minimum safety _l4 5 injection) SI-1A trips, reducing the load a further 235.6 KW to
'2199.9 KW. IY I I 1 EI I ,I I
I. = =-ut 1
$) EA-FC-90-062, Rev.0
,, y '
ATTACHMENT 8.1-/o-I"
- r u psE m /O
, 4l'ALCULATION 0RM PED-4P--3.3 PREPARA110N, REVIEW FORM . Page No. 5 of 5- AND APPROVALCALCULATION NO* ~
fc d ass 2_ PRODUCTION ENGINEERING CALCULATION
SUMMARY
SHEET Rev.No. 1 [ CONCLUSIONS g Referenco the ' attached Load Shed Information Summary for DG-2 g for- load information. on individual equipment loaded on DG-2. The load totals for DG-2 are as follows: Total-Non-Load.Shed Intermittent Load : 208.6 KW t Total-Non-Load Shed Continuous Load Total Sequential Load a 588.0 KW. 1869.7 KW 9' Therefore, the total load which would be. loaded on DG-2 as a result of LOCA coincident with a loss of offsite power is-588.0 KW + 1869.7 KW = 2457.7 KW g i After approximately 2000 seconds the ventilation fane VA-3B and [ VA-7D would be expected to unload by approximately 25% of rated KW or 73.6 KW. This would reduce the load to approximately 2384.1' KW. At RAS 3740-seconds intoload the aevent.(minimum safety l b. injection) SI-1B' trips,. reducing the further 235.6 KW to-2148.5 KW. l_ f f} PED-QP-3.34 I. ~ i
,;.7,7,,_ , , I !t , EA-FC-90-062, Rev.0-
;, ATTACHMENT 8.1- it j[ U ammam i ~ /b 'I CALCULATION PREPARADON, REMEW . AND APPROVAL CALCULATION NO*
4 c FORM PED-QP-3.4 Form Page_ No.1 of1
;; pc w a> .
PRODUCDON ENGINEERING:DMSION CALCULAMON' SHEET , Rev.No.
.j .
REr. NO. 1.' O LOAD SHED INFORMATION FOR-DIESEL GENERATORS DG-1'& DG-2
<I. ' Attached Jare the Load' Shed Infornation Susanaries for -
' Diesel Generators DG and DG-2 g Each. suunnary was
[ database- which Lfrom a- .Knowledgeman _ developed
! contained ~'~ load information for each electrical device e ' included in the calculation.
The>Iheading'of the printout'contains the page number, title,: revision namber and revision date. The first
- three; columnst contain the source bus number, breaker I number and' device tag number, respectively. The next-column- shows the load shed status for each tag. The column 'will! have,a "YES" for load shed loads, a "NO" 1 for not~ load shed" loads and a " SEQ" forfsequentially-loads..
-The; column (LOAD) and, the sixth column
( fifth' (INTERMITTENT' LOAD) contain the actual-value of the cload 7 1n Kilowatts .(RW). If the load is continuous, the 'value- will be; located in the " LOAD" column. If-the;(load! is -intermittent, the' value 'will be in-
" INTERMITTENT LOAD"~ column. For equipment which would. constitute .no load in an emergency > situation, such as welding receptacles, cranes and-fuel handling equipment,~ both columns will be sero.
",- l The 'next two columns contain the cycle time'(in l- for applicableL valves. If the valve fails seconds)t he time will be in the- "OPEN" column.
open,
.Similarly, if the valve fails closed, the time will be shown in the _"CLOSE" column.. The final two columns contain the related schematic drawing-number and any comments c
I'< ? '
~
After al1 of the equipment records have been printed, the; load totals <are printed on the last-.page. Given
? :are. the total not load shed intermittent load , the total not load
'1 J
=
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g lh ii ' EA-FC-90-062; Rev.0-L . ATTACHMENT 8.1-12.
]g ag '/2 CALCIAATION PREPARATION, REVIEW AND APPROVAL.
CALCULATION NO*- FORM PEN 2P-3.41 Foem Page No.1 of1 a pg- pg ., 7 , . i; PRODUCDON- ENGINEERING . DMSION: CALCULATION' SHEET Rev.No. 6 REF.
- NO.
. shed' . continuous load (dead load)= Land the total' sequential, load. The- total not load- shed intermittent . load ~ is the sungnation of the loads: for-each tag which had a "NO" in the load shed' column and; the value of the:locdiin the " INTERMITTENT LOAD (KW)"
. column. The' total dead load is the-sumnation of the
- loads for each: tag which had a "No" in the~ load shed column and- the value-of the. load in the " LOAD (KW)"
column.- The total sequential load'is the sununation. of ' the . loads for each . tag ;which had a "S::Q" in the load shed column. The value.for each sequential load
.is :in the " LOAD (KW)" column. The final number shown.
is. the total' load on the diesel generator, which is the sununation ' of the total dead load and.the total
. continuous-load.
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E, . EA FC-90-062. Rev.0 , ,7,5 ATTACHMENT 8.1.a4, l mum i CALCULATION PREPARATION, REVIEW AND APMt0 VAL FORM PEEMnP-3.4 Form Page No.1 of1 M M NO* ' Fc ra ' ' - - ! I PRODUCTION ENGINEERING INVlWON CALCULATION SLEET Rev.No. 6 i1 l E 2.0 EXPECTED CONTAINNENT FAN LOADING REF. NO. The expected loading for the- containment percenta$e(%)ofnameplat venti ation fans VA-3A, VA-3B, VA-7C I and VA-70 is a function of atmospheric density within : containment. The- loading is expected to follow the ! I containment pressure profile. shows the expected containment pressure profile (two The following graph 1 cases are shown) and an expect time load curve. The -} I curve loading extremes are bounded by full load at maximum DBA pressure and 50% load at nomal pro DBA environmental co.tditions. For the-purposes of this I calculation the '.ainimum post DBA load will be assumed to 75% for conservatism. I . I 1+ I LI . I ,I I I 1 1 l l:- - l- _ _ _ . . - . - - . - . . . _ . . - . - - - - - . . - - - - - - . . - . - -
l EA FC-90-062, Rev.0' ATi g T 8.g g r L CALCULATION PMPARATION,ItEVIEW AND APMIOVAL P0ftM PED-4P-3.4 Form Page No. I af 1 NM NO* l l pg CD 1r-'i PRODUCTION ENWERING DIVHtl0N -- - CALCULATION N Rev.No, d [ L nsP. NO. ! EST*d tATED CONTA130GNT COOLING i
$d FARMLOAD AS A FUNCTION 9psit') oF CouTAInonDIT PRESSURE !
', 60 - - RAS : (Min. SI) -
- 100 I f' N Expected containment Motor -
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. . . _ . _ _ - . _ . _ . . . . _ _ . . _ _ _ _ . - . . . . . _ . - - - - - - . ~ . - - - - - . -
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, EA-FC-90-062, Re8 5 ATTACHMENT 8.1. a6 l CalcPreparation,ReviewandAp!
PEO-QP 3.5 Pa e 1 f2 royal CALCULATION NUISER Reviewer's Checklist-Calcu ations g In a WA
- 1. Is Calculation Cover Sheet attached and completed, as required,to the calculation? /
I 2. Is the calculation objective stated? Was this achieved? Y
/
l t
- 3. Are in uts correctly selected and incor- i porate into the analysis? .
- 4. '
>< Haveinputsand/orassumptionswhichre!uire confirmation at a later data, been iden 1fied on the Calculation Cover Sheet and in the ;
calculation body! t
- 5. Are the applicable codes, standards, I,
regulatory requirements, and other references including issue and addenda identified such that they are traceable to source document? -/ I- ; 6. Wasana$!h!riatecalculationmethodused? Was the theory appropriate? [ ' g 7. Haveassumptionsbeennotedandjustified! 8.. Are the calculations free of arithmetic
, errorst >
- 9. Is the calculation consistent with the design basis requirements?
.10.
11. Is the conclusion stated? Is the calculation legible and suitable for [,/ '
~I sicrofilming? 7 l l I
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. . PEDtQP-3.36 H _
. _ . _ _ _ - _ ___ _--- __ _ _____ _-- _-__- _ _ _ _ - - - _ red o 1 .- '
EA-FC-90-062.Rd.l I . ATTACHMENT 8.1-r7 Calc Preparation, Review and Approval I PED-QP-3.5 Reviewer's Checklist-Calcu ations Pap 2 of 2 CALCULATION NUMER fc#>>n x.<..L ; El E 1/A . l 12. Are all blocks'on the Calculation Cover ./ Sheet addressed correctly 7 Y l 13. Have Forms PED-QP-3.2, 3, 4 and 8 been used and correctly completed?- ;j
- 14. If the calwlation has been pre sursedeanothercalcu!? tion,$aredto as all the g@ f//1/f0 va id information been trantferred in the new calculation 7 d i
I . t t I I REY! EWER CO M NTS: i I : I I . LI ,I' #I 1 #A/C
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- 1. Arekhecalculationmethodsaccurate g and appropriate? /
- 2. -Are input data sufficiently detailed? / l l 3. Are the calculation assumptions reasonablef /
- 4. Has the basis for engineering judgement been included in the calculation, when I used? /
I 5. Is th+ calculation documented sufficiently
,uch usat the' analysis is understandable to someone useeter.t in the discipline without recourse to the Preparer?
/
6.- -Have the design interface requirements been satisfied? /
- 7. Are the results reasonable and do they resolvethecalculationobjective? / l
- 8. If an alternate calculation was used to verify the adequacy of the analysis, is it l attached to the calculation?. 7 I,, g. If qualification testing was used to verify i l
-the adequacy of the analysis has it b I documentedusingaretrievablesource,een or s attached to the calculationi v'
- 10. Are calculations involving Technical I 5pecification values and associated margins of safety identified? /
i f INDEPENDENT REf! EWER C M NTS: I I / h $A =; Ip.g.go Independent Rev p r Date
- h. PED-QP-3.40 Rev. 1 ,
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CALCULATION REVISION SHEET IREY. NO. DESCRIPTION / REASON FOR CHANGE INm n t. z s sur I l l l 1 1 d l 1 b' l s . mas
EA-FC-90-062, Rev.0 0 j
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ATTACHMENT 8.15 waas a ' i l CALCULATION PREPARATION, REVIEW- AND APPROVAL 'l FORM PEIN3P-3J FORM Page No. 3 ~ of 5 CALCULATION NO. ! q'p' FC '" ' - ' ' ~ ~ ~ ! I ' PRODUCTION ENGINEERING CALCULATION -
- 5 i
SUMMARY
SHEET Rev.No. 4 , l'. Non-load shed loads which are used intermittently are not ! considered to be part of the total longer term load on the l f diesel generators.
- 2. Equipment which is used infrequently, such as welding I receptacles and stress gallery disconnect switch, are j assumed to have no load. !
,g il 3. When % efficiency or power factor information is not l- available, .a power factor = 0.80 and a % efficiency = 0.95 a will be used as typical values for electrical equipment. .l l 4. The diesel geaerator model assumes that the sequenced load 1 grroup has accelerated to full speed and is running at ispected load.
- 5. RAS is assumed to occur with minimum safeguard actuation maintaining the highest diesel loading for the maximum 1, expected time on each diesel generator.
- 6. This model atsumes that no manual restart of equipment such !
as air- compressors, turbine plant cooling pump, and Auxiliary Building ventilation fans occurs. g 7. The charging pumps are ass.uned to operate at full load for l the duration of time covared in this calculation. l 8.- The calculation represents the worst case in that equipment 1 which could. be running (not intermittent) is running on I- each safeguard train at the time of the loss of offsite l power and DBA. y 9. For conservatism the battery chargers are assumed at full l- load and. the two non safety related inverters are assumed to be on their respective bypass transformers. i 1 i I
_ _ _ _ . _ . _ _ _ . . ~ _ __ . _ . _ _ . _ . . _ _ _ _ . - . _ _ . . . _ _ _ _ . . _ . _ _ _ _ _ _ _ I EA-FC-90-062, Rev.0 ATTACHMENT 8.1 car.mm a E' 2 CALCULATION PREPARATION REVIEW AND APPROVAL CALCULATION NO' FORM PED-4P-3.3 - FORM Page No.4 of 5
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~-
PRODUCTION ENGINEERING CALCULATION
SUMMARY
SHEET Rev.No. / INPUTS
- 1. Sargent & Lundy Electrical Load Monitoring System (ELMS)
Printout.
- 2. Electrical Load Distribution Listing (ELDL), Vol. 3, 4.16KV and 480V Buses and MCCs.
- 3. GHD&R Drawings 11405-E-3, 4.16KV One Line Diagram 11405-E-4, 480V One Line Diagram, Sh. 1 '
11405-E-5, 480V One Line Diagram, Sh. 2 11405-E-6, 480V MCC One Line Diag., Sh. 1 11405-E-7, 480V MCC One Line Diag., Sh. 2
- 4. GE Drawings 177B2371, 480V MCCs Elementary Drawings.
- 5. EEQ Manual, Section 2, Containment LOCA Response Curves. '
l
- 6. USAR, Figure 14-6-6, Containment Response
- 7. USAR, Ser: tion 6.2.5, Time to RAS REFERENCES ]
i
- 1. USAR,.Section 8.4, Emergency Power Sources
'2.- Stone & Webster Calculation (16472.19), Confirmation of D1 and D2 Loading.
I
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I ' EA-rC-90-062, Revoo ATTACHMENT 8.1 0 43 car.Ns a J I CALCULATION PREPARATION REVIEW AND APMIOVAL FORM PED--QP-4.3 FORM Page No. 5 of 5 NO.
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' FC PRODUCTION ENGINEERING CALCULA110N ~
l SUMMAfW SHEET ~ Rev.No. 4 CONCLUSIONS Attached arethe Load Shed Information Susunaries for DG-1 and note the load shed status for each LI DG-2. device, These summaries the load in KW, the intermittent load (if applicable), and the cycle time.(in seconds) for apprcpriate valves. l j l i To determine the loading on each diesel generator, the total
, sequential load and the total non-load shed continuous load are needed.
I found. The total non-load shed intermittent load will also be Reference the. attached Load Shed Information Susanary for DG-1 I I for load information on individual equipment loaded on DG-1. The load totals for DG-1 are as follows: I Total Non-Load Shed Intermittent Load : Total Non-Load Shed Continuous Load Total Sequential Load
- 2224.8 KW 61.33 KW 293.5 KW I
l Therefore, the total load which would be loaded on DG-1 as a l result of LOCA coincident with a loss cf offaite power is .. 293.5 KW + 2224.8 KW = 2518.3 KW ,I ........... l After approximately 2000 seconds the ventilation fans VA-3A and VA-7C would be expected to unload by apprc,ximately 25% of rated [- KW or 73.6 KW. This would reduce the load to approximately 2444.7 KW. At RAS 3740 seconds into the event (minimum safety I injection) SI-1A trips, reducing the load a further 235.6 KW to 2209.1 KW. I I I
.I -
I - I. _ _ _ _ _ _ _ _ . __ ...-,e,- -. -
I' EA-FC-90-962, Rev.0 ATTACHMENT 8. car. pas a I CALCULATION PREPARATION, REVIEW AND APPROVAL ' FORM PED-OP-3.3 FORM Page No.5 of 5 CALCULATION NO. FC I'l ' PRODUCTION ENGINEERING CALCULATION
SUMMARY
SHEET . Rev.No. d CONCLUSIONS waforence the attached Load Shed Information Sununary for DG-2 3 for load information on individual equipment loaded on DG-2. , The load totals for DG-2 are as follows: j Total Non-Load Shed Intermittent Load : 210.1 KW > Total Non-Load.Shed Continuous Load : 49972 KW .' ' O. " . 7.r,7y) l Total sequential Load : 1894.1 KW gfgp y Therefore,. the total load which would be loaded on DG-2 as a
-result of LOCA coincident with a loss of offsite-power is
- . - ..m. -
h,2KW + 1894.1 KW = 25NNSKW ,.3 <;; . g W. j ..... ..... . After approximately 2000 seconds the ventilation fans VA-3B and VA-7D would be expected to unload by approximately 25% of rated KW or 73.6 KW. This would reduce the load to approximately
- 2323.7 KW. At RAS 3740 seconds into the event (minimum safety
, , injection)
SI-1B tripsi reducing the load a further 235.6 KW to . Ir,.. -2099ri KW.
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~1. Is Calculation Cover Sheet attached and /
completed, as required,to the calculation? -
- 2. Is the calculation objective stated? Was this achieved?
I 3. Are' inputs correctly selected and inc.orporate? into the analysis? ire
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- 4. Have inputs and/or assumptions which .
confirmation at a later data been ide fied on the Calculation Cover Sheet and in the calculation body?
- 5. Are the applicable codes, standards
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- 6. Was an appropriate calculation method used? Was
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- 7. Have assumptions been noted and justified?
g '8. Are the calculations free of arithmetic errors? /
- 9. Is the calculation consistent with the design /
basis requirements? v I 10._ Is the conciusion stated?
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- 12. Are all blocks on the Calculation Cover Sheet
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- 13. Have Forms PED-QP-3.2, 3, 4 and 5 been used and i_.
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,14. If the calculation has been prepared to supersede
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REVIEWER C00mENTS: I r PED-QP-3.33 Rev. 0 7/89
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tF YOU DO:NOTLRECEIVE ALL PAGES LISTD, PLEASE CALL 00R WORD + [: l: l PROCESSING DEPT.,- (919)t77-2720, EXT. 212. i m 1 Attached 1s a: data sneet thas shows the engine jac4et hg , 1 water alarm set.S 300'F and shutdown i 118'F. Long -i Egi ...r.u.n. e s.... .sur. ...r 10 'r .., e. eve. sn. n r. of the cylinder heads. . ,I L- . NOTE :- FOR WATER TEMPERATURE IN EXCESS:0F 190'F . R ' At0V! At3 POWER DERATION' PER CURVE (200 i,r., 210'F) U WITH AM81IPT- AIR (COMBUST 10N AIR) TRArtRATURES ASOVE 90'F.
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zggj,y) associated with our determination of b mean n' in Festion (58)? Each data point z, was obtained with an uncertainty Substituting this result into Equation (5-7) yields a general chameterised by its standard deviation a Each of these data formula for the uncertainty of h mean e,. points contributes to the determination of b mean e' and there-II'd , (5-10) fore each data point contributes some uncertainty to the deter- ,**-{IIIII'#)E - IIIII mination of b final results. How are these contributions - accensulated? : In Citapter 4 we i m*_,,,.," a formula (see Equation (4-9)), for 5-2 INSTRU# RENTAL UNCERTAINTIES combining the unseertainties of terms contributing to a single result. The variance e,' of the niean s' is equal to b sism of the For many experiments the fluctuations in measuresnents are variances e/ of b individual data points z, weighted by the due to the finite precision of & instruments used in making h squares of the effects ap'/az, which the data points have on the measurements and are not directly correlated with the values of result. the quantity measured. These fluctuations are sympteenetic of the fact that the measurements s re made with uncertainties;i.e., .
,,e . ,p[38[ --
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(5-7) no random measurement is expected to he exactly accurate becauw the experinnental equipment is not sufficieently preense b This approximation neglects correlations between the measure- yield the cor ect value for each measurement. The uncertainty ments 24 as well as second- and higher-order terms in b expan- . i.roduced into the final result is called an instrumett'ai sacer-soon of time variance e,', but it should be a reasonable approxima- .,ty, as opposed to statietical Huetuations to be described in the tion so long as none of the data points contributes a major portion sw.xt section. The resulting errors in tiie final determination are de Snal emult. elassified as instrumental errors. - If & uncertainties of b data points are all equale, = ,, we can use Equation (5-5) to find the effect ap'/ar which each data Q #et d Exarnpid-1. The point z, has on & determmation of the mean p . g, . m MM with a udnty fw ] each dsts point which is known to be e = 0.rd10 em. All of the : an' a t Z i 1 (M) meesurements are made with h same experimental apparatus. $ $ Q : ai ~ al([N *df " N and the finite preension of Liais apparatus, characterised by e g y 4' _ Combining Equations (5-7) and (5-8), b estimated error of & results in a spread of chaervations over several centinieterso:c ooe I , e- - ESTitrATES OF MEAN AND ERROft5 TI g yf 79 DATA REDUCT90N AND sRROs ANALYSIS 9 o
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m 37_ - , r:ouped around & known length z = 20.000 cm. Figure 2-1 experimental conditions, the mean p must be estimated according shows a comparison of b dispersion of the data points with h to Equation (5-6) known and estimated parent distributions which are assumed to gg,g,f) be Gaussian. ,~ g g* (5-14) The length of b table is estimated, according to Equation and b uncertainty in the snean , is estimated according to (2-7), to be , ~ f = 20.028 ein, and b precision of the experi. mental points is estimated, according to Equation (2-10), to be Equation (5-10) o ~ s = 0.48 cm. Since the uncertainties of all b data pointa I (5-15) are equal ,, = e, & arguinents leading to Equation (5-9) are 'a' ~ zyf,, ) valid and we can estimate the uncertainty in our determination of b mean to be e,~ s/v'N where N = 100. This yields an ! " hem Se """t be known froen other experiments. I j It often happens that b relative values of the << are known, sacertainty of ,, ~ 0.05 cm which is only slightly larger than the but the absolute magnitudes are not. For example, if one set of j actual error of 0.028 cm. data are acquired with one scale range and another set with a g diNnent scale rae *he e, may Wqual wiein M set W dire Equal uncertainties For experiments such as that of i by a known i en the two sets, as would be the case s,f e, Example 5-1 where time uncertainties are all equal e, - e, Equa- range. In such a case, ne rMar tion (5-5) gives the best estimate of the mean p.
D *PN'"*' se meluded as weighting factors m, b values of e, ~i etaminadon , sin y and its uncertainty, and b e6eedade 1
,~f,N I r. (5-11) niagnitudes of > can be estimated from the dispersion of the data p.. its ari.. J the mean.
The uncertainty of the data po.mte , can be estimated from the Since 19 tion (5-14) is independent of the absolute magni-data, if it is not known, according to Equation (2-10). tudes of the a,, its ~orm is unchanged a~s- g y Z(r4 - f)' (,M 2) > p~Nz w; e Combining Equations (5-9) and (5-12), we can estimate & uncer. The absolute magnitudes of the e. een be estimated from b aserope cerience of the date, e*, evaluated as in Equation (5-12). tainty a, in the determination of the mean ,
,z
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a, = ~ (5-I3) ,
,, z _ I'"*
n s. _ n=w:<r. ' e i By similar analysis, we could estimate & uncertainty of ,, itself
'8 (N - I)I*I yy I
- "' The uncertainty in the mean ,, follows froen Equation (51 e (5-14). $* h Unequal ssecertainties If the uncertainties of some data 1 ,8 g O di
'a, " z( f,,'s) ~N m o points are diferent from those of others because of changes in the 2 s mRNm3 OF MMN AND MaOa3 M h
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- 4 o
- 0.9900 = 0.9 4 3 4 Iti r H j' citM N O g f5 '
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e .m. 77.ra of ==*.**. osv. [4 reve *v l
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wD.' d' YEe Safety-Related A Non-Sofety-Related p*** iO e i Onent Om aya pgjatpc powgg n;ggjp a cg wad >Y Date l I W FT CnLNGs/N ffA7/oA/ mi. u.. n, t . o s . we. R******d by _ - .y
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.eto l
sau ) ~<~o sstro -ie merca o ana 1, <r erren,'oeo meren co te me.:) l ' wst r,. F-(o.st ao meu) * +q(o. tost r nr.v ' as )(0 t555He)) t - 1 , I < o.sost "'% >~ (rss "%) (o:toAo) i av ) )' l- -
+ !o. ost ***/s.t (vss "'/v)(o.cos */as;(o.sor1)(too usl'
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- on9M FOR WINO Jt*fCD WOIC ATOR W(t op , s (o.t7as & t ."'.EY+ 00 ,
0.o263
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4 cases, per mg7(ojt o log /CAi setoAr/7o##A# A&. h TrelsA889 R WOW -emme sysrgo% neeuppcso ATT h M k S $ev' 0
*d*v-#**** X **-***v-***** **** i/ d /6 onent opsenenn p.eggIC 90we*R DISTMILT Freeeren >V Dese Promet 77 cAtuour/ symrioAe me*-** bV Dm.
l pr.l. No. 7753 -OS sew. No. - Appemd bV Date IAl) wown spero 1o meren iano 2.,45 martR, ooe ontTER (. 8o men) i . . 0,eae.,,e i..,n<meu,!o.>ast *% to.n.<enns un nt l , t ooo .. }
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l , (0.,os,"'% (m "%) 'o.tno)bv ) 1
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fo.rost '"'% (7as "%)(o.oo s )(e*%)(o.<)(sv) ? g ioo x .
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/'t - 1 q
g i,. - f L I-0 . [c. 952 3 ,, ' Jl; sto.9159 mPM foR THE ERF ComPU7fst ~ b - 1 w, cap,, a {o.st oe + 0.0861 + 0.08tel + 0.0012 + 0.ool0 4 }
+ t.53 II _
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s (o.95tI] E
= 0. 9 7 58 rn r8 fog opw cosGeg I _ - __ _ .. _ . _ _ _ . - - .
. 4 I -emessesse .
ces. N mrffsgotas/cd c hoew/704feGrA-h MafWB K
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ousas c #N4aA sumeic. so=in auta,er R***** W osie a M*k F7 C4 Nouw srA riarv #* * *** W Date . ,5 a.i. .. mt .o s ... _ u-w .e,* ! ^
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.i l- =[4.107o I;E ;
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* '3)TEMPfR ATUR6 -it.?tT!S I,. ly 3 Trme t. (o.sq33'c)*+f8!*dIo.104o)(oRh' l p, =
.; ( 'oo . / :
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= [o. :57 8,I wio.39 7 t *C Colt GAF CoMPuTCit
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= t o.3 9 4'1
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= t o. Aol.o *e foe ofLTA TeenPCMAlliMC in/o!CATOR k~ere.,.9...m,.,7,o.o.y+o.o,ro.o..ot+o.....G'4
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TABLE 1T MTEOROLOGKAL S YSTfin ' A cctannc y ' conspe ransct* n )
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MarEz er werea y
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o-so ser av j une 2 W8MD fS*argrras 12.6272 yet tir.r249 merez. po f 2,62F2 tren YES
~g R o fg l7 75 ;, ,
.,..ers n, 7FMPERA7anE t0,S'c i o.5972 I83947 i g [32 3 YES N/4 yrs k g
*C.- t i e o 3 DELTA t 0.05 % t'AOL43 ygS t 0.+ 60
- Ato L0.6666 e
w g} ;. fgs ,,
=,. ,..,.r. =_ Av.=r c .c e -
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% i s
VAL eoE. SYSTEh1 !G MOT infh Cet19UA90CG FOR MAMGE Of 9-S MPwf. 4YSTEM ~ r$ /W i j t . ceMPLIANC E f*K 0-30: NPM. ' ' g
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sysren is in cane uAwer roe it.z ~2s' MPH ret- rA s . F F F g ; - p2 =' -
- s. ;
o i
% I - - _ _ _ _ _ _ - _ - _ _ - - - - _ _ _ _ - _ - _ _ _ _ _ _ _ _ - - - - _ - _ . _ - _ . _ - _ - - _ _ _ _ _ _ _ _ _ _ _ _ - - _ - _ _ _ _ _ _ _ _ - _ - - _ _ - ~ _ _ _ _ _ - _ - - - _ . - - - - - - _ - . _ - - = _ _
e ..
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NL*M%. n... n \
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g .r (s.t ;... o u n < n. i. c r s ca c t u o t l ~Z - ) 7 = 'AvtttA Gl N C /NTit VAL , f -
*[ o 3,4nt h irv G INTJRVA:. '
.Eu ,t.nnon or lovsinnintufous Mtpotrv& ,
Cyg= Timi AvtRAG6o VALs4Le Engott l
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" EA FC-90-062, Revo '0 ATTACHMENT 8.5- 7 j ons.pna m 7 .;
' CALCULATION PREPARATION. REVIEW AND APPROVAL FORM PED-4P-3.3 CALCULATION NO.- .
FORM Page No.4 of 5 ! FCd 6091 i E. . PRODUCTION ENGINEERING CALCULATION g SUMMAIN SHEET Rev.No. , g INPUTS / REFERENCES REF. !
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SUMMARY
SHEET Rev.No. d L CONCLUNONS I sed -es 6f25/ete DG-( 4 ,4 A h,
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qg EA-FC-90-062, Rev. O N3 ATTACHMENT 8.5-15 Calc Preparation, Rev h and Approval PE0 @ -3.5 Pa CALCULATION NtMBER Reviewer'sChecklist-Calcu!.e1of2 ations i Fcfsrey m a sa
-l 1. Is Calculation Cover Sheet attached and comp'deted, as required,to the calculation? /
I 2. Is the calculation objective stated? Was this achieved? / Are inputs correctb selected and incor- 'y I 3. porated into the ana. lysis? Have inputs and/or assumptions which require
, 4.
confirmation at a later data, been identified on the Calculatier. Cover Sheet and in the calculation body? /
- 5. Are the applicable codes, standards, regulatory requirements, and othat references p including issue and addenda identified such j that they are traceable to source document? _
- 6. j/
Wasatagpropriatecalculationmethodused? Was the asic theory appropriate?
- 7. Haveassumptionsbeennotedan'djustified? /
- 8. Are th' calculations free of arithmetic .
/
.,,0 ,;
l 9. Is the calculation consistent with the design basis requirements? / _
- 10. Is the conclusion stated? /
- 11. Is the calculation legible and suitable for j aicrofilaing?
I I I I ' 1 ^ *fD @ -3.36 I' ' Rev. I m- - ~ , - ser r
I CalePreparation,Reviewandkpproval EAoFC-90-062, Rev. O ATTACHMENT 805-1f PED-QP-3.5 Page 2 of 2 CALCULATION NUMBER , i Reviewer's Checklist-Calculations ' Fc pf s987 I m a na
- 12. Are all blocks on the Calculation Cover 7 l Sheet addressed correctly?
I 13. Have Forms PED QP-3.2, 3, 4 and 5 been used and correctly completed?
,/
If the calculation has been prepared to I 14. supersede another calculation, has all the valid information been transferred in the V
/ a new calculation?
I I I REVIEWER C(39 TENTS: 8 I I I I o L. i n ,. este httpr[/ ' I I I L P : ,-3.37
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' ATTACHMENT 8.5- /r =
c Calc Preparation, Review and Approval- . .-
,T E ' PED-QP-3.7c . .-Page 1 of:1- CALCULATION IRDSER 5 >
1 Independent Reviewer's Checklist:- Calculations-
,4^ . Fcp( 5987
- ["3 Ili 50. 5/AL
- 1. 'AreLthecalculationmethodsaccurate p ,
-and' appropriate 7. /
hQ : 2. -
^
Are input data sufficiently detailed? /
!3. ,
'Are tho' calculation assumptions reasonablef /-
em f4. lHas.the basis for engineering . judgement 9* -been included in the calculatic,n, when p - used? :/-
.1 ( 5.- Is the calculation documented'sufficiently J'm" Q - such that the analysis is understandable to g,' someone competent.in=the discipline.
!without recourse to the Preparerf [ * ;-
d <c $ '6. .Have' the design: interface requiremerts y ! 5, been~satisfiedf-
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Ze Q ' 7.- Are the results reasonable and do they y 1 4,% ,
. resolve the calculation ob,jectivet 1
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, .q 8.: ,If.an alternate calculation was used to yl
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verify the^ adequacy of the analysis, is it'
; attached to the calculation? I m o 4 a 'EM , 9. ! .If qualification testing was used to verify d p5 '# the ader acy of tb analysis has i+ b d y documenL1 using & retrievable source,een or 1 L attached _ the calculationf: 7 Ji G w '
S v i10i -Are calculations involving Technical. T C cification values and associated margins 1' gn safety identified?- j-g IlWEPENDENT REVIEWER CSOENTS:
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PED-7-3.40 i
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- _ 'EA-FC-90-0G2 Revo 0-F DG-- 1 2000hr. DERATINGi@107FL(6-25-90): Arracumeur 8.6-1 Lhod[Doto fromLColci FC03382, Rev.' 1
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EA-FC-90-062 Rev.-0 ATTACHMENT 8.6-2 file:diesell ibis is for DG-1 (6-25-90) 2000hr. dorated curve. Cold englae start at 167 dayees F entside ambient. Eagles idled at no load fra 14:38 to 14:45 shore load was 486 KW and lacreastag to 90% of full load by 14:47.
-
- theasured JWB Graphed JMD + Turbola + Calc. IIA-52A Englae. Turhe Istata outside Aab.
STATUS illlE SEC. Ilam- Gauge Ch. 51-50 Ch. 14-19 Ambient DeltaG beltairb DeltaG Deltairt 40ERATE DERATE KW Proftie Nel 86.0 - 85.9 107 14e.0 110.0 20.0 24.04 1.000 2654.9 14:35 126.0 86.6 - 85.8 187 176.1 110.7 20.1 24.14 1.000 2654.0 SFf(14:38) 14:40 156.8 98.2 87.9 147 180.3 112.2 18.0 22.04 1.000 2654.0 14:45 162.3 87.7 107 183.0 112.9 18.2 22.29- 1.808 - 2664.0 2509.1
..e(14:47) 164.8 98.7 87.6 1a5.2 113.4 18.3 22.33- 1.aos 2654.s 25es.1 nas Is6.9 91.s - 187 93.6 86.7 107 200.2 216.8 19.2 23.24 0.927 2450.7 24B2.8 788 15:08 181.0 87.5 107 203.4 1.'9.8 18.4 22.44 0.921 . 2443.8 2447.9 1688 15:15' 185.0 96.6 87.9 107 203.7 119.2 18.9 22.05 0.929 2442.8 2435.5 2000 185.7 97.1 98.1 - B.6 187 204.3 119.4 17.3 21.34 0.920 2440.9 2435.5 2580 15:30 187.0 99.2 88.3 107 294.6 120.8 17.6 21.64 0.9 V. 2430.8 2435.5 3488 15:46~ 187.8 88.5 181 294.7 129.8 17.4 21.41 0.W6 2431.2 2435.5 3740; 187.3' 90.4 99.4 - ' 88.5 107 294.7 *20.8 17.4 21.41 0.916 2431.2 2199.9 3740 187.3 9B.8 88.1 107 204.8 1261.6 16.8 20.84 0.916 2432.4 2199.9 4398 16:08 188.8 88.9 107 294.0 .J.4 16.0 20.04 0.914 2426.4 2199.9 5288 16:15 138.0 101.4 89.8 107 204.9 -121.1 16.9 29.94 8.915 ' 2428.6 2190.9
.6189 16:38 188.0 188.2 101.0 88.8' 107 205.1 122.1 17.1 21.14 - 8.912 2421.4. 2199.9 188.0
{ 7000f 16:45 88.1 107 204.8 '123.5 16.8- 28.84 0.909 2411.2 2199.9SuprLY(17:05) 7988 17:00 '188.8 142.7 183.0 89.6 187 204.3 123.3 16.3 29.34 0.999 2412.7 2198.9
'8888 17:15 188.0 164.0 89.2 107 204.7 '124.7 16.7' 29.74 - 9.906 2402.5 2195.9 ,
.9788 17:38 18B.0 85.1 '147 205.8 128.2 17.8 21.84 0.896 2377.2 2198.9 D151551(17:41)
'18888 17:45 188.8 186.4 85.2 187 ' 205.7 130.8 17.7 21.74 9.891 2364.2 2198.9 11588 18:00 - 188.4 . ' 185.3
. 88.8 187 205.1 126.3 17.1 21.14 ' O.895 2376.5 2199.9 1240B 18:15 188.0 107.2 :
DFLASAilW
- 1. An empty cell la t;m IllE cohans signifies that the .219 Englas Gauge. Turbo latake, and Ambient Temp, mere llaearly_ late /polated tetagen the higher and leesr potets.
- 2. JMB Ea0las Gauge data mas takaa at 18 ela, laterwals, therefore, values shaus were linearly laterpolated if they did met accer en a 15 adente laterval.
c 3. Salta6 = Eraphed Ambient Mamared entside Ashlent + 1.62 - 1.5;~ Accamets for lastrummet uncertainties.'
; 4. : Soltairti - Graphed Ameilent - lleasured getside Ambient'+ 1.62 + 1.32; Accounts far lastrument uncertalettes. ' [5.140EAAE is ehtalmed free the Om dorattag curve (attachasat 8.2).
56.-: BEBAIE BB ls 40EBA3E emittplied by 266digt (the bees 2000hr. W ratlag EBB dayees F air latake).- ~ L7.s Calc. Fuefile IRI is the 108 leasing based en W93 calc. 8FC83332, Rev.11. . 7 2 8. ihe yeenbestas eses imE sec..a. g y
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e EA-FC-90-062 Rav. 0 ATTACliMEHT 8.6-4 flle:diesell.' Graph: DG187.PIC-This is for' DC-1 (6-25-90) 2000hr. dorated curve. Cold engl6.e start at 187 degrees F entside aehlent. Englas idled at no load fren 14:38 :s 14:# atore lead uns 406 Ku and lacreaslag to 90% of full lead by 14:47. Turbola + Deltairt adjusted M start eut at lei degrees. 5 JWB Naasured Eagles Turbo intd e amtside Ash. Graphed JWO + Turbola + ' Calc. WA-52A 4 183 SEC. Time Gauge th. 51 Ch. 19 Ambient DeltaG Deltairb DeltaG Deltairt 40ERATE DESAIE KW Profile KM STATUS i 14:35 126.6 - 86.0 85.9 1#.9 - 107.0 20.0 107 24.04 ? est 2654.0 14:40 156.0 - 85.6 - 85.8 107 176.1 '" 7 20.1 24.14 1.000 2654.0 0FF(14:38) 14:45 162.3 -98.2 87.9 167 180.3 109.2 18.0 ~22.04 1.000 2654.0. i; e(14:47) 164.8 98.7 87.7 1107 183.0 '105.9 18.2 ~ 22.20 1.000 2654.0 2509.1
' let . 166.9 91.8 87.6 107 185.2 118.4 18.3 22.33 1.000 ' 2654.0
" 2509.1
~75 --15:00 181.8 93.6 ~ 85.7 107 200.2 113.8 19.2 23.24 0.935 2481.4 2482.8 1600 15:15 185.0 M.6 87.5 187 203.4 116.0 18.4 ~ 22.44- 0.929 2#5.5 2447.9-2000 185.7 . 97.1 87.9 107. 203.7 116.2 18.0 - 22.95- 8.929 254.5 2435.5
~2508.'15:38- 187.8 98.1 M.6 107 204.3 116.4 17.3 ~ 21.34' O.928 2462.6 2435.5 3408 15:M 1887.0 99.2 B.3 107 204.6 117.8 17.6 21.64 S.924 2452.5 2435.5 3748 187.3 99.4 88.5 107 204.7 117.4 17.4 21.41 0.924 2452.9 7435.5
-3740 187.3 .99.4 88.5 107 204.7 117.8 ' 17.4 21.41 0.924 2452.9 2199.9
'4308 -16:00 188.0 99.8 80.1 107 204.8 117.6 16.8- 20.84 0.925 2454.1 2199.9 c '5208.16:15 .188.0 141.4 88.9 107 204.0 118.4 16.0 . 20.04 0.922 2448.1 2190.9
. Eles : 16:30 188.0 188.2 89.0 107 204.9 118.1 16.9 20.94 9.923 2450.3 2199.9..
7000 16:45 188.0 101.0 M.8 147 205.1 119.1 17.1 21.14 S.921 2443.1 2199.9 7900 17:08 188.8 182.7 89.1 167 204.8 - 120.5 16.8 20.84 0.987 2432.9 2199.9 SWFLY(17:05) 8000 17:15 180.0 103.8 89.6 147 204.3 120.3 16.3- 28.34 0.917 2434.4. 2195.9 i: 978B 17:30 15.0 ~ 104.4 B.2 107 204.7 125.7 - 16.7 20.74~ 0.913 '2s24.3 2195.9 , lette 17:45 188.8 186.4 88.1: 107 205.8 125.2 17.8 21.84 9.984 2398.9 2199.9 OuM151(17:41) 11580-18:00 188.0 15.3' . M-2 147 295.7 127.0 17.7- 21.74 8.809 2305.9 2195.9 - 1248 18:15' 18B.0 187.2 M.8 147 205.1 125.3 . 17.1 . 21.14 0.904 2308.2 2490.9 . , EWLAntiles: ,
. If An empty cell in the ilIE column signifies that the .38 EaStae 6euge. Terho latde, and Anhiest Temp. more llaearly laterpolatal hotamos the higher and louer points.
- 2. ' .38 Engine Gauge data uns tahoe at IS alm. Intersels, themiere, values shown more linearly laterpolated If. they did met escur en a 15 miente laterval.
I. ' 3. Setta5 = Eraphed Ambient - Enesured antside Anhiest + 1.62 -;1.5; Acceusts for lastruent uncertalaties.
- 14. Saltairb = Eraphed Ambient - st:eaured Gutside Anblent + 1.62 + 1.32; Accounts for lastruent uncertaintles.
35, 4AEBAIE is ehtaiaod frem the EIS derettag curve (attare==* 8.2).
- 6. ' MAAIE III is 4MRATE neittplied by M6end (the lese 2000hr. El ratlag 800 degrees F air latake).
' 7. . Calc. Profile _mi is the IN leedlag hosed en WWEt calc. 8FCS3524 Row.1. - l : 8. 1he paph togles uhers IIIE SEC. = 0. y W W s. M M M SQ W W W W:M:=m M 56 ~M -~ u mW . . + - W ..
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ffle: diesel 3.c1 L SG-1 Graph of 1/2hr. 4hr., and 2000hr. dorattags with load data - _ free calculation RC3M2, hav.1. Amtside ashiant temparature - IST Dog. F ,
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Seceeds . leg. Tag - 49erate Gerate 101 Proflie IN Ratlag :
.8' 208.0 '139.8 : 0.801 - 2541.8 2500.1 20E3.6 let 208.8 130.0i .0.801" 2541.8- :2500.1 2063.0
-1800 208.0 130.0 "8.881 -2541.8 2443.2 2063.8
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, '3MS 208.8 138.0 0.881 2484.5 - 2435.5 2008.8
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- Calc Preparation, Review and Approval PED-QP-3.5- . . .
Page 1 of 2 CALCULATION HWSER 1 , noviewer's Checklist-Calcu ations ' lg g Fc454w 1 L 5, IE Et- E "
-1.- Is'CalculationCoverSheetaI:tachedand #
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l, 2.- !s the calculation objective stated? Was-
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#E 3.- Are inputs correctly selected and incor-15J porated into the analysis? /
/ 4. - Have inputs and/or ass tit s which re ire c
confirmation-at a late data, been idenbfied-on the Calculation Cover Sheet and'in the p calculation body? / j 5.
'Are the applicable codes,. standards, i;
regulatory requirements, and othertroferences iI- . including issue:and addenda identified such
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/ j mN .
l 6. Wasana$propriatecalculationmethodused? Was-the asic theory appropriate? /
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- 7. Have assumptions been noted and justified?: / _
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design basis requirements 7: R l , 10. 11. Is the conclusion stated? Is the' calculation legible and suitable for
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1 ia 13.- Have Forms PED-QP 3.2, 3, 4 and 5 been used-
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CALCULATI0li limeER [0
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a Independent Reviewer's Checklist - Calculations FC.pgq w I hk'; R 'g Q ; i~ , s.E ' i 1. ; Are the calculation methods accurate ! 6m and appropriate?. !
- 2. ,LAre input data sufficiently detailed?; /'
q . 3.' Are'the ' calculation assumptions reasonable? / '" E 4.. Itas the basis for engineering judgement ;
- 1. >
beer included in the calculation, when . i ? useet !.
- 5. Is the' calculation documented sufficiently such thet the analysis-is understandable to
- a. someone competent in the discipline g without recourse to the Preparerf f .
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- 7. . Are the results reasonable and do they'
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.Rev..0 , DG-~2 -2000hr. DERATHG L@'1'03F (7 .1'6-90)Tracunsur 8.10-1 Lood- Doto from Colc. FCO3382, Rev. 1 2.700. 1 2.600 - e
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- 2. [ asitas - Graphed Ambient - Ilmesured tatside Adhiest
- 1.621- 15; Accamats for lastrument uncertalettes. - Rav.LO-
- 3. < 8elt:Irt' Eraphed Ambient - Ilmasured est36de Ambient + 1.62 + 1.32;. Accommes for lastrument uncertalettes.~ ATTACHMENT 8.10-3 '
- 4. 40ERAIE is ehtatand frun the tse dorating curve (ateart===* 8.2).
- l. ;- 5.t.aEam mIf is 4AEAME mittplied by 3E6e88 (the base 2000hr. Inf rattag We dayees F air intake). -
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EA-FC-90-052 DG-2 2000hr. : DERATING- @'103F (7 .17.-90)$E1c mswr s.u-1 i Lood Dato. from Colc. FCO3382. Rev. -1 12.700 _ 3 1
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EA-FC-90-062 l Rev. O ATTACliMENT 8.11-2 file:diesell Itts is for 85-2 (7-17 99) 2000hr. dorated curve. Cold eaglee start at M3 doyees F entside adlent. ta0las start at 15:56. leaded to 2425 su at 2 82.
' JMB Nessured Calc. WA-52A Eagles- Torto lagde ' entside ash. Eraphed JMB + .Isrhola +
STAINS I K SEC. Iles ' Gauge . Ch. 51 Ch. 14-19 . Ashlent BeltaG asitairb GeltaE Deltairb 40ERAIE SERAlf M Profile W 112.9 14.1' 16.54 1.000 2654.8 8FF 36:88 164.8 96.8 88.8 - 183 178.1 88.8 183 180.9 113.7 14.1 16.M 1.800 2654.8 2457.7 l 8(16:02) .366.8 96.8- , 8s.8 les 183.3 n4.4 14.1 16.94 1.000 2654.8 2457.7 l n8e le8.1 97.5 S.8 143 200.1 119.9 15.1 17.M 8.918 2437.3 2431.4 l 700 16:15 185.8 182.8 88.8 183 202.1 121.9 14.1 16.M 8.913 2422.8 2306.5 l 1600 . 2 30 188.0 185.8 186.1 M.4 143 - 203.2 122.7- 13.8 .16.58 S.911 2417.7 2B4.1 l 2008 188.4 90.8 183 205.1 123.9 13.1 15.M 8.987 2400.3 2384.1 l 2588 16:46 - 192.8 188.0 183.8 118.8 90.4 183 205.1, 125.9 13.1 15.M 8.902 2393.9 23S4.1 l
. 3409 '17:08 90.8 143 206.4 125.4 13.1 15.M . 8.904 .2308.1 2394.1 l 37# ' 193.3 189.4 188.4 90.9 183 206.4 125.4- 13.1 15.M 8.904- 2306.1 218.5 l 37 8 -193.3 98.8 207.1 123.9 13.1 15.M 8.987 2408.3 21 8 .5 l 4300 17:15- IM.0 108.8 183 118.8 88.8 183 289.1 126.9 14.1 ~ 16.M 0.809 2306.6 218.5 l 6288 17:38 195.8 98.8 183 208.1 125.9 13.1 15.M ' 8.902 2393.9 21 6 .5 l 6189 17: 5 195.0 118.8 98.8 183 209.1 . 126.9. 13.1 15.M 8.800 2306.6 2148.5 l
'7089 18:00 - 196.8 111.8 7908 18:15 ' 19 6.8 - 114.8 98.4 183 209.1 129.9 13.1 15.M 8.881 2364.9 21 # .5 l 113.0 90.8 183 208.1 128.9 13.1 15.M 8.804 2372.1 216.5 l 8 58 :IS:38 195.0 Saes is:4s 196.8 n2.8 9s.8 its 20s.1 127.9 13.1 15.M 8.8si 23n.4 21a.5 -l 196.8 112.8- 96.0 183 208.1 127.9 13.1 15.94 0.887 23n.4 21 8 .5 l 18880 ~39:00 194.0 112.8' 98.8 183 287.1 127.9 13.1 15.M 0.807 '2379.4 2148.5 l
'11588 19:15 112.8 88.8 183 ' 205.1 128.9 14.1 16.94 8.884 2372.1 2148.5 l 128 5 19:30 - 192.4 '
.186.8 n8.4 as.8 - 183 281.1 127.9 15.1 p.M 0.8s7 2379.4 21a.5 l 13ses .18:e
> 14rso- assop 383.8 : ut.8 - as.8 143 19s.1 128.9 .15.1 u.9e - 8.ese 2372.1 21e.5 V aguaarms:-
ti. An augty cell in the TM cohen signifies that the .R8 Eagles Gauge, Isrhe latde, and Ashlent Temp. unre llamarly laterpolateu ketuses the higher and lamer potats. [2. .B8 EaBine Gauge data mes tdan at le sin. latervals, there the sessured value does est occur at a 15 ala. laterwel, the nest bilper reading uns used (ceaser
- 3. Deltas - Graphed Ashlemt - measured entside Ashleet + 1.62 - 1.5; arr w s for instrument uncertaintles.
- 4. Seitaith - Eraphed Mient - Ilmesured entside Aeleet + 1.62 + 1.32; Accomets for lastrusset uncertalettes.
- 5. 40E8m is ahtaland free the Ele Gerattae curve (attacheest 8.2).
' 6. MBE 108 is assmear amittplied by 266est (the base alesbr. Elf rattag NB doyees F air latake).
- 2. Calc. Seefile W ls 80s Inf leedlag honed QB W99 calc. 8Ha3382, Ger.1.
8.1 Be paph tagias asese VM SEC. . O. 4
'EA-FC-90-062 I Rsv. 0-A = 8.12-1
.DG-2 DERATING -@103F AMBlENT-L 2.600 d Doto from 'Colc. FCO3382. Rev. 1 i
c- -2.500 -
- ;gg . 2.400 - -
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- 2.200 --
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.+: KW Lood Profile .
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;; (103' Deg. F' Maximum Ambient . Limit) ~
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'2.640 N
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.2.560 x \ V h
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' WEATHER TOWER TEMP. IN DEG. F
-2000hr. Deroting _ ~
a. _ . _L W W W W W W
- Wp, *- .
0; h ~ ~ , E E E. . . . , g -- M g g M f g ".[ g "_ g -g-g n
- EA-FC 062 :
2--
?Ravf 0' ATTACHMENT #8.13-2
?A ,
' fileidledel4 _
L' . This graphs a curve of 2000hr. durated pesar vs.' amblest temperature.
.. 86-2 :.
' thstside 2000hri Salta T~ Tarte 4 'Amallable Jhelect Berated W Tarts 1 stake Air. JIS- Deratlag- M-M.8 - N64 25? M.e f22 1.M - 2664.81 65.8 - 2664 -- '25 90.0 - 205 1.008 -2654.8 ~
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ATTACHMENT 8.14 g* DIESEL GENERATOR NAEPLATE DATA-I Model Number............................................................A-20-C2-Serial Number....................................................... Y, 70-C1-1034
-r Continuous Ratinct .
'1.
a Volts................................................................ 2400/4160 I Current (Amps)..........................................................782/452 xvA....................................................................... 3250-
.E Frequency ( Hz ) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .'. . . . ~ 60 3(~
Phase........................................................................ 3-Power Factor............................................................... 0.8
&' I .
RPM........................................................................900
~TemperatureRise('C):
'I Stator-Thers...........
Rotor-Res................................................................. 85
# ................................................... 60
+b
- 3 KVA Peaking.....................................................3575, 2000Hr/Yr.
TemperatureRisePeaking(*C):
-Stator-There.............................................................
105 Rot o r-R e s . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Rotation..........................................................CCW 9 BRG END
-c
;, Insulation Class:
N St8 tor......................
$i R0 tor.............~..........................................................H
. . s, ................................................F Excitation A
Volts.............................................................144= 1Excitetion Aaps............................................................ 100 a Phase'5equence........................................................... 1.3.2
-I NOTE: I
.n -
The 2, above information was obtained from actual nameplate by RSK on July 1990. I
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v; ; (, ,, e W .- EA-FC-90-062
* ,-y TkCHMENT8.15~
- f. ,.
[ 's , g w S Seemen 2 k . GENERA 10R CHARACTERIS7ES '
, a s esels :-- -
N TYPE OF SERVICR R'N's ammW sesides anstate-
; MODEL . A-20 A 20 A 20 MBD
- RA11NG KW 2750" 25(i0 2300 2880 KVA 3440 3825 2875 2825 s --
-P.F. 02 04 02 03 ARMATURE CURRENT- AMPERES
' ,I + -
Wye . 477 434 399 365
~
. Delta . 836 751 691 632 Stator Tenspersense Rise *C. 10A 56A 47A 39JD: ,
L TERMINALVOLTAGE . Wye 4lde -
. 4160 4160 4160
-Dales' 2000 2400 2400 2000 S: SPEED- RPM ,
900, 900 750 790;-
- < REACTANCES PER UNIT 9 RATED KVA BASE .
L Diseet Axis Syndmonous,Xe. 1.76 140. 1.267 8.199 Quadsstase AsisSynclunnman.L 1JD6 0.963 0.760 4 805
,, Disest AsisTsundant,Xe . ' O.462- OA20 0.277 - 4 358
^-
; Dhest Axis Sebasammiset,Xm" 9.298 0.271 0.1775 0.1825:
. Negaths Sequence,Xs . 0.2325- 0.211 - 0.225 62055 IssoSequence,L 0.117 0.106 - 0.1077- 80995
- E: TIME CONSTANTS SECONDS 9 75'C.
B- + Disast Axis Tsausbet Open Circuit.Te.o 4.340 4.340 4.340 L 4.340 '
.Disest Amis Sebtamment Shout Circuit,'Te* - 0A17 OAl7 0A18 ODIS gi Disset Amis Tamlaat Short Chestt, Ts' O.654 0.654 0420 642D 3! SHORTCIRCUIT RATIO' O.62 048- 'l.04 1.14 BALANCED T.LF. 14 14- 10 - 10
; REGULATION ATRATEDLOAD PERCENT 43.1 40.65 3547 27.26
SYNCHRONIZING COEFFICIENT - KW/ RADIAN PugLead $870 5660 6240 9960
.E- NoLead 3250 3250 3780 3780
,' B!
FIELD DATA-h at 78t.(00 mas)- 1.292 1.292 1.292 1.291-I
- ameimm*= At No I.med, Rated Voltage (Amps)
Escitation At Rated Lced and Voltage (Amps) Plaid Tesspessaue Rise-T. 39.2 105.1 60A 39.2 9747 50A 55.0 130.22 9)A
$5.0 820.79 SDA Ig EPFICIENCY- RATED KVA AND P.F. 97.21 97.26 96.50 96.54 5: TDTAL WEIGHT-POUNDS 18,100 18,100 ' 18,100 18,100 Stator 9,000- 9,000 9.000 - 9,000-Rotor ,
s,100 s,100 8,100 8,500 End Housingand saastas IA00 1 A00 - 1,000 IA00 2f
. WR2.lb. R.2 12,830 12,830 12,830 12,E30 l ig , TYPICALCHARACTERISTIC CURVE,5es Sessica2 Page iI Pass 12 Pass 13 Bees 14 :
B, , POWER UNIT CAPABILITY CURVE, see Seetion 2 Pass 15 Pass 15 Page 16 Pass 16
, --._ . - - - . . . . _ _ - ~,. _ . . .. ,. , _ _ _ _ - - _ . _. _ - _ _ _ _ - _ , - - - _ _ - - - - _ - _ _ - - -,,, _ _ - - _ - _
EA-FC-90-062 Rnv. 0 1 DG-1 i,6-26-90) MWO - OP-ST-DG-0001- ^"^""" 8 l'-' 110 Fon: exh(ossumed) @l9:45. off @O0:01
-108 -
./ - ,
- 106 - 8 N
- 104 - ,
4 4 10-4 - N 4
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86 - 84 - 82 - 4 80 -
- 78 - .
19:45' 20:15 -20:45- 21:15 21:45 22i15 22:45 23:15 23:45 00:15 00:45 01:15- 01:45 Time
'O- . Front Cob. - @ -'3' ~
~
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.Rav. O ATTACHMENT 8.I6-2 i ,
This is for 85-1 (6-26-98) eastside cabinet front t l3* .. S' -Legger Point 49 itse - Legger peint 42 La ger point 45 - Gastside Ashlent - Esmerater letde ,
- 39:45 :95.s 95.s - 94 ' N.s
- l. N:tB - 98.8 let.S 3
M:45 ; 95.8 105.8 ' ISS.S
- N:30 95.0
) 4-303.4 185.8 -. 95.4 J ' N:45 145.0 ~ ~ 305.9 23:00 - 95.8 305.8 M5.0 = 98 - 95.8 21:45 : .187.8 387.8 j' 21:M 185.8 - 385.8 M.s " ~ 23:45: 95.0 187.8 105.8 22:8B- 95.0 107.8 . 305.8 95.9 I~' 22:45 I 167.0 185.0 92.s 22: N : 387.8 304.8 22:45 95.8 ' 187.8 M3.8 - i' '23:00 91.s 385.0 ISt.8 23:55 92.0 347.8 105.8 95.8 , ~23:5 145.8 185.8 M.S l 23:45 E' M7.8 185.8 95.8
- _ -24
- 00 389.3 - 305.5 48
- 45 ..'
S7.3 142.3 382.8 88: 5 ' 97.2
' 98.9 - rISS.3 93.2 09:45 - 98.3 90.0' 95.9
- i. -> 88:09 98.I 99.3'
- 08:35 - " 95.9 -
95.3
- 95.7 - 92.4 SI N W.I . '98.3 04:45 M.3
- 95.6 : - 98.7 - 73 95.4 '
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EA-FC-90-062 Rev. O i lV2 -(7--16-90) MWdL90 2170 - Anacunsur 8.im Fon:of f@ 1330.sup@ l 717,exh@ 18.50.of f @ l 935
- . 112 110 -
.108 - '
106 - -
-n ._,
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$ 96 - " "
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' _ - Time
- D ' Fro.nt Cob. .O 3 ~+ Front Cob. @ '8' 10: 1 Air intoke to Room. A Gen. Intoke Air
- m -
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EA-FC-90-062 Rev. O ATTACHMENT 8.I7-2 l
~
w Itts is far BC-2 (7-36-90).setside cablest front
. [Aueragel
'3' 8* Getside Auttent Legger Polat 40 Ilse : Legger Pelat 42 Lemer potet # :
' Palats 14-19 Generater latake
. ' 33-M 85.0 35.e 85 . M.e .
l ;33:45 37.8 m.g g i-. gg,, l 34:00 : 90.0 32.3 :
' 34- g,g
_ l14:35~ 93.4 , 97.0 85 3m.g 54:38 92.0 95.0
- 34 g.g
.34:45. : 94.3 . g.g g gg3,g .
- 15:48 : . M.s -gy.g _g- 182.8
. 15:15 - M.e ' - 97.3 g 3g3,g
' 15 38 M.e - 333.3 87 185.8 15:45 97.0 333.3 gg gg,,
- 36
- 00 - 97.0 .
333.3 gg ggg,g
- . > 36
- 15 - ' 97.0'
' 333.0 g gg,g 16 33.s -188.8 as 13.3
.34-45 90.0 333.3 . gg gg,,
37:88 99.9
- 13:'. 5 ;
103.0 ' s~ 3g,3 M.e 333.0 33.s _ 30 p ;u== ..., l .. ,, . p .-17:45 90.8 - g3.3 ' gg gg,g 88:88 -98.8 90.8 m 337,3 l8815 98.8 g3.3 gg ggy,g
' 38 30 -
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~ R3v. O DC-21(7- 17-90) .MWO 90- 2170. ^"^ """"' 8 2 8 -1
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Outside Cobinet Front - Fon Off-J110 - - - -
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108 - ' s 106 - 104 - k c102 -
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f,' 96 -- n 94 - 92 - 90 -f ^ ^ ^ ~ ^ ^ ^ ^ ^ ^ s i - i .- i .. . 16:00 16:30: 17:00 .17:30 18:00 :18:30 19:00' 19530 4 20:00 Time : 0- Front Cob. @ 3' +. ~: Front Cob. @ 8'T
.. o .. 'Intoke Air to Room a: Gen. Intoke Air:
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.EA-FC-90-062 ; .Rav. O 7'
ATTACHMENT 8.18- , 4
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this is for SG.2 (7-17-98) entstes Aabinet nunt- .
'Averaea:
P -- ' 3* S' Setside Au6 W.* Lagter Pelet # - ~ ilme ; Lamar Point 42. - Leger Pelet 46 Palats 34-;0' - Generator Islake 1
-16:40 M.S M.S 80 ' 95.8
, '36:35 M.S 95.8- 30 : '300.9 [ 36:M i ~ - M.S : W.S - . SS ' 16:45 90.8 183.8 l
' MS.S 98 105.8 17:80 ' 47.8 - ISS,4 M ISF.S ;
;' ;17:15 l 98.8 ' 302.9 M i 105.0
' 17:M 98.0 '_. %I.S 1
- 80 15.4
-17:45 . 188.:: - 305.8 98 198.8 :-
4_ 38:88 sel.S -105.8
- 98
- 118.8 '
38:35 305.8 '305.0 - 98 138.8
- _ 38
- 30 101.8 ~ 105.9
" 90 -35.8 IS:# -
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188.0 300.0 90 ' lit.S
.-16:00~ let.S 384.0 90 lit.S IS:ta . ISA.S ISS.S !
90 100.9 6 :30 ISI.S 384.0 SB .ISS.S l
~ IS:45- 100.8 ISS.S at :SP.C 20:00 - 188.S l IA2.8 as 15.0 L. f 1
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2Rev.10 l Q g, o I .V] s ATTACHMENT 8 193 '! u^+ y; r 4
- ansesammeeausgensesmassessmeus . '.aMs W '
The ensemuse noe ier massa asemens et any emar amassen usepsunse T. than 1 4tPC shall est unasse the easses. ' 3 l1 . For seems, n. b. e. f. I: Tempenmue noe = 0.9 iT. - T.) - l
. For noms c. a. s. h: Tw noe = 0.005(T. - T.) - .. ,.
t." . wasse T 'the hengpet temposumme ss given by the toileannt shie #* *'
.i Isene e AM eekse : < .
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A 11K IWC -j B letPC 13PC -
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Pedersee values ei asuksame manpamano absue etPC ase stPC. GrC. OtPC.115'C. L TASLE 38.f. Temessasse mee est amesedimeno one passesses amassess assesse ' [ Class en samaman sense $ .A; 8 F. H #
- lassmal hessessuer I
All masse mie 4.15 somme sesor er susmer ' "tPC 4tPC 11FC Tenu==esweesee asneessee assuri - trC tUC larc . !J5'C =i :, Tasaissene.sesse :-- : mesure WC WC titPC . 12 K i t t Mesen m eessesamme womem. L.u nomse asser WC- 4WC IlrC j- ,e All suer essen WC' ' art - nWC 15T $ Fement honessuse , d Osse assue wah 1.la essasse anew er hasher . - *lUC - MC 11rc i 'f A Tendl==enames annaeumeuse sad 6messisel SC aft !!rt 13C .-
. Aav sueur en home sentist man 48 tusse WC- WC . IIrc ' 13C '. ' ,
. ( All amor esse essen St ' art tWC IWC
"[ Mers: tesse se emesser essesumme es WC:.93eN almonds. Tesommes asamunese tv me !
susumane susenesL o The tune vaangs ser ansie phase and poivphase meusman assare shall be 5.15.30.so ?'- ^ man, ano comanuous. All sheet.ame usangs-ase masse mesa a less test wesen small 0- .= comumence ween uw wasangs ano pans ei the meer ese wahan 5'C of the auseens ;
. t tenur,seesse; . :;
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- 90. Somee Faseer. Geessee ousemos museona6 ama sesoreWessespewer unsesse ase 4
, q, given a " service saseer. ' wassh a&&ours me sneaar es aoever guusser sham maad herespewer wineur enamens ses ussensessa sweessa. The meer is seemoed at scene veience ama ameusarv. The seness somme sesess anr 1.4 ist usass send to se % be; IJS for h a % - 7..
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ATTACmiENT!8~.20-1:
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.a GE Nuclear hergy:
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July 29, 1904 45 m, < aca'.,8,2.< t, h ? Y*. ' . . Mr. W P. Schwartz , , f t Acting Manager - Electrical /I&C Engineering-Omaha Public Power Distract a B, .. 444 South 16th Street Hall-Omaha, Nebraska - 68192-2247 pt; ' i f MBJECT:- GE Static' Exciter 3S7938SA212A11 J REFERDICE: '
, G.P. Schwartz Leeter PED-FC-90-2415 'i '
Lto R.D. Royal Dated July 16. 1996 '
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Dear Mr.iSchwartz:
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T- - GE Wuclear Energy has forwarded Omaha Public Power District's (OPPD) h-J g JGE
. static._exciter. Drive Systen,t Sales, Virginia, technica13y respons
.following:' GE Drive System after review cf OPPD's request offers the
'o-The sub1ect Exciter system was originally annufacturad and?
." : shipped by the Wayneboro. Virginia Plant 20 years:ago. :This
-business moved to Sales. Virginia le years <ago.
- o' 4
No files..technical data folder is available for this exciter-in the oi p It is most diesel likely vendor.- generator the exciter was afspecial application'for thisc h o-
)
b- , The osciter panel'aupplied by-GE was placed'in an enclosureLalong- -
<- with other support equipment to comprise the Baergency Diesel Generator (EDG) vendor's total' system. - ;
Because of the aforementioned. -GE cannot provide OPPD with a cost quotation I -which to base'an investigation.as requested in the. referenced letter. since we However, it is our opinion the open a 50 degrees C ambient temperature. by GE will have no problem working in esciter panel as originally supplied 4 GE total recommends systaa to get theOPPD appropriate contactanswersthethey EDG vendor and obtain heat run d seek.
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J. , lIf you_ have additional questions or comments.. please advise.:
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' Sincerely,
, -l R._D.fRoyal I.., . Manager Electrical /IK services Nuclear' Serv 1ces Department Central Territory' I I RDR/HAS g eca P. Vovk'- OPPD 3 D. Brager ' - GC '
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- DG-1 (6 .25-90)1 MWO..90?-21.71 AnAcuu m 8.21 Fon:off @14i38. supply _@17:05,exh @l7:41
'108
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;- Revo 0 ATTACHMENT 8.21-2
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file:dlese1: This is for SG-1 'NZ} eastside cablast front.
~
. Average ,
3' 8' - . Outside Ambient Legger rotat 49- , . Time. .Legger Polet 42 Leger Polet M Potats 14 Esmerator Intake 'g 14:15 M.2 _ - 86 5 . 85.9 M.0 -
.14:38 85.I' . 87.4 - "85.8 '87.4 14:# :86.7 87.5 - 87.9- 30.3 15:08 : M.8 ' 87.3 ~ - M.7 '93.1-3 . . 15:15 87.5 GE.,3 ' 87.5 97.3
~ 15:30' 88.4 80.1 88.6 98.2
- 15:46 '38.5 90.2 88.3 -100.3 16:00 80.0 98.2 '.80.1 100.3 ~
. : 16:15 - 80.5 90.7 E0.9' 101.7 - l 16:30- 90.4 91.3 80.0 102.6 16: 4 ~88.4 90.4 36.8: 102.6 17:48- 90.8 - 92.2 89.1 101.2
'37:15 - 93.9 M.7 89.6 H.7
..17:38 - 93.8 96.1 89.2 96.4 17:# . 143.4 1M.5 ' N.1 99.1'
- 18:06 145.4 IM.6 L88.2 '100.5
_ _ 18:15 - 1M.4 - IM.9 88.8 98.8 I
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ATT4DeE~T SJE ! k DIESEL GENERATOR.- EXCITER CABINET
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- h. DG-2 64 65 66 67 74 69 70 71~ 73 ;
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- FRONTi VIEV
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,,, LINTERNAL PANEL' TEMPERATURES IN F ,
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, A -- .B C: -D E F G H J gg ,,
m ~ i LDG-1 ?(6-26)- "110- 103. 104- 109 106 103 :108 105 104 86 , c
. 9 DG-2 (7-16):' .120 100 98 110 103 98' .111 103 98: 89 1 ti .
L DG--2 :(7--17) - .125 l103- :101 11 3 106 :100 .11 3 .10 6 '100 90
.NOTEi. LThef above temps, are approximations .of actual field data, p i Li L ATALOGGER POINT '
m .
-;SEE ATTACHMENTS 8.16-8.18; and 8.21:
,, 42 f"8 "DovD 1 1 FOR' GRAPHS 'DF POINT 42 AND
,. AMBIENT. TEMPERATURE. _ cue _nte n.ter.n _iacs _
i \' - l l 4 atan ! TOP VIEV' DF CABINET NOTEi DG-1T(6-26) INFD FROM DP-ST-DG-0001 , DG-2: INFO FROM MVD .90 2170 SKETCH FOR EA-FC-90-062i R0 s 7/90 '1
-_.-.~__.._.._.;---._-~-.-3_x-- - -
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- i. 7 Rav. O AnA unsur 8.23-1, DG- 1 L(6-26-9.0);
- INSIDE/OUTSIDE CORRELATION ~
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- 19:45.:20:15 20:45 21:15 21:45 22:15 f 22:45 23:15 :;23:450'00:15. 00:45 01:15-'01:45
.\ . _. ;. TIME' m? _ :: O : BOTT. LEFT . '
+ BOTT. MID. o BOTT.RIGHT:
4~ A: EAMBIENT '- 1X. L;f j :.a.- :3* FRONT - EFg - VA--52A1 STATUS ~
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EA-FC-90-062 R=v. O ATTACHMENT 8.23-2 as.1 (6.M) mam AF assief 888T. cab. MWS EE. Seti. LEfi gefi. 308. SSIT. Rient 3* Fedet IIA-5M Smelf . IIEE CN. M CM. 19 08. 23 - AIBMet 08. 42 FAS IJ8EL ISP. 19:*5 88.8 88.5 88.3 M ES 4 20:W M.2 M.8 _96.3 .98.4 M 28:15 348.8 5 20:30 E3 E7 95.6 143.0 FM(asemee) M 28:46 M3.0 M 21:00 lee.3 e 1.9 RM.6 90 306.8 M 21:15 M7.8 75 24:38 306.0 188.8 25.4 146.8 M. 21:M M7.8 M 22:09 346.2 . 386.8 AM.2 M7.8 75 22:35 27.8 75 22:38 146.1 388.9 348.7 387.8 M 22:45 147.8 M
; 23:00 387.8 '315.9 306.2 146.0 75 '
23:55 - 147.S M 23:38- ~187.2 187.2 187.5 146.8 75 _ 23:46 387.8 M N:GB 100.3 108.6 308.4 300.3 eff(et:48) M' 08:45 342.3 M. 08:38 97.9 93.0 97.6 98.9 M 88:46 98.3 M St:8B M.6 _ M.3 96.1 98.1 M Mats El M N:2 98.6 97.7 98.3 98.1 - M N:46 98.5 E7 97.4 M E6 M T m
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EA-FC-90-062 Rev. 0 I Ana unen a.24a j
' DG-2' (7- 16-90) .
INSIDE/0UTSIDE CORRELATIOt1 108 , .106 - - - - 104 - 102 - > 3 100 - . , ff < 98 - '
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15 t 94 - -
=
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84 A OFF(13:30) . SUPPLY (17:17): EXHAUST (18:30) OFF(19:35)
~~
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.13:30 14:00 14:30. 15:00 '15:30 16:00 16:30 17:00--17:30 18:00 18:30 19:00 19:30 20:00 TlWE
~
01 BOTT.- LEFT + 'BOTT. MID.' o 1 BOTT.RIGHT. A AMBIENT .x 3' FRONT VA-528 STATUS
= - -
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EA-FC-90-062 Rev. O ATTACliMENT 8.24-2
--86-2 (716) m A m af leEleE agli. CAS. IEn d C .
BSll. LEfi SSii. mie. asti. Slesi Assafar 3' feGet M-52A lagspf . IlsE . CN. 66 . C5. 68 C5. 73 08. 34-19 Q1. 42 FAA LASEL 1EsF. 13:38 M 43 83 86 E 82 13:# -- 86 6 SE 87 SFF(13:30) 82 14:08 88 80 3 84 98 82 14:15 92 - 92 98 85 93 82 14:38 92 92 98 M 92 82 14:# M M 93 86 M 82 15:00 M 93 93 85 M 82 15:15 M M M 85 M 82 35:38 96 96 96 87 95 82 15:6 97 97 97 E 97 82 - M:00 M 97 97 88 97 82 M:15 - 98 96 98 8 97 82 M:30 M 98 SS 88 98 82 M:6 M M 98 8 98 M 17:00 M 98 98 m 98 82 17:15 96 M 98- B 99 SWPLY(17:17) - 82 17:38 90 98 - MS 88 98 82
- 17:5 les les let 88 98 82 14:e les .MS net 98 98 82 2 :15 . let . IM net 88 90 ~ 82
-18:30 let AM lel 98 145 EEIA16T(18:30) 82 m:# les les 305- 80 les 82 19:00 M6 ~ ~ le6 186 88 186 82 39:15 146 M6 185 88 106 82 39:38 188 le6 lee 88 106 - SFF(19:35) 2 19:# W3 302 lel 88 nel ' 82 38:88 28 Ni let 87 10 82'-
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I EA-FC-90-062 Rev. 0 2 A DG-2 (7- 17-90) CHMEM 8.25-1 Iris DE/OUTSIDE CORRELATION-FAN OFF 101 - - - - - - - - ^
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- 98 - -
97 - = F g c 96 - E 95 - 3 , O t 94 - . i a
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, _ a 16:00' 16:30 17:00 17:30 18:00 18:30 19:00 19:30 20:00 TIME
~O ' BOTT. LEFT + BOTT. MID. O BOTT.RIGHT A AMBIENT X 3' FRONT .
'7 '
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EA-FC-90-062 Devo -0 ATTACHMENT 8.25-2 35-2 (7-17) F a mers SF is$ lee SSII. C 2 . M W 5 E E.- BMI. (fFI B0ff. mit. Stif. SMael AISMat 3' Fadst m-52A - ItsE - Ca. M 08. de 08. 73 01, 14-19 08. 42 FAB LADEL M:08 SB B 88 at 98 NF M:35 93 92 91 as M M:30 96 M 93 88 'N 36: 6 97 W 96 90 - 98 17:48 W ~W 96 90 97
' 17:35 98 98 W 90 98 17:38. 98 98 98 m 9B 17:# 90 : 90 90 98 let 38:GB let 188 388 98 M1 IS:15 let let let 98 M1 ,
38:39 let 300 28 .Se Mt M:45 Mt let Mt 90 300 39:48 - Mt MS let 98 - 141 19:15 let net Mt 90 341 19:38 M1 300 ISI 80 21 IS:# MS 389 21 5 let 38:08 300 90 308 5 let 4 w
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q- - I EA-FC-90-062. Rev. 0 Attachment 8.26 I. i p, I in i J ir 3i.. I I .. i t I Letter from Ted Fryar of Morrison-Knudsen a to Randy Mueller, dated 2/21/80 ,
-(12pages) *
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- ATTACHMENT 8.26-/
L' j " {gMS '
. onwe:% REELS _, ,
. O gA c,0NST. REC.
l} EMEmTE $D3REF, .
; February 21, 1980- '
O NlA i> thsha Public Power District INmAL: i J\
- Fort Calhoun Nuclear Plant Fort Calhoun. Neb.
- Attention: Mr. hadv MuaQ Refe : P.O. M6079 Reg. #91
'I
- PS !WO 5256 Gentlemen: -.J Supplementing my letter dated January 22. 1980 I am pleased to enclose pl theDiesel by data sheets prepared from the infomation we had to rate your stand-Generators.
The ratings'with a 50/50 solution of water and' ethylene glycol'in' the hg engine Jacket water cooling system art:
' W Ratines M M N Continuous (*) 2402 W 2330 W 2000 HR5/ YEAR 2654 W 2257 W j-4 HR$/ YEAR 1/2 HR/ YEAR 2000 W 2453 W
, 2583 W 2727; W 2781 W 2510 m 2654 W 2709 W l '
(*) This rating is:ta DEMA standards and merefore ma 105 overload for two (2) hours in a twenty four (24) yhour be operated percid. at a J E; If we may be of further service by working with you to increase the \ Es <. capacity of the generator sets, please-let me know. ! I Thank you for the oppurtunity to work with Omaha Public power District. j Very truly yours, i QWERSYSTEMS
.g H WtRISON-KNUD5EN DIVI 5!0N ]'
~
CT i. ,--. J 1I t s't>c% ' Ted Fryar X" i l 3 1 l
\
Manager. Technic'al services ; TF:wp cc: Mr. Wa Steele - SPPD i Purchasing Dept.
=l Harry . ter. P50. Eng. Dept.
Rao Kattoju. PSD. Eng. Dept. i Milton _sharpe. PSD. Sales Dept.
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] + P. O. 80X 1928 n0CKY MOUNT, NORTH CAn0UNA 27001 I ALL 645 TURBOCHARED ENGINES . (900 RPM) . . EMRENCY STANOBY DUTY
-. These ratings' apply to Emergency 5tandby Applications ONL'Y.
- 20GQ HrfYr 200 Hv/Yr e Hr/Yr 1/2 Mr/Yr '
20-645E4 3950 SWP 4100 BHP 4150 BNP 4225 BHP I 16-645E4 3320 SNP' 3420 SNP 3485 SHP 3520 BHP lt 645E4 2425 BNP g, 2500 BHP 2525 BHP 2574 BNP Thh above ratings are not cumulative and are not subject to overload. I
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. scuenem assomeeu [A.rt.90-062, Rev. 0 '. ATTACHMENT 8.26- 3 l J Diesel Generator lystem Rating:
Engine Dereting Factors - I. ' Radiator Fan Drive Senerator Cooling Fan' 50/50 Glycol Solution 80HP 20hP in Cooling Idater 18 WP B matP Engine Air Intake Ambient l
. ., - Hone-Darsta for 100 F I. '
Gerate for 110 F 100 HP 200 HP
. Engine Ratings 9 90'F or below Continuous- 2000 HR 4 Hour 1/2 HR~
Engice . 3600 3950 l 1 g Derattags g 4150 4225-280 BHP / lod z.746 m.746 g - E475 G E737 x.746 3887 m.746 Gen eff. x .97 Ever x .97 x .97 x .97~ E40Z G Este smoo EsB3 Engine Ratings 9'100'F Continuous 2000 HR d' Hour
, 1/2 HR Engine 3600 BHP. 3950
' Deratings.
g g 4150 g 4225-Gen ~eff. WG W W W Engine Ratings 9110'F Continuous 2000 Ha 4 Hour 1/2 HR
, . Engine 3600 BHP 3980 4150 41:
g, y a m 'A' 4 m.7a. j een erf. g g g g 3
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1ti . . s. L .. r" J: ' y seem sn m aane m ' EA-FC-90-062, Rev.~ 0 ATTACHMENT 8.26-f-Iy = o , at 105 above the rated load for 2 hours in any 24 hour . ratings,do not nave an overload factor. The other Generator Ratings 0110'F air intake temperature or below: l' < Continuous 2600 m i
.. . 2000 HR 2880 W
* 'I Slycolsofution:-Diesel En ine Generator lystem Antings at OPPD (Fort ,
h Amount 9 Air-Intake to Diesel Engine M 100'F 110'F l Continuous 2000 NR 2402 W 2G4 W 2330 W 2257 W 4 HR - 2583 W 2510 W 2d00 W i g 1/2 HR - 1853 W 2727 m 1781 W ~ 2654 W 270g W H I - 1 13 gg 1E - l O f , i P I _ _ ____._ _. _
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- EA-FC-90-062. Rev. O !
AT M ) 8.26- r l OPPD ORDER 44079
- 1 DATA SHttTS !
Engine Data: ya Manufacturer - 'B andal - Electro Notors Corp.Motive Division of Genera ; Serial Nos. to-**5:4, 2 cycle I I Engine Speed - 70C11052 and 70C11016 Continious Rating 900 RPM' 3
- 3600 SHP 9 90'F a. .
o Speed Control - altitude. nd less than 7200 ft i Woodward US-4 Gov. Part No. 852 Serial Nos. 975804. 975005 j (il Generator Onta:- Manufacturer - Electro Motive Division, General' Model Motors Corp. lE- - A20C2 E- Serial Nos. - Generator Speed - 70C11024 and 70C11066 ' Voltage '900 RPM I 2000 Hour Rating Power Factor Continu1ous Rating 4180 volt 3250 KVA/2600 W
-3575 KVA/2860 W Air Cooled .8 i Ratings given 9 Meghanical. Blower 85 C Stator and,60'C Rotor max -
temperature { .
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n-g Radiator Data: j5 ' Manufacturer - Model - Young Radiator Company Serial Nos. - 'D242007 NC1310 ', l Fan and Gear Sox VM6312 and YM6313 (I Manufacturer - L Model- - Western Gear Corp. i I SSV-117 Serial Nos. - Ratio - - 3004 and 3003 , Service HP - 1.5 : 1 104 I t 3 Generator faciter - Manufacturer Regulator. i 3: Model
- General Electrie Co. i Current Forcino Device - 5tatie 35793058212A11 AC Regulation Device 357932YA i
- J DC Regulation Device -
357932M4196Al 357932MA197Al , 3
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. LOADING N RY ATTACHMENT 8.26-B (loth D1esels start)
% gr rim 3gG. M.P. aTART PULL IN PRIOR (QAD NO IQTAL LUs4D QN UNIT w 4 FINAL (gg IQi ON UNIT Wi siasT Kw evtL in Kw
-1 ON UNIT E 10- 750 900 1$00 0 900 2
1500 560 13 1350 " l 3 4 18 30 750 450 1620 900 540 2700 1500 560 1567 2100 2467 3250 3067 1567 2127 900 2127 2667 3027 LI .. 2463-I- 1 - I ~ I \l - I .g H I >
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h. EA-FC-90-062, Rev. O ATTACHMENT 8.26-7 \ ]W LO40!NG SEOUENCE BOTN O!ESEL5 START ASSUMPTIONS FOR LaA0 Mn0EL CALCULATIONS Acceleration time for each setor is 2.5 seconds. For the purpose of K.W. calculation each H.p. is con. sidered equal to one KVA. Thus, 750 H.P. MOT = 750 KVA Load.
'$s Start Power Factor = 0.2 Start in Rush Current = 6 times rated current Start G = 6 x KVA a 0.2 = (1.2 x KVA) K.W.
Pull in W = 2 x Rated KVA = (2 x KVA) K.W. 1 LOAD BLOCK #1750 H.P. = 750 KVA. 3 3 Start W = 1.2 x 750 = 900 W~ Pull in W = 2 x 750 = 1500 KW Lead on Unit at End of Step #1 = 750 H.P. = 750 x 0.746 = $60 m. LOAD BLOCK #2 1350 H.P. Start G = 1380 x 1.2 = 1620 KW Pull in KW = 350 x 2 = 2700 KW Load on Unit at Start of #2 = 1620 + 560 = 213010d Load on Unit at Pull In of #2 = 2700 + 560 ='3260104. Lead at End of Step #2 = 560 + 1350 x .746 = 1567 KW
'LQAD BLOCK #3 ----- 750 H.P. ' (SameasStep#1)
Start lod = 900 KW , Pull In KW = 1500 KW I Load on Unit at Start of Step f3 = 1567 + 900 = 2467 KW.
' Load on Unit at Pull in of Step #3 = 1567 + 1500 = 3067 KW Load at End of Step-#3 = 1567 + 75 x .746 = 2127 KW
,l LQAD SLOCK #4 ----------a----
' 450 H.P.
start IQi = 450 x 1.2 = 340 KW l Pull in W = 450 x 2,a 900 KW Load on Unit at Start of Step 84 = 2127 + 540 = 2667 KW Load on Unit at " Pull In* of Step #4 = 2127 + 900 = 3027 10d g Load on Unit at End of Step 94 = 2127 + 450 x .746 = 246310d I I 4 5 Lg-
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- EA-FC-90-062, Rev. 0:
,, ATTACHMENT 8.26- l?..
5200 ENC 2 0F LDADING - ONE O!ES2L $ TARTING I.' Assumptions as in the previous for case. making Load Model Calculations are the same I ' LOA 0 SLOCK #1 480 H.P. Start W = 480 x 1.2 = 576 W Pull in W = 480 x 2 = 960 W l Lead on Unit at Start of Step #1 = 576 W Lead on Unit at Pull in of Step #1 b 960 W Load on Unit at End of Step #1 = 480 x .746 = 358 G g' LOA 0 BLOCK #2 ----- 1225 H.P. Start W = 1225 x 1.2 = 1470 W
- Pull in W = 1225 x 2 = 2450 W Load on Unit at Start of Step #2 = 358 + 1470 = 1828 W I Load on Unit at Pull.in of Step #2 = 358 + 2450 = 2808 KW
. Load on Unit at End of Step #2 = 350 + 1225 x 0.746 = 1264 W LOA 0 SLOCK #3 ------------- 1060 H. P. *'
Start KW = 1060 x 1.2 = 1260 KW
,3 Pull in W = 1050 x 2 = 2100 KW B- Load on Unit at Start of Step #3 = 1264 + 1260 = 2524 KW
- Load on Unit at Pull In of Step #3 = 1264 +2100 = 3364 W Load on Unit at End of Step #3 = 1264 + 1050 x .746 = 2047 W LOA 0 BLOCK #4 ------------ ' 47.5 H. P.
Start W = 475 x 1.2 = 570 KW I Pull in W = 475 x 2 = 950' W
- l. sad on Unit at Start of Step #4 = 2047 + 570 = 2517 KW Load on Unit at Pull in of Step #4 = 2047 + 950 = 2997 KW Load on Unit at End of Step #4 = 2047 x .746 = 1401, LOADING SUPHutY (ONE O!ESEL'ONLY START)
ITEP TIME 52C H.P. STAR 7 PULL IN . NO< PRIOR LOA 0 KW W TOTAL LOA 0 ON UNIT FINAL LOA 0 ON UNIT W aTAnT KW PULL a m ON UNIT W 1- 10- 480 576 960 l2 3-13 18 1225 1470 2450 358 0 376
'1828 960 2808 358 1050 1260 2100' 1264 1264 j4 30 475 , 570 950 2047 2524 2617 3364 2047 2997 2401 1
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j l l EA-FC-90-062 E Rev. O L Attachment 8.27 L. i n, m n i i I> ! v .t
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" EA-FC-89-026. Rev. O, FCS Diesel Generator Ambient Temperature
'l UpperOperating) Limits c (48Pages
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W* I 3mC1AL Z.~' h j EA-FCo90-062, nev. O ; Engineering Analysis Preparation Engineering Analysis %dTA%C.*3/ At6 Review and proval l Rev. No. d Fom PED-QP .1 Page~1 of 2 EA Page No. A Engineering Analysis Cover Sheet I File No. Total Pages 4 7 1
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EA~ TITLES. Fcs Deessk hSW4 ate 4. AMSIEMT TCMWWA7ust
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l j QA CATEGORY: REPORT TYPE:
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j T ' C>4CQE [ )LimitedCQE C>:3 Analytical R9 port { ( )FireProtection [ ]Special fi f ( ) Revision ; GI INITIATION: . 1 t i 2 . Responsible PED Department MscuA$rc4 L as7 Responsible Department Head SAM A Anm.58# / 8 *E /~ ST ,I> Preparer
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#h / Mh Dat' 8~2 /-89
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Dat s (( .,
" Vendor / PED Department No. 357 Vendor / Dept. Code Due Date E zs-a#
b' ; ENGINEERING ANALYS!$ TYPE: OTHER: f3
. Electrical Equipment Qualification -(EEQ) '
Computer Code Error Seismic E ipmentQualification(SEQ) ' e
. Core Relo Analsis( , ,
Analysis (CCE) Nuclear Mat'l () V
' Fire Hazards Ana sis Accountability (NMA)
' Cable Separation nalysis l [ ]
' ' Operations S ort Associated Circuits Anal s Analysis-h Safe Shutdown Analysis.( SA)
CA)
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USARJustifcation(USJ) X DISTRIBUTION: Copy- !' Name & Sent Copy l Group Name & Sent Location (X) Group
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