ML20207K501
| ML20207K501 | |
| Person / Time | |
|---|---|
| Site: | Fort Saint Vrain  |
| Issue date: | 12/04/1986 |
| From: | Almajan A, Antoinette Lewis, Ryder R GENERAL ATOMICS (FORMERLY GA TECHNOLOGIES, INC./GENER |
| To: | |
| Shared Package | |
| ML20207K390 | List: |
| References | |
| 909204, TAC-63576, NUDOCS 8701090435 | |
| Download: ML20207K501 (204) | |
Text
{{#Wiki_filter:' 4 A . 4 l5 . A E V.10f,2) GA Technologies inc, ISSUE
SUMMARY
TITLE EFFECT OF FIREWATER C00LDOWN USING EES O R&D APPROVAL LEVEL 2 BUNDLE ON STEAM GENERATOR STRUCTURAL INTEGRI &8 3 gN DISCIPLINE SYSTEM 00C. TYPE PROJECT [ DOCUMENT NO. ISSUE N0/LTR. M 22 CFL 1900 1 909204 N/C QUALITY ASSURANCE LEVEL SAFETY CLASSIFICATION SEISMIC CATEGORY ELECTRICAL CLASSIFICATION QAL I FSV-1 FSV-1 N/A APPROVAL T3 PREPARED ISSUE A DESCRIPTION / BY FUNDING APPLICABLE ENGINEERING QA CWBS NO.
! ^
PROJ T PROJECT si n N/C DEC 0 4 W A.C. Lewis . J . Kennec.y Initial Release 29K 106 b R.H.Ry o
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/.f n CONTINUE ON G A FORM 1485-1 N EXT INDENTURED Report pages 1 thru 22 = 22 Appendix A Al thru A6 = 6 Appendix B B1 thru B20= 20 N6757 TOTAL PAGES 48 8701090435 861230 PDR ADCCK 05000267 F PCR REV I SH REV SH 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 ~6 REV SH 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 (MTROYER.AAWOR) 99,133,138 SR-7385 PAGE 1 0F 48
a i l - 909204 N/C i CONTENTS
- 1.
SUMMARY
. . . . .......... . . .. . ... . . .. . 3
- 2. INTRODUCTION ........................ 3
- 3. METHODS AND ASSUMPTIONS . . . . . . . . . . ... . . . . .. 4 4 CREEP BUCKLING OF REHEATER TUBES .. . . . . . .. . . . .. 7
- 5. SUPERHEATER II HELICAL BUNDLE . . . . . ... . .. . . . . . . 16
- 6. SUPERHEATER DOWNCOMER . . . . . . . . . . . . . . . . . . . . 19
- 7. CONCLUSIONS . ........................ 19
- 8. REFERENCES ............... . . .. . . .. . . 19
- 9. CALCULATION REVIEW REPORT . . . . . . . . . . . . . . . . .. 21 APPENDIX A. Thermal Data of Steam Generator SUPERHEATER II Support Plate and Tube During Firewater Cooldown . . A-1 APPENDIX B. Materials Property Input for FSV-HTGR Steam Generator Firewater Cooldown Analysis .. . . B-1 TABLES u.1 Sanicro 31 Material Properties Used For Creep Collapse Analysis . . . . . . . . . . . . . . . . . . ... . 10 4.2 Collapse Time of Reheater Tubes . . . . . . . . . . . . . . .. 15 l 5.1 Superheater II Loadings . . . . . . . . . . . . . . . . . . . 18 FIGURES 3.1 Steam Generator Layout ................... 5 4.1 Modified Creep Subroutine . . . . . . . . . . . . . . . . . . 9 4.2 Effect of Pressure on Collapse Time . . . . . . . . . . . . . 11 4.3 Effect of Temperature on Collapse Time .. ......... 12 4.4 Temperature History . . . . . . . . . . . . . . . . . . . . . 13 4.5 Pressure History ......... ... . ... .. . .. . 14 5.1 Superheater II Suppcet Structure . .. . . . . . . . ... . 17 6.1 Superheater II Support Cooling System . . . . . . . . . . . . 20 I
i Page 2 1 1 i
909204 N/C
- 1.
SUMMARY
This document presents the results of a structural evaluation of the most critical regions of the steam generator during a single cycle cooldown from power using firewater in the EES tube bundles. Simple but conservative methods were used to show that this one-time event will not violate the integrity of the steam generator pressure boundary. The local helium temperatures and pressure vary during the event, l but are characterized by two major segments:
- 1. A short period (about 1-1/2 h) during which the helium pressure peaks to 700 psig and the tube metal temperature is less than i
1300*F, followed by:
- 2. A period of approximately 2 h during which the helium pressure is 350 psig and the maximum metal temperature is 1660*F.
These conditions will not cause failure of the tubes. However, a potential for creep collapse of the tubes exist if the condition of 1660*F and 350 psi are held for more than 20 h.
- 2. INTRODUCTION The structural evaluation focused on regions of the steam generator which were determined, based on previous evaluations of similar loading events, to undergo the most severe loadings (see Refs. 7 and 8).
Under EES cooldown conditions the reheater tubes and their supports have uniform temperatures and low internal pressures, so that very low tube-to-tube support interaction loads are generated. The most severe pressure loading event is where the maxima of external helium pressure and tamperature can combine with zero internal pressure in the tube. This severe loading event can arise in the Fort St. Vrain plant if it is Page 3
. 909204 N/C postulated that the steam side of the reheaters are vented to atmos-pheric pressure while the tubes are externally loaded by the primary helium coolant pressure. This expected external pressure, ccmbined with the hottest helium temperatures (calculated using hot module and local helium hot streaks) impinging on the tubes, sugEests the potential for creep buckling mode of failure of the reheater tubes be evaluated. No other " Primary Stress" loadings on the the tubes were identified as acting during this cooldown event.
The temperatures used in this evaluation were taken from Ref.1 Which gives helium and water temperatures, and from Appendix A of this document. These sources provide temperatures of the helium and selected-structural members during the event (a couldown from 105% power level). This one-time cooldown event is equivalent to an ASME (Ref. 2) Level "D" event and, as such, thermally induced stresses need not normally be considered unless there is justification to do so. In this evaluation the structural evaluations of thermally induced stresses have been considered because of the large temperature difference between the cold firewater and the hot helium. l The purpose of the evaluation is to show that the structural integrity of the primary pressure boundary of the steam generator will remain intact even when firewater is used in the EES tube bundle to cool down the reactor from 1055 power. 3 METHODS AND ASSUMPTIONS The methods and techniques used for this evaluation were based, where possible, on existing analyses of the steam generator. Additional I detailed analyses have only been performed where absolutely necessary. With water in the main steam tubes (EES bundle) (see Fig. 3 1), these tubes will remain cool compared to the helium flowing out from the hot reactor core. The reheater tubes will be at the same temperature as
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. 909204 N/C the hottest helium from core, (this temperature was calculated including the hot module and hot streak effects). The EES tube support structure is also heated by the helium, but part of the structure is cooled by contact with the cooler tubes. The temperature difference between the tubes and -the tube support structure causes differential thermal growth between these components, and this growth produces loads and stresses in the EES components. . The loadings from this firewater cooldown event were compared to the loadings from the normal steady-state 100% power condition. The stresses for the firewater cooldown were obtained by-ratio from the stresses for.the steady-state 1005 power condition.
The differential thermal expansion between the superheater downcomer (see Fig. 3.1) and the support structure was found not to be a 4 significant loading during this event. By comparison with the tempera-ture differentials in the 100% power case, it was determined that the thermal displacements would not introduce significant loadings during this event. The tube support structure will not be at the hot helium , temperature, as it is cooled by a positive flow of cold helium from the l circulator outlet. Its temperature will therefore be closer to the water temperature than to the helium temperature. The creep buckling behavior of the reheater tubes under the external pressure of the helium was evaluated using the GA computer code GA BUCKLE (Ref. 3) . This code is derived from the Pan method (Ref. 4). I j Thermal shock loading of the Sanicro 31 material of the superheat II material was not considered for this analysis, as it was not shown to be a significant loading.for the reheater firewater cool-
- down (Ref. 8). The thermal shock at the superheat II is significantly less as the firewater. is heated during its passage through the economiser, evaporator and superheater I tubes.
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909204 N/C 1 The concerns regarding sensitization of the Sanicro 31 material are addressed in Appendix B of this document. The firewater cannot cause sensitization due to its short time and low temperature during this j event. 4 CREEP BUCKLING OF REHEATER TUBES The empty reheater tubes will be exposed to the hot helium flowing from the reactor core. These reheater tubes will be at temperatures equal to the hottest region of the core outlet, mitigated only by the amount of mixing the helium encounters between the core outlet and the
- reheater tube being evaluated. The Sanicro 31 reheater tube material will be subjected to creep at these high helium temperatures, and, as j the reheater tubes will be externally pressurized, a creep buckling collapse failure mode may be possible. To evaluate this condition, the j GA BUCKLE computer code (Ref. 3) was used.
The creep rate information and other material properties were supplied in Ref. 5 (included as Appendix B of this document). The I Sanicro 31 reheater tube material is a European Alloy 800-type material } which met the required material specifications of Alloy 800 Grade 2 at the time the steam generators were built. For the analysis nominal reheater tube diameters and wall thicknesses were combined with the worst-case tube ovality allowed in a small-radius, cold-worked inlet j tube bend, (as specified in Ref. 6). This is conservative, since the critical location for tube buckling is not likely to be the small-radiue 4 bend where the double curvature of tube wall provides extra stiffness. 1 The most likely location for a tube to experience a buckling failure j . mode is in the regions adjacent to a small-radius bend. This is where the ovalization that occurs at the apex of the bend (caused by the manufacturing process) is carried over into the adjacent unstiffened straight tube. Additional conservatism is incorporated, since the maximum ovality of the inlet tube bends has been assumed to exist in ! conjunction with the maximum helium hot streak temperature. At the Page 7
. 909204 N/C inlet tube bends the helium will have traversed the reheater tube bundle, which will have promoted mixing of the helium hot streaks. The reheater outlet tube bends will be slightly hotter than the inlet, but the maximum tube ovality is significantly less. The maximum ovality at the inlet tubes (bottom) is 12%, whereas the outlet tubes (top) have a maximum of 9% (see Ref. 6).
i The creep subroutine of the GA BUCKLE computer code (Ref. 3) was modified to incorporate the creep equations for the Sanicro 31 (Alloy 800) for the range of high temperatures of this event (see Fig. 4.1). The material properties used are shown on Table 4.1. These were taken from Ref. 5 and are included as Appendix B of this document. The creep buckling computer program, GA BUCKLE, which is based on a method by Pan Ref. 4, calculates the time for the tube ovality to attain the value which causes the tube maximum local stress to equal the yield stress of the material. This program uses constant values for temperature and external pressure, so a parametric study was performed i to evaluate time varying parameters. The results of this study are presented in Table 4.2 and shown graphically in Figs 4.2 and 4.3. Actual values of pressure and temperature vary significantly with time (see Figs. 4.4 and 4.5). There is, thus, a significant margin against creep collapse of the reheater tubes in this case. The calculated creep collapse time is greater than 20 h at 1660)F and 350 psi. The conserva-tive structural model assumes a 2-h time period at the combination of the actual pressure as shown in Fig. 4.5, and the maximum temperature of i 1660)F (note that the 1660)F actually occurs over much less time as l shown in Fig. 4.4). l i A further considerable conservatism exists since, even if the tube does undergo creep collapse, the pressure boundary is not likely to be ruptured, because the residual creep ductibility of the material as substantial at such high temperatures. .The tube could probably collapse to a flat strip and not rupture the material. ~
, Page 8
909204 N/C__ FUNCTION ECREEP (CURTI , DT, TEMP , STRESS , STRAIN , DS , IOP , II, MTYPE) C CREEP EQ. EC=A=(STRESS ==AN)=(TIME ==CAMMA) C MTYPE=1 A800H C HICH TEMP C MTYPE=2 T22 C HICH TEMP C C DOUBLE PRECISION C IMPLICIT DOUBLE PRECISION (A-H,0-Z) C i C0 TD (100,200), MTYPE i 100 U1=-1.21626D04 U2=1.07849003 U3=0.47166 U4=5.141660004 U5=-19.0780 CD TO 101
; 200 U1=-1.22004 U2=-1.169D03 U3=2.125 U4=5.64004 U5=-25.49 101 T= TEMP C= (T-32. ) = 5. /9.
TR=T+460. CAMMA=1./(U2/TR+U3) X=1./CAMMA AN=-U1/TR=CAMMA A=10. . = (- 102 IF (II.EQ(U4/TR+U5)
.1) =CAMMA)T,C, AN, A,CAMMA 10 FORMAT (5X,'c T A (ANWRITE 6,10)
CAMMA',/,5X,5016.8) B=(STRESS /1000.) ** AN TBAR=(STRAIN =100./(A.8)) =X CD TO (1 1 CONTINUE,2), IOP C CREEP STRAIN INCREMENT ECREEP=Aa B= ( (TBAR+DT) = =CAMMA-TBAR = = CAMMA) /100. RETURN 2 CONTINUE C TIME INCREMENT ECREEP= (DS.100. / (A.8) +TBAR= = CAMMA) . .X-TBAR RETURN END Modified Creep Subroutine Figure 4.1 Page 9
_ 909204 N/C TABLE 4.1 SANICR0 31 MATERIAL PROPERTIES USED FOR CREEP COLLAPSE ANALYSIS Young's Coer. Therm. Yield Temperature Modulus Exp. 10,- Poisson's Stress
'F Exp 10* psi in./in.*F Ratio psi
. 1800 . 17.20 1.050 0.431 6,500 1700 18.20 1.035 0.419 9,500 1600 19.20 1.020 0.408 11,500 1500 20.20 1.005 0 398 13.000 1400 21.10 0.990 0 389 14,000 1
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909204 N/C l l 1 I ml E0 Cl
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909204 !UC TABLE 4.2 COLLAPSE TIME OF REHEATER TUBES 12% OVALITY (HOURS) Temperature (*F) Pressure psi 1800 1700 1600 1500 1400 832 0.0 2.32 19.0 196 2600 800 0.0 2.81 23.3 242 3270 780 0.0 3.17 26.7 279 3800 760 0.0 3.60 30.6 323 4430 740 0.0 4.15 35.0 373 5170 Page 15
l h l , 909204 N/C l h
- 5. SUPERHEATER II HELICAL BUNDLE A structural investigation of the superheater helical bundle under the thermal expansion loading was deemed prudent, even though a similar evaluation of the reheater helical bundle (Ref. 8) has not revealed any problems. The superheater II support structure is more flexible than the reheater helical bundle (see Fig. 5.1), and this greater flexibility reduces the thermal stresses. The pressures and temperatures of this loading have been compared to the pressures and temperatures of other load cases, as shown in Table 5.1. The stresses caused by the firewater cooldown have been approximated by using the 100% steady-state stresses and factoring them by the ratio of the applied loads. The firewater cooldown stresses were approximated as follows:
Stresses due to dead weight = No change = 2,156 psi Stresses due to pressure = (8138)(-613)/1822 - 2,938 psi Stresses due te bearhug = (9091)(175)/136 - 11,700 psi Stresses due to wall AT = (51714)(135)/210 - 33,240 psi Primary stresses = 5,094 psi Total stresses = 50,034 psi Primary membrane allowable stress S, = 23.300 psi @380aF Allowable stresses due to all loads 3S, = 69,900 psi @380'F. The firewater cooldown pressures and tube wall thermal gradients are lower than in the 100% power case. The total stresses are not signifi-cantly different from those in the steady-state 1005 power case. The stresses and loadings for the 100% power case have been taken from Ref. 7, and the loadings for the firewater cooldown are included as Appendix A of this document. The structural integrity of the steam generator is not likely to be compromised due to excessive tube / plate interaction loads during the EES firewater cooldown event. Page 16
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._ 909204 N/C
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TABLE 5.1 SUPERHEATER II LOADINGS Loading Plate Temp. *F Tube Temp. *F Temp. Diff. Plt.-Tbe. Condition Tube External Internal Tube Inlet Outlet Inlet Outlet Inlet Outlet Wall AT*F Pressure Pressure P.Diff. Full 1099. 1132, 963 1097. 136. Load 35, 210. 690. 2512. 1822. Quarter 932. 1032. 875. 1032. 57. O. Load 87.5 589. 2419. 1830. Transient 1110. 1135. 995. 1090. 15. 45. ? 9A 920s. 469. 2713 2244 Transient 1110. 1135. 997. 1100. 113. 25. 9A @50s. ? 469. 2713 2244. Transient 1085. 1120. 965. 1105, 120. 15. ? 469. 2713. 2244. 9A @l00s. Transient 1015. 1045. 915. 1015. 100. 30. ? 469. 2713. 2244. 9A @300s. EES F/W 455. 301. 286. 294 169. 7. 128. 700. Cooldown 87. -613 1 75% Power EES F/W 468 302. 293 296 175. 6. 135. 700. Cooldown 87. -61 3. . y 105% Power o
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- j 0 Information on full and quarter loads and on transient 9A were obtained from Ref. 7, Section 6.3. p.16.
1
t I. l . i 6. SUPERHEATER DOWNCOMER Because the superheater support structure is cooled using cool helium from the circulator output plenum (see Fig. 6.1), the difference in temperature between the superheater downcomer and the superheater support structure are very small (see Appendix A) and will not cause i significant differential thermal expansion. Therefore, a comparison of l the temperatures used for analysis of the 100% power case with the firewater cooldown temperatures was sufficient to confirm that this region would not suffer failure during this event.
- 7. CONCLUSIONS The results of this structural evaluation of the most severely loaded regions of the steam generator, during a single cycle firewater cooldown from power by using firewater in the steam generator main tube bundle, has shown that the most critical region is in the reheater.
This is because the reheater tubes are at the hot helium temperature and are externally pressurized, making creep buckling collapse the critical mode of failure. This evaluation has shown that the reheater tubes will not suffer a creep collapse during a single firewater cooldown event provided that the power level is limited so that the maximum helium temperature is less than 1660*F for less than 20 h and the corresponding maximum helium pressure is not more than 350 psig. No other regions were found to have high atr(sses during this event.
- 8. REFERENCES
- 1. Potter, R. C.,
" Firewater Cooldown with 300*F EES Exit Temperature (1.5-Hour Delay)," GA Document 909052, October 6, 1986.
- 2. ASME B&PV Code, Section III, and Code Case N47.
Page 19
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.- ... . _ _ . - ~ - , . - _ . .. - - - - - - - - - -
909204 N/C 9 3 Krishan, M., GA Internal Memo 306-4426, " BUCKLE User's Manual," July 1980.
- 4. Pan, Y.S. , " Creep Buckling of Thin-Walled Circular Shells Subject to Radial Pressure and Thermal Gradients," J. of Applied Mech. , March 1971, pp. 206-216.
- 5. Lindgren, J. , " Materials Property Input for FSV-HTGR Steam Generator Firewater Cooldown Analysis," GA Memo MC:114:JRL:86, October 29, 1986. (See Appendix-B.)
- 6. GA Document GGA-D-41, Issue A, " Quality Assurance Procedure for the Colling and Bending Qualification," March 4, 1970.
- 7. GA Report No. GADR-9, " Stress Report for Fort St. Vrain Steam Generator," October 1, 1970.
- 8. Lewis, A. C., et al., "Effect of Firewater Cooldown Using Reheater, on Steam generator Structural Integrity," GA Document 909190, November 1986.
- 9. INDEPENDENT REVIEW REPORT The calculation review report is discussed on the following page.
i i Page 21
wvmw. v vwn o CALCULATION REVIEW REPORT TITLE: EFFECT OF FIREWATER COOLDOWN U3ING EES APPROVAL LEVEL 2 BUNDLE ON STEAM GENERATOR STRUCTURAL INTEGRITY QAL LEVEL 2 OlSCIPLINE SYSTEM 00 C. TYPE PROJcCT DOCUMENT NO. ISSUE NOJLTR. M 22 CFL 1900 909204 N/C INDEPENDENT REVIEWER: M. T. Jakub ORGANIZATION 660 m /7 i i REVIEWER SELECTION APPROVAL: BR MGR ~
! { DATE #!M b
// / /
v REVIEW METHOD: YES NO ERROR DETECTED ARITHMETIC CHECK LOGIC CHECK / Ok - l ALTERNATE METHOD USED # SPOT CHECK PERFORMED N , COMPUTER PROGRAM USED Ccmpariscn te Ref 8 f W REMARKS: (ATTACH LIST OF DOCUMENTS USED IN REVIEW) Se f. 8 and the referenettc of Hal clccumerk. l l CALCULATIONS FOUND TO BE VALI AND CONC IONS 0 B CORRECT: INDEPENDENT REVIEWER
% /- ag NOVP4
- DATE SIGNATUflE Page 22
909204 N/C ) l
. I l
APPENDIX A THERMAL DATA 0F STEAM GENERATOR SUPERHEATER II SUPPORT PLATE AND TUBE DURING FIREWATER C00LDOWN Page A-1
. l 909204 N/C i
, I SH2 SUPPORT PLATE AND TUBE TEMPERATURE Appendix A of GA Document 909190 N/d' defines a method for the
- evaluation of steam generator support plate and tube temperatures. This same method was used to evaluate the SH2 support plate and tube temperature for emergency cooling from 1055 power.
Computer run ST 4249 is the SUPERHEAT evaluation of steam generator performance for a cooldown from 105% power. This analysis is based on
" steady-state" conditions at the peak helium temperature. This run contains the tube temperatures and the boundary conditions needed to evaluate the support plate temperatures. Computer run ST 2143 is the evaluation of the support plate temperatures for.the conditions defined in the SUPERHEAT run. Tables A-1 and A-2 contain the results of this analysis.
1 ,i 4 i Page A-2
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909204 N/C i TABLE A-1 l OPERATION AT 105% Distance l from Top Mean Tube Temperature Tube Wall AT (Inch) (*F) (*F) 1.86 293 135 5.58 283 89 9.31 284 59 13.03 286 40 16.75 289 27 20.47 291 18 24.20 293 12 27.92 294 9 31.64 295 6 35 36 296 4 Page A-3
909204 N/C TABLE A-2 OPERATION AT 105% MEAN SUPPORT PLATE TEMPERATURE Distance from Top Temperature (Inches) 'F 0.0 468 3.72 428 7.44 386 11.17 359 14.89 341 18.61 328 22 33 318 26.06 31 2 29.78 308 32.50 304 37.22 302 l l l Page A 4 l
909204 N/C EESH1 SUPPORT CYLINDER AND DOWNCOMER TEMPERATURES The EESH1 tube bundle is supported by the EESH1 support cylinder. This cylinder is located interior to the inner gas guide (see Fig. A-1). The space between the inner gas guide contains the downcomer tubes. As seen in Fig. A-1, cold helium from the circulator discharge is used to cool the support structure. Under normal operation the helium flow in this region is about 2% of the total helium flow. For emergency cooling, where the total helium flow is in the order of 2% of the normal design flow, the support cylinder cooling flow will be very small, but it should prevent gas flow from the mainstream from entering the area between the gas guide and the support structure. Considering the following conditions: (1) cooling flow at approximately 80*F, (2) EESH1 main helium flow at 320'F at the hot end and 82'F at the cold end (per SUPERHEAT run ST 4249 for cooldown from 105% power), and (3) the downcomer at the hot water temperature of 300*F. The maximum support cylinder temperature will not exceed 300'F. i i } 1 l 4 t l i Page A-5 i
. i
_ 909204 N/C L -
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. I, I
l PERFORATED
/ -
- ' i N il0T REllEAT STEAM FLOW PLATE ",
w : SUPERHEATER - OUTLET TUBES :
. .?
SUPPORT CYLINDER COLD RETURN ,' GAS FROM - ' l CIRCULATORS l l
^
~ . . _
i , Superheater Support Structure Figure A-1 Page A-6 l '._,__.. _.m_._____ __ _ ._ _ _ _ , _ __ _ _ . _ . _ , , . . . . _ _ _ _ . . . _ . . _ _ _ _ . . . _ . _ _ - ,_ , _ _ _ _ . _ _ _ _ . . . . . _ . , . _ _ _ _ _ _ _ _ _ _ _ _ . .
I l 909204 N/C APPENDIX B MATERIALS PROPERTY INPUT FOR FSV-HTGR STEAM GENERATOR FIREWATER C00LDOWN ANALYSIS Page B-1
909204 N/C IN REPLY FROM J.R. Lindgren REFER TO IEC 124:JRL:86 TO R.H. Ryder DATE November 24, 1986 SUBJECT Responses to questions Regarding FSV-HTGR Steam Generator Emergency Cooldown Analysis Per your request, the answers to questions on (1) the effects of sensitiza-tion on the extent of stress corrosion cracking of Sanrico 31 and, (2) thermal shock effects on the heat affected zones of weldments in Sanrico 31 are given below.
- 1. SANRICO 31 Sensitization Effects on Stress Corrosion Crackinat (SCC)
, Chromium carbides precipitate in Sanrico 31 at temperatures between 1000 and 2000 F (540 to 1095 C) which can make it susceptible to granular corrosion in hostile environment in the temperature range from 1000 to 1400 F (540 to 760 C). When cracking occurs in sensitized material in oxygen containing low chloride environments, the cracking occurs along grain boundaries leading to the supposition that the cracking involves dechromised zones adj acent to the grain boundaries; whereas in non sensitized material cracking is transgranular. However, the stress corrosion cracking even with sensitization in the Sanrico i 31 steam generator is expected to be minimal for the following reasons:
- 1. The alloy has a composition providing resistance to stress corrosion crack-ing and when tested in deoxygenated steam between 1000 to 1400 F (540 to 760 C) it forms a strongly adherent oxide layer so that its creep resis-tance is unaltered (Ref. 1).
- 2. The water chemistry in FSV-HTGR is controlled so that the presence of oxy-gen anc chlorine which cause SCC are maintained at levels where SCC will not occur. The chemistry of the fire water introduced under accident con-dicions is ' not similarly controlled but the short duration (220 hours) of the event makes it likely any occurrence of SCC would be minimal.
B2 1
909204 N/C
, 3. In the Peach Bottom-HTGR where Alloy 800 steam generator tubing which has a composition very similar to Sanrico 31 tubing, no SCC due to sensitization was found to have occurred (Ref. 2).
- 2. The Ductility of Heat Affected Zones in Sanrico 31 Weldments and Thermal Shock Effects In general, the tensile and stress rupture ductility of the heat affected zone (HAZ) of Sanrico 31 type Alloy 800 weldments are the same as for the parent metal (Ref. 3) including ductility in creep tests up to 46,000 hours in duration. Instances have been reported (Ref. 4) where brittleness and liquation cracking have occurred in materials like Alloy 800 where elements other than normal Alloy 800 constituents were present or alloying elements such as copper and silicon were present in higher than specified amounts. This is however, not known to be, or expected to be, a problem in the FSV-HTGR steam generator tubes. As a result, the effects of thermal shock on the heat affected zones of Sanrico 31 should be the same as for the parent metal. The lowest end of life ductility projected for the parent metal and the HAZ is 8%
tensile elongation. REFERENCES 1. J. Blanchec, and H. Coriou, " Review of the Corrosion Resistance Properties of Alloy 800 in High Temperature Steam," Proceedings of Petter Interna-tional Conference, March 14-16, 1978, pages 241-262.
- 2. " Metallurgical Examination of Primary Circuit Components from the Peach Bottom HTGR, GA-A14506, February 1978.
- 3. Stannett, and A. Wickens, " Alloy 800 Tube Welds - Assessment Report," ERA Technology Ltd., Dec. 1982 (not for external distribution).
- 4. D. McKeown, " Review on Welding Alloy 800," Proceedings Pettern International Conference March 14-16, 1978, pages 371-387.
JRL:HDR i cc W.R. Johnson A. Lewis D.I. Roberts i .l B3 i
909204 N/C INTERNAL CORRESPONDENCE GA 1076 IN REPLY FROM: J. R. Lindgre J. B. Wattier REFER TO TO: R. H. Ryder W DATE 11/12/86
SUBJECT:
Addendum to " Materials Property Input for FSV-HTGR Steam Generator Emergency Cooldown Analysis" MAB:114 JRL:86, Dated October 29, 1986 At the request of W. R. Johnson, the references applicable to the materials input given in memorandum MAB 114:JRL:86 are given below.
- 1. Sterling S. A. " Temperature-Dependent Power Law for Monotonic Creep" GA-A13027, hrch 1976 2.
Aerospace Structural Metals Handbook, AFML-TR-68-115 1979 Publication, Code 1103, page 11, Fig. 3.062. Modulus of Elasticity at Room and Elevated Temperatures 1/2 Cr - 1/2 Mo T-1 steel. 3. Wattier, J. B. to W. G. Hardin "A Temperature Dependent Creep Equation for Carbon Steel" 209:25:78, February 14, 1978.
- 4. Smith, G. V.
" Evaluation of the Elevated Temperature Tensile and Creep Rupture Properties of 1/2 Cr - 1/2 Mo, 1 Cr - 1/2 Mo, and 1 1/4 Cr - 1/2 Mo 1973.
Si Steels' Prepared for the Materials Properties Council, ASTM DS50, 5. Smith, G. V. " Supplemental Report on the Elevated Temperature Properties of Chromium-Molybdenum Steels (on Evaluation of 2 1/4 Cr - 1 Mo Steel) Prepared for the Materials Properties council, DS6S2, 1971. 6. NRIM Creep data sheet No.-3 (1972) and No. 11 (1974) " Data Sheaets on -~ the Elevated Temperature Properties of 2.25Cr-1Mo steel. 7. NSMH Vol 1 Design Data, Property code 2206 Part 1 Structured hearials, Group Equation2,Page Low Alloy Steels Section 2, 2 1/4 Cr - 1 Mo, Revision 1, Creep 1.3, Young Modulus, pages 1.0, 1.1, 1.2; Revision 0 Property Code 2110, Piosson's Ratio. 8. Wattier, 1980. J. B. " Alloy 800H Creep Equation" GA Doc 906211 page 6, Aug. 9,
- 9. Wattier J. B. to D.
I. Roberts " Determination of Maximm Allowable Primary Membrane Stress, So, for Temperatures in The Creep Range for Alloy 800H" MAB 29:JBW:83 March 3, 1983.
- 10. Schill, T. V. to M. P. Ranson "Incoloy 800 Data Package" No.C-45, Huntington Alloys, Inc. Div. of Inco, h rch 24, 1981.
- 11. Telecon J. R. Lindgren, GA and J. M. hetin Inco "Minimm Residual Tensile Ductility after Thermal Aging Alloy 800 grade 1 and Creep i
l B4 I k I t I
909204 N/C Equations / Data for Alloy 800 grade 1 up to 1800 F," October 17, 1986. ., 12. Discussion J. R. Foulds and J. R. Lindgren GA "Mininmun Residual Tensile Ductility of Alloy 800/800H after Thermal Aging" October 16, 1986. 1 J 4 = l I I i i BS i
- - . . - . - . . . . . _ _ _ . . . _ _ . . - . . . . - . . _ _ _ . _ _ _ . _ . - - , ~ . - _ _ _ _ _ - _ _ - _ . _ _ - . _ - - - . - - _ . - - - . . . . _ ,_.-_--
90920dN/C I PRON (hP J.R. Lindgre L/J.B. Wattier In mErty
' REFER 10 M C:124:JEL:36 TD R.R. Ryder/ Alan Lewis Proj ect 2970106 D&TE Oct ober 29, 1986 SERIBCT Materials Property Input for FSV-87UR Steam Generator Emergency Cooldown Analysis The following data on asterials properties were provided for creep collapse, thermal shock and bearhug analyses: .
- 1. GEEP COLLAPSE ANALYSIS 1.1 Creev Ecuations 1.1.1 T-2 (1/2 Cr - 1/2 No steel)
U 'U U Los t = b los a + T 2+D3 Icg c, + b + U3 (1)
.T T B
Log i ,= B + 1 + .B 2 los a . (2) T T
= 1 1.989551E+01 - .3 017 . 6549.50580 3,g u T T e,= ti, Los e, = los t + log i, Log t = Log - log i Substituting for log i, Eq. (2)
Page B6
909204 N/C e Logt= 2 log a + los e, 1
-B T 0 T
equating coeff in Eqs. (1) and (2) gives U = -B 1 2 U = 0 2 U = 1 3 U4 = -Bg
- U S"~0 i
a
= %/hr t = time hrs _
a = strain (%) i e = kai log t =B +BT+B"*B 0 2 3 8'
= 3.252998E+01 - 0.01590 T - 0.07424 a - 0.00165 T log a Tertiary = 0.525 t r t ( 3000 hr, temperature 9001 oF i 1400 e in kai e > 0, i e < min nitimate tensile strength at temperature T in or 1.1.2 T-22 (2-1/4 Cr - 1 No stes!)
ng 'n Los t = 2 log a + +n log e, + _"4+n 3 T T 5 T t
, Page B7 -- - - - + - ,,-,-r-----e ,,. -,__--,-n. --, , ~ , - . - , - - - - - - . . . . . , - - . . , , ,--g e---- ,- -----n-+ a e,-,-9e r--,c--
909204 N/C where t is time (hours). e is stress (ksi), s e is creep strain (%), and T is absolute temperature (OF + 460). Power Law Coefflef eats Complete Power Law *
- Limited Power Law
- Anasaled Annealed 2-1/4 G-1 NO Alloy 8005 2-1/4 G-1 NO (for 1200-1800*F) i Ug -1.22 x 10 4 -1.126 x 10 4 -1.21626 x 10 4 .
U 2 -1.169 x 10 3 1.033 x 10 3 1.07 84 9 = 10 4 U 3 2.125 0.7232 0.471666 U 4 4 5.64 x 10 4.913 x 104 5.14366 x 104 0 5 -25.49 -21.52 -19.0780
'los e 0.145 0.116 900 - 1200*F 1000 - 1200*F Best fit The time is limited by initiation of tertiary creep, t, can be esti-mated from the rupture life, t,, 3 by t
3 = 0.525 t, , a>0,
, a < min ultimate tensile strength at temperature T where j
los t, = C, - 10.307 los a - 0.03691T + 0.004638T los e (from NSNE) . N0'IT. : e = MPa, T = 'I j The lot constant C, had an overall average value of 47.253. sith an average value of 47.395 for annesled asterial only. 1 0 Page B8
909204 N/C f 1.1.3 Alloy 800H u '3 2
- los t = - los a +m 3 log e, + __4 + 35 T
.T T
,-12162.6 3,g , , 1078.0 + 0.471666 l og e, +
T T - 19.0780 T Log (t, + 3) = B 0 + Bg /T + B2+B3 los a
= -17.0212 + *
+ 0.785712 - 12379.81 log a T
t, = t ruptwe in hours T = *F + 460 'F = 1200* to 2000*F e = kai a > 0, a < ultimate tensile strength at temperature T B 0 = -17.0212 By = 48158.12 B 2 = 0.78572 B 3 = -12379.81 0.994 0.2% t 3 = 0.385t r where t 3 = time to tertiary creep in hours B log i,= B + 1 + .B 2 log e T T
= -17.0212 + 48158.12 , 0.78572 log a T T _
i l . 1 . Page B9
909204 N/C 1.1.4 Alloy 800, Grade 1 B B Los t r =B 0 + d + 2 los a 20 to 1000 hours T T
= -1.668672E+01 + 077.79675 _ 10621.82464 3,g ,
T T t, = time to rupture in hours t 3 = time to tertian in hours = 0.385t9 W ' T = 'F + 4 60. 'F = 1200' to 2000'F , a = ksi, a > 0 a < ultimate tensile strength at temperature T Log i =B _ 1 + _2 los a m 0+7 T
= 2.344083E+01 - '* +
- T los a T
i,= minimum creep rate %/hr 1.2 Younr's Modulus See attached sheet A-I for T-2 (1/2 Cr - 1/2 Ho). A-I, A-III, A-IV for T-22 (2-1/4 Cr - 1 No) . 1.3 Poisson's Ratio See attached sheet A-V for T-22 (2-1/4 Cr - 1 Mo) . We suggest were not found. that values for T-22 be used also for T-2 for which values 4 - Page B10
909204 II/C 1.4 Tield Streneth See Figure 1 and la for yield strength vs temperature for T-2 and Fig. 2 and 2a for yield strength vs temperature for T-22.
- 2. 71rP2 MAL SB03 ANALYSIS 2.1 Lowest tensile ductility for Alloy 800H tubing in temperature range RT to 600*F. taking into account thermal aging environment, and cold work.
The effects of thermal aging are the most significant at 1100'F ( 600*C) and those effects on room temperature ductility appear to saturate at about 40.000 hours so that at the end of life the minimum RT tensile ductility would be 8% total elongation. worked Alloy 8008. This is true for both solution annealed and cold _ The tensile ductility of cold worked material initially is less than half of that of solution annoaled material, but spon thermal aging at temperatures of about 1100*F f or 40,000 hours the dsctilities of sointion annealed and cold worked Alloy 8005 are essentially the same (per discussions with Jude Foulds of GA and J.M. Martin of Inco International, Inc.).
- 3. BEARHUG ANALYSIS ne lowest RT to 600*F tensile dactility for the coiled past of Alloy 800H tube bundle (i.e. . not tube bends) taking into account thermal aging and environment is 8% total elongation.
His minimum is reached due to thermal aging effects as discussed in Section 3 above. JRL:MDR cc: J.R. Foulds Y.R. Johnson D.I. Roberts Bil Page
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PART I - STRUCTURAL MATERIALS GROUP Z - LOW ALLOY iscr.LS SECTION 2 - 2 1/4 Cr-1 Mo REVISION: 0. 5-1-77 YOUNG'S E DULUS (Cont'd) TABLE II - DYNAMIC YOUNG 's MODULUS
**S I UN IT S DEG C TEMP. (US UNITS STRd.S INS P APENTHESES)
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CA 143 6 909204 N/C f -p g
"" ' ^ ' 3 DATA BOOK GENERAL ATOMIC COMPANY " " " ' '*
- ,= PART
- VOLUME GROUP:
I-STRUC URAL MAicxIALS 2 LOW ALLOY w -'t MATERIAt.:
.REV!slotJ: -0 2 1/4 Cr - 1 Mc DATE: 11-1-75 ' i m E:
PROPERTY C::DE: 2110 POIS20N's RATIO (DYNAMIC AND STATIC) 1
- 1. Applicability l 1.1 Product forms per specifica:icns listed beicw-Seamless Tubes and Pipes SA 325-P22 SA212-722 P1are SA 357-Gr22 Bars and Rods SA 225-F22a 1.2 Annealed =aterial only
- 2. Gracnical Dau:
The ca:a pains en whics dese ecuatiens; are based will .be incoroc in a subsequen issue gf this pr::per:y. I-
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\ ATTACHMENT 8 l l l
Attachment 8 to P-86682 Page 1 of 4
SUMMARY
OF STRUCTURAL AND METALLURGICAL EFFECTS OF A FIRE WATER C00LDOWN TRANSIENT a UPON THE EES AND REHEATER SECTIONS OF J THE FORT ST VRAIN STEAM GENERATORS
REFERENCES:
- 1. NRC Letter Butcher to Lee, dated November 1, 1985 (G-85459)
- 2. PSC Letter R.F. Walker to H.N. Berkow, dated December 20, 1985 (P-85488) j ATTACHMENTS TO P-86682:
- 4) " Fire Water Cooldown Using One Reheater Module (1-1/2 Hour Delay)," General Atomic Technologies Report No. 909113A, 12/03/86
- 6) "Effect of Fire Water Cooldown Using Reheater on Steam Generator l Structural Integrity," General Atomic Technologies Report No. I 909190A, 12/12/86
- 7) "Effect of Fire Water Cooldown Using EES Bundle on Steam Generator Structural Integrity," General Atomic Technologies Report No. 909204N/C, 12/04/86 l 1
- 9) " Analysis of the Capability of the Fort St. Vrain Steam Generator l to Withstand the Fire Water Cooldown Transient Following an )
Appendix R Fire" Rev. 1, Proto-Power Corporation, 11/86 l l DISCUSSION: l The purpose of this report is to summarize the structural and metallurigical effects upon the Fort St. Vrain Steam Generators of a postulated Fire Water Cooldown Transient following a 90 minute Interruption of Forced Circulation (I0FC) from 105% reactor power. The summary includes a cooldown of the reactor using a Reheater section or an EES section of a steam generator. This transient could occur as a result of a High Energy Line Break, a Design Basis Earthquake, a Maximum Tornado, or a major fire outside the congested cable areas. Four reports (Attachments 4, 6, 7, and 9) were prepared to address some concerns about the capability of the steam generator modules to withstand the injection of relatively cold water from the plant's fire protection system during a cooldown using either the Reheater or EES sections of the steam generators. These reports are in response to the Reference 1 letter which requested that PSC provide an evaluation of the effectiveness of this mode of cooldown, considering the possibility of damage caused by occurrences such as water hammer or overpressurization. Additionally, PSC, in Reference 2, committed to addressing a vapor lock condition that could prevent establishing
Attachment 8 to P-86682 Page 2 of 4 fire water flow through the steam generators. The results of these reports as related to the subject transients are presented below. Structural Effects of Introducing Cold Fire Water Into the Hot Steam Generator A review (Attachment 9) was made of the original design _ calculations (GADR-9) and other relevant documents. The review indicated that the steam generators were well designed from a structural standpoint. The stress levels for the transient were compatible with ASME limits and fatigue usage factors were also acceptable. No locations were found where the loads induced by the thermal expansion / contraction caused secondary stresses with primary stress characteristics that could cause failure of any tube upon one application of the load. Thermal shock was found not to be a problem for one cycle of the subject transient for the ductile materials of the steam generator tubing. A concern, however, was raised about the response to a thermal shock of the Sanicro-31 (Alloy 800) tubing located in the Reheater and Superheater II. These tubes were originally cold formed and were not stress relieved, resul ting in reduced ductility. General Atomic Technologies prerared a report (Attachment 6) which addressed these concerns for the reheater cooldown. It was found that the introduction of cold fire water would result in a worst case strain of 0.49% compared to an end of life ductility of 8%. This is considered to be a suitable factor of safety for failure of any tube. Additionally, the Attachment 6 report found that thermal shock induced strains in the tubing welds presented no problems. The thermal shock in the Superheater II section of the EES were similarly found to be within acceptable limits in the Attachment 7 report. The ; limiting factor affecting acceptable power levels for a Reheater cooldown was found in Attachment 6 to be creep buckling of the carbon steel tubing in the EES section. In this scenario, some of the EES tubes would be subject to external reactor pressure and to helium flow et the reactor outlet temperatu.e. This situation would result in tube creep buckling given high temperatures for a sufficient period of time. Buckling of the tubing was used as the failure criterion. This is felt to be conservative as the actual failure 1 criterion is the loss of the primary coolant boundary, i.e., a thru- ; wall crack in a tube. Buckling of the tubes would not necessarily l cause a loss of the primary coolant boundary particularly when the i material ductility at the temperatures involved is considered. l Attachment 4 reports that the allowable power level considering these l effects is approximately 40%. l Flow Path For Steam from a Steam Generator and the Potential for a Vapor Lock Condition A detailed review of the geometry, arrangements and heat transfer and i hydraulic characteristics of tne EES section has been performed 4
Attachment 8 to P-86682 Page 3 of 4 (Attachment 9). It was concluded that with one fire water pump operating, flow can be established and maintained in all six modules of an EES section without vapor lock (i.e. total flow stoppage occurring in any of the modules). It was found necessary to control ] the primary coolant flow rate to prevent steaming in the EES section which would result in increased back pressure and reduced cooling i flow. l l Effects of Water Hammer on the Integrity of the Steam Generator } Steam condensation induced water hammer results when cold, subcooled l water comes in contact with pockets of steam in a closed piping l system. Under certain conditions, the steam pocket will suddenly l collapse, creating a localized depressurization at the void. The j resulting pressure imbalances at the water / void interface causes the l water slug to accelerate towards the void. Pressure pulses occur and < travel through the system when the slugs collide. An event of this i type occurred at San Onofre Unit 1 and is described in NUREG-1190. The Attachment 9 report determined that damage to the steam generators due to condensation induced water hammer will not occur for an EES cooldown. Effects of Overpressure Conditions Due to Boiling on the Integrity of the Steam Generator Tubes I I The concern was raised that a rapid increase in system pressure could occur if steam bubbles were to form in a water filled steam generator tube during cooldown, resulting from the large volumetric expansion of the flashing water. This could be caused by a sudden increase in heat transfer in the steam generator due to a large, sudden increase in circulator speed. Emergency procedures of Fort St. Vrain preclude this condition from occurring. Once the steam generator is flooded j with fire water, helium flow is initiated and is controlled to I maintain liquid conditions at the steam generator outlet. This will l prevent boiling in the steam generator. I In the event that helium flow were inadvertently increased to the 1 l maximum 3% design core flow rate achievable for a fire water driven l circulator, boiling in a water filled section could occur. The i Attachments 9 and 4 calculations show that overpressurization in this I case would not occur. l 5 Metallurgi:al Effects Upon Steam Generator Tubing of the Fire Water l Cooldown fi ansient l A study w1s perforraed to determine what metallurigical effects would occur in t1e steam generator tubes due to the prior service life and the Reheater and EES cooldown transients. The steam generator tubing materials can be divided into two groups. The first is the Sanicro-31 tubing found in the Reheater and Superheater II. The second is the remaining tubing consisting of 2-1/4Cr-1Mo, 1/2Cr-1/2Mo, and carbon steel. l
..._ _ _.____._ _ __ . --J
5 Attachment 8 4 to P-86682 Page 4 of 4 1 The Sanicro-31 tubes are potentially subject to metallurgical changes as a result of their service life prior to the cooldown transients. These changes include recrystallization, sensitization, and precipitation aging, and can have a negative influence on the fatigue life, residual toughness, and residual ductility of the material. A , loss of fatigue life is not a concern as the transient would be a single-cycle event resulting in plant shutdown. Extensive long term experience with the material in welded construction in elevated temperature service, together with considerable laboratory data, indicates that the material retains sufficient toughness to assure notch-ductile behavior under the loading rates applicable to the cooldown transients. The reduction in residual ductility, however, raised concern about the tubes surviving the thermal shock and
; increased bending loads caused by the cold fire water flowing through i
the hot tubes. The Attachment 6 and 7 reports investigated this and
- found that the tubes and their welds have ample margin to survive the cooldown transients at any point in the plant's life. Additionally, 4
the Attachment 6 report found that sensitization to stress corrosion cracking does not present a problem due to the short duration of the transients. i l The second group of materials mentioned above is subject to corrosion when exposed to the chemically untreated fire water for extended periods. .These tubes could corrode approximately 10 mils per year. The corrosion rate could be enhanced by erosion caused by particulates found in the fire water. For the low flow velocities involved and for the length of the cooldown, corrosion of-these tubes
- is not expected to be significant.
I i i i I l
I t ATTACHMENT 9 W
MLT -8 6 - o(. 4-q ANALYSIS OF THE CAPABILITY OF THE FORT ST. VRAIN STEAM GENERATORS TO WITHSTAND THE , FIRE WATER COOLDOWN TRANSIENT FOLLOWING AN APPENDIX R FIRE Revision 1 INTRODUCTION The Fort St. Vrain Nuclear Power Plant is a High Temperature Gas Cooled Reactor. There are two steam generators in the plant each , consisting of six modules. Each module is comprised of two separate and independent sections, an Economizer-Evaporator-Superheater (EES) section and a Reheater (RS) section. The EES section produces steam from feedwater for delivery to the high pressure turbine. The Reheater section provides additional heat energy to the steam from the helium circulator turbine exhaust for delivery to the intermediate pressure turbine. The steam generators are once-through with helically wound tubing. The tubes contain secondary water / steam coolant and have primary coolant helium on the outside. The lower temperature steam generator tubing consisting of the Economizer, Evaporator, and Superheater I sections are constructed of Cr-Mo low-alloy steels. The higher temperature Superheater II and the Reheaters are constructed of the alloy Sanicro 31 which is similar to Alloy 8008. Figure I shows a schematic of a steam generator module. Secondary side cooling water flow is normally provided from the Peedwater System. Condensate and Fire Water are used as backup for the Feedwater to provide cooling water flow during certain abnormal and emergency conditions, such as following a major fire defined in 10CFR50, Appendix R. The purpose of this analysis is to address some concerns about the capability of the EES section of the steam generator modules to withstand the introduction of cold water from the plant's fire protection system in the event that the plant's preheated feedwater and condensate are lost as a result of an Appendix R fire. These concerns are:
- 1) The effect that the use of fire water will have upon l the design life of the steam generator modules.
- 2) The possibility that fire water flashing to steam in the steam generator tubes could result in a vapor lock condition that could prevent establishing the required fire water flow through the steam generator.
- 3) The possibility that water hammer caused by the col-lapsing of trapped steam pockets could adversely affect the steam generator tubes or their heat removal capacity.
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- 4) The possibility that a localized overpressure condition could develop which would threaten the integrity of the !
steam generator tubes, t These concerns are addressed in this report assuming a 90 minute interruption of forced circulation and primary coolant heat removal following operation at 100 percent power. This report is also conservatively based upon a final 1000 gym fire water flow rate through the EES section of one steam generator as addressed in Section 14.4.2.2 of the Fort St. Vrain FSAR, and 1600*F helium temperature entering the steam generator. These values are conservatively high, as concluded in recent reanalysis of the safe shutdown cooling scenarios. l DESCRIPTION OF THE FIRE WATER COOLDOWN TRANSIENT i The Fire Water Cooldown Transient would occur in the unlikely event resultthat both of an feedwater Appendix and condensate flow were lost as a R fire. The scenario begins with the occurrence of congested cable area. a fire in the reactor or turbine building outside a As a result, helium flow and cooling water flow to the steam generators are presumed to be interrupted for 1-1/2 hours. as a result of aThe quake, or a maximum tornadoe. high fire water cooldown transient could also occur energy line break, a design basis earth-j During this period, plant piping systems are realigned to allow for resumption of steam generator (EES) cooling using fire water. This would include the depressurization of the EES section of the steam generator which will be used for safe shutdown cooling. The EES inventory would first be dumped into the steam / water dump tank, with final depressurization being acccomplished by venting the loop to atmosphere. Steam generator tube metal and helium outlet temperature profiles during this 1-1/2 hour period are shown on Figures 2 and 3. The scenario assumed that only the EES of one steam generator is i available for forced cooling. Prior to resumption of helium circulation within the PCRV, fire water flow will be established i through the available EES section. The initial flow of fire water will be through the still hot feedwater piping, EES tubing and steam piping, and EES tubing, causing the fire water to flash to steam in,feedwater piping. The accompanying volumetric change will choke the flow to approximately 65 GPM. As the fire water cools the piping and tubing, steaming will be reduced, lowering j system pressure drop and increasing fire water flow. 4
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Subsequent to flooding the steam generator, helium flow through the core would be established. One circulator would be utilized, powered by its fire water driven pelton wheel. Helium flow would be controlled to maintain liquid fire water conditions at the steam generator outlac, with the flow rate ranging from an i initial rate of approximately 1-1/2 - 24 to a final rate of approximately 34 of design core flow rate. STRUCTURAL EFFECT OF INTRODUCING COLD FIRE WATER INTO THE HOT STEAM GENERATOR - This section addresses Item 1 on Page 2. Of concern are the short term structural integrity of the pressure retaining parts and the effect that a single fire water cooldown transient would have upon the fatigue life of a steam generator. A review was made of the original design calculations (GADR-9) and other relevant documents. The review indicated that the I steam generators were well designed from a structural standpoint. - The stress levels were within ASME allowables and fatigue usage ! factors were also acceptable. The steam generator tubing was { designed with sufficient flexibility so that the stresses due to ' axial expansion and contraction were relatively low. No loca-tions were found where the loads induced by the thermal expan-sion/ contraction caused secondary stresses with primary stress 1 characteristics. The use of tire water for safe shutdown cooling would be categorized as an emergency or faulted condition. Section III of the ASME Code does not require that fatigue calculations be performed for the thermal stresses which occur during an emer- j 1 gency or faulted condition. The reason for this is that emergency or f aulted conditions will occur for a very liniited ! number of times during the life of the plant. Ductile materials , will withstand high levels of stress for a few cycles without experiencing fatigue failure. An analysis was performed in order to quantify the thermal shock stress lev:Is in the steam generators during the Fire Water Cooldown scansient (Appendix I). The analysis investigated the behavior of the steam generator cooling tubes during the subject transient. The tubes are the section of the steam generator subjected to the most severe thermal shock during the transient as they are in the active heat transfer region. The analysis was based upon a conservative set of temperatures for the fire water and helium flows. The tubes in the steam generators have neither fire water or helium flow for the first 1-1/2 hours of the event. At 1-1/2 hours cooling with 80*F fire water begins. This is prior to start of helium circulation. The assumption of 80*F fire water is conservative because the initial .
flow will be superheated steam at approximately 400*F. Steam temperatures entering the steam generator will drop to approxi-mately 350* in 30 seconds, and remain at 350' for approximately 10 minutes, until steaming stops (Appendix II). Thus, tube metal temperature will be slowly lowered during this period. The assumption of 80*F-leads to calculated stress levels which are significantly higher than the stress levels which would actually exist. Then, af ter equilibrium is established, circulation of the 1600*F primary coolant helium is started which begins to heat up the now water flowing tubes. The analysis shows that even with the conservative assumptions used that the stress levels are not significant from a fatigue standpoint. The addition to the fatigue damage usage f actor due to one cycle of the Fire Water Cooldown Transient is on the order
, of 0.005, which is negligible.
FLOW PATB FOR STEAM FROM A STEAM GENERATOR AND THE POTENTIAL FOR 4 A VAPOR LOCE CONDITION - This section addresses Item 2 on Page 1. A detailed review of the geometry, arrangements, 'and heat *f transfer and hydraulic characteristics of the EES. section has been performed. . I It has been concluded that with one fire water pump operating, flow can be established and maintained in all six modules of an EES section, without vapor lock and flow stopage occurring in any of the modules. However, as discussed previously in the section entitled Description of Fire Water Cooldown Transient, during the initial period of cooldown, the helium flow must be reduced to approximately 1-1/24 to 24 of design core flow to prevent boiling in the steam generator. If significant boiling were to occur in the steam generator, fire water flow through the steam generator would.be significantly reduced, resulting in tube metal temperatures approaching the inlet helium gas temperature. EES tube damage could possibly occur at this elevated temperature. Existing emergency procedures require that the primary. coolant flow rate be controlled to prevent steaming in the EES tubes. EFFECTS OF WATER EANNER ON TBE INTEGRITY OF T8E STRAN GENERATOR - This section addresses Item 3 of Page 1. " i Steam condensation induced water hammer results when cold, subcooled water comes in contact with pockets of steam in a closed piping system. Under certain conditions, the steam pocket i will suddenly condense, creating a localized depressurization at . the void. The resulting pressure imbalance at the water / void interface causes the water slug to. accelerate towards the void. i j Large pressure pulses occur when the slugs collide, producing pressure waves which travel through the fluid. High system a 4
operating pressure will further accelerate the slug, increasing the water hammer loads. These loads could result in piping and hanger damage. An event of this type occurred at San Onofre Unit 1, and is described in NUREG-1190. In order to fully ' evaluate the potential for water hammer during this transient, a consultant (Dr. C. S. Martin of Georgia Institute of Technology) with expertise in this field has been I retained. His evaluation indicates that damage to the steam generators occur. Incoming due to condensation induced water.hammet will not cooling water will push al.1 steam put of'the, . continuously sloping, small diameter tubes ahead of the water without trapping pockets of steam, a condition required to cause
, water hammer. Low (near atmospheric) system pressure at the water / steam interface, low cooling water flow rate, and little or no subcooled conditions at the interface due to heating of the cooling water as it passes through the hot inlet piping also minimizes the conditions conducive for water hammer to occur in the steam generators. , . .
.. 4 Pressure waves resulting from the unlikely occurrence of water hammer in the inlet piping and traveling to the steam generator will not affect steam generator integrity. Significant reduction in the size of the water hammer induced pressure would take place at the entrance to the steam generator tubes, due to the re-duction in individual flow areas from the inlet piping to the tubes. Further, the outflowing steam in the tubes will also absorb and attenuate any pressure pulses. Typically, water hammer occurring in feedwater piping may damage piping and valves, but not feedwater heaters, due to the reduction in flow area at tube inlets.
2 EFFECTS OF OVERPRESSURE CONDITIONS DUE TO BOILING ON TBE INTEG-RITY on Page OF 2. THE STEAM GENERATOR TUBES - This section addresses Item 4 Overpressurization will not occur. A rapid of the steam generator tubes due to boiling i increase in system pressure could occur if steam bubbles were to form in the water filled steam generator tubes during cooldown, resulting from a large volumetric ex- ! pansion of the flashing water. This could be caused by a sudden l ' increase in heat transfer in the steam generator. Emergency procedures of Fort St. < I Vrain preclude this condition from occurring. Once the steam generator is flooded with fire water helium flow conditions at is theinitiated steam generator and controlledoutlet. toThis maintain liquid will prevent boiling in the steam generator. . If the helium flow is inadvertently increased to the maximum design core flow rate of approximately 34 for a f1;e water driven circulator, boiling in the water filled steam generator could i occur. Although system pressure could rise due to the formation 1 5
of the steam bubbles, the rise in pressure would increase the flow rate of the cooling water discharging from the system. Further, 'the volumetric expansion f rom water to steam signifi-cantly decreases at higher pressures, reducing the amount of water required to be displaced by the steam. Additionally, safety valves on the main steam piping near the EES modules would begin to open at pressures less than system design pressure which would further accommodate any volumetric expansion from water to steam. The calculations of Appendix III show that these factors limit the system pressure to less than the system design pressure, precluding tube damage. During flooding of the steam generator prior to initiation of primary coolant flow, steam formed as the fire water contacts the hot tubes and piping will be vented to atmosphere. S pressure will not exceed fire water pump shut off pressure, ystem which is significantly below the design pressures of the steam genera-tor, and the feedwater and main steam piping. Thus, an over-pressure generators. condition would not occur during flooding of the steam t e l .
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mio.. ton 9 , 7, ' GROTON, CONNECTICUT cari c;;, 7 q , g4 t p cuea ygC PROJECT
$ , G, g, SUEJECT g g, (TR6CS N6 @ 32 i L O(/r of 6EC il l 4Mt/5 .
m kl los% cane fow, & == 2 74, COO Ab' AwnmoL$. mu.of 3% ce a-Oc% 0ud L loop a MTk, ' C Nn e.y == 2 3 E, fo o < o. o 3 > 2.
= I c' 7io /d5 n, ~a ,
= lklio x/74-2g (/ soo - to o) '
= 3I./ v/ o ' N Ju-
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t cac o g_ g av _ eux 6a34 PROTO POWER CORPORATION GROTON, CONNECTICUT miow, g' ' ' an p.7 7_ p 4
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" 3Sil46f 4, (f. fA, SUBJECT gg, (14 (~4 3 pG( fp 30/L0UT OF 665
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(cd p.h i~ I 6 I)
$g 44 coicc *T 5 ers (fe u of i+e u um %
u AP = 7 I - 12. 3 = 5 3. 7. e* , i 4 Pg = 6 2 , ( _.n - n.1 , A. <
/+4 <-4 9 4 t l.c a s 7 - 6.6 4 N + 31
=
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- . N= 22.~% 3 lbss. . Tat McDuq:-
x . _ _ . _ _ _ _ . _ Gr (H pn) 3o+ t= w D a der r' 0,C % Gs. & & ceo r y
%'y sui lo tuck 1$u Jin p 4 ze , -1~
<Au C6e 6r ca< CJ 44 4 /4,4 E
^
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cac * ** PROTO POWER CORPORATION 6fc i -
** g y M micwm y7 GROTON, CONNECTICUT om f- 2 7 - 8 6 cuENT ffC ,
PROJECT S , (y 7", A ; susaeci n4x, gg e55 pv E To 1 oIc.o crr 4 oF EES m bf f. 0, h volv m *-
~ i, dL % EEI &c 6 N = 3l.r2 gc 3 L owB hid Xu afer wX1. w, cofw SXeg os g. s it % Aykur motsib 4. . ~x udt
(
&uhakmmeA lo = cn &m cousig -fs aa usc.wt ,
0 ( As ~ maKu 7 facC W d o.A r Austik Zo afu % <oJL as~. 4 ~ fla gn3m wm,' fr ut om4mc Er Les I% #< e4 % b% A- & &I"*t .4 & -e*d'm
& ah ab , s ca a r &c awecx tL wieuu- ( uh To,& = Td , &
imy
=2Q -
k mye las %f< A w k hg y / .m.,r %ses
. mo A 6_. ,
c=c a 6 (-o i * -- ** F ,54 PnoTo PowsR coRPoRADoM mia w m 5, 7-anom. connecncw an p,7 ) , p 4 y_ , ,, q ,,Q4, CUENT f$( P % JECT G, G , T f) SUS)ECT M gy gjf($1 pqE '70 80lLQy[ Qf 66$ hC SCd y Yw fova l D P= %\ pu (%= zr 0 $' F ) ogd P= _ I
= ST.17
.o p-+=t Z) ben C Yo l, w E = 3 I [2. y fEl f
=. l f~ O7 .3 l /k;.
- 3) dr =
? = y649. 4 , 4,73799 BC MA53 l(02.3 1 db *
- wd ,= := Ze 4. 7 R *tR S
= R. 5*\ 59 IE W db. w o. & SM ON6 ,5&ca/D Q, f g yQ Mjy et d h d f. de hacs ac &
WoSy dr, & uop'sd dw L,
l cac e fg.o; e- au 9 y 34 PROTO POWER CORPORATION GROTON, CONNECTICUT mow, g , 7 om g, g 7 , pg CUENT PS( PROJECT 4,C, f, A SUBJECT M A )(, yfg {f 3 )vg 70 30/(, 0(/7" Of 665 k WG Llo d C, N' e v'
- L y+"b<(V.-y)],/%e
/p 4v a
=
imt 4 Hgf (6.I24 ,orui)'= inz,3i _3I.F2 C c 3 63.15f/r
% e>Ga n v'ouvmg s} econk d by %
Mffutea k vdumCud f(w a nd our u one- CC EE S x azon k. 14 5- R / = 12.243's = 0, $( 7 p Ar = (r5 v tr),, = 2 7.4 4 7 w ,oi?4c = a m,
, b V7u ,
= 0.392 - o '% 7 == o. o 8 ) 0 9
PROTO POWER CORPORATION 6 t- o s ** /o y 5+ po rm 4g urt GROTON, CONNECTICUT - p 7 7, g
** 771 TF " ~ *T 6 II 4 6 9 cuENT 99c PROJECT 4 g, 7 A SUBJECT M 4 g c.,%E45 pvE To 3os4.o u 7 oF 66f 08we ' du <dy mt, c.y w Jg kg k 4 N -%U p. % CAs u, $s %<c g flo% Y YM y W U $y tido (biSing lempendu 2u ci p(c.t.su u ol % dw .
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- Q-0 ( L'* - ti a 34 GROTW, COMECMCW momrm g - are ""_
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cac w) fg m == *w PROTO POWER CORPORATION t z. , 34 ! GROTON, CONNECTICUT m.oi.rm g p r' S-21--4
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CUENT PgC PROJECT 4, C , q' A l suaxcr m gy , sig.gs5 pvE 'To EWtuouT of EE ,5 i N.Cc -tLK, w ha. A f 4 u rer f w p % o r & wrg pcam O I60 7 "* d
> F""*'S w w <.
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@vrv v
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~) l%s = 4l l5 e a l . s 2. -
12p 05 45 t) Cf- -2C43.+ y l'2 9%o6 = d* CG90
.t 6 . s t c.
w l' yn, -- l3.3 % o B W
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, f ', = . o 2 4 3 + , (o,g gi 0 "4 - ~ _ _ _ !]98:f~ 61/.h --- -
cauc e (,g og PROTO POWER CORPORATION mow, m_ m l3 , 54 l GRMM. COMECDCW 47 cart 5 - 2 2 -f G cuENT pgc m ,, , _;i 6f PROJECT S. G. f A , Sua>ECT MK 6%E 55 PV6 % of B ol (.3 (/1- EEC v= 0.0 2 '+4 \ dt*
in < @,
- I f '
Y h b == . D 13, T-
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Avuy sp d[(c' cleon'rp kwofw m v1% Jy s b gia h - hV = _4 U c LOA
- 4t [1 rce , L ]OO o.,f7.3 ht 7,j GZ. %. fa ?.-41.15
PROTO POWER CORPORATION cate" 6f-Ol w,ow,
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f CUENT fp{ PROJECT f,6 7A SUEUECT Mg, $-ff.656 DV6 7d 30ILOo f oP 6(i Sc & mscuo.Gn % Cb Edu. ~ fo = 42-m,,, -= 2 2.% 3 < (* jM} .= L & 9. 04 Astxe A Tr . 2 49. 04 /(z = 4.o2 fg*
. . c. bV e. v 'M OVm Q 7'= (7oop& 't Gsim cc Golma M11Ety ~re E TI m E WVIf69 , \l6 V16 y, fts wx w d .[o " Y:-
hom e nddn.c d pwp .s d -of} pracua.
) Pc 160 pA ~a 9,,, /
= cr /o f 0.c o ri c -c p
l
') 6pu n !M4 + z= m.s ct? sW 17 %,G4 62,c
CAC @
- PROTO POWER CORPORATION 6 f-O( .
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~ ?2~ b CUENT pgg PROJECT yn7F "* 15 iI4 6(
g, g, p 4, SUBJECT gg, j fqg C,5 pv E T 30/ t o /f 0F EEC l hvM b tLS (s 7un = n i 39 9E
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$22. } $Tb MAK,hvG!U =
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- 62.2 7 n l r l Vh l
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= 143.04 .
2 l m u. L 21+
) A &ACf ov&t ~
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%{ PROJECT 4, C , 1~ A SUSJECT yy q f Q$$ Qf -[0 QO f ( Q () f C $' EE$
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# G me, fn ik GCd ' flow un G ymh4
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?w '
l '+ 0D p aa-.
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%efoa, n TL S2 xwds %r LC 4~ k
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eAw.elg ta % ya C.G m o sz 6- upm &c' J mosC setA $Z \ . b Vw. == M A cc ia, * [ %o - %)
= 17 36. 44 x ( o. 0743 - o. oi s ir) 3
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$ m ap A m <- taw L cu &/lo.s %
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b % ,n,
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=
C3. 2 5 f
c^c " 6f- o f
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"" 19 y 34 o,io ro,i o,rg GROTON, CONNECTICUT f' ~' - 7~ 2 2 ~ b, l
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cuENT PSC PROJECT g , g, y, p usseci ppy , q -fg4g pug 1y go o cov7- ,p ggg O Svtw r y con f.n u u bg Is aor snradec .
@b iMuGC 4W EnnGL M HGkT TO W1 5
[4iG ik tvrr co W cTA vr, se. 'THnf 4 m= d.MOL
;7ptra e/Avaa.4 n N rc Ar 4 touse ret = u M tw Sa G+ C e% S -076 in Axs M V M t'RMS S Ulf ts -ra ea tesi rnmu .im mas ,
- f. By G h Git M (o n n ctL v 8 0 0 M j
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(bO 1. v), w= 5/ - M ~r
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.m. g rc , <4g -t r 6c Mrs did f.- t4. u,fa W & co u G d d +
(Uey.Q, - CLp (Ibo pQ , o. a h t.
= 37C 71
- rr,i* 31,rz.
=
5 t 2., 4.g , 6C (AU.<.) c , g ( +2, 4. _ G. 2.L 3 3 r,9 3
=. - 12 ,'2 7 I B6
( AVc,v.) , = '4"1, /I T -(2.,2 7-I __. _ g i g 4. g AU = g,4 g, # Ij 04 4 V 2.C 2 =-1,04 2,3 09 R Dbth*a) d wouf11 cm c79 ii ud, s. . {
% ene a y er emm mmae-
PROTO POWER CORPORATION C^'C
- 6f. o a -
** 7 i c, 34 onowron cart GROTON, CONNECTICUT 4, 7' 7,7 7 _ f b '
cuENT pfC ffffP **
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PROJECT ei , O 7 A , SUILJECT gg, (TM.@S $ pg& Q 3)(c 0 V T oF EET FNo TWIHP6tLATJW /*10f 7* SE A CC Awa
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~~ ~ r.n 8 ees, =7rmysr "ENT pfr "
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= m, su 4&x (ze a,,
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hidLf- TfmP c4 o a s. p SF W/G,prJ7
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10kl /~L 0&) //fd/A'M h/9.C / 494) f1477) &0FFF)C/Edr Com/MEEP 70 SMy>V /=~40tJ tsd-rE72 022. 3 cit.'W6 sierE12 , THrs 77tB r rrmferdrear
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cuc w y_ j m esca 73 ,77 PROTO POWER CORPORATION anow o,n GROTON, CONNECTICUT M I/E b CUENT g{ f* 5 :f . ** *7.rHyt 8 PROJECT g
*m)X/m&p S79*1f 'M/ To BdMouT~ dF fff 7/~ E F0LLeed)A/4 4x/AtLYS/S /C 7 V a' R A/d l 80La77sa s >= M i re72#rMr 73escess 6 t/E M d f u m t- remP, 4 Nr + 5 =-/Go0*t6i3# = l166,6
- 2. 2.
Ty~ g, 4 G r t Q .e. _- /6pd'+ //94,,$*,. ;333 p p gjg,zog z 2.
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caec w (9g p< esas y y , y y PROTO POWER CORPORATION m,o w on GROTON, CONNECTICUT m oars 22M 6 "cano CUENT PROJECT
<; .r ~~ pryygr g 7 g--
M ECT yngy g7333[ pp,y yg pg,g, , g y ,p gy$ f w s m a P r a r.c u e r R = PhA)PTL Ad, / &
&?0 PU6 /200'F =
=
. 6 76 (wr c, % rd
/(= //Esr coapaeinury
= ,/9 672elF7-Me-> [EEF,C ,P6 53)
(' 4 = p a xz n) p r aze M47-f (z2sr]*( : 'lf"' Yzl'7
= 77,18 879lfR 'FT**F f,F677 Bo/u,06 (zer 8, worrx , 4 =/g sa fra re-z2
& F* ,Fr a Q M 4)All WS/f74A/Cd', by
= 2k (RER 8, P4 V-/r)
Do A(.
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}EF. f,fb ) ~ ?f__ 3 __ _
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reu are - (J-)(>.a) i HR F/f
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p= f = S76 e 7 g *- E zs =
,012790
/
$ $
- 5900 ~
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& 'E = ,0/S~287 A 7~ =
$R I hr ~ %i [2fM k P4, 3-Zo)
ATp=y .0/21We 835,5
.0/r287 (/400 ~ 6/3) * =:
.000l')e /0, T D G = ,015287 f/6 00 -6/3) =
A 7a = . 6 0 2 / 71 (/6du~6/3j '= 190. 6 o/S'287 4 7=987 = MOO-0>2
csucono g / .p *- M g(s or3 Y PROTO POWER CORPORATION cao w on f GROTON, CONNECTICUT my fA 286 mo cuem pg( g .co.c gj, g
**' 5 c6 7A'
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'fa -=
l ryg- - s Tp;- - s % . /600- 83fS* ' 0' ' = 69% . z_ -
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~E fv5M ct.ststo "F"741*aun w
' -.a - n.-,a l /200 *F RifD F0% Nf,,,,, f ) g F ort st/0M- 8d/4///t5 W #7FA ' l b =,0 23 E. Re 8 N . sz] . ( I (7.fE3f6.5'-23 7EatiL*27/Es #7 BVer .Pa/sp 7"EMER,47#26
& R = l '70 0 ' /.f/4, 7~ =gp/3 *f d~ddC/tL#7f 'PA OPE 2 prJ' .f.2on, f7(fc'))fp CH427 ort 79;, 39 ' 4-7~ 7 = 6/)*F, d13 "F = ff/3 -se.) + z'?3 e f16 K 1
-is .d.:1 /
4 = R 2 */'d .e c - Saf/0-T,e/s-f7=,/f9,,M.pg A Y* W h ,- T ,' = /! / o f =W q/f 3 u ( = , S03i Q -- , 21/ 87M y H2 fr.p i A 73 pik yy, y,p
i CALC W g g j Mv , PAGE g 7 g y
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c :r =)ggygy PROJECT g p, SUSJECT gg (,ggg pg yn yyyy gp ffj f = '2yf #lfe clp19Yj l I=896,9/Y */#% 2 2.
/f =_ 77- DJ _ ?C .Q Ar = . 0 o/ FPP F7 y 9' > t-
[g = .h Pi 8A [896,FW lHe) . S!h r-
;oe/p97F7*(S*'/74p7)(/j774,/py--yz}
= 2, /60 /$O 87t1 h = .0 23 f*l 9/*yx-fy'-ph/So,Ido } S ( /0),133 2 F7"
- lN, W? bc = b y =/4 f/7 f' = 168h BTR hf-FT-f
- f)/E' = ??,28 = ,G12.TVO I
Zs= 1626 ~ = 000/03 Se: St.1' :
. 00Z l'? ?
EE= . 0 /6'2 2 /
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GROTON, CONNECTICUT 7 f/g. 4//(f
,, g, m ,egj,,pp CUENT g( JECT g g 7g SUSJECT g g fy g g Qf f0 $d)Q$7 $f 5$
47 g . 0/2 9 V0 400-(s)3 = S3 f
. oirz z i 47]= s60oI03 f600~(.pl3)~~ 7
.0/r22/
1
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M/ . ,c/S22/ 9 9 ? ' =/600 -6/3 ' (~ . K3 = /&00 -t'3 7 - Y = 6 9/ ([ tore ro ar.renz m' F)
&g =/(p00 ~ = //// (Ct est' To $UHpffD izos ,)
a est Yu = 7dd* I i
- . _ - . - . - - ,-,--,..,_.n,-_ _ - -,_ -... ,,, -
-,- _ ,_ - _ . . , - , ,.,,,-,...,.-n7-
! CALC No g [ - f Mw .
PAGE g g PROTO POWER CORPORATION mowa GROTON, CONNECTICUT p can g g gpff g CUENT g PROJECT g g i
* % x sisF.cc Pt/r ro Boe.sur o f r c .s
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9ECTION - ID -WDIV- K(FIX)- K(VAR)- EPS - EL -FLOW- TF - MIN - MAX gl 34 (#) N
~ 1 : 1 - 2X ,10.020, 0.5, 12.3, 522.1,1.500D-4, 1.3, 1, 100.0, NA , NA 2 2X - 6X , 6.065, 0.5, 8.3, 251.1.1.5000-4, 9.7, 1, 100.0, NA , NA i
3: 6X - 6A , 7.981, 0.5, 2.5, 61.4,1.500D-4, 0.6, 1, 100.0, NA , NA f0N k 4 6A -A , 7.981, 1, 5.0, 29.9,1.500D-4, 17.7, 1, 100.0, NA , NA 5: A-B , 9.516, 1, 33.4, 68.1,1.5000-4, 4.2, 1, 100.u, NA NA b- 6 : 8 - S# , 9.172, 1, 2.7 136.3.1.5000-4, -60.6, ( 1, 100.0, NA , NA 7: B'- C , 9.172,1.81, 1.8, 94.2.1.500D-4, -0.3, 1, 100.0, NA NA j(S : C-D , 3.152, 6, 11.2, 102.1,1.800D-4, 9.0, 1, 100.0, NA
, NA 9: D-4 , 3.346, 6, 2.6, 26.2,1.500D-4, -4.6, 1, 100.0, NA , NA los 4 -
10 , 0.874, 100, 98.9, 486.4,8.202D-5, 27.9, 1, 100.0, NA , NA 11: 10 - 12 , 0.724, 324, 184.8, 26.0,8.202D-5, 2.3, 1, 100.0, NA , NA 2: 12 -12.1, 0.724, 324, 0.0, 2444.5,0.202D-5, 4.8 1, 100.0, NA , NA 13:12.1-12.2 O.724, 324, O.O, O.O.B.202D-5, O.O, 1, 100.O, NA NA G65 14 12.2- 14 , 0.724, 324, o.0, 0.o,8.202D-5, O.o. 1, 100.0, NA',, NA I) 15: 14 -14.1, 0.550, 324, 0.2, 1821.7,8.202D-6, 2.7, 1, 100.0, NA , NA 16:14.1- 15 , 0.550, 324, 0.0, 0.0,8.202D-6, 0.0, 1, 100.0, NA , NA
*(17 15 - 16 , 0.590, 324, 1.6, 166.8,8.202D-6, 4.6, 1, 100.0, NA , NA g 18: 16 -16.1, 0.590, 324, 0.0, 1541.4,8.202D-6, -3.3, 1, 100.0, NA , NA 19:16.1- 17 , O.590, 324, O.O. O.O,S.202D-6, O.O, 1, 100.O, NA , NA 20 17 - 20 , 0.590, 324, 2.6, 270.1,8.202D-6, -11.0, 1, 100.0, NA , NA 21 20 - 21 , 0.768, 108, 0.1, 15.3,8.202D-6, 0.0, 1, 100.0, NA , NA
'l. '22: 21 - 26 , 0.969, 108, 23: 26 - F , 3.803, 6, 2.3, 1.3, 525.6,8.202D-6, 23.0,1.500D-4,
-27.9, 4.6, 1,
1, 100.0, 100.0, NA NA NA NA
,-I 1*24: F-G , 5.826, 6, 2.7 208.2.1.5000-4, 49.0, 1, 100.0, NA , NA 25: G - B* , 9.586, 1, 3.5, 24.4.1.500D-4, 0.0, 1, 100.6, NA , NA 26: G*- H 10.820, 1, 2.5, 31.2,1.5000-4, 0.0, 1, 100.0, NA , NA g*p g 27: H- I 28: PV-2229 , 5.826,
, 5.826, 2, 2,
3.0, O.O, 37.6,1.500D-4, O.O,1.500D-4, 0.0, 1, 100.0, NA , NA l G.O, 8, 100.O, 245.O, O.9 29: I-I* ,11.540, 1, 1.5, 47.6,1.500D-4, 0.0, 1, 100.O, NA NA 64.'IBUN 30: I*- J 10.114, 1, 0.5, 11.1,1.5000-4, 18.8 1, 100.0, NA
, MA 31: J-K 12.500, 1, 2.3, .70.9,1.500D-4, 35.7, 1, 100.0, NA , NA 32: K-L 14.312, 1, 1.6, 40.1,1.500D-4, -6.6, 1, 100.0, NA , NA '
'l 33: L-M 21.562, 1, 0.5, 6.2.1.500D-4, 11.0, 1, 100.0, NA , NA 7 ',
( 34: M-N , 5.761, 1, 3.3, 70.8.1.5000-4, 31.0, 1, 100.0, NA , NA #1
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USE PUMP CURVE 10R ENTER FRESSURE3 (Y/N):Y? PUMP (S) ARRANGEPENT (ONE=0 - PARALLEL =1 - SERIES =2) 0? FLOW 8 PUMP =1182.50 GPM AT 1002F , PUMP HEAD = 102.23 FT/ STAGE FILE: EESLOOFW.DAT -- TOTAL NUMBER OF SECTIONS = 34 I SECTION ID K FLOW P(IN) P(OUT) ) 1 : 1 - 2X 10.020 20.4 591,250 144.3 140.6
- 2
- 2X - 6X 6.065 12.3 591,250 140.6 122.1 3 6X - 6A 7.981 3.5 591,250 122.1 120.8 4 r 6A - A 7.981 5.5 491,250 120.8 111.7 5: A-9 9.516 34.5 491,250 111.7 105.3 6 . B - B' 9.172 4.9 491,250 105.3 130.6
, 7 B'- C 9.172 3.4 271,409 130.6 130.6 i S: C-D 3.152 13.2 81,875 130.6 122.7 9 : D-4 3.346 3.1 91,875 122.7 123.9 10: 4 - 10 0.874 111.4 4,549 123.9 94.1 11: 10 - 12 0.724 185.6 1,516 94.1 94.1 12 -12.1 0.724 72.5 1,516 h,l12 06.1 St.3
) 13:12.1-12.2 0.724 0.0 1,516 St.3 81.3 i
JM 14:12.2- 14 0.724 0.0 1,516 St.3 St.3
** PRESS <CR) TO CONTINUE **
T SECTION ID K FLOW P(IN) P(OUT)
$15 14 -14.1 0.550 45.4 1,514 81.3 N 114:14.1- 15 0.550 0.0 1,516 75.0 75.0 75.0 17: 15 - 16 0.590 5.8 1,516 75.0 72.5 g18 16 -16.1 0.590 38.6 1,516 72.5 70.6 i
U9:16.1- 17 0.590 0.0 1,514 70.6 70.6 20 17 - 20 0.590 9.4 - 1,514 70.6 74.5 I 21: 20 - 21 0.768 0.4 4,549 74.5 74.4 22: 21 - 26 0.969 13.7 4,549 74.4 35.0
! 23: 26 - F 3.803 1.8 81,875 85.0 92.8 l -
24: F-G 5.826 6.9 81,875 82.8 61.5 i 25: G-G' 9.584 3.9 491,250 61.5 41.0 j 26: G'- H 10.520 3.3 491,250 41.0 60.7 l ' 27: H- ! 5.826 3.6 245,625 60.7 59.9 l 28: PV-2229 5.826 0.0 245,625 59.9 55. 8 CR: W=843,820 DP= 4 7. 8 X =9. 3E 1 - 29: I - !* 11.540 2.3 491,250 55.8 55.7 30: I '- J 18.114 0.7 491,250 55.7 47.5 i , 31: J-K 12.500 3.4 491,250 47.5 32.0 32: K-L 14.312 2.2 491,250 32.0 34.8
!, 33: L-M 21.562 0.6 491,250 34.8 30.0 l e 34: M-N 5.761 4.4 491,250 30.0 12.3 ; ** PRESSURE AT END OF SYSTEM = 12.3 PSIA 8
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. CALCULATION No.: 68-02 1
FILE No.: 75114ss I
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o.ri GROTON, CONNECTICUT E N VS # I6 atteam , f .ca w .7 7 ,g g g CUENT g PROJECT SUBJECT Drscossro4 *. THe. TRA0SriE NT e EpJe too s: DER E.O BE.GDJS wrn4 THE L oss oF Fee.OwnTEf( Ago cIRcotArcoe Ar loo *?e power . THE ccotrMG FL Ow o F FrRE.wAM.[( .rs Esrqat.ISHE.O APTER A 9o mcaurE oe.tAV, APTE.Q preE-WATER, Flow g4 AJ GEE.u ST1V2TED THE. g c.nR CO LAro RS ARE STPRM.D Ae b &00*F HELID rh EtoTERS THE. SvAm. GENERAT13RS. 7 THIS TR Ao S re.Or 4 EA6S TO T\.0o S EPe. RATE. TVmpe.nxtuRE Exc.ORSIo4.1 fog SomE OF THE STEAM GesaE RAToR c.ompoNEt4T.S. THESE. ARE THE. CooLaxb OUG. To nae FIRE.wATE.R. FLovd FOLLoWE.O Gy THE. HE.ATIOG OV THE. HELiV M PRT/nAR Y cooLA4 T. . THE. R @IO c.coLIO G 400 NEAToaco oP THE. C.cm90NEr4T4 RESULTS EN STRESSES OVE. TO THE RE.sTnAI.wT To Ex.P Ares.IcM oF'FE.RE.O GYcoot-RAciroes/ M AT6.R.rm L ADOrc.e.e)T To A G EVE.ra P o rut. TH E.S E STRE.SS GS ARE SELF-G.QortT GRATTOCo A 4 AS Suc s ARE SG.co y D AR$r -STTM56.5 T H ESE. SE.Co aJ DA R y STREst ES w)n L Nor c.Aus e. A s TR vtT URAL FArtuRE uPoy A s DJGLe. A 09 trcATrtyv . THE Y ARei O G CTECTIDMAG LE orotY orV TH E GA5rs oF fbsSr. GLY C04TQ EBUTDJG TO A FATr.GUE TYPG. fan uRt. s. e 9
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TO Q UAN TIF Y TI4 C STTRESS LEVEL.S AM b TH E rR EF FECT U PO N THE F A n b.OE LEPE. OF THE. STEhrh GEMERATO RS 3 DIF F E.Re 0 7 L.oe.Arcoru s W trH .t2J TH E S TEArn. G EME.R.ATO RS A Q s, E V A L.u ATEC. WE LO CAT"CDNS C HOS EN AQE ThE coo tDac, TU GES wrrHTQ THE A CTIV E .N EAT TR ANS FER AR EAS O F W E S TE A m Ge rd t-(taro R S. THES E AREA 2 w Ertt. C.H or EN AS THE V art. sue Oe cTED To e oTH TH E RAPCD coot.oae AND H EAT U P. C 0 4 S tr.ItvAT.n) E. r;SS U m P T.tn N S Ang, rh Aos. RECsoAROrN6 THe. C.00LD4/H6Arrv6 TR ANsrE.crs AMO rr Is FELT Thor THe. STRE.S$ N UMGfl25 C.ALCO LAW B ARE, G om CouS E.RVATruE. AND RE. PRE.SE.N ATU)E. O F n4 tc MoST C.ib.i uc.AL. AREAS OP TH E. STEarh GEME.RAro R.S. A SDt PLE AND COMSE.RVArrVE. moost r.5 Chose.0 To s crnu Le TV TH E SEHAyrOR o F TH f Coo rN6 TURG5. TH E. m o O E.L IIS USG.D TO OCT RrhoJG THE TuGE TE. re ipG.rLANt 2 G L AT DrFFe RC:rJT LOCAT. tot 4 AY VARIDOS TTrnES. A ComPuw R pro 6ft.AN W A vSE.D Tb CALCu LATV TH E.1 E. V A t.uES FoR714E V A R.EDUS STE Arn GGAjd.II.ATOR WGES, A PRoGR.A m AGE CAL.tv6 Arc R, M Ay G6 U C 6 0 "T O V 6 G.L E Y TN6 1 CJfuT OF' TM G. 9 0 6(4 TAM . e. I l
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{.ALCoVN m st A SrmPLIFIED , C.cos Eft \/ArDJt. l A9Prtorwe.a r.s vsC.O To mo O EL T7+E S TEh m C,0.N E RA To ft Tu GtLS . TH6 RC AO.E Tw o SEP C: n. ATE. TRANS EErJ r 3 Co N S ID6.RGD. Tw: Esc, ene A R Aero eoo LDet.wa Po u et.v60 R. Y A H G. AT- U P. NtMETY rhoa vrt.s ELAPSE G ETW EE4 TH t, CIRCu LATIDN Loss oF Pcf.bWAW.R/ A iJ b T H E., rN rTT A TIo M o f: FIREWATER Flow . DuRr0 G ru e. 9 o n IN u TL 9Enre ra, Tat REi4gATER, SUPE.RHEAT1 Eft. Ii.IT, EVA90RATOR AND E. tom O m I.TC:R TUGE.5 C. COL 00W N , m C. 77 rn P ER.ATURE, c.ORVES FC>R Ti-R 5t. TUGGS As A PUMCTIDN OF Trmi A FTER Loss oF FE,0WAwR/ CIRC.OLANIbra ARG SHowo Da Fr chu RES, 2. Au Q 2. . AT 90 m ru uTE.S THG. m Av I.rn o m o F ALL TH E TOG 6 Tern PE.R.AivaEs cs Approx rnigwf. 7Bo* F. nd THE. FoLLoWDJ C> CA L.CU L.A7CDAJS TH E TE rnP E6LATU RE O F ALL ruse s IJ., CO N S E RV A Tru e.Ly As s u rn E 6 To 06 7eo ' S tug.SE Hov Tue.E,0 ARG TH EM S un JW.tWED ToAFLew oF Ware rc W H nt s C.s c.oM S6.R - VArDJG LY Assum s.D TOGE ac " F. THrs
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cucw 73.e, m_ wa y c, e 3 PROTO POWER CORPORATION GROTON, CONNECTICUT mwg "5 we CUENT g PROJECT susanct f EE.DWAwR L.DJ E. W NH IL N OT G LOWN Do weJ PREG R T D TVE. ru u a r-T TID N OF F.TREWATE.R Flow . TV E. T7 fh PER A TJ RE RESPO N S G TH R O U 6 H TWE TMIC X > JESS OF TH E. TUG E. EL PR ECL".tTV.D G Y THE. E QU AMN 5 He wr4 .c0 A1 TAC.Hm EUT* A . THL5 EQu A TIb ev PR EDIC T3 TH 6. TV mP E.RATVRE. R ESpoNs s oF A S t AQ H E.ATEb/ C.co L60 ON orJ E. SIce. (.arru AN Acco.mtrc GouNOAGy 0 M T M E OTW ER . THE. AQrGmTEC BQUrJDAG y ( ' CS C.orJSE.RVATIUC:. AS rr PRE.brcTs A th o(2s l S e v me TMt.Rm AL enADIEMT TH A4 Acm A L LY
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FOR THE. S E. ton rd TRAosIEMT w sarts rs A HEAT - OP TRaycq THE TOGE5 Ag e. As s um rn E.O To H ANJE REAc.H E.D A SrcA6y i STA R TED1PERATURe OF 80* F . THE.Y AAE THEN SUGJrtTED To A FLbW OF %Co *F OJE:.R TH E CtJTsIDE SurtP ace vJcn-t n4E
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i "THQ: F6 L L O W T N C. C.ALC. O LA TI~O*VS S Ho(-d TV 6 STO.ESS LG.VELS As b F Atrr,u 6, CALC U LArroNT F O R. TD.A N C ."Oi:.NT 2. A . TN E3 TGA'OS ctr NT "tt T14 E C.Oo L BOLO 4 QV "U4 E O. R oS " T\4.CC K WALL O F TM E. SUP6RH EATE R. E TOOLFS. THE.5E CALC O A T".CDM S A RG TV PccAt OF THOSE FOR TH G. o714e.(( Tu G 6.5, D4 E. (?.G.su LTS o F w(*Ir.H AG.+ SH o w r0 IU ' FreauRE. y... . I 4 1 l i I I l t
c46 c w 9p _o f e_ % 7 c, 2.3 PROTO POWER CORPORATION on.o w on g oart , , , GROTON, CONNECTICUT ,g CUENT PROJECT SURECT t 4 E L.ASTre sotuTTou Q STRESS EQUATIOMS - TE MP E RAn.J RE RESPo rJ E. 31: A WN C.y U2.N oER ( D/t. > t oh Tw t 4 TErnpe ftATune t, rad rag.ar 7-Rom Tue ave 11At,e rh ETM. TV mPERATVRE TA T O "tH t. Ex,Pos EL s u R FAc.E. TEmN.nATuGE Te, rs OGTAmEA FRom THE PRoDuc.T gg ATp W H E.R E nie, " Tc - TA . oTp THE TEMPERRWttf., GG Acci!.NT FR.om THt ) Av E. RAGE me.TA TE,mPE.fLATVRt. TE, TO THt., m Su t A rEL SORE AC.E. M/nPUE.RATV RE To r.s 06Thr.NED P RbM TH c. 9 Ro Dut.n M. ATA Mo" TA ~ Yo _ l i # l l USmG OMW TH E. TH rov GH WEC.KMESS GRAD E. ' TH6 STO(.S! C.omPON GiA/T S OM N E OPOSLED soReAce ARe t , k " - 6 A r s q g. O.TA l- Y . I 4 b k
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w rm A Tp - Tp - Tc = (60 - 783 3 - 7 00
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STRESS e.xce.G.Os TME. me N.Rm L. Y.EE.LC STRCSI (AS.DJ Tk r3 CASE 1 Tk.n Rte.A S 6 NS FOct THr.: bGn 4 U) THE, PLAsrI c (: Low as.q urRs.S THAT TMG. VO L.u m E N OT C.H A NG E . S c . TH A T THC i 6 F F E.c. i .uje Po :cs soms RA Tze A 9 pro At i- a.t. A f E.R. 9 EC T L Y POSTIC. GATIb oP O.6 ANO (O 9 tA s 3 c. STRA DJ RG.Oc:sTRrGOTtnu wn.t
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.500 80.0 680.7 162.1 501.9 -530.3 -74.7 9420f 120700
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.700 80.0 603.6 148.6 442.4 -469.7 -59.0 83402 104400
.000 80.0 567.2 143.3 416.3 -438.4 -53.8 77900 97000
.909 80.0 532.9 138.6 392.1 -408.1 -49.4 7250c 90100 1.000 80.0 500.7 134.! 369.7 -379.5 -45.6 67400 836ee 1.109 80.0 470.8 130.4 348.9 -352.7 -42.2 62602 77700 1.209 80.0 442.9 126.7 329.7 -327.6 -39.1 58200 72100 1.309 80.0 417.0 123.4 311.8 -304.2 -36.3 54000 66900 1.409 80.0 392.9 120.3 295.2 -282.5 -33.7 50200 62200 1.509 80.0 370.5 117.4 279.8 -262.3 -31.3 46600 57700 1.609 80.0 349.7 114.7 265.5 -243.6 -29.0 43300 53600 1.709 80.0 330.4 112.2 252.3 -226.1 -27.0 40200 49700 1.809 80.0 312.5 109.9 239.9 -210.0 -25.0 ;.7300 46200 1.909 80.0 295.9 107.8 228.5 -194.9 -23.2 3460c 42909 2.009 80.0 280.4 105.8 217.9 -101.0 -21.6 32100 39800 2.109 80.0 266.1 103.9 208.0 -168.0 -20.0 29800 37000 2.209 80.0 252.8 102.2 198.8 -156.0 -18.6 27700 34300 2.309 80.0 240.4 100.6 190.3 -144.9 -17.3 2570c 31900 2.409 80.0 228.9 99.2 102.4 -134.5 -16.0 2390f 29600 2.509 80.0 218.3 97.8 175.1 -124.9 -14.9 2220c 27500 2.609 80.0 208.4 96.5 168.3 -115.9 -13.8 20600 25500 2.709 80.0 199.2 95.3 162.0 -107.6 -12.8 19100 23700 2.809 80.0 190.7 94.2 156.1 -99.9 -11.9 17800 22000 2.909 80.0 182.7 93.2 150.7 -92.8 -11.1 16500 20400 3.009 80.0 175.4 92.3 145.6 -86.1 -10.3 15000 19000 THROUGH WALL TEMPERATURE AT EQUALLY SPACED STATIONS - DEG F FROM STA 9 AT INSULATED SURFACE TO STA 10 AT FLUID BOUNDARY TIME STA 0 STA 1 STA 2 STA 3 STA 4 STA 5 STA 6 STA 7 STA 8 STA 9 STA 1_
.050 780.0 780.0 780.0 779.9 779.6 777.7 769.4 741.6 670.1 527.4 306.C
.100 779.9 779.8 779.1 777.0 771.0 756.3 724.9 665.8 568.~ 428.7 251.c
.150 779. 4 777. 5 774. 0 766. 8 751. 7 723. 9 677. 2 605. 6 505. 0 375. 8 223.
__ - --- - ... - -.. ~~. . C
, * . s v. tos.. .~a.. .... ... ...
CL 5-- a
- e. ,
WALL THICENESS = .205 IN. CONDUCTIVITY = 10.5 BTU /HF-FT-F. FILM COEFF. = 10000 BTU /HR-FT2-F. DIFFUSIVITY = .00700 IN:/SEC. E
- ALPHA = 226.3 FSI/F. FOISSON'S RATIO = .36 STRESS INDEX = 1 FLUID TRANSIENT: STEF CHANGE FROM 780 TO 80F. ~1TRAu s.It wT P_ A EVENT TIME TFLUID T(0) T(10) TAVE DT(1) DT(2) SN SF MAX SN .638 80.0 748.8 153.2 561.1 -591(3 -112.2 105000 144o00 MAX SF .167 80.0 780.0 217.0 682.7 -421.3 -255.0 74800 165400
.100 80.0 780.0 251.6 710.6 -327.9 -295.0 58300 163100
.200 80.0 779.9 206.5 671.1 -453.9 -237.7 80600 165100
.300 80.0 778.7 184.9 640.0 -523.5 -193.4 93000 161700
.490 80.0 774.4 171.6 613.5 -562.7 -160.6 100000 157000
.500 80.0 766.0 162.3 590.0 -583.0 -136.2 103600 151900
.600 80.0 754.1 155.4 568.7 -590.8 -117.9 104900 146800 i . .700 80.0 739.3 150.0 549.0 -5?0.0 -104.0 104800 14180e
.800 80.0 722.6 145.6 520.7 -583.5 -93.4 103600 1!6800
.900 80.0 704.5 141.9 513.4 -573.0 -85.0 101800 132000
- 1.000 80.0 685.8 138.7 497.1 -560.0 -78.4 99500 1273ee I
1.190 80.0 666.7 13S.9 481.6 -545.4 -73.0 96900 122800 1.290 80.0 647.5 133.4 466.8 -529.7 -68.5 94100 118400 1.300 80.0 628.5 131.1 452.6 -513.6 -64.7 91200 11420e 1.4PO 80.0 609.9 129.0 439.1 -497.2 -61.5 88300 110100 1.500 80.0 591.6 127.1 426.1 -480.8 -58.6 85400 106200 i 1.690 80.0 573.7 125.3 413.5 -464.6 -56.0 82500 102400 l 1.790 80.0 556.4 123.5 401.5 -448.7 -33.6 79700 98800 l 1.820 80.0 5!9.6 121.9 389.9 -433.2 -51.4 76900 95200 1.990 80.0 523.3 120.4 378.8 -418.1 -49.4 743ee 918ee 2.0f0 80.0 507.6 118.9 368.1 -403.4 -47.5 71600 88500 l 2.190 80.0 492.4 117.5 357.7 -389.1 -45.7 69100 85400 2.200 80.0 477.7 116.1 347.7 -375.3 -44.0 66700 82700 2.380 80.0 463.5 114.8 338.1 -362.0 -42.4 64300 79300 2.490 80.0 449.7 113.5 328.9 -349.1 -40.0 62000 76500 2.560 80.0 436.5 112.3 320.0 -336.6 -39.3 59000 73800 2.690 80.0 423.8 111.2 311.4 -324.6 -37.9 57700 71100 2.790 80.0 411.5 110.0 303.1 -313.0 -36.5 55600 68600 2.890 80.0 399.6 109.0 295.1 -301.8 -35.2 53600 66100 2.990 80.0 388.2 107.9 287.4 -291.0 -33.9 51700 63700 3.090 80.0 377.1 106.9 279.9 -280.6 -32.7 49800 61500 THROUGH WALL TEMFERATURE AT EQUALLY SFACED STATIONS - DEG F FROM STA F AT INSULATED SURFACE TO STA 10 AT FLUID BOUNDARY TIME STA 0 STA 1 STA 2 STA 3 STA 4 STA 5 STA 6 STA 7 STA 8 STA 9 STA li
.100 7 5 .0 780.0 780.0 780.O__77_9._7_777o9_749 4 73@o@ AA0a 8@&L @ "5i a 0
4 0.- 774.4 772.4 765.8 752.4 726.5 689.8 671.1 !4c.* 44!.E :15.e l'..-
.. 65.N
>.y 766.0 762.0 752.9 734.1 70!.7 658.5 595.e 517. 4: 1.! 2 2.e 1e!.!
754.1 750.0 7!7.2 714.4 679.5 6!0.4 565.! 48!.7 TEr.! C'5.! 155.4
.700 739.3 734.5 719.8 694.2 656.3 605.0 577.4 459.3 365.C 261.6 150.0
.800 722.6 717.0 701.3 673.9 634.4 582.1 516.7 438.6 349.1 250.4 145.6
.900 704.5 699.0 682.2 653.8 613.6 561.1 496.6 420.7 374.8 240.9 14:.9 1.000 685.8 680.1 662.9 634.1 593.7 541.7 478.4 404.8 322.! 272.8 178.7 F+b@[2' l
WALL THICKNESS = .205 IN. CONDUCTIVITY = 20.3 BTU /HR-FT-F. FILM COEFF. = 10000 BTU /HR-FT2-F. DIFFUSIVITY = .01148 IN2/SEC. E
- ALPHA = 197.6 PSI /F. FOISSON'S RATIO = .3 STRESS INDEX = 1 FLUID TRANSIENT! STEP CHANGE FROM 780 TO 80F. NuSE.NT 3A EVENT TIME TFLUID T(0) '(10) TAVE DT ( 1) DT(2) SN SP MAX SN .446 80.0 742.7 207.7 572.3 -531.5 -98.8 75000 102900 MAX SP .176 80.0 779.3 271.2 667.4 -432.9 -179.7 61100 111800
.209 80.0 778.4 261.3 657.0 -454.5 -168.5 64100 111700
.409 80.0 752.8 214.2 586.1 -529.4 -107.3 74700 105000
.60s 80.0 703.2 191.3 530.2 -519.4 -79.2 73300 95700
.808 80.0 646.8 176.6 482.6 -482.6 -64.7 68100 86400 1.006 80.0 591.6 165.5 440.8 -439.4 -55.7 62000 77700 1.299 80.0 540.3 156.3 403.7 -396.7 -49.1 56000 69909 1.496 80.0 493.6 148.3 370.5 -357.0 -43.7 50400 62700 1.699 80.0 451.4 141.2 340.8 -320.8 -39.1 45300 56300 1.898 80.0 413.5 135.0 314.1 -288.1 -35.1 40700 50600 2.096 80.0 379.4 129.3 290.1 -258.7 -31.5 36500 45400 l 2.20e 80.0 348.8 }24.3 268.7 -232.2 -29.3 32800 40800 2.406 80.0 321.3 119.7 249.4 -208.5 -25.4 29400 36600 2.699 80.0 296.6 115.7 232.0 -187.2 -22.8 26400 32800 2.898 80.0 274.5 112.0 216.5 -168.0 -20.4 23700 29500 i 3.098 80.0 254.6 108.8 202.5 -150.8 -18.3 21300 26500
' i 3.298 80.0 236.7 105.8 190.0 -135.4 -16.5 19100 23800 l 3.496 80.0 220.7 103.2 178.7 -121.6 -14.8 17200 21300 l 3.699 80.0 206.3 100.8 168.6 -109.1 -13.3 15400 19100 3.889 80.0 193.4 98.7 159.6 -98.0 -11.9 13800 17200 4.098 80.0 181.8 96.8 151.4 -87.9 -10.7 12400 15400 4.298 80.0 171.4 95. f5 144.1 -79.0 -9.6 11100 13900 l 4.405 80.0 162.0 93.5 137.6 -70.9 -0.6 10000 12400 l
- 4. 6 00 80.0 153.6 92.1 131.7 -63.6 -7.7 9000 11200 4.800 80.0 146.1 90.9 126.4 -57.1 -6.9 8100 10000 5.099 80.0 139.3 89.8 121.6 -51.3 -6.2 7200 9000 5.200 80.0 133.3 88.8 117.4 -46.0 -5.6 6500 8100 5.408 80.0 127.8 87.9 113.6 -41.3 -5.0 5800 7000 5.609 80.0 122.9 87.1 110.1 -37.1 -4.5 5000 6500
- 5. 80f 80.0 118.5 86.3 107.1 -33.3 -4.1 4700 5800 l 6.000 80.0 114.6 85.7 104.3 -29.9 -3.6 4200 5200
e OL
@D 23 WALL THICKNESS = .125 IN. CONDUCTIVITY = 20.7 BTU /HP-FT-F.
FILM COEFF. = 10000 BTU /HR-FTO-F. DIFFUSIVITY = .01148 IN2/SEC. E
- ALPHA = 197.6 PSI /F. POISSON'S RATIO = .3 STRESS INDEX = 1 FLUID TRANSIENT: STEP CHANGE FROM 780 TO 80F. @d~W MA EVENT TIME TFLUID T(0) T(10) TAVE DT(1) DT(2) SN SF MAX SN .194 80.0 734.9 263.7 582.8 -469.2 -84.5 66200 90100 MAX SP .098 80.0 775.5 320.1 657.7 -415.7 -129.8 58700 95300
.020 80.0 780.0 470.7 744.6 -172.3 -187.7 24300 77300
.040 80.0 780.0 404.0 717.9 -271.2 -178.3 38300 88600
.060 80.0 779.7 365.1 695.0 -338.4 -160.7 47800 93100
.080 80.0 778.3 338.3 674.6 -385.5 -143.5 54400 94900
.100 80.0 775.1 318.3 655.9 -418.5 -128.4 59100 95300
.120 80.0 769.7 302.4 638.5 -441.0 -115.6 62300 94900
.140 80.0 762.3 289.5 622.3 -455.7 -104.9 64300 93900
.160 80.0 753.2 278.6 606.9 -464.4 -96.1 65500 92700
.180 80.0 742.7 269.3 592.3 -468.5 -88.7 66100 91200
.200 80.0 731.1 261.2 578.3 -469.0 -82.6 66200 89500
.220 80.0 718.7 254.0 564.9 -466.9 -77.4 65900 87800
.240 80.0 705.8 247.6 552.1 -462.8 -73.0 65300 85900
.260 80.0 692.6 241.8 539.6 -457.1 -69.3 64500 84100
.280 80.0 679.1 236.4 527.6 -450.3 -66.0 63600 82200
.300 80.0 665.6 231.5 516.0 -442.7 -63.2 62500 80!00
.320 80.0 652.0 226.9 504.8 -434.4 -60.7 61300 78400
.340 80.0 638.6 222.6 493.9 -425.7 -58.4 60100 76600
.360 80.0 625.2 218.5 483.3 -416.8 -56.3 58800 74700
.380 80.0 612.1 214.7 473.0 -407.7 -54.5 57500 72900
.400 80.0 599.1 211.0 463.0 -398.5 -52.7 56200 71100
.420 80.0 586.4 207.4 453.2 -389.3 -51.1 55000 69400
.440 80.0 573.4 204.0 443.7 -380.2 -49.6 53700 67700
.460 80.0 561.d 200.8 434.5 -371.1 -48.2 5:400 66000 l
.480 80.0 549.9 197.6 425.5 -362.2 -46.8 51100 64300
.500 80.0 538.d 194.5 416.8 -353.4 -45.5 49900 62700
.520 80.0 526.5 191.6 408.2 -344.7 -44.3 48700 61200
.540 80.0 515.3 188.7 399.9 -336.2 -43.1 47500 59600
.560 80.0 504.4 185.9 391.9 -327.9 -42.0 46300 58100
, .580 80.0 493.7 183.2 384.0 -319.8 -40.9 45100 56700
. .600 80.0 483.3 180.6 376.3 -311.8 -39.8 44000 55200
?
.620 80.0 473.2 178.0 368.8 -304.0 -38.8 42900 53900
.640 Bh.0 463.3 175.5 361.5 -296.4 -37.8 41800 52500
/ .660 80.0 453.6 173.1 354.4 -288.9 -36.8 40800 51200
, .600 80.0 444.2 170.7 347.5 -281.7 -35.9 39800 49900
.700 80.0 435.0 168.4 340.7 -274.6 -35.0 38800 48600
.720 80.0 426.1 166.2 334.1 -267.7 -34.1 37800 47400
.740 80.0 417.3 164.0 327.7 -261.0 -33.2 36800 46200
.760 80.0 408.8 161.9 321.5 -254.4 -32.4 35900 45000
.700 80.0 400.5 159.8 315.4 -248.0 -31.5 35000 4!900
.800 80.0 392.5 157.8 309.4 -241.7 -30.7 34100 42800
' 06E'/23 HALL TH2CllHESS - .24 IN. CONDUC TIVI TY z 10. ? S TV/HP-F T-F .
FILM COEFF. - 80 S TU/HR-F T2-F. DIFFUSIVIT! .00725 IN2/SEC. E
- ALPHA - 223.9.PS1/F. POISSON'S RATIO z .365 STRE23 INDEX = 1 FLUID TRANSIENT: S7EP CHANGE FROM 80 TO 1600F. ( \ b)
EVENT TIME TFLUID T(0) Tcle) TAVE DT(1) Dic2) SN SP MAX SH 1.294 1600.0 119.3 120.6 139.7 s1.3 10.2 10800 14400 MAX SP 1.220 1600.0 116.4 177.7 13s.8 of.3 10.3 10800 14400
.100 1600.0 50.0 103.1 64.? 20.5 13.1 3600 8200
.200 1600.0 30.3 110.5 81'.5 33.8 13.0 6000 10o00
.300 1600.0 81.5 128.1 94.3 43.0 12.4 7600 11400
.400 1600.0 83.6 135.4 09.0 40.2 11.8 8700 12VOO
.500 1600.0 86.6 141.7 103.6 53.5 11.4 9400 13400
.o00 1600.0 *0.0 147.5 108.3 56.4 11.1 9900 13800
.700 1600.0 93.8 152.9 112.9 58.3 10.8 10300 14100
.900 1600.0 97.* 159.0 117.5 59.5 10.7 10500 14300 000 1600.0 102.2 162.8 122.1 60.3 10.5 10600 14400 1.000 1600.0 106.5 167.6 126.7 60.8 10.4 10700 14400 1.100 1600.0 111.0 172.2 132.3 61.1 10.4 19800 14400 1.200 1600.0 115.5 176.8 135.4 61.3 10.3 19800 14400 1.300 1600.0 120.0 181.3 140.4 61.3 10.2 10800 14400 1.400 1600.0 124.5 185.7 144.9 61.3 10.2 19800 14400 1.500 1600.0 129.0 190.2 149.4 61.2 10.1 10800 14400 l 1.600 1600.0 133.6 194.6 153.9 62.1 10.1 19800 14300 1.700 1600.0 138.1 199.0 158.4 60.9 10.1 10700 14300 1.800 1600.0 142.6 203.3 162.9 60.8 10.0 10700 14300 1.900 1600.0 147.1 207.7 167.4 60.6 10.0 19700 14200
- 2. 000 f o 00. 0 151. 6 212. 0 171.8 60.4 10.0 10700 14200 WALL THICKNESS = .205 IN. CONDUCTIVITY = 10.8 BTU /HR-FT-F.
FILM COEFF. = 90 BTU /HR-FTO-F. DIFFUSIVITY = .00725 IN2/SEC. E
- ALPHA = 223.9 PSI /F. POISSON'S RATIO = .365 STRESS INDEX = 1 FLUID TRANSIENT: STEP CHANGE FROM 90 TO 1600F. [26)
EVENT TIME TFLUID T(0) T(10) TAVE DT(1) DT(2) SN SP MAX SN 2.608 1600.0 132.2 219.6 161.3 87.4 14.6. 15400 20600 MAX SP 2.276 1600.0 122.2 209.6 151.2 87.3 14.8 15402 20600
(b El ( _; v
.200 1600.0 80.0 119.5 86.5 28.0 18.9 5000 11600
.400 1600.0 89.3 135.4 92.9 46.9 19.0 8300 15000
.600 1600.0 81.7 147.4 99.3 60.0 18.1 10600 16900 i .900 1600.0 84.3 157.4 105.6 69.1 17.2 12200 18200 1.000 1600.0 88.0 166.1 111.9 75.4 16.5 19100 1.200 1600.0 92.4 174.0 118.2 13!00 i 79.8 16.0 14100 19700
- 1. 4e9 1600. 0 97.4 181.3 124.4 82.7 15.6 14600 20100 1.600 1600.0 102.7 188.2 130.5 84.7 15.3 14900 20300 i
1.800 1600.0 108.0 194.8 136.7 85.9 15.1 15200 20500 2.900 1600.0 114.1 201.1 142.8 86.7 14.9 15300 20600 2.200 1600.0 120.0 207.3 148.9 87.2 14.8 15400 20600 2.400 1600.0 125.9 213.4 155.0 87.4 14.7 15400 20600 2.690 1600.0 131.9 219.3 161.0 87.4 14.6 15400 20600 2.800 1600.0 137.9 225.2 167.0 87.3 14.5 15400 20500 3.000 1600.0 143.9 231.0 173.0 87.2 14.4 15400 20500 3.200 1600.0 150.0 236.8 179.0 87.0 14.3 15300 20400 3.400 1600.0 156.0 242.6 184.9 86.7 14.3 15300 20300 3.609 1600.0 162.0 248.3 190.8 86.4 14.2 15200 20200 3.800 1600.0 168.0 253.9 196.7 86.1 14.1 15200 20200 4.999 1600.0 174.0 259.6 202.6 85.8 14.1 15100 20100 i WALL THICKNESS = .205 IN. CONDUCTIVITY = 20 BTU /HR-FT-F. FILM COEFF. = 80 BTU /HR-FT2-F. DIFFUSIVITY = .01100 IN2/SEC. E
- ALPHA = 193. 8 PSI /F., POISSON'S RATIO = .3 STRESS INDEI = 1
! FLUID TRANSIENT: STEP CHANGE FROM 80 TO 1600F. [36) j EVENT TIME TFLUID T(0) T(10) TAVE DT(1) DT(2) SN SP MAX SN 1.815 1600.0 111.3 160.4 127.6 49.1 8.2 6800 9100 i MAX SP 1.729 1600.0 109.1 158.2 125.4 49.0 8.2 6800 9100 t
.109 1660.0 80.0 98.8 82.7 12.2 10.0 1700 4500
.200 1600.0 80.0 106.4 85.4 21.1 10.5 2900 5800
.300 1600.0 80.3 112.3 88.0 27.9 10.3 3900 6700 i
.400 1600.0 81.0 117.2 90.7 33.1 9.9 4600 7300
.500 1600.0 82.0 121.5 93.3 l 37.1 9.6 5100 7800 j
.608 1600.0 83.4 125.4 96.0 40.1 9.3 5600 8100 i
.700 1600.0 85.1 128.9 98.6 42.4 9.1 5900 8400
.Bef 1600.0 87.0 132.3 101.2 44.2 8.9 6100 8600 i .999 1600.0 89.0 135.4 103.9 45.5 . 8. 8 . 6300 8700 1.009 1600.0 91.2 138.4 106.5 46.6 8.6 6400 8800 1.109 1600.0 93.5 141.3 109.1 47.3 8. 5 6500 8900 1.208 1600.0 95.9 144.1 111.7 47.9 8.5 6600 9000 1.309 1600.0 98.3 146.9 114.3 48.3 8.4 6700 9000 1.400 1600.0 100.0 149.6 116.9 48.6 8.4 6700 9000 1.500 1600.0 103.3 152.2 119.5 48.8 8.3 6000 9100
\ ,. . _ --. _ - - __ - - - - - - - - - - - - - - -- - - - - - - - "' '~
Fu L 3l : 5 WALL THICFNESS = .125 IN. CONDUCTIVITY e 20 BTU /HF-FT-F. FILM COEFF. = 80 BTU /HR-FT2-F. DIFFUSIVITY = .01100 IN2/SEC. E
- ALPHA = 19~.8 FSI/F. FOISSON'S RATIO = .3 STRESS INDEX = 1 FLUID TRANSIENT: STEP CHANGE FROM GO TO 1600F. (45)
EVENT TIME TFLUID T(0) T(10) TAVE DT(1) DT(2) SN SP MAX SN .781 1600.0 103.9 134.4 114.0 30.5 5.1 4200 5600 MAX SP .742 1600.0 102.2 132.7 112.3 30.5 5.1 4200 5600
.190 1600.0 80.1 98.8 84.4 15.9 6.4 2200 4000
.290 1600.0 81.5 106.5 88.8 23.6 5.8 3300 4900
.3PO 1600.0 84.4 112.3 93.2 27.3 5.5 3000 5300
.490 1600.0 88.0 117.4 97.5 29.1 5.3 4000 5500
.'500 1600.0 92.0 122.1 101.9 30.0 5.2 4200 5600
.600 1600.0 96.1 126.5 106.2 30.4 5.2 4200 5600
.790 1600.0 100.4 130.9 110.5 30.5 5.1 4200 5600
.000 1600.0 104.7 135.2 114.8 30.5 5.1 4200 5600
.990 1600.0 109.0 139.4 119.1 30.5 5.1 4200 5600 1.990 1600.0 113.2 143.7 123.4 30.4 5.1 4200 5600 I
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- F = 6/d' *2 A(0< ro m TKxJin s tia.c & M k p csu g;s, wc ntam :
( T~s = 3 6o *F == f 20 E-Ta = I fo F = GN 2 NdTE} Auh's tik G. adesG d 4 A , n ,, u r Cm , hy i (; f , = .ngi4 g t o.g ; (uo h g po ),(,,,o w y l
cate so FZ - t o RE, SAGE 7h PROTO POWER CORPORATION GROTON, CONNECTICUT oao w en g,;, care g g 2) - ( 6
,,,,,,,g sc," 4 El i 4 d L CUENT ps;( PROJECT p:4 y gg, '
SUBJECT MS S gNy fsM G l.L Pi 4 E- LL #1 R
- 6) h c,u By Q,4 j l h =. h.. N. = A c . ( p .Pr)"
L L Nr =-
, Heo1 'Tcw & & uiaf ml%E d of Au ra+paruu.(5), (as-1 L=C%ar s %9,y }.hr.*/(.
7 N %dn b eM fy y 0 of % Pc S f 0 = g pun t
.% = % 42 % ;g s r, eL
/
p t (3r = repor . f 1 h m ,e w o y / ,
= ./ *A St i oea t oas WW
---.-,---,,,,._.--.m... ,cm,.m, . . . - _ - - _ . _ , . - , _ , _ . _
_ . , - , . , _ , . _.,.___,y. , , __ ,_. _,,, __-,-.,,-,,,___..,,..,%-m-, .
,,.w..-
catc ~o p _go aev E 2}m39 7 PROTO POWER CORPORATION m a,saroa GROTON, CONNECTICUT g g' care gg _ g p g g
, g ,
CUENT p g (, PROJECT ppg, gq SUB.ECT gqq gy p; (J g y'; y (- l Fog g g g qff,,, y , , %f J T-7 Ehr y h a-My c8- hda w p M p. of& c1 fim
- q. 9 , a 6 :
T p' u = Tp Ts _. 65943CO - 4 65 # F 2 L > By 4, f @ M# 7 = 7o0
- 0, f 2 = 5 7 5 pm_ w T(o A (k TA E c .(
HE uvm een p.h I O.2 33 F= V,27g
/F = 0 069 kF = 0,il f Pry -
o, c 6 7 3 I I
\
4 5 C + 4 (s o 0$ D ( ba. Caty iE R VA'fl C M , Fod l TA <E 7 It1= F~utLa H GI & r-H-~ oF The SMo vD, LLW o C H IL, By (2EF, 3, 6) S'.t -S'; f
'J .
- 2. =- 2 E S~ 7
C ALC No g7 ,g ag, r' PROTO POWER CORPORATION ca,o w en pAGE L p " j GROTON, CONNECTICUT 4i
" ,1, l / - 1 S8 6 asv>e*EO 4 7p sCB W 7{p,4g{
CLIENT {gg PROJECT {gy GQ SU6 JECT QQ f; QQIq "Tl M G Vf Vtf_6 Q, A TEll. ft, ?r = (tfI) (0.233.) (na)(Mo) { sG- L)(o.u?) (o .o u )' ( li r)
=. I, o 99 x i o 57 du C = 0.11. %d h=I 4 ud h e, n = Co, n e ) , c o. n tD , ( l.oa, ,?f (Is~. C ) .
= I 4 . ~5 hI} _
R,W =. I _,c ,94,g~ g7l4 g;,1lgjo, go,) (u 2- i)
- 3. l. } "
Y h T e,sa = Ts + Te = ic~ in 2- , av p z.
=
230 R ___
cAcso g2 g o ae, ease g g , g a
' PROTO POWER CORPORATION oa,cu raa -
GROTON, CONNECTICUT 9,7 oire , , _ q D ,, g b aEv'tWED 4C0 NG } { l j g { CUENT pgC PROJECT Fgy _ {Q susseCT EE6 F t. o o D /^/ G TIM E ul Fi R E W 9 R R. I (t[PE$$opwa.) 9 I 0,lA 2 2-7 = -
=
- 3. + n ?
p, = 0. 0 G 8 h e= 0.1o f Fr p = o.66 3 C
= I
= l
@r -
2 +oa 6c 3 30 (fr < 0 =. (2 Mf(0.2 92i)(T7.2)(Wo.)'(160-Ib)[0.663 (O.oS9)' [Ho)
= ,, W x n o "
O c, sg = g (0,123)(l,775,gf (25,5)
= 16,5
catcso $2-tO 3 0 o, 7 Y I a o' f PROTO POWER CORPORATION ca,o w ca GROTON, CONNECTICUT g7 care i g . p f.,. pg
,,,,,,,C ,c, ,c
(, g CUENT g{ PAOJECT fg y ,,, { Q SUBJECT 6 65 F L O O D / M 6- TIM 6 N f8 C E *ME (v') n,ge l O M b M M y,'h 4 L4CC#$ j
; L=P=L 12-y I
r= L20 + i ( = t 6 C"' F J~ f u s p., . t o,39
/e~- 2. w l f F ~~- OsOSf ky = 0. o 9 rF \ Pr, = 0.660 i
F = AT= lf0 '~/f~0 ~ $ O gf (o.3E.) pu)6ddo) (o,6) ( C (qrg x 0 -- (k) (o.os4) ' (62d _ - - -- - _ _-_ _. . -_31031lb - _
cite so g g.g g ae<
**cc 3 I cc 39 r PROTO POWER CORPORATION oa curca y, ; . d '2 7 - 8 6 GROTON. CONNECTICUT aeviento gg see w g {g#4 g g CUENT %g PROJECT pgy, gg SUBJECT G E- { gg o g f yy 7,p 6 pf gg pgg L C- 0.G L C "a n-l+ /
h e, v- .-
'+
- 9I L (o. sis ), (g.oz e sor )'N __ 14 4
%. ) -
U sou o.bpsC oJL [h ko Mc Co b e- ov<c A 9g,,0; ,o, & di d .k & %A pay n (p. & A 5*auo,or =
- 17. G l x (i 5 4c ) = 2 c +, z. pl2At o a utc ~
6tvavowv 2 H ) I' IT. Gl u (2 5,5 fr ) = 4-+9 A ,% , = fr 'fy , p s c e Agg = 3350 M/m . ou w ( tty Ry 9 ) so. - b ^' e,a s =4. 2- x 4- + 1
= (A. 2} (I. & = 4, I 2 6 +.1 4
- 2) b c,4 5 =. l4.[xl.7 =- 24.3 h k c,g --
- 16. [v I.7 -= Z f. I
- 4) be' s r = 14 4 1779 = 12 I 5 24,q,t C s) h g,,, = t.i I fo n) c EE (
l ca.c so f 2-1 o ae< fg l{ PROTO FOWER CORPORATION GROYON, CONNECTICUT osia s4roa y,7 amos 3 L y care Il 2 f - F b aeweaso y7, y c see w 7 6 // i 8 L cuenT pg c, PROJECT pgy. gQ ? SUBJECT tt'Gg ;Q,copt A/G 7161 E gj Fa tt.E L4A If(L i C4 t-( Ul AT6 P v56 0 By f/toH.A M Hw v. Na,sr= = 24, 3 H M - l 'ik h ,,, hap e, h, m 2+,6 H C45 = I Io
'T WS SUcsLP%9,: & Ua$ 6tAJer s rw o./j ekcu pw us a Ass wA , cs mer w cGd h gful. tRe unum / -tRu wlwecA x scp Adg , @c & @Ho*p % -s-
- 1. s ok 4 nyacs of ha A ~G
,4 w A bss. L -% c d k A mi,k c
- z. A m,aw e4su 6 c4 &uq a g o _a3y tu s %
Pfen. . b bswr" a kra- awedt . S' [. Ab & be.- Se m h A nkdnd e, gones uid he.of % sfu Gm % &f Pkm 9 lo (T=dk,II,I3) ccwlcLunt' dx roKc. %
~~;c to Lc year so~es.
I cate No y ? - , o aev "ce 3 3 0, f9 ( PROTO POWER CORPORATION oa,ou roa g care f f g (, g4 ,' GROTON, CONNECTICUT
, ,9 ,c CLIENT fgg PROJECT ~ 7 g y gq l
SUBJECT gg p g;') o 3 f g (7 -ffgf f/ ft 8.,6 dAIb i
! %8d of TEh PEfL AT J IW AuvM Proo Uc .
Ts = 3 L, t=
, Ty == Ifo
- P AS R, A s
*b c,g s = 7, / + 2 4. 3 = 31,4 A ST = R,sr + Ne, cr = l. T + 24. 3 = 2 (,, o (8 ,
=
b>)w m = f _f 14,2 i 31,4- + 2 6, o
.. Ohg :::::. ' overtA L L p gkr = ,i p d 6 5 * - I (* ) = I 8 0,4 Q ,,,
T s =. 550-Ifo.9 = %9,1 vn 3#0 Eh L
- 4%s = %5r , ATsr = 2Dx(ul.1-50)=lf?,(
l h e,se M.t 1. f3 ::: 3[.73.l-f[h.b = [h$,[ !
'OE @ dmc A Hovr as g,g ,,,, g g pga
l
,e CALC P*O gQ.g g aEv
- AGE Qg gj PROTO POWER CORPORATION ca,c. rea
\ GROTON, CONNECTICUT g g* care
,7 g, pg aev.eato gp seew 75 ; / 4 p 2 cueNT SUBJECT pg 4 PROJECT gy,gg
{ GGQ fg n g p) QG TjM[ flRE Q( Q'TG k l i 5, fb , HB HC C * E 9 b cvs- thu cxm A hk cacff'uds L Tit vodu* aud; k.$/ = Soo N 4<f. Y ( urs 3 i C 1 HB .=. t o o o i (Golcias) ! H 6 =. 50 (sren D i
- ant. hy'ad Va0<ac %sude Gs 6e s , m Rnhd by N. ID .n p 3-20, 1 kh tm(e._ l l , PPc Mc..E2-Ii Jr-
-6, : b d ' & Q'y A ce#MCeud i
c oing m u.:a g o- 4 g m t ee _ d e duc d , & ' d. aeMw i
cas c ~o g 2 io ae.
*aa 34 ,, 4 $
PROTO POWER CORPORATION GROTON, CONNECTICUT m,c,,s. roa y, q oare g g ,,7 9., p 4
, ,g CUENT f4 ( PROJECT pgy ,, g g SUBJECT 6 FS FL0CD)N6 T/M d[ Pld6 iMC E' EY , b><klAdW CL Y
% capu-a ss a se bLa byw icaor-e k %
(& <aEa. . A a, 4 & 4Weufs a klh , ud seheGJ #m au adh e e e ATp ( w4d, & whu*4 -[/*v Mt L' u be pw a b6
- Y " 5
%d vi(). & ut.,. O Ab $ m Ni So
) zee f Y wor >u. . he,.t:frwife rJi.
rk.Idf iuvekt&c l'o b coefhnh4. C
cuc w g I ig at.
**ci J G e, 3 q PROTO POWER CORPORATION c aurea 4 , 7' GROTON, CONNECTICUT cart g g ly. g4
,, y g , , g cuENT p4 (, PROJECT QV,gg SUBJECT gg f pop; AJC " tim 6 W/ F LE I447E/L
- b. A U (T {L /Ni$ l[O ~Tntiv 19 0 )
L 'G d % $ ate ef w Cwed L p u s u.
/ & w3[ d or TIME =0)
(0 ftsisem Cta c< w d Ferwrs< suenceoets ( 1 = 1 ro +) Fy &J. I2. T = 4-o 3. 4 # F CD Mitv sianM Sa6espogas Aac miy sTfaM d n/es (I= 16 To 29) R/ 8a[11 T= loco "F l l
, (ll', ) ssm krv6n.eitx2. (>u. A,<ncnm Ex t- 0
( vives St 9 . E w vo M it-6 K 7= Glo*P
I cate ~o q,2 jc aev aast 3 '6 'J9 PROTO POWER CORPORATION GROTON, CONNECTICUT on,o. irca g cart g g , p p pg
, , , , ,, ,o
) cuENT pq{ PROJECT pg , {g SUBJECT g 64 Fco o p lN O CM6 IA/ Fi R 6 W AT A i i bone i o : 6 t'A fora n:vt. 6 l h{ ' V dd fl[4 k ( T = 7 6o
- f:'
i E46 $ 's YH W EC TINp t.c-4 p s
- 0 UNSW!? VWfl$
&oS65 'l3 ( /ff Su f6h h EIA"TYPt. X
= 0* .
) i i ) i l 1 ( , l 1 ! l
cacc so g 2 g o AEv PAGE 3 p , jQ PROTO POWER CORPORATION cmo w ca 4,7, omrE GROTON, CONNECTICUT gg Zf- /6 g cuENT f6C PROJECT 74 4 S&ECT ggq qtgy O yp (, igg 9,j p j y Q. k ; i APD6t\/D U M - It % bd c& & R.ve % mp e[cd f AC when w TA prop m i ,-
'I 6EW o L " w EGnurGd =d &
! cuned A s s&_d 3 m (c) ron r L WN Gb (1) w deel (>< p ID,
& A vdum Aumd fn (-rime-pstTwdME) w- sGak . oDoup ad -nm E , r., &c uoth , a. ,
G Gg. g 26 S um ds i (26 ,yvenav enow . oavm e= _t <, D c o- a.A M , Ls ery&ha % d 4 f m a. 1
% O (h a b l
- s. .
M OV 06 j LD NI N $ MN(Is l
l l sev ca c ~c .S 2 -I o SAGE } g , g PROTO POWER CORPORATION on,s s.rca y,,, . ire GROTON, CONNECTICUT , , 7 7, g aewe*eo gp .ca ~og f,4 g g cuem p4 c esosect FGv. G.q, suasect g p g o p ;fgc,. 7l M g gj pf EG Lt en g_ REfeieetV c4 s L, WC ce t c utagT1stv' ?2 - 01, clahd II- I3- f 6 2, PPC c a t t u en-n ow' 92-OT, sc2 d II- I i - P b 3, Foa.r s r. V pa oa a PDani 0 T~S A C 4, A , 7, C h a.( ma.n , HEAR TR AWs FE e , ' Mcgro.+ H.d (- g, G A- D14-9 7 f,
" ssm esnea ana ,ne re en u.
T & /t F o It M A N L 4 /H o PEL- 5 MND D A -r o 'l e c o v c rf a w > csiv(vt AL .WTOM e e loM ifA d Y, G, f5V Pi P i a ce < PE c- , I - it4 - 2 C, A DA- I lo , q, PSc. s nine nNsanwrz. s oEs M 6-l Anl 0 PGttfort MA U C8 , r,enget gz. gym t g u,
- 2. GA Do c, # 90 9I2D , E E S Cc0L Dc cd^/ I~#0 0'1 gy0/o TouktL v soiv & c.omoeiv c p-rG 'op. Fr e E' a u tt. ( t T Ha DE L A y ) , Md ll- Il- 14 (C 9, ~1hGR tts o O Y Nn n1t E.sANO 9ta N @er PWaPE(2Tib$
of M L ' VM ; " k'V&ll o '- DYM &f *2 5 k "- ( 10, d. M. Ro hu n e and 7. 7. No/ ten eTF / e ds , , Pavo8aoK OF HEAT T n n W E E r2 , Mc frw. Ho *//
\\. PPC cesc,vtafon) i2, Fsv p e n s oiv ci 2 2 - I I, M L It g g f P - z - t 2.
f A P P &IV D l K CA CNo g),-lO L REV PROTO POWER CORPORATION ,c,,, o,3 PAGEAl *3 GROTON, CONNECTICUT p soru m Il- 3 f - 8I#
"'*'*'4@_ff g #""
CUENT nii4g2 PROJECT pg g ECT ,rc o , , ,o ca M A,, , o O ,o n OF t,4 , , , , ,A ,4 sup*wv To EES
**'Tihe
( *T ) cu) ( su) $EM6 ' As"5' aaI N " *'
- c. i m,.) p
.FNC
- wo(.0 u n oe.vu e.o. : . o. u. oJ) t %a i tpr*) ,p=m NAM eTIa.a m A h 'T-8 i s.o 10.75 T.%7 41.1 2572. 37.I 1572.'
1 37. t h 2-4 54.o i1.0 9.616 e i .fo I i 296. I S4.E I i t 1% \34.5 h 9-10 104.2 n2 0 9.i12 47.o t e r. Ao. 250.2 1 ibb40 2.5 0 2 h to-ii 7 t.9 fo 12.0 9.i12 47.o i1492. 172.6 1 1i491 i 72.9 in-12 26.e 4.5 3.15'2. B.to 732. 22.1 6 4418 t32. 7 l p = 4 S at cm syssa, yu acue,H ht EES Moows5 p s 49 i 2 -2.9.( s p=491 c/, e.E . p , soo gi =5 6 p(no .s 4.so 3. ,5o e.io i s.s . 4 i3 e e 2.e 2. s ( 18 -19 7. 3 4 50 3.346 7.tl t 76.3 6.4 ro lose 38.4
@ 184o, F 409 h 19-20 27.5 t.25 666 . 6 t li 57.4 6 3B tos Gl97 699..
90-11 .89 l.25 .S74 .617 19l .204 noe 2 o6. 3 22..o 22-23 s.57 n.oo . 124 374 t .20
.298 324 3S9 9 6. (. I
@ 51 5,3 lif.6
@ n 2u s7 i.oo . 724 . s i4 72.e i o.co s2.4 2sss7 3499.2 i gg3A-24 et t.oo .124 .374 79.1 i1. 15 324 25r.28. 3 s o 7.
- h24-25 6e t .co .550 . E'4 9 127 0 9.79 324 4 ii AB. 3 t 72. .
h 15-26 82 i .oo 590 . Ei2 M .3 i . 2.e 314 4 bas. 41o. (1) s 6F R.F T 1. . D O A UM M f. wo u m ~ . - ^c* .- - -
l A PP6 N Qld CALC NO g "), - g g aEV PAG PROTO POWER CORPORATION caiouren GROTON, CONNECTICUT P W ^ cars , , .g q , g g CUENT PROJECT (26J]2 W #" 75ii4 9 2 p;; W - E t ! SUBJECT Tei A L 9 iPi W w 6 Ac. Ao rs AawA~ a pr mu% ei aa D A*T u I
- (. T w a aa. w m u s ma). c.acTiduED ) .
l
~ v. ciu DN64' C FT) (,iui (,io)se$N$$w, dW I'
- c. FTS) !
un i =mu o.o. T. c. Anni M aa 7***'- 8"' CN 2e,- wAss sesA pa ru M*** ' *.'*'E A A
\'J/ 27 Gi i .co 5'40 . 512. i o4.5 S.42. 324 14504:.. 3 o 5'2. 6 37 -
26 13.28 t .oo .59o . 512. 23.2 2.o5 32.4 75i7. en.4.5 19-29 .AB i .co 768 .322 t .oS ,1 A"I iet i I b. fo li.3 29. 3o 2 S.9 1 15 .969 .490 49.I 7 33 108 5 3c 3. 79i.6 v 3i
@ 5419.Gs ~ h 'J. 1 7.3 4.5 3.803 4.55 i 15.2 727 6 e 9 1.'2 4 3.b s w. iT *am a s.sc. rnr su ww=w tao K 'o A.ru. g , ,gq e ,, ,,
32 I o n. 8.r5 5.826 35.5 i i 4 t o. 154. i i 4 Bo ts4 32.- 33 19.5 44.0 9 596 S t.% 5467. 48.9 i 5417. 42.9
@ 3234- - 4.14 10.25 10 22 115.4 4422. i t. T I 1G.L2. t 1.7 14-35 26.5 t (,.25 l o.S2 1o385 tis.4 rs.t I to395. r 5.l f3s-m 2.i i 4. o i i.s 4 1 .
49.2 ss i.9 a. 34 i ss s.s 4.34
\
l35A-h/ 34c 19.2 2.15 5.926 31.5 2070. 2 t.S t 2oTo. 27.9 m-37 19. G.4 2.5 4.4 t l 19.1 k 6132. 21 9 i 12.33. 2. t.9 ' 35-I SS 23.5 %.75 E.S 2t. 33.5 2673. 35.S ! i I c.t.73 35.% l t l
AP P6 N D [K CALC No Q,. I O "E*
**G% 3 y 2 PROTO POWER CORPORATION on o u roa GROTON, CONNECTICUT P " ^u^
cart U, 7 g, CUENT
***@O AAA PROJECT 75n4e2
[gQ SUBJECT "1*oTAL p t o tog uA*A hoo Aara n c- r u c. rad A AT u "d 'T - 10V6 & Cart) Clu) L%) crt*) Clu) e l [ TOTAL. 77An Suas e on. i aca.w o. a .o. -- e mfi wmes C t W es.aa AusA r.(grg em Aas.A I war.e. ( 38- th 5.54 B.75 5.S2G 33.5 G ao. 8.45 1 c.Sc. B.45 3 O Gj61,1 Too,2 9 h :e 39 45'.S t 4.o i t . E4 49.3 7 6 7 4.f. ttt.4 I 7674.(, t 5%.4 3Cl-40 9.33 i 2. .O 10.1 33.0 t o454) 24.7 I to45 24.7
@ Ao- 41 73.9 14.o i 2.5 31.2 7654.6 2 41.9 i 19 34.6 2.4 t.5
@ 4i4 2. 47 8 tr r.) n4 3 4o.5 4 s67. 112.9 i s s 67. n s.9
@An- 43 11. t 24.0 2156 eT.3 3291 s 2. 7 I 3 291. e 2.7 Q
v 434+- 4.5 24.0 2156 67.3 1334. 25.4 1 is34. 25.4 ausa 44-
-r FTl r3.o ggg.e 1 o 5.0 2cos.b 9\o00. 357.4 1 4tooo. 3 57.4 r aTI-57 2. io.9 10.7 5 4 561 19.9 6 _. 696. 27.0 0' 572 -
1 & cts ~. 27.o FT3 5.5 g.626 7 625 12.7 6 2 36.3 I l.o 1 239.3 16.0
@ 933,3 3E,o ~
l k
. s.
- ,. iii .. :-: ci.:...ces tas to co:i own an EE5 looc c/ f re t .4 e GL( ' E 2-I O li sia 20 n .id:
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- 1 : 'Ec:n.:rinN' + Eoiling + sserheating
- 2 : Ectit y + Sucerbesting p. loF4 25 * =3 Sv:grr45ttm 0:U 3 'EIILt:D 27 T.O D : :Fi+: to G!at bstine tr.it Zone I hai (sone) toiliN Caltviite1 Ee of bass enlity of kater 4 the EM of Zone i 25 '
2 ' it Otter Verg3ble; Gre e.cipined as tre, occur 12 50 019 (FiiEEL(2h. Mist 2h id(20,T.UG(23).AREAIN(29),!PI)DE(29) 20 01170dillh.Gi:42D ,Cid5 ) .E0llt f 23),GJR(29), A0VT(29) 43 ' 43 ' Set all constras 5012EEi: 29 'hWer of Fist IrFifer 20 Dei 60 IIAIF'E'i: 10 ' Frew.c, of G,ts;t of Fesults 70 FX= ID ' Total Fiw Ene. ffM 80ef ault) 7279I:.3278'5at.)fa*10nTes:gr3t9fe,deJF(Default) 74 hF6: (ii.si ' Wit of E.;;:. ration. ETU/LEn (Cefault) 76 UW:1: Gi: 54 're Cic4citter 4ter & 5 team, ETV/(Lfaldes R) 73 'Kaitation b+3t Transfer C:.nstants M SI6"J.: MM1713: Efi: !!: SE,*5: Sli/A1EFS: SE5i= S!6 Mill /(2/EFS-1)) 53 'Cor,ective heat iraniter Constants Gutstce EES Tubes
- -0 G i: 16: H;57: 17 94 ' Connective neat Transfer Constants INilCE tubes 95 Fi: FA: O l@: Hi: 50 " uter, Eatlig, 5 teas, BTV/(HRbT2*deg F) trA TA"ER: 550+E0 "htent' Teteerature outside Steaa Generator Shrouj, deg.R 105TFIRiWTK: E.) 'Ir.:ortg Fire V+ter Temrature, oe9 F 109 ' Steel heat Ca:acittei, ETili(LEuoeg.R) 110 Fi> I:1 TG 7: U5iEEUD: .1116: fEII: FOR I:8 TO I;0ES: CFSTEEL(1)=.llt: EIT 120 GEi;iiri: 1 lin Stec. SEG.Di 130 INTER'iR:IETAE4 '5et Chut Freuncy Counter so as to Outcut at Startly Tise
!?!
154 ' Inc'st Initial V+hes frca 'EEiOXLVR' rA Vse Defaults 115 'TGli D : Te c+nture of Tiuij Cosina out of Zone I, deg.F 137 'TUD : iewerstwa ef inll cf) Zore I 133 '0IM D : Fate o' Fett Flos GR ff Gall of) Zone I & into Cmlig Fluid, Eii)/hR 111 '(/DD : Kaie of Nat Flo, IE0 Gall of) Zone I & out of EES Ambient, ETV/bR 113 ' 155 FKini:!';UT*LG:0 i:ifiR VRlES FFGM FILE 'EESCOLVR' (Y/N)':FS:lF F6:'n" if Fl:'ir TG E7019 10 0 FEN "EEiGU,C FG ii:;.7 Ai 81: Ll!E Irfidel.0VNms: It(tlT81.T!!'E.GFM.T97FG 165 F0; i:17012i/Ei: i:4;et,my.T0Vi(D.Ti(1), GIN (I),Q0VT(D,9)AL(1):lf (ER(D00 TG E4illfinT 167?UT:0.0iitt 17060iG155 173' 150 FiA 1:170 7: Tiil): F3 at: TGVi(I): TA(1): EIT 184 T&tS):610:iGli@:610:Ta(91410:TGJT(9):610:TA(10M50:T01T(10)=650:TW.(ll):70 lE3 TGlT(ID=7%:iU12):760:Tiliisil):7%:TA( 13)=730:T0llT(13)=730: TV.(14 )=730: T0!!ill i:730 190 F% I:15 TO 12Gi5: TA(D: 107A: TGJT(D= TWL(D: EXT: TIE: 0 194 ' 135 FTA 1:17012iMi: T.*.a D: TA(I): iEli 'For proper Output at Starting Time 200 6050B 174 'To fat Elises +nd Areas lia ' 233 'iimt .4:n Frosram Start; 3i4 FRlhi 3% 'A3k for Confiraetton of Vei45 for Run for (hanoe) 310 FRINITLO'J REE (Fm: ~:FN::UEVT Fss: IF 6FM80" TEN GFft-VAL (GFtt$) - 320 FKikT'%iiSiliA TEE toe:.F): ':TMT::07tT TMil: IF TSAT60" TEN TSAT=VR(TMill
i
- ~
- Fs:'.! riAT // Eid.Li;.'. i~ 5.iu. ': iG. : P. Fbi Wil: IF hFila" TO hFi:. . nFli <
n.!' . {4l' ,I' ' 55i. ' Q;tulate bri, Rat Ocacities for Vater and Steam. ETV3/(rftkg.F) E) RECT: 9XItyr: K'd: r"OitCF4: Ki: rF;Ti(Fi A y., p g g 7 /., 333 ' 44 'Os%t reidti e.en (10:.iTREMELT'ilri) Secc:n; 410 IF I!.7EKLUjjiUE) i-EN GOTO 610 f' 2 5 4 419 ' 4:0 (1.5: it.TE*'.R: 0 Keset Ogtest Interval Counter 420 FFPii " Tire:': TIS:'iE:i *.,~sII.T IJ5 INT 844 64 MINS': TIE /60; 415 FFilti * [ FliK:':Fn:'yn - TIAT:';TcAT:'T l': FniNT 440 FOR !=1 T0 IZ@Ei 415 FRif.i trilWZO'.E ta: i- t;i~:ts:* sil) EL: ete ';l;T0l#(D;E0Ill(D;TWL(D: 150 FSINT USIWQ- it.izt* 2 " Eli=tf I'"":0IN(!):00lH(!); 455 IF EDILLID='E' TG Fai:.7 U51:.P -- 1:444.ts';01)AL(D ELSE FAINT 460 IF 1 015 T @ 60TO 450 445 F;i:J:PJUT 'FEEis (CA/ 10 (0'.ilVI. ',0tW: CLS 470 F5ini 'TiPE:': Tire:'iECi #::FRP.T USINTitt.64 min $'; TIE /60: 475 FEit.i
- I PJS:':Tix:'y.s - i!!J:';7 FAT;'F l': FRINT 460NEXT 443 '
AM FRINT: Y:CSR*.IN
- 50) CEF SE6:0: Fi.s E 13).FEi6 il(ED ' Clears kettoard Buffer 5.;3 ' Allow Chance of Fk, anj iaturation Values, anj storing of Results at this Tine 510 IWJi'EA6E VRRS 4.0 511 OLD OP.Ei (N/y)';AES 510 IF Eil:'y' (A mit:',' (R VI,LU,?.illOO Tr0 60cM 2000: LCGTE Y: FRINT SFA:El(50): UXATE t: 6070310 521
%3' ' Store in 'RK00L.VAI.' and Return to LINE 310 (seel.
- 0) ' Calculate tw Tran5ter o.st of Zones (t, fire water) 610 TIN:iFIFE.TR 620Fr/3 1:1101:ij.I5, TRf D: ikUEW(D: Ir.X{(D=l: QVAL(D:0: E0Ill(D:' *:NEIT 630 F@ I:1 TO IZ0*E5
(.s4 'Srancn ta A:crcerive ists> tine tued on value of IECE(D 655 OH IMIE(D Gri)E E,1255,1500 W' 637 TIN =TM: MR(D=iG:;T G IF Kilt:D:'5' TO (NR(14=t1-GEREFTi(WWD0iD*100 ' Calculate Quality 6 End of Zcne een acclicable 643NEIT 613 '"'Cniculate ni ail tercerature; 6c0 FOR I:1 TO !Z.::Ei
%) Gik: 0.iD/isXG.ilTirE 'Fest Transfer Irr5tde Tubes d; ring DELTATIE 60 ' Calculate beat irarifer PJG 20res fr.w Ambient 670 IF WT(D:0 TO WJiiD=0: 6070 600 ' Slin for norrEE5 Zones 6i0 TU: TUU+L60 630 IF I'UsTi.9 is (# Rill:0: 6070 800 %eclect Any Heat loss TO FGi FROM Zore 710 TE0LD: (i2thTU)/2
- initial Gueis of Temp. of Shroni 720 FRak SFJ>uTW102 + Ti40.0'2)*f TAMER +TW110) 730 hRiT= 5E5Ti(tim (UP2 +Tg2st(TM+TMr.t.0) 740 HA5: KAE6ai: R5T: HC57657 750 H0lF= 1/( 1/MS + 1/RiT ): fBJT(D: HOUTtWT(D*(TAER-TWLR) 760 T5EE: T*415 - Wi(D/S:2)i(DtWA5) ' Refined Guess of Teep. of Shroui 770 IF res(Tis-T!50LD)/T580LD).00ll TrG TMOLD: TS$: GOTO 720 780 730 ,' Con.eraence (Nck. If met, rimt ascunt of H.T. has been stored in Q0VT(D g; raji = (hji(Di36M.ELTATi5 'Edernal Heat Transfer during Time Interval 610 CELTATFJJ: (fhji-GIUl(M;.55(DACFSTEEl(D) ' Change in Wall Teecerature E20 TVKJll): TOD+:.ELT;iEG 'NewWallTemperatureforeachZone O) ! EXT g3;.r...
840 INTERVAL: INTERAl.+1
- - i; ',: *ici. E. . ; i r n si' M t Aj ame Oi,tsut Frebeno C.vter & Tise, t.e- se:e;- 04LC- "2~
670' s75 '111119)EEG! TINE 5 gra c e m e a A cia' Eii '52 routine for ;:-w tnat is tehavim as EC. (a Fossibly + EV + 94) FA IF inti)= TIN Te TGji:T:N: gin (1)=0:REilfN E 3oc 4 FJ f.LE;i: F4 ' t.:. EFT stores f.FE.DX!) Interal Keat Transfer Area that has rot ret been utilized Ei ' N;io,e 0: chat te:er;ture achievable by Ecoronizing is T97 or TR(1), whicN.er is lo.er 310 IF TAtt)>T9T TG TG)T: T9T ELSE TOR: TR(I) i20Tif.VG: 1 TIN +iG!i)/2
- 9) (E(= PGti10.:T-Tiu ': X Econ:eizi N achievable in Current Zone 940 fEC: GEC/6r.tlTA(1)-iJJ31) ' Area tnen reqJired for Max. econ,
- 9) if iGji: T9T TG 1010 M0 '.4t A lines nch if ::.ne can't toil the water, ie TR(!)(TEAT 970 iT AED =R ETT T 6 Gim i): (AC: FETiffi 371 ' tlf Area found in LINE 340 is less than Area lef t, rn wre Heat Tr. is possible.)
- 9) IGE: (RE:T14/12; 217A t i)-TIN 1+rGlilN)/(MCW+ REFT *HW/2) 330 GINf!): tGt(IOJT-TIN): FErnN 1% '
1010 '% on frce Nre il Zore is resibly tuilim the Fire Water, ie TR(1))T9T 1010 IF f.EC: REFT is ir0CE:2: F/R 1%0: GIN (!):GEC: RETl2 10M IF AECfREFT TO E.T01065 1040' Net 2liresaccirifZoneistoosmalltoachieveboiling 10M T0J = (RE;TtWl22GTA(!)-TIN)+rGtilN)/(MCV+ALEFT*W/2) 106) 0i51)= rattTG,T-Tim: RET.E 1070' 1@ 'Icne is tNn troeed boilim veter (ie AEC/ALEFT) 155 ECillt1)=T 'iet 'Estlinf Flag 1050ALEFT: REFT-tic: GEAE~i: W6trTAT 'Nx. Eoiling achievable 1100 (AV: REri!411 Tit l)-TC.T) 't0TE:TG1T:T9Tfrceearlier 1110IFIF 1120 @=GERETT GEVMAE;T TG 1170TG 15ZE:3: 609A 1560: rEAEFT:0: QiN(1)=rAC+t<EV:KEMN 1130 %t 3 Lines acch if Zons can't also start to suwrheat the steae 1140 14:CE 2: GES 1%) 11% GEAEFT: EAEFT-U: Gial): GEC+O ' .and T0lT:T9T 1160FEi% 1170 ' Zone is tNn swN+ ting tro 1180 ISIE:3: 9EE 1%) ' then all satse:uent ones also are! 11M 6: EaEFi: (EAE~i=0; :Ei: E//WEstiA(1)-T9T)) ' Area used to tott 120) RE;i: REFi-AEi ' Area a.lilitle for Sucerheating 1105 TOR:TAti): TMVi: tiMT+ TOR)/2 1210 Gin: r,C5t(T0)T-T97) 'inim Sucerheatir9 achievable in this Zone
!?20 fe: 49/(kMt!E(!)-TiR5)) ' Area tNn re44trej
[3) IF /&: REFT TO GIN:i): (AC+0EV+S: RETIM 1210 %t 2 lines accir if Area lef t is n:.t erouah to achieve sax.surerheatiN 1250 TGJi= tREFTiriS/2*GTAti)-19T)+r45179T)/(MCS+ REFT 1HS/2) 119) W : FI,52:7017-TSAT): 0i21): GEC+E+G: RETWI 1270' 1280 ' 1290 '9trcotina for Zae teha.is as EV. ( Ard Fossibly also as SH) !?i5 ECli.$tl)=T 'Eciling Flag for Outcut 1297 IF A T' (InTIN T6 Ei=iiN: GINf!):0: RETip % Heat Transfer Fossible! 13G) R EFT: f4EAINti): Ei: EAEFT ' Maxi u boiling achievable 1310TGA:T9T 'Trw if Zore is only evaporating; () sed as first guess 1320 AEV: Ei/SEttiR(1)-i9T)) . Area then reagired 1330 IF AEV: REFT TG CiNii):3: EAEFT=0: INCE=3: 60SUB 1500: RETLM IM0 IF i.Ei: REFT T6 0i01330
- 13) 'Next line an iss if Zoa is ret sucerheating at all
iii) ;Ev: .Erivis.il<l -Ti 7.: GiaE T:iERETT-GEV: 0!ht !)=Ei.EiiAN q>'( n 1I70' 1%0 '7N 20m is tNn t :ie] swerNattr9 tN steam " li-N IM0CE:3: 6:6.E 15(4: Ai. EFT = REF7-AEV: GGLETT: 0 'Used to calculate QUE(D
/HfA W 'E6T 14(4TM: TWUI): TiA6:i191+T0iT)/2 1410 G : P3iT00i-i!AT) 'N surerNattN '
g, 4 o ;- Y 1420A5h:Q!e/mit:T4.il)-T9'!5J ) .a4 Area rNutred ILM IF AiW:AEFT TO Ol!.ill:iEMiH: RETGN 1A13 '4t 2 ItN5 sesly if Area lef t is ret eNogn to achieve sax.swerNatiN IL50 TGJT= LEEFir4/21: 21 rA ( 1 )- T 9 T ) + <SI T9T ) / ( ES+ REFT *HS/2 ) 140 Qis: raiTM-TMT): QIm11: ENiet: RETWN 1470 ' l 1444
- l 1130 '9hrouttN for 2 ore that is swerheat N OfU 1500 IF IA(I): TIN TO TJ.iT: TIN: GIN (1)=0; RETSN % Heat Transfer Fossible!
195 T0ji: TV_(1): 197o= (IlWiWT)/2 ' First Guess - True if b. Superheat:N is esist.le 1510 GiH= KittTJ!T-Tills: Ai4: Gik/ Git (TA(11-ISAVG)) 1520 IF aim =491 Nil) TO Qimi): QIW: RETWN lim T0;i= (E9tMI)D6/ittitTa(D-TINJ+%51 TIN)/fK$+5 GIN (!)1HS/2) 1520 G= KitiTGli-Tim: Ga D=iiH: FETAN 1%0 ' 1564 ' 1570 ' Swr.:otice ta set re;ately 2cnes to ret Nsitble twe of tehavior 1530 F% J:1 TG IDM5: ICEU): IGE: TOT: ETGN 1537' 19?3*
!?is '9hr.witm to 5tcre W5 at tise=TitiE in EE5 Crit.VA 2%) NEN 'EEiyi.L!!E' FO: G.TFVT As t1 2010FEINTil. 'DM-V;i? IEi.- V41.TET.
N20 'JITEll, TIME: W. TiAi: HF3 -!NT.GT-EIT.GT-QUAITf' 20W FOR !=1 TO IDM5 in)FE:'r:1 MlW st, ua& 350 tal ,taat ts:titsettants,st.t"",tt.t"",844.es';l,T01'Til):rc( D:qlv i,:g;;i D su li 2(40 W4 Ell: FETJ.N 2?M ' 2?i7' 2353 '9hrwtim to store esi and area values 2 3 3 'h353fi. lea ius FAi5t t): 25728: WAi2): 112%:: 455:3): 1(4408: M%(4): 11132t M10 mms 5): 442i4: r#5i6): 1140 0: M55<7): 61974: M55(8): 595.34
!!!20 4%@: 2iMit: Fid5:10): 15C it: $ %(11): All4M: MSS (12): 46334 MMr4%il7):
M40 MM(13): 3E-:4: Pai5(14)= 75178: $55(15)= 5419fA: MSS (16)= 691.28 11E4: r;%;1D: 54174: M%t19): 16228: M%(20): 10'6 54
%50 Mi34.21)= 6M2.it: Miii22)= 7674.68: MSS (23): 10454: MSS (24): 7834.4 K40M5S(23):
370 M%i25): (2474: E55@= 12918: E3.2% M35(27): 13ht:910008MSS (28J: K40 ' Internal Nat Transfe; Areas. FT'2 F730 #EMN(1): 37.16: EEAl*2)= 134.5t: GEAIN(3): 250.20: E9INf 4): 172.64 5100 E 91* 5): 172.74: ESINf 6): 40.5%: EEAIN(7)= 685t: MEAIN(B): 118.H 3110 #UIN(9) 34?).23: MEAiml0): 38074: EDIN (ll): 31724: MEAIN(12): 4104 5120 M91N(13): X52D: E91:i(14): (44.5t: EEAIN(15): 812.94: 43. 4 MEAIN(16): 3130 E9iN(17): 1545: EDIN (18): 48.98: EDIN (19)= !!.78: MEA!N(20)= 75.18 3140 GGIN(21): 1(4 3: MEAL
- 22): 138.48: E EAINf23): 24.74: E S IN(24): 241.64 1150 E U IN(25):
5160 E G IN(29): 388l?S 54: MEAIN(26)= 62.78: MEAIN(27): 25.48: MEAIN(28): 357.48 3170 'bternal Heat Transfer Areas, FT'2 5130 FAT (9): 40.515: FAT (10): 44 t6: 31N FETI.7d A0Vi(ll): 56.34ts: A0UT(13)= 66.9416
CALC No 3 2-t O aEv SAGE l y . PROTO POWER CORPORATION oa,o:saron g, GROTON, CONNECTICUT cart
,;,g 4 g CUENT fgG PROJECT F4 V E Q. i SUBJECT A y.yp ( g EyT g. com fg g fggggy gEg gyg flt 16 Fl 0 Q Re N gs -
k .,. M M VM rae ueret m e,.gu (G?& (* D N Nb& ( P50'ed f
(#) O Co.om') (A.2 3%.S EGS. 3 IA G lo00. 0 (t) /0 76. f -n - -u- -i,- 999,9 6 O (/.om') 1o7.5 76l,6 /Go.1 16 6 917,6 40 0.54 119 7- 360. 0 (62.3 153 9 /9. 3 12 o (r.o d 12l,5 -o- -n. -.- 379.7, 15o (2.6 4 12 +,1 -n- ->i- -n- q u, i I f O U 3 m') 12 7.1 -ir - -n- _ , , . - a4 6 f.3 2Io(%) I21,3 -i,_ _ , , _ ._ n _._ 9 ( 2. 'l 24o (+.a Q lu.1 359.5 P6 t.1 i f2, 957.3 2?o (45 4 i So.4 351,o (63.3 Isi 947,1 !
(w) Boo (6.o Q 155,'3 _n- _n_ -n- 92P.I 33o(5.54 17t.2. 152,4 163.4 I5o f 9 2 ~*
~*~~
' Pean u 3(O(Gs0& SAMG ~l'~ ~ ll SOI'0 NoT* Es
'. Sio l'5Q 2. 2 4 1 . 359,0 (63,3 15; h t. 2. 400 254.8 %3.o 154.6 I59 7oI. l
CALC NO g 7-l Q AEv PAGE J, o, Z } PROTO POWER CORPORATION oscuron 9 , 7- ca r' GROTON, CONNECTICUT f l - 2 4 - f (* !
,,,,,,, ,c,,
9 g , j Q g 7_. CLIENT pyC PROJECT pgG gg, susaecr ggg ggg g ,
, G M P v T16 ( T(off M M RECU LT 5
- DME FLo ou Tse c h,4 hr M h<. T ww-4-2o (?.0,0 21 g, i K7.o f6o.5 157 45.3 45o ( Mm) 342 1 7co.o fs2,3 153 498.2.
(fo (f.O.) yg,4 359,5 fft,7 16 2- 4I0. 5 Sio ( r.s ,,d 37 r,3 754 + r67. 6 I5o % 9.7-54 o (9,o > ,) 656.1. 35l.4 161.6, I34- 3 5 f,4 97o (9.6 ) G fl. 2- 732.'l 984.4 I o 7- NA ("#[C (*)4co (80.0m) 129.4 7(?.9 /16,5 17 3 3 Z. 7-6 5o (io,s ,) 191.o '3 o 4. 9 9oG.5 72. 3 i ?. i 6 6 o (l'.o m) 906.) 110.5 9)7.) TP 4 o 4. 9 69o(it.4,) 100( . f 27 3,I 929.6 44 2 5'2. + 12o (12.om) lo 6M, 244.4 94 9,3 2+ 2 M, l (*) ll o 1149,o lo 7,o 91c 17,~4 198 9 "o "* aas u n c-y) _890 (IA.Sd .- -
- - I47.0 ' '[' (4) L ON P v16A. 79.4 d1ou TS F ott -t hec e vimes . APPEAfL ON 7HE 1~O L L O Lk.NG. PA 0 ES NOR : AHti 70 I IV TS M EN'TIoWEp OW THE PA t N70vT3 AtL E 7 tom g e r, 2 , DWvg- Mi/4 f2.-PF- 05 (4, -ol 3,u. I 4 2]
1" FitE: EEW.6t. 03,7 du (4&C F2-/C
-w!'.'- U FID- k(W)- EFS - E E- Ts - g . m w
p !*.. I: 1-4 ,10020. 1, 15.1,53.9,15000-4, 7.4, 1, 0) 0 m g D.8 g. 3 o s- 2 2 j 4-6 , 6.M5, 1, 8.3. 151.1.1.5000-4, 26.8, 1, 80.0,' m ,' g
) - 6-7 ,7.961, 1. 2.5, 61.4.1.50 @ 4, 0.5, 1, 60 0 m u 4 { 7 - 8 (1) , 7.670. 1. 50. 29.9.1.50@4, 0.0, 5, 403.4,' M ,' u 5 . 8 y (2) . 9.51o. 1. 386. 66.1,1.F/)0-4, 4.3, 5, 403.4 m'y 3, . 109 -10 (3), ,9.172.1.61.
9.172. 1, 2.7, 136.3.1.5000-4, -60.6, 5, 403.4,' M'M
-11 (4) 1.8, 94.2.1.5XO-4, -0.3, 5, 403.4' S : 11 -12 (5) , 3.152. 6. 12.8. 102.1.1.50 & d, 9.0, 5' 403 4' m'm M
9:12-18(6a),3150. 6. 1.16, 0.00,1.5000-4, 0.0, 5, 403'4 10: 18 -19 (6b), 3.34 6. 1.20, 26.20,1.5C @ 4,
~ m's M'
5, 403.4,' m*M 11:19-20(7),op>j.,. 108. 104.50, 500 80.8.2020-5, -4.6. 27.0, 5, 403~4' m it.20-21c6a),0.874.109. 0.01, 12.22,8.2020-5, 0.9, 5, 610.0' 4, m'u 13: 21 , 1.44,
-22 (60), 0 698. 3;4 000,8.2020-5, 0.0, 5, 610.0, m ml m 14., 44 -Q(8c), 0.@. 3 210.10, 26.02.8.2020-5, 2.3, 5, 610.0, m,m
- 15. g 4W9) , 0 ,ea. 044, 0.00,1172.80.6.202>5, 4.8, 5, 610.0, M ' ra
- 16. 4 A-24 (10), 0 724. 324. 000.1271.50.82020-5, 0.0, 5, 650'0' m'u 17:24-25(11),0550,324. 0.21.1621.70.8.2020-6, 2.7. 5, 760~0' u 18: 25 -M (12), 0.5M. in. 1.64,166.78.8.2020-6, 4.6. 5, 760.0, s, 19: a 4, (13), 0.5N. 32 , 0 00,1541.40,0.20 & 6, -3.3, 5, 730.0' m'm M'u p): 27 -N (14), 0 SM. 324. 2.60, 270.*0,8.2020-6, -11.0, 5, 730.0, m'M y , 28 o(151), 0 76.s. 108, 0.14. 15.31,8.2020-6, -0.9, 5,1000.0, m'M g:. 29 -30(156), 0.969.100. 2.25, 525.9).8.20 & 6, -27.0, 5,1000.0, m's p 24 -31 (16), a 9:t3, 44: 31-22(17),5.6M.
- 6. 1 27, 23.03,1.5000-4, 4.6. 5,1000.0' m'u
- 6. 2.7, 208.2.1.5000-4, 49 0, 5 1000 0' 25:J-32416a),9.566. 6. 32, 4.2,1.5000-4, 0 0, 5,1000 0, M ' '"3 N:w32E(16b), 9.h s't
- 3. 0.3. 16.0,1.5000-4, 0.0, 5'1000 0 m'M 47:325-33 (18c) 9.5%, 2. 0.1, 4.2,1.5000-4, 0.0, 5,1000.0, M'M 28.g>-13419a),10 620. 2. 03, 2.8.1.5000-4, 0.0, 5,1000.0, m'm 29:m-34 (150),10.6cv. I 5. 0U. 1.8.1.5000-4, 30: 34-34420a),10.63.15. 0.6, 1.8.1.50 @ 4, 0.0, 5,1000 0' m'M 31:34A-346t20b),1083.1.2. 1.7, 13.4,1.5000-4, 0.0, 5,1000'0' M'M 32:348-15 (20c) 10.820. 06, 0.0 510000' M ' r*
0.0,'
- 1. 14.2.1.5000-4, 5'10CO.0' m ' tk
): 35 - % (21), S X 6. 2. 3.0, 376,1.5000-4, ;d; 9,'-2229. 5.6N. 00, 0.0, 5 1000 0' M ' la i: a -a (22),11.520.
2 0.0.1.5000-4, 0.0,8,'1000l0,2990'09 35 36: 29 -40 (231.10.!!4.
- 1. 1.5, 05.
47.6.,1.5000-4, 11.1,1.50 @ 4, 0.0, 5 10u0 0 18.8. 5,'1000 0 5's 07: 40 -41 (243,12.5M. 1. 1, 2.3, m ' 'a 70.9.1.5tXO-4, 15.7. 5,1000'0' m M
,j 4 (25).14.312.
(26),21.564. 1, 1, 1.9. 05, 40.1.1.5000-4, 3.7. 5,1000.0, M ,' m v 6 2.1.5000-4, 11.1, 5,1000.0' m'u 40: 43 -44 (27),21.562. 1, 1.6, 2.5.1.50 @ 4, 4.5, 5,1000'0' M ' a 41: 44-Fil (28),14 ixc- 1, 1.1, 12.9.1.5000-4, 13.0' 5'1000'0' M'm 42:FTI-FT2(29a),9.M2. 0.7,
- 1. 13.6.1.5000-4, 6.0, 5,1000'0' M'M 43:FT2-FT3(29b), 7 652. 1, 1.4, 8.7.1.5000-4 0.0, 5 0 M M
' . .1 4 0.0,8,'1000[0,'t363.0,'l.0 1000 45: f,5254 , o 652, 1, 0.0, 0.0,1.5000-4, 0.0, 8,1000.0,3040 0' 1 0 46: FT3-f74 ,7.981. 1.7, 18.7,1.5000-4, 47: FTA-FT5
- 1. 1.6, 5,1000.0 M m 11.%8. 1, 1.3, 14.0,1.5000-4, 0.0, 5,1000.0, m,m M 's isMoz rrr Mrs m.e awn. A c r w z:v es '
ras awa a as swwa oa n. cuawcadr m-s at YH/S CALCUL47?d$ 88& P7' 7%4f7' 7W 7=%fp p 1T M P 5 2 477(2 E3 MSEZ;> 62E AC .cWWit/ nt/ r#f , ABWf F/4.F. 72f M #2 EDn~02/M Cw d 7f* wUS M7 EFFEC.:r 7yd' 26srL71 8F 7%.c d 44 CRl.4'r// d,
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4
\
FLOW = ss 2 6 Fit fJ 12: USE Ft n O A E KK E C B F EiiGE1 (Y/Wl:Y? FIf{ WATERf =1), CGCEGIE(=2) OR IACi(=3) N: 1 ? l Fi.N(5) AREA */E1E;iT (fjE=0 - FELLEL=1 - 56iE5:2): 0 ? g P.i # FELTON FEEL FLOW = 125 GW FUA 4 F1# = 69.20 ffM Ai 1(6
& HEM =112.88FT/ Stale FILE;EEVIII.0AT - N). F SEUFlii: 48 - TWi-FHAE SECTIONS'OIVIDER: 10 ECTION 10 L FLO'J F(IN) F(Ol#)
1: 1-4 10.020 15 9 M.CO) 158 0 157.1 2: 4-6 6.M5 10 0 34.600 157.1 It5.9 3: 6-7 7951 24 34, 9 ) 145 9 145.8 4: 7-8(1) 7.870 5.3 34.600 115.8 143.8 M:IN=0.057 OUT4.058 5: 8 - 9 (2) 9.5!6 1:.7 34.fi/> 144.0 138.2 M:lN=0.039 OUT4.041 6: 9-10(3) 9.172 2.9 34.600 138 2 137.7 M:IN=0.044 G R=0.044 7 : 10 -11 (4) 9.172 1.8 19.116 137 8 137.7 M:IN=0.025 O R=0.025 8:11-12(5) 3.152 12.2 5.767 137.4 132.9M:IN=0.063 GR4.065 9 : 12 -18 (6a) 3 150 06 5.767 !?2 9 172.7 M:IN=0.065 OR=0.065 10: 18 -19 (6b) 3.346 1.1 5.767 112.8 132.5 M:I M .058 O R 4.058 11: 19 -20 (7) 0 W .115 2 320 132.6 109.7 M:lN=0.046 OlR4.055 12:20-21(83) 0.874 0.3 310 109.7 109.6 M:IN=0.063 OUT4.063 u FTESS (Cio TO C0 JIM.E 42
~
SECTEN 10 K Fi/M F(IN) F(0UT) ' 13: 21 -22 @ ) OE38 0.7 107 109 8 109.7 M:lN=0.020 GR=0.020 14: 22 -23 (Sc) 0.724 210.2 107 103.7 94.4M:IM.031OUT4.036 15: 23 -23A(9) 0.724 30.1 107 944 92.0M:I M .036 0UT=0.037 16: 2 h' il (10) 0.724 12.7 101 92.0 f4.3M:IM.037 OUT=0.039 17: 24 -25 (11) 0.59 134 107 83.1 77.0 M:lN=0.070 G R=0.061 IS:25-26(12) 0.5M 4.4 107 77.1 76.0 M:IM.070 OUT4.071 19: 26 -27 (13) 0.5 N 13.4 107 76.0 67.2M:IN=0.071OUT=0.000 20 27 -28 (14) 0.5M 7.2 107 67.2 65.1M:IN=0.000OUT=0.082 21:28-29(15a) 0.768 04 320 64.5 64.0M:IM.163 OR=0.164 22:29-30(15b) 0.969 !!.9 520 646 59.0M:I M .102 OUT=0.ll2 23: 30 -31 (16) 3.803 1.1 5.767 58.8 58.1 M:!N=0.131 G R=0.133 24: 31 -32 (17) 5.626 4.9 5.767 58.4 57.8M:IM.056 OVT4.057 25: 32-?2At18a) 9.5i6 30 5,767 57.9 57.9M:IM.021OUT=0.021 26:32A-32S(lib) 9.5.% 06 11.533 57.8 57.8 M:I4=0.042 0 R 4.042 27:32&33 (18c) 9.5!6 01 17,300 57.7 57.7 M:lN=0.063 OR=0.063 28: 33-33A(19a) 10.620 0.3 17.300 57.7 57.7 M:IM.050 OUT4.050 29:33A-34 (1%) 10 820 03 23,067 57.6 57.6 M:IM.066 DR=0.WA ' 30:34-34A(20a)10E20 0.3 23.067 57.6 57.5 M:I M .066 G H 4.066 31:344-348GA)10820 0.5 28,833 57.4 57.3 M:IM.063 OlR=0.083 32:345-15 (20c) 10.820 0.6 34.600 57.2 56.9M:I M .100 G H=0.100 33: 35 -36 (21) 5.826 2.7 17,300 56.2 52.9 M:IM.175 0UT=0.186 u FRESS (CR) TO 0 %Ilu.E 44
ETir;; (ALC !] _I:_ 10 k FLr# F(lo RM) 34: Fv-7??3 5626 00 17.300 51.9 330Wcr= 17,356 35: 74 -39 L22) 11.540 1.4 A-r T' 6 P. 5 * # 2 34.600 33.9 32.7 M:!M.150 M:0.163 36: 39 -40 (23) 10.114 0.4 34,600 32 4 32.1 M:I M .202 M =0.204 37: 40 -41 (24) 12.50) 2.2 34.600 32.4 31.6 M:l* 0.132 M 4.135
'f: 41 -42 (25) 14 312 1.5 34.600 31.7 31.4 M:l*0.103 M=0.104 39: 42 -43 (26) 21.562 0.1 34.600 31.5 31.5M:!*0.046OVi=0.046 40: 43 -44 (27) 21.562 0.0 34,E40 31.5 31.5 M:I* 0.046 M =0.046 41: 44-Fil(28)14.000 0.7 34.600 31.3 31.1 M:!
- 0.109 M 4.110 l 42:Fil-FT2(294) 9.562 05 34.600 302 29.5M:l*0.241OUT=0.247 i
13;Fi2-FT3(19b) 7.652 0.7 44: V-52:43 34.600 27.6 24.9 M:IM.409 OUT4.451 7.652 0.0 34,600 249 24.3 Vcr= 130.038 LS: HV-5252 7 652 0.0 34,600 24.3 22.8Wcr= 88,075 46: FT34T4 7.951 0.8 17: FTifi5 11.938 1.0 34.600 23.5 14.6 M:l*0.522 M =0.695 34,600 17.0 16.1 M:!*0.274 OUT4.291 46: FT54T5A 11.9E 1.0 17.300 16.5 16.3M:IM.142OUT=0.144 2t FE59fE AT D4) ff 5YSTEM = 16.5 F51A FEFEAT WITH IEW 010171% (Y,lJ)?
(A ' C E?-10 TIME: 0 fiC5: 0.0v hie (FLO.= 100 fin-IMT= 327 F- 0 M)RE) D:st 1: T- VIR= 403 Af ) R: 403.4 - c cINT: 0 @00 EIT= 0 00+00 Ar' & I S ** O ME 2: T- VIR= 403.4( ) R= 403 4 - Q- INT: 0 @ 00 EIT= 0.00+00 ME 3: T- Vi;= 403 Af 1 R= a)3.4 -- (c INT: 0.00+00 EIT: 0.@00 M E 4: T- VTR= 403 4( ) R= 203.4 INT: 0.00+00 EIT= 0.00+00 ME 5: T- G: 103.41 ) R= 103.4 - Q- INT: 0.00M EIT: 0.00+00 ME 6: T- VTR= 4)3.4( ) R= J)3.4 c - e INT: 0.@00 EIT= 0 @00 NE 7: T- VTE: 403 at ) E= 403.4 IWi: 0.00+00EIT=0.000 DJE 8: T- G= 610.0( ) R: 610.0 INT: 0.@00 EIT= 0.00+00 M E 9: T-Vi;=6100( ) R= 610 0 INi: 0.00+00EIT=0.00+00 D)E 10: T- G: 650.0( ) E= 650.0 INT: 0.00+00 EIT= 0.00+00 NE 11: T- WTR= 7M.0t ) R: 70.0 IhT: 0.00+00 EIT= 0.00+00 ME 12: T- VIR= 760.0f ) R: 760 0 - Q- INT = 0.@00 EIT= 0.00+00 ME 13: T- Vi;= 730 Of ) R= 7N 0 - Q- INT: 0.00u)0 EIT: 0.00+00 DIE 14: T- VTR= 730.0( ) R: 720.0 - Q- INT: 0.@00 EIT= 0.00+00 ME 15: T- Vi;=1000 Ot ) R=1M 0 -- Q- INT: 0.00+00 EIT: 0.00+00 FSESS (CD TO G.ilMI. ME 16: T- Vi;=1000.0f ) R=1000.0 INT: 0.00u)0 EIT= 0.00+00 ME 17: T- VIR=106).0( ) E=1M.0 INT = 0.00+00 EIT= 0.00+00 NE 18: T- VIR=lM.0
) E=l@ 0 - Q- INT: 0.00+00 EIT: 0.00+00 NE 19: T- VIR=l@.0( ) R=1000.0 INT = 0.00+00 EIT= 0.00+00 NE 20: T- VTR=1000.0( ) E=1M.0 t - i- INT: 0.@00 EIT= 0.@00 ME 21: T- VTE=lM.0( ) R=lM.0 - fe INT: 0.00+00 EIT= 0.00+00 NE 22: T- hisf 1000 0( ) R=lM 0 INT: 0.00+00 EIT= 0 00+00 ME ME 24:23: T- VIE =iM0( ) E=1000.0 ihT= 0.00*)0 EIT= 0.00+00 T- VIE =1000 0( ) E=lM.0 INT: 0.00+00 EIT= 0.00+00 NE I5:
IfSE26: T- VIE =1000.0( ) R=lM.0 - fr- INT = 0.00+00 EIT= 0.00+00 T- VIR=1000 Of ) R=1000.0 - Q- INT: 0.00+00 EIT= 0.00+00 ME 27: T- VIE =1000 0( ) R=l@.0 - Q- INT: 0.00*)0 EIT= 0.@00 NE 28: T- VTA=1000.0t ) R=10':0.0 INT: 0.00u)0 EIT= 0.00u)0 ME 29: T- VIR=1000.0( ) R=1000.0 INT = 0.00+00 EIT. 0.00+00 FLfA A TE W M): 100 ? 69 2 fAitMTION TEtt (MF): 327 ? 1 % .3 RAT OF EVMf#ilfE 15iWLEa): 888.8 ? f/,5.3 I
in FhE: EEEG. D tu ' igil.?, - 10 DIV- UFil)- MVW- Eis - E!. -Fl..- IF - MIN - f,4
. r' "a -' "C~ ~
48 1: 1-4 .10 @ . 1, 5.88, 522.1.1.5000-4, 2.1, 1, 80 0, 2: 4-6 , 6.ri5. 1, M.M /tr* 8 7, 7 ' # 2 3.37, 292.7.1.5000-4, 25.9, 1, 80.0, M,M 3: 6-7 ,7.981, 1, 091, 61.4,1.50&4, 0.2, 1, 80.0, 1 M,E 4: 7 - 8 (1) , 7.870, 1, 4.9, 30.1.1.5000-4, 0.3, I, 140.!, M,M 5: 8-9(2),9.516. 1, 37.8, 597,1.5000-4, 4.3, 2, 356.3,0.0000,0.0415 6: 9-10(3),9.172. 1, 0.98, 136.3,1.5000-4, -60.6, 2, 356.3,0.0415.0 3 02 i 7 : 10 -11 (4) , 9.172.1.81, 0.42, 942,15OFA, -0.3, 2, 356.3,0.3202,0.5127 8 : 11 -12 (5) , 3.152, 6, 10.4, 102.1.1.5000-4, 9.0, 2, 356.3,0.5127,0.6162 9 : 12 -18 (6a), 3.150, 6, 0.62, 000,1.5000-4, 0.0, 2, 356.3,0.6162,1.0000 10: 18 -19 (Eb), 3 346, 6, 0.59, 26.20,1.5000-4, -4.6, 2, 356.3.1.0000,1.0000 11: 19 -20 (7) , OR6,106,104.30,195.30,8.2020-5, 27.0, 5, 372.4, M,M 12: 20 -21 (Sa), 0 874.108, 0.01, 12.2.8.2020-5, 13: 21 -22 (Sb), 0 8% 324, 0.72, 0 00,8.2020-5, 0.0, 5, 430.7, 0.9, 5, 430.7, M,M M,M 14: 22 -23 (Sc), 0.724, 324, 209.50, 26.0).8.2020-5, 2.2, 5, 430.7, M,M 15: 23 -2M(9) , 0 724. 324, 0.00,1184.30,8.203-5, 2.3, 5, 607.4, M,M 16: 2 M-24 (10), 0.724, 324. 0.00,1283.00.82020-5, 2.5, 5, 649.4, M,M 17: 24 -25 (11), 0 550, 324, 0.21,1818.00,8.2020-6, 2.7, 5, 759.0, M,M 18: 25 -26 (12), 0.5 % . 324, 0.77,166.80,8.20&6, 4.6, 5, 759.7, M,M 19; 26 -27 (13), 0.5M. 324, 0 0),1540.10,8.2020 4 , -3.3, 5, 730.3, M,M 20; 27 -28 (14), 0.590, 324. 1.34, 270.10.8.2020-6, -!!.0, 5, 730.0, M,M 21: 28 -29(15a), 0.768,108. 0.12, 15.30.8.2020-6, -0.9, 5, 981.0, M,M 22: 29 -30(15b), 0.569,108, 1.48, 525.60.8.2020-6, -27.0, 5, 981.0, M,M 23: 30 -31 (16), 3.M3. 6, 0 66, 23.00,1.5000-4, 24: 31-32(17),5.826. 6, 4.6, 5, 983.2, M,M 1.26, 208.2.1.5000-4, 49.0, 5, 989.3, M,M 25; 72-32M18a), 9 566. 2.3, 26:32A-32S(lEb), 9.5M.
- 6. 4.2.1.5000-4, 0.0, 5, 990.7, M,M
- 3. 0.3, 16.0,1.5000-4, 0.0, 5, 990.7, M,M 27:125-33 (18c), 9.5%, 0.04, 28: 33-1M(19a),10R0,
- 2. 4.3.1.5000-4, 0.0, 5, 990.7, M,M
- 2. 0.3, 2.8.t.5000-4, 0.0, 5, 991.0, M,M 29:3M-34 (196),10X0.1.5, 0.3, 2.8,1.5000-4, 0.0, 5, 991.0, M,M 30: 34-34420a),10.820,1.5, 0.0, 31:344-34St200),10 820,1.2.
18.0.1.5fx0-4, 0.0, 5, 992.8, M,M 0.3, 13.4,1.5000-4, 0.0, 5, 992.8, M,M 32:348-35 Gk),10 820, I, 0.42. 14.6.1.5000-4, 0.0, 5, 992.8, M,M 33: 35 -26 G1), 5K6. 2, 2.12, 38.1,1.5000-4, 0.0, 5, 994.6, M,M 34:FV-2229 , 5 RS. 2. 00, 0.0.1.5000-4, 0.0, 8, 994.6, 299.0, 0.9 15: 26 -39 G2).ll.540, 1, 0.7, 47.6,1.5000-4, 0.0, 5, 996.4, M,M 36: ?3 -40 G3) 10.lli, 1, 0.2. 37: 40 -41 G4).12.500, 11.1.1.5000-4, 18.8, 5, 996.6, M,M 1, 1.2, 70.9.1.5000-4, 15.7, 5, 998.4, 38: 41 -42 G5),14.312. M,M 1, 0.9, 40.1,1.5000-4, 3.7, 5, 999.0, M , M'
?3: 42 -G G6),21.562. 1. 0.0, 6.2.1.5000-4, !!.1, 5, 999.2, M,M 40: 13 -44 (27).21.E62. 1. 0.0, 2.5.1.5000-4, 4.5, 5, 999.2, 41: 44-Fil GS),14.M, M,M 1, 0.52, 12.9,1.5000-4, 13.0, 5, 999.8, 42:FTI-FTIG9a), 9 562. M,M
- 1. 0.34, 13.6.1.5000-4, 6.0, 5, 999.8, 0;FT2-FT3G9b),7652, M,M 1, 0.52, 8.7.1.5000-4, 0.0, 5, 999.8, 44: V-52989 ,7.652, M,M 1, 0.0, 0.0.1.5000-4, 0.0, 8, 999.8,4363.0, 1.0 45: kV-5252 ,7.652, 1, 0.0, 0.0,1.50(&4, 0.0, 8, 999.8,3040.0, 1.0 46: FT3-FTA ,7.981, 1, 0.47, 47: FTA-FT5 ,11.338, 18.7,1.5000-4, 1.6, 5, 999.8. M,M 1, 0.8, 14.1.1.5000-4, 0.0, 5, 999.8, 48: FTS-FT5A 11.938, 2, M,M 1.0, 0.0,1.5000-4, 0.0, 5, 999.8, M,M i
l
FL(q = 75.6 F M A 1 5 ' #l USE FIN CWW [% EkTE3 UEGAE) (Y/N):Y? FIRE WATER (=1). CMOGIE(=2) OR IACM(=3) FlN: I ? Ayr8 FWFiS) Ai6,%EiOT (GE=0 - FARALLEL:t - SERIES =2): 0 ? ' f, 8 08 2 3 FEl. TON WEEL FLOW = 13 En? FLOW 6 Fin = 75 E0 En A7100F rW FGO =112.73FT/$iASE FILE:EE!Ufl.0AT - NO. CF ECTims: 48 - T@fMSE SECTIONS'OlVIDER: 10 SECTION 10 L FLOW F(IN) F(0UT) 1: 1-4 10 020 16 6 37,900 157.8 156.9 2: 4-6 6E5 9.9 37,900 156.9 145.7 3: 6-7 7.961 23 37,900 145.7 115.6 4: 7 - 8 (1) 7.570 55 37.900 145.6 115.5 5: 8 - 9 (2) 9516 368 37,900 It5.5 144.8 I:l* 0.00 OR= 4.15 6: 9-10(3) 9.172 3.3 37,900 144.8 145.6 I:I k 4.15 0UT= 32.02 7 : 10 -11 (4) 9.172 2.2 20,939 145.6 115 6 I:l*32.02 OUT= 51.27 8 : 11 -12 (5) 3.152 12.5 6.317 145.6 113.01:1551.27 OUT= 61.62 9:12-18(6a) 3.1% 06 6,317 113.0 142.6 I:IMI.62OlR=100.00 10: 18 -19 (6b) 3.346 1.1 S.317 142.4 142.1 I:!* Il00.00 O R=100.00 11: 19 -20 (7) 08861151 351 141.9 117.0 M:l*0.046 0VT=0.056 12: 20 -21 (8a) 0.874 0.3 351 117.0 !!6.9 M:I M .059 OUT4.059 u FRESS (CFJ TO Cf.EilVI u 5ECTim 13 k FLOW F(IN) F(0UT) 13:21-22'Sb) 0.656 0.7 117 !!7.0 117.0 M:l>0.019 GR=0.019 14: 22 -2318c) 0.724 210.1 117 116.9 102.8 M:IM.029 OUT4.033 15:23-2M(9) 0.724 23 7 117 102.8 100.2 M:IM.03600T:0.037 16: 23A-24 (10) 0.724 32 4 117 100.2 97.2M:I*C.038OUT=0.039 17:24-25(11) 0.59 38.7 117 97.0 83.9M:150.070OUT=0.081 IS:25-26(12) 0.59) 4.3 117 84.0 82.8 M:!M.071 OUT4.072 19:26-27(13) ) 590 32.8 117 82.8 73.3M:1>0.071 OR=0.080 20:27-28(14) 0.59) 71 117 73.3 71.1M:IM.080 OUT=0.083 21:28-23t15a) 0.768 0.4 351 70.4 69.9 M:I M .162 GR=0.163 22: 23 -30(156) 0. % 9 11.7 151 70.4 64.6M:Ib0.102 OUT4.!!! 23: 30 -31 (10 3V>3 1.1 6,317 (44 63.6 M:l* 0.130 GR=0.132 24: 31-32(17) 5.826 49 - 6.317 63.9 63.3 M:IM.056 0UT4.057 25: 32-32A(18a) 9.9A 3.0 6.317 63.3 63.3 M:15 0.021 GR=0.021 26:32A-32S(lib) 9.566 0.6 12.633 63.2 63.2.M:IM.042OUT=0.042 27:326-33 (18c) 9.5E6 01 18,950 63.1 63.1 M:!M.063 0UT=0K3 28: 33-3M(19a) 10.620 0.3 18,950 63.1 63.1M:!M.049 OUI 4.049 29:3M-34 (19b) 10.820 03 25,267 63.0 63.0M:IM.0660UT=0.0fA 30: 34-344(20a) 10.820 0.3 25,267 63.0 62.9 M:IM.066 0UT4.066 31:34A-34B(20b) 10.820 0.5 31,563 62.8 62.7M:IM.083GR=0.063 32:348-15(20c)10.620 06 37,900 62.5 62.3M:Ib0.100OUT=0.100 33:35-36(21) 5.826 2.i 18,950 61.5 57.9 M:IM.175 0154.186 u FfESS (CR) TO OMINI u I l
)
SECfiON 10 k FL@ Fi!U A0VT) (m c ~;.,m
~
34:FV-liis 5.F;16 0.0 16,950 S79 36.3Wce= 19,090 - 35: 36 -39 (22) 11.540 1.A 36: 39 -40 (23) 10.114 0.4 37,900 37.4 36.1 M:!N=0.149 OUT=0.152 ATf. b p. 3 or: 2$ 37,900 357 15.3M:IM.200OR-0.202 37: 40 -41 (24) 12.500 2.2 37.900 15.7 34.8 M:lN=0.131 OUT=0.135 38: 41 -42 (25) 14.312 1.5 37,900 15.0 34.6M:IM.102OUT=0.103 ! 39: 42 -13 (26) 21.562 01 37,900 34.7 34.7 M:!M.045 0UT=0.045 ! 40: 43-44(27)21.562 0.0 37,900 34.7 34.7 M:IM.045 05:0.045 41: 44-Fil(28)14.000 0.7 37,900 34.5 34.3M:IM.1060VT4.109 42;Fil-FT2(29a) 9.M2 0.5 37,900 33.3 32.6M:I M .240 GR=0.245 13:FT2-FT3(29b) 7.652 0.7 3 7 , 96) 0 30.5 27.6M:I M .406 0UT=0.447 14: V-52989 7.652 00 37,900 27.6 26.9 Wcr= 144,362 45: W-5252 7.652 0.0 37,900 26.9 25.3Wcr= 97.851 46: FT3-FTA 7.981 0.7 37,900 26.0 16.7M:lN=0.513OUT=0.666 47: FTA-FT5 11.E 1.0 37,S)0 19.3 18.3M:lN=0.265OVi=0.280 48: FT5-FT5A II.M 1.0 18,950 18.8 18.5M:I M .137 OR=0.139 41 FRES9.EE AT EM) 0F SYSTEM = 18.8 F5IA REFEAT WITH EV 0:GITIO6 (Y/N)? 1
Tiri: 10 sci: 017 mi [FLD 69.2 6FM-TMT= 356.3 F- 0 NORD CAL ( [2-IO a t 1: T- ViR: 200 2( ) R: 364 3 - Q- IhT: 4.20+06 EIT= 0.000 AW. 3 P 'O e F 2 DM 2: T- WTR: 3%.3(B) R= 383.5 INT: 6.60+06 EIT= 0.00+00 - I: 415 l NE 3: T- VIR= 156.3tE) R= 389.7 thT: 8.30+06 EIT= 0.00+00 - != 32.02 N E 4: T- b7R= 1%.3(B) ht: 2.7 - Q- INT: 5.D06 EIT= 0.00+00 - I: 51.27 DM 5: T- VIR= 156.3fB) R= 379.7 IhT: 3.10+06 EXT = 0.00+00 - I: 61.62 ZGE 6: T- VTE: 1%.3(E) R: 377.! INT: 8.50+05 EIT= 0.0M0 - != 64.46 D M 7: T- VTE: 372.418) R= 383.3 - Q- INT: 1.10+07 EIT= 0.0040 - I:100.00 i ME 8: T- VTK: 430.7( ) R= 571.5 INT: 1.@06 EIT= 0.00+00 ZOE 9: T- ViR: 607 il ) R: 607.4 - Q- INT: 3.10+06 EIT= 0.000 i DM 10: T- VIR= 643.4( ) K= 649.4 - Q- INT = 7.30+05 EIT= 0.0M0 29E 11: T- Vi;= 759.0( ) R 759 0 - Q- INT: 1.90+06 EIT= 0.00+00 ME 12: T- WIR= 759.7( ) R= 760.0 INT = 1.30+04 EIT= 0.00+00 20E 13: T- VTR= 730.3( ) R: 730.3 IhT=-5.!M5 EIT= 0.00+00 ZGE 14: T- WTR= 7M.0( ) R= 730.0 - Q- INT =-5.60+03 EIT= 0.@00 ZGE 15: T- VIR: %1.si ) R= 981.0 IhT= 4.3066 EIT= 0.00+00 4 ESS (CR) TO DATINUE. ME 16: T- VTE: %).2( ) R: 999.4 INT: 3.60+04 EIT: 0.0040 ME 17: T- VTR= 989.3( ) R= 999.9 - Q- INT: 1.10+05 EIT= 0.0M0 20E lE; i- VIR= 950.7( ) R=100).0 IhT= 2.40+04 EXT: 0.@00 ZGE 19: T- VTE: 931.0( ) R=1000.0 INT = 5.30+03 EIT= 0.0040 20E 20: T- VTE= 972.8i ) R=1000.0 INT: 3.00+04 EIT= 0.0M0 ME 21: T- VTK: 994.6( ) R=1000.0 - Q- INT: 3.10+04 EIT= 0.0M0 20E 22: T- VIR: 9M.4f ) E=1000.0 - Q- IhT: 3.10+04 EIT= 0.00+00 DM 23: T- VTE: ?)6.6( ) R=1000.0 - Q- INT = 4.3043 EIT= 0.0040 ZONE 24: T- VTR: 998.4( ) R=1000.0 -- Q- INT: 3.00+04 EIT= 0.00+00 Z9E 25: T- WTR= 93.0( ) K=1rX0.0 INT = 1.2D+04 EIT= 0.@00 IfM 26: T- VIR: 999.2( ) R=1000.0 INT: 2.60+03 EIT: 0.0M0 DM 27: T- b7R= 999.2l ) R=1000.0 INT: 9.90+02 EIT= 0.00+00 ME 28: T- VTE: ?M Bi ) R=1000.0 INT: 8.@03 EXT = 0.00+00 ZGE 29: T- b7R: 999 8( ) R=K00.0 INT: 4.30+02 EIT= 0.00+00 FLOW RATE (GFM): 692?758 SATISATION TEMP. Wg F): 1%.3 ? KAT OF EVriffATION (BTWLE=i): 665.3?
N la. C E[-13 Arr 8 p, 11 oF 2 ~' tu FILE: EEDXLCAT 24 SECil0N WlV- k(FII)- HVATO- EF5 - EL -fl.- TF . MIN - MI 48
- 1-4 .10020, 1, 5.68, 522.1,1.%A4, 2.1, 1, 80.0, M,M
- 4-6 , 6.(f.5, 1, -3 37, 132.7,1.5000-4, 25.9. 1, 60.0, M,M
- 6-7 ,7.551, 1, 091, 61.4,1.FG4, 0.2, 1, 60.0, M , M-
- 7 - 8 (1) , 7.870, 1, 49, 30.1.1.5000-4, 0.3, 1, 80.4, M,M
- 8 - 9 (2) , 9.5:6, 1, 37.6. 59.7,1. % F 4, 4.3, 1, 89.5, M,M
- 9 -10 (3) , 9.172, 1, 0.E 136.3.1.%&4, -60.6, 1,124.1, M,M
- 10 -11 (4) , 9.172,1.61, 0.42, 94.2,1.F44, -0.3, 1, 174.7, M,M
- 11 -12 (5) , 3.152, 6, 10.4, 102.1,1.5 4 4, 9.0, 1,209.5, M,M
- 12 -18 (64), 3.150, 6, 0 62, 0 00,1. % F 4, 0.0, 1,222.4, M,M
.': 18 -19 (66), 3.346, 6, 0.59, 26.20,1. % F 4, -4.6, 1,222.4, M,M
- 19 -20 (7) , 0.6E4, 10i 104.30, 495.30,8 2020-5, 27.0, 1,240.2, M,M
.:20-21(Ea),0874,108, 0.01, 12.2,8.20&5, 0.9, 1,256.7, M,M >: 21 -22 (6t) 0.618, 324, 0.72, 0.00,820&5, 0.0, 1,256.7 M,M 6: 22 -23 (8c), 0.724, 324, 209.50, 26.4),8.2020-5, 2.2, 1, 256.7, M,M i:23-3(9),0.724,324, 0.0).ll64.30,8.2G5, 2.3, 1,293.2, M,M 6:23a-24(10),0.724,324, 0.00,1263 00,8.2010-5, 2.5, 1,341.8. M,M ': 24-25(11),0.550,324, 0.21.1616.00,8.20&6, 2.7, 2, 359.0.0.0000,0.0068
- 25-li(12),0.590,324, 0.77,16660,8.2020-6, 4.6, 2, 359.0.0.0068,1.0000
.$ : Ei-27(13),0.590,324, 0.4).1540.10,8.2020-6, -3.3, 5, 439.5, M,M 1: 27-28(14),0590,324, 1.34, 270.10,8.20 & 6, -11.0, 5, 582.6, M,M 1: 28-29t15a),0.766,108, 0.12, 15 'A,8.2020-6, 4.9, 5, 666.5, M,M 2: 29 -30(156), 0 969, 108, 1.43, 525.60,8.2020-6, -27.0, 5, 666.5, M,M 3: 30 -31 (16), 3 F;3, 6, 0.64, 23.00,1544, 4.6, 5, 673.3, M,M 4: 31-32(17),5 Sit, 6, 1.26, 208.2.1.5000-4, 49.0, 5, 721.0, M,M 5: 32-32R(IBa), 9.564, 6, 2.9, 4.2,1.5000-4, 0.0, 5, 735.8, M,M 6:32fc32S(Ift), 9.566, 3, 0.3, 16.0,1 5 4 4, 0.0, 5, 735.8, M,M 7:328-33 (18c), 9.566, 2, 0 04, 4.3,1.9.10-4, 0.0, 5, 735.8, M,M 3: 33-33A(19a),10.620, 2, 0. 3, 2. 6,1.F;00-4, 0.0, 5, 739.4, M,M 3:33A-34 (15b),10.820,1.5, 0.3, 2.8,1.'Blei, 0.0, 5, 739.4, M,M 0: 34-34AG0a),10.820,1.5, 0.0, 16.0.1 S & 4, 0.0, 5, 761.1, M,M L:34A-342(ifh),10.6'20,1.2, 0.3, 13.4,1.F44, 0.0, 5, 761.1, M,M 2:348-35 (20c),10.620, 1, 042, 14 6,1 5 4 4, 0.0, 5, 761.1, M,M >: 55 -36 (21), 5 K 6, 2, 2.12, 38.1,15000-4, 0.0, 5, 784.5, M,M 1: FV-2229 ,5.626, 2, 0.0, 0 0,1.5XO-4, 0.0, 8, 784.5, 299.0, 0.9 5: 36 -39 (22),11.540, 1, 07, 47 6,1.F44, 0.0, 5, 811.9, M,M 1 ,: 39 -40 (23),10.114, 1, 02, 11.1.1. 9 & 4, 18.8, 5, 816.0, M,M ': 40 -41 (24),12.500, 1, 1.2, 70.9,1 5 4 4, 15.7, 5, 849.7, M,M s: 41 -42 (25),14.312, 1, 0.9, 40.1,1 5 4 4, 3.7, 5, 872.0, M,M ): 42-13(26),21.562, 1, 00, 6.2,1.5000-4, 11.1, 5, 879.9, M,M ): 13-44(27),11.562, 1, 0.0, 2.5.1.50CO-4, 4.5, 5, 882.9, M,M 1:44-fil(28),14.000, 1, 0.52, 12.9.1.5000-4, 13.0, 5, 925.8, M,M 2:Fil-FT2(29a),9.562, 1, 0.34, 13.6,1.50@4, 6.0, 5, 928.1, M,M 3;FT2-FT3(29b), 7.652, 1, 0.52, 8.7.1 5 4 4, 0.0, 5, 928.1, M,M 4: V-52989 ,7.652, 1, 0.0, 0.0,1. M W 4, 0.0, 8, 928.1.4363.0, 1.0 5: W-5252 , 7. 652, 1, 0.0, 0.0,1.5000-4, 0.0, 8, 928.1.3040.0, 1.0 3: FT3-FT4 ,7.961, 1, 0.47, 18. 7,1. 5X0-4, 1.6, 5, 928.1, M,M 7: FT4-fT5 ,11 1 8, 1, 0.8, 14.1.1.5000-4, 0.0, 5, 928.1, M,M 3: FTS-fiSA ,11.9 % 2, 1.0, 00,1.5000-4, 0.0, 5, 928.1, M,M
RC.i = IM i 6M Ai 14 ' Uit Fin CtM (OR ENTER FEEMGE) (YIN):Y? ' FIREWATERt=1) C00EGiEs=2) LA IACm=3) F1#: 17 FVHS) #AWEf1ENT (GE=0 - FARALLEL=1,- SERIES =2): 0? p ' j3 P /g ap2 3: FELTW m RW = 125 6W R0W e Fin = 155.3) Grn AT 100F FtN Kid) = 111.43 FT/5TA6E ' FILE:EE5CffA..DAT - 10. F SECTI0tG= 48 - T&FM5E SECTION5'OlVIDER: 10 SECTION 10 L FLW F(IN) P(OH)
!: 1-4 10.020 16.9 77,650 156 1 155.2 2: 4-6 6.065 91 77,650 155.2 113.9 3.6-7 7.961 2.2 77,650 143.9 143.7 4: 7 - 8 (1) 7.870 5.5 77,650 143.7 It3.6 5: 8 - 9 (2) 9 516 39.0 77,650 143.6 141.6 6: 9 -10 (3) 9.172 3.6 77,650 141.6 167.5 7 : 10 -11 (4) 9.172 2.3 42,901 167.5 167.7 8 : 11 -12 (5) 3.152 12.5 12,942 167.7 163.8 9 : 12 -18 (6a) 3.150 0.6 12,942 163.8 163.8 10: 18 -19 (6b) 3.346 1.1 12,942 163.8 165.7 11: 19 -20 (7) 0.616118.1 719 165.7 154 2 12:20-21(Sa) 0.874 0.3 719 154.2 153.8 u FRE55 s) TOC $ilWI u SECTIW 10 A FLOW F(IN) F(0UT) 13: 21 -22 (Eb) 0.898 0.7 240 153.8 153.8 14: 22 -23 (Sc) 0.724210.4 240 153.8 152.7 15:23-2?A(9) 0.724 37 9 240 152.7 151.7 16:23A-24(10) 0 724 39 2 210 151.7 156.7 17:24-25(11) 0.550 47 9 240 150.7 149.8 I:'* 0.00 GR= 0.68 18: 15 -26 (12) 0.590 52 240 149.8 148.3 I:!N= 0.68 OUT=100.00 19: 26 -27 (13) 0590 272 140 148.3 134.0 M:!N=0.071 GR=0.078 20:27-29(14) 0.590 62 240 134 0 130.1 M:lN=0.084 G R=0.067 21: 28 -Zi(15a) 0.7fA 0.4 719 128.7 127.9 M:Im0.161 OR=0.162 22: 29 - 3)(156) 0.969 10 0 719 128.9 119.9 M:I
- 0.101 G R=0.108 23: 3) -31 (16) 3.04 3 1.1 12,942 119.6 !!8.2 M:! M .127 0UT=0.129 24: 31-?2(17) 5826 4.6 12,942 !!8.8 117.7 M:1 5 0.056 OR=0.056 25:32-72/d18a) 9.586 3.0 12,942 117.8 117.7 M:!N=0.021 Ol#=0.021 26:12A-32E(!$t) 9.5% 05 25,F23 117.6 117.5 M:lN=0.042 OUT=0.042 27:33-33 (18c) 9.586 0.1 38,825 117.4 117.3 M:!*0.%3 OUT=0.063 28: 33-3?4(19a) 10.820 0.3 38,625 117.4 117.4 M:!N=0.050 OUT=0.050 29:33A-34(136)10.820 0.3 51,767 117.2 117.1 M:IM.066 0VT4.0%
30:34-34Af20a)10.820 0.3 51,767 117.1 117.0 M:IM.067OR4.M7 31:344-348(20b) 10.820 0.5 64,708 116.8 116.6 M:l*0.084 GR4.084 32:348-35 (20c) 10.820 0.6 77,650 !!6.3 115.9 M:l*0.101 OUT4.101 33:35-36(21) 5.826 2.7 38,825 !!4.3 107.4 M:IM.178 OUT4.190 u FESS G) TO CSTNI u l l
g SECTICC 10 UL( O #O Wr= 40,187 ( 22) 1 5 '
' 72 0 69 6 M:lN=0. jag g 0.151 f 39 -40 123) 10 114 04 f7 r ~
- F. G op 2
~
4 -4 ( 5) 1 .3 2
' 6 6.M:lw.1$h.0.35 77' !) 8M:I M .104 M :0.105 39 d2-d3(26)21.562 0l 77gg f7.1 67.1 M:!N=0.046 M:0.046 '0 13-44(27)21.562 00 77,'6 9 67.1 67.1MI M 046 M =0.046 d!: 44-FT! (28) 14 g ) 07 77 666 66.3 M:I M .ll2 M =0.ll3 J2:FTI-R2(29a) 9562 05 n'69 43:U2473425b) 7652 a6 77's U ' 6I 7 M:lN=0.249 M.-0.254 44: V-52993 7652 0'0 n'ggn 56.3 52.1 M:I M .424 M -0.472 g-g 52.1 50.7 Wr= 286,839 15: HV-5252 7652 0'0 7.69 50.7 47.5 Wr= 194,050 46: FT3-F74 7961 0'7 7' .1 M IM.559 M=0.g3g 47: FTA-FT5 11.9g O 77 g'o g'6g M 27.7 M:I M E M =0.368 48: FT5-FT5A 11.918 l uFFE55:5 EAT 00rfsg7N-285;'IA 2S'9 28'3 #I M IU M *0.181 SEFEAT WITH e gegygcgg; gyjyg
ilri: 1.)> EEC5 5 On C6 IFtG': 150 4 6F;t-Ti4T: 159 F- 0 @.W #'lC ~ zc/E 1: T- W= 80 El ) R= B3 5 INT: 5.7044 EIT= 0.0040 NE 2: T- VIE = 98.l( ) R: 108 9 - Q- INT: 1.3046 EXT: 0.00+00 ATT,3 P. I4 oF 2 NE 3: T- ViR: 1501( ) R= 155.4 - Q- thi= 3 904 EIT: 0.00+00 K8E 4: T- W: 199 3 ) R: 217.6 thT: 3.70+06 EIT: 0.00+00 KrE 5: T- W: 219 7( ) R= 2?2.6 INi: 1.50+06 EIT: 0.00+00 N E 6: T- WiR: 225.l( ) R: 242 2 INT: 4.00+05 EIT: 0.@00 N E 7: T- WiR: 255.2( ) R: 255 2 INT: 2.304 EIT: 0.004 F/E S: T- WTR= 258.l( ) R: 260 3 INT: 2.20 05 EIT: 0.0040 NE 9: T- Vi;= 328.3( ) R: 328 3 - Q- INT: 5.D06 EIT: 5.5045 L:tE NE 11:10: T- G= T- WTE: 155 3( ) R= 155.3 INT: 2.0046 EIT: 5.LOS 159.01B) R= 159 2 - Q- INT: 7.20+05 EIT: 6.6M5 - != 0.68 NE 12: T- V R: 159.0tS) E= 159 0 IkT: 1.@02 EIT=0.68 0.00+00 - I: ND:tE E 14:13: T- m= 15 5(E.) R= AD 5 - Q- thT: 6 ED+07 EIT= 4.@05 - I:100.00 T- WiR= 582.6( ) R: 673.1 - Q- INT: 5.@06 EIT= 0.00+00 NE 15: T- VIR: (46.5( ) R= 702.2 thT= 3.20+06 EIT: 0.00+00 KE55 G) T0 N.7NE. 3 NE 16: T- VIR: 673.3( ) R= 7E4.5 IkT= 2.50+05 EIT= 0.00+00 ate 17: T- VTR: 721.0( ) R= 929.9 - Q- IkT= 1.004 EIT= 0.@00 EtE 18: T- kTR= 715 St ) R= 956.8 IhT: 5.60+05 EIT: 0.00+00 NE 19: T- WiR= 739 A( ) R: 966 2 INT: 1.D05 EIT= 0.00+00 NE 20: T- VTR= 761.l( ) R: 968.1 - Q- INT: 8.2D+05 EIT: 0.@00 D:#E 21: T- Vi;= 754.51 ) R= ?!3 4 INT = 8.E0+05 EIT= 0.00+00 K E 22: T- WTE: 611.9( ) R= 946.7 - Q- INT: 1.004 EIT: 0.00+00 ItE 23: T- VTR= 816 Of ) R: 940.8 - Q- INT = 1.60+05 EIT= 0.00+00 NE 24: T- VIR= SJ9.7f ) R= 937.5 - Q- INT: 1.D06 EIT: 0.0040 NE 25: T- VT;= 872.0( ) R= 954 6 thT: 8 40+05 EIT= 0.00+00 D:tE 26: T- ViR= 879.9( ) R: 970.2 - Q- INT = 3.0045 EIT: 0.00+00 D:tE 27: T- VTR= EF2 9( ) V.= 971.8 - Q- IkT= 1.10+05 EIT: 0.@00 NE 28: T- VT;= 925 8f ) R: 994 7 - Q- INT: 1.604 EIT= 0.00+00 NE 29: T- VTR= 928.l( ) R= 971.8 - Q- thT: 8.50+04 EIT= 0.0040 FLW RATE (GFM): 150 4 ? 155 3 St.RUTICtl TEMP (de; F): 159? lEAT OF EVtff.iRATliA (BTU /LE*); f43.3?
g(TION m rkE: EEiUS. CAT m
- 10 G- hiin- M E- EFS - El. -t'L- TF - FG - t'41 W( 82~ $
46 1: 1-4 ,10020. 1, 5 SS, 522.1.1.5000-4, 2.1, l. 80.0, M,M M 7- B I l5.s2:, 2: 4-6 , 6 E5. 1, 3 37, 292.7,1 5000-4, 25.9. 1, 80.0, W,M 3: 6-7 ,7.551. 1. 091, 61.4,1.5000-4, 0.2, 1, 80.0, M,M 4: 7-8(1),7670. 1, 49, 30.1.1.5000-4, 0.3, 1, 80.0, M,M 5: B - 9 (2) , 9 516, 1. 37B, 59.7,1.5000-4, 4.3, I, 80.1, M,M 6: 9 -10 (3) , 9 172. 1, 0.96, 136.5,1.M&4, -60.6, I, 80 6, M,M 7 : 10 -11 (4) , 9 172.1.51, 0.42, 94 2.1.5000-4, -0.3, 1, 81.6, M,M 8 : 11 -12 (5) , 3 152, 6. 10 4, 102.1,1.5000-4, 9.0, 1, 82.5, 9 : 12 -18 (64), 3.150. 6, M, M 0.62, 0.00,1.944, 0.0, 1, E 8, M, M 10:18-19(6b),3346. 6. 0.53, 26.20,1.5000-4, -4.6, 1, 82.8, M,M 11: 19 -20 (7) , 0 E26.108.104.30, 495.30,8 2020-5, 27.0, 1, 83.0, M,M 12:20-21(Sa),0674.106, 001, 12.2,8.2020-5, 0.9, 1, 83.3, M,M 13: 21 -22 (Eb), 0.8.4. 224, 0.72, 0.00.82020-5, 0.0, 1, 83.3, M, M 14; 22 -23 (Sc), 0 724, 324, 209 50, 26.00,8.2020-5, 2.2, 1, 83.3, M,M 15: 23 -23A(9) , 0 724. 324. 000,1184.30,8.2020-5, 2.3, 1, 88.3, M,M 16:2M-24(10),0724.324. 000,1263.00,8.2020-5, 2.5, 1, 104.8. M, M 17:24-15(11),0550,324, 0.21.1618.00,8.2020-6, 2.7, 1.149.0, M, M 18:25-16(12),0590,324, 0.77, 166.80,8.20 N , 4.6, 1,189.9, M,M 19: 26 -27 (13). 0 530. 224. 0 00,1540.10,8.2020-6, -3.3, 1, 220.1, M,M 20: 27 -28 (14), 0.5 9 . 324. 1.34, 270.10.8.20 N , -11.0, 1, 257.2, M,M 21:28-29(15a),0.768.108. 0.12, 15.30,8.20M, -0.9, 22: 29 -30(15b), 0.M9.108. 1, 257.2, M,M 1.48, 525.60.8.20 N , -27.0, 1, 257.2, M,M 23: 30 -31 (16), 3 % ). 6. 0 66, 23.00,1.5000-4, 4.6, 1, 270.7, 24: 31-32(17),5826. 6, 1.26, 208.2.1.5000-4, 49.0, 1, 278.8, M,M 25: 32-D(18a), 9.5M. 6, M,M 2.9, 4.2,1.5000-4, 0.0, 1, 206.3, M,M 26:3E2Bt 18b), 9.5M. 3. 0. 3, 16.0,1. M & 4, 0.0, 1,286.3, 27:312-33 (1Ec), 9.5%. M,M
- 2. 0.04, 4.3,1.5000-4, 0.0, 1,286.3, M,M 28:33-5119a),10820. 2. 0. 3, 29:3D-34 (19t),10.O.1.5.
2.8,1.5000-4, 0.0, I,289.0, M, M 0.3, 2.8,1.5000-4, 0.0, 1,289.0, M,M 30:34-34M20a).10.G.1.5. 0.0. 18.0,1.50CO-4, 0.0, 1, 293.5, M,M 31:34A-34Bt2Ct),10.820.1.2. 0.3, 13.4.1.5000-4, 32:348-35(20c),10620. 0.0, 1, 293.5, M,M
- 1. 0 42, 146,1.5000-4, 0.0, 1, 293 5, 33: 35 -36 (21), 5 X 6. M, M
- 2. 2:12, 38.1,1.5000-4, 0.0, 1, 300.1, M,M 34:FV-2229 .5626. 2. 00, 0.0,1.5000-4, 0.0, 6, 300.1, 2 % .0, 0.9 35: M. -39 (22).11.5.0. 1. 07, 47.6,1.5000-4, 0.0, 1, 305.9, M,M 36:39-40(23)10114. 1, 02, 11.1,1.5000-4, 18.8, 1, 309.4, M,M 37:40-41124).12.9), 1, 1.2, 38: 41 -42 (25),14.312.
70.9,1.5000-4, 15.7, 1, 312.9, M,W 1, 09, 40.1.1.MX-4, 3.7, 1, 318.1, M,M 39: 42 -13 (26),2~. 542. 1, 00, 6.2,1.5000-4 11.1, 1, 321.0, M,M 40: 13 -44 (27),21.562. 1, 0.0, 2.5,1.5000-4, 4.5, 1, 322.1, M,M 41: 44-Fil (28),14 000. 1, 0.52, 12.9.1.5000-4, 13.0, 2, 332.7,0.0200,0.2140 42:FT1-fT2(23a),9562. 1, 0.34, 13.6,1.5000-4, 6 0, 2, 332.7,0.2140,0.2141 13:FT2-fT3(25t), 7.652. 1, 0.52, 8.7,1.50(&4, 0.0, 3, 332.7,0.2141, M 44: V-52983 ,7.652. 1, 00, 0.0.1.5000-4, 45: W-5252 ,7652, 0.0, 7, 332.7,4363.0, 1.0 1, 0.0, 0.0,1.5000-4, 0.0, 7, 332.7,3040.0, 1.0 46: FT3-FT4 ,7961, 1. 0 47, 18.7,1.5000-4, 1.6, 3, 332.7, M,M 47: FTA-FT5 ,11.938. 1, 08, 14.1.1.5000-4, 48: FT5-FT5A .11.338, 0.0, 3, 332.7, M,M
- 2. 1.0, 0.0,1.5000-4, 0.0, 3, 332.7, M,M
R(i = 7134 yti AT !@ (4(c E2 :C USE F1A7 CtME (CR Eh3 FF.EMiSE1 (Y/N):Y? 2 FIRE WATERi=1). OME tslEI:2)06IA(Mi=3)Ftti: 1? F:AfiS) AM6ENEh7 (GE=0 - FARALLEL:1 - ERIEi=2): 0? D.8 P. I b C# FELTON WEEL R0W = 125 FM FLW G FUF = 729.40 FM AT 100F Fit? RAD =104.51FT/STA3E FILE:EE50XL. CAT - 70. OF SECTims: 48 - M-FME SECTIONS'OlVIDER: 10 ECTlW 10 k FLOW FflN) P(0VT) 1: 1-4 10.020 14.4 M4,700 147.7 146.0 2: 4-6 6 (65 82 M 4,700 146.0 131.2 3: 6-7 7.951 1.9 364,700 131.2 130 8 4: 7 - 8 (1) 7.870 5.4 364,700 130.8 129.8 5: 8-9(2) 9.516 33.8 364,700 129.8 125.2 6: 9-10(3) 9.172 3.2 364,700 125.2 151.0 7: 10 -11 (4) 9.172 2.1 201,492 151.0 151.0 . 8: 11-12(5) 3.152 12.4 60,763 151.0 145.1 9: 12 -18 (6a) 3.150 0.6 60,7&3 145.1 115.0 10: 18 -19 ((b) 3.346 1.1 60,783 115.0 146.8 11: 19 -20 (7) 0.8661174 3,377 146.8 125.4 12: 20 -21 (Sa) 0.874 0.3 3,377 125.4 124.9 u FREES (CR) TO CaffiN:Iu ECTIW 10 k FLW F(IN) F(WT) 13: 21 -22 (Eb) 0.8.4 0.7 1,126 124.9 124.9 14: 22 -23 (Sc) 0.724210.3 1,126 124.9 !!9.6 15: 23 -ZM(9) 0.724 37 1 1,126 119.6 !!7.9 16: 2ik 24 (10) 0.724 33 7 1,126 !!7 9 116.0 17:24-25(11) 0. 550 (3.8 1,126 116.0 112.1 18:25-26(12) 0.5% 4.6 1,126 !!2.1 109.9 19: 26 -27 (13) 0 590 33 9 1,126 109 9 109.6 20:27-28(14) 05% 70 1,126 109.6 113.7 21:28-29(15a) 0.766 0.4 3.377 113.7 114.0 22:29-W156) 0 969 11.2 3,377 114.0 124.3 23: 30 -31 (16) 3.803 11 60.783 124.3 122.4 24: 31-32(17) 5.G 4.8 60.7&3 122.4 102.6 15: 32-32Af!8a) 9.585 30 60,7&3 102.6 102.6 26:32A-32S(!Eb) 9585 05 121,567 102.6 102.6 27:325-33 (18c) 9.5% 0.1 182.350 102.6 102.6 28: 33-3M(19a) 10.0 03 182,350 102.6 102.6 29:3M-34 (19b) 10.8N 0.3 243,133 102.6 102.6 30:34-34A(20a)10.83 0.3 243,133 102.6 102.6 31:34A-348(20b)10.G 05 303,917 102.6 102.5 32:348-15(20c)10.0 0.6 364,700 102.5 102.5 33:35-36(21) 5.83 2.7 182,350 102.5 102.1 u FEE 5S (CR) TO CSTI:4I u 1
!ECTIO'. 10 t Fl&' FilN) F( M ) '
34: FV-2223 56M 00 162,150 102.1 100.5 Ucr= 819,700 35: M -39 (22) !! 540 14 364.700 100.5 100.5 kTT, 3 P. O oF 2
% : 33 -40 (23) 10.114 04 M4,700 100.5 93.0 37: 40 -41 (241 12.50) 2.2 364,700 93.0 66.7 M: 41 -42 (25) 14.312 1.5 364,700 66.7 E5.6 I:l k 0.00 M : 0.16 39: 42 -43 (26) 21.562 01 M4,700 656 83.2I:I
- 0.16 M : 039 40: 13 -44 (27) 21.5(2 00 M4,M S3.2 82.4 I:l k 0.39 M : 0.47 41: 44fT1 (20 14 000 07 M4,700 82.4 80.7I:1 5 2.00 M : 21.40 42:Filfili29a) 9Si2 0.5 M4,7f.8) 80.7 77.7 I:1 5 21.40 M : 21.41 43:FT2fi3Gt) 7652 06 364,700 77.7 65.4 1:l
- 21.41 M : 22.33 44: V-52E3 7E52 0.0 MA,700 65.4 62.7Ucr=1,292,329 45: kV-5252 46: F13fT4 7652 00 364.M 62.7 57.1 Wcr= 861. M 7951 07 M4.700 57.1 29.5 I:l
- 23.16 M = 25.11 47: FT4415 11.9% 1.0 MA,W 29.5 16.8I:1525.11OUT=26.80 48: FT54T5A 11.9it 1.0 182,150 16.8 12.3I:1 5 26.80 M : 27.80
- FFES$1.EE AT E?C ff SYSTEM = 12.3 F51A KEFEAT lilTH E' WOITiff$ (Y/N)?
J Y
4 Tir2; 600 E: 1000r.II:5 ( FLOW: ($1.2 W - TiAi: 3327F1 C o t t. 82- 3 NE 1: T- Vih: 60 Of ) R : 00 0 - INT: 4 50+02 EIT: 0.@00 - f' ZONE 2: T- WTR: 50.2( ) R : E0 9 INT: 5.5M4EIT:0.00+00 20E 3: T- VTK: 80 9f ) R: 62.6 INT: 2.@05 EIT: 0.00+00 ZONE 4: T- VTR: 62.3( ) R : 66.6 INT: 4.5M5 EIT: 0.DOO ZU E 5: T- VTA: 82 7( ) R : 84.6 INT: 1.005 EIT= 0.00+00 ZGE 6: T- WTE: 62.8( ) R : 84 6 thT: 360+04EIT:0.@00 20E 7: T- WT;: $3.2( ) R : S3.4 INT: 1.5M5 EIT: 0.00+00 ME 8: T- Vis: 83.3( ) R: 83.5 thi: 1.004 EIT: 0.0M0 ME 9: T- WT;= 93 2( ) R: 93 2 IhT: 3 006 EXT = 1.10+06 ZGE 10: T- WTR: 116 3( ) R: 116.3 INT: 7.9M6 EIT: 1.10+06 ZGE !!: T- VTK: 1616( ) R: 181.6 INT: 2.2D+07 EIT= 1.2D+06 ME 12: T- VIK: 153.2( ) E= 198 0 thT: 2.6M6 EIT= 0.@00 ZGE 13: T- VIR: 250 9I ) R: 250.9 INT: 2.lM7EIT=1.20+06 ZGE 14: T- WiR: 263 4( ) R: 270 0 - INT: 4 D06 EIT: 0.@00 ZGE 15: T- ViR: 272.3f ) R: 275.3 IkT: 3.0M6 EIT: 0.00+00 FEE % <(R) 70 ($iWE. ZG E 16: T- Win: 273.4( ) K= 293.5 IkT: 3.@05 EIT= 0.00+00 NE 17: T- VTE: 264 2( ) R: 326.7 INT: 3.7M6 EIT: 0.0M0 NE IS: T- VTK: 288 4( ) R: 344.5 INT: 1.4M6 EXT = 0.00u)0 ZGE 19: T- WiR: 259 6( ) R: 360 4 INT: 4.2045 EXT: 0.000 20E 20: T- WTE: 237.3( ) R: 363.1 INT: 2.60+06EIT:0.00+00 NE 21: T- vie: 302.S( ) R: 337.7 DJ: 1.90+06 EIT= 0.00+00 ZGE 22: T- VIR: 3089( ) R: 315 8 Ita: 2.1066 EIT= 0.DOO NE 23: T- VIR: 309 64 ) R: 332.8 INT: 2.9M5 EIT= 0.00+00 N E 21: T- VIR: 316 0( ) R: 330 5 IhT: 2.10+06 EIT= 0.@00 20E 25: T- VIE: D) 1( ) R: 113.7 INT: 1.40*)6 EIT= 0.00+00 29E 26: T- WiK: 321 B( ) R: 338.7 INT: 5 @05 EIT: 0.@00 NE 27: T- VTR: 322.41 ) t= 338 9 thT: 2.lMSEIT=0.DOO ZG E 28: T- VTE: 332.7(B) R: 532.3 INT: 6.@07 EIT= 0.@00 - I: 21.40 294 23: T- WiR: 332.7 61 R: 313.6 INT: 3.30+04 EIT: 0.@00 - I: 21.41 t FLOW FATE (GFit): 661.2?723.4 SAT!EAfl$ TErs' (MF): 332.77317.9 KAT OF EVAFWAT!W (BTWLEa): 684.97696.5 i i ( I i i
- E17[.y.
htFILE:EEF5LDAT14: s2i?- UFIX)- W)- NC N' 46 EF5 - EL -FL- if - O - r-. 1: 1-4 ,10020. 1. 5 08,, 522.1.1. 9 )0-4, 2.1, 1, 80 0 M,M Arr, 8 p. W e 2 2: 4-6 . 6 065. 1. 3.37, 292.7,1. 9 & 4, 25.9, 1, 80.0, M,M ; 3: 6-7 ,7561. 1. 0.91, 61.4,1.5000-4, 0.2, I, 60 0. M,M l 4: 7 - B (1) , 7 670. 1. 49, 301.1.5000-4, 0.3, 1, 80 0, M,M 5: B - 9 O , 9 516, 1. 37 6, 53 7,1. 9 & 4, 4.3, 1, 80.0, M,M 6: 9 -10 (3) , i 172, 1. 0 53, 136.3.1.5000-4, -60.6, 1, 60 0, M,M 7 : 10 -11 (4) . 9 172.1 11. 0 42, 94.2.1. 9 & 4, -0.3, 1, 80 1, M, M 8:11-1215),3152, 6. 10 4, 102.1.1.5000-4, 9.0, 1, 80.1, M, M 9:12-18(64), 3.150. 6. 062. O M ,1.5000-4, 0.0, I, 80.1, M,M 10: 18 -19 @ ), 3 346, 6, 0 59, 26 20,1. 9 & d, -4.6, 1, 80. l. M,M 11: 19 -20 G) . O M6,108.104.30, 495.30,8.20&5, 27.0, 1, 80 2. M, M 12: 20 -21 (54) 0 874, 108. 0.01, 12.2,8.20&5, 0.9, I, 80.2, M,M 13: 21 -22 (Sb), 0 838. 324. 0.72, 1 00.8.20 & 5, 0.0, 1, 80.2, M,M 14: 22 -23 (Sc), 0 724, 324, 209 50, 26.00,8.20&5, 2.2, 1, SiL 2, M, M 15: 23 -IMt9) , 0 724. 324, 0.00,1184.30,8.20&5, 2.3, 1, 81.3, M,M 16:2M-24(101,0724,324 000,1283.00,8.20&5, 2.5, 1, 63 5, M, M 17: 24 -25 (11). 0 550, 324. 0.21,1818.00,8.20&6, 2.7, 1, 87.1, M, M 16:25-26(12),0530,324. 0 77, IM 80,8.2020-6, 4.6, 1, 69.7, M,M 19: '6 -27 (13), 0 530, 324. 0.00,1540.10,8.20 & 6, -3.3, 1, 94.0, *, c 20:27-28(14).0530.124 1. M 270.10,8.2020-6, -11.0, 1, 98.8. M,M 21: 28 -29t15a), 0 7M.108. 0.12, 15.30,8.20 & 6, -0.9, 1, 100.1, M,M 22: 29 -30115b), 0 96).108, 1.48,525.60,8.20&6,-27.0, 1,100.1, M,M 23:30-31(16),3803, 6, 0.66, 23 00,1. 9 & 4, 4.6, 1, 100.7, M,M 24: 31 -?2 (17), 5 526, 6, 1.26, 208.2.1. 9)0-4, 49.0, 1,104.0, M, M 25: 32-72Mita), 9 SM, 6, 29, 4.2.1.50@4, 0.0, 1,108.9, M,M 26:?Ite-1281 lit), 9 SM, 3, 03, 16.0,1. 9 & 4, 0.0, 1, 108.9, M,M 27:311-33 (ISc), 9 SM, 2. 0.04, 4.3.1. 9 & d, 0.0, 1, 108.9, M,M 28: 33-3M(19a),10 820, 2. 03, 2.6.1. 9&4, 0.0, 1,111.1, M,M 23:3M-M (15b).10 820,1.5, 03, 2.8,1.5000-4, 0.0, 1, !!!.1, M,M 00:*,401.1204)10.620.1.5, 0.0, 18.0.1.50@4, 0.0, 1,114.9, *,M 31:34'r-315t 20b),10 K0.1.2, 0.3, 13.4.1.5000-4, 0.0, 1, 114.9, W,M 12:M45 (20c),10 6?). 1. 0.42, 146,1.50@4, 0.0, 1, 114.9, M,M 33: 35 - M (21), S E S, 2, 2.12., 38.1,1. 9 & 4, 0.0, 1, 12tl 3, M,M 34:P'-2229 , S E6, 2. 0.0, 0.0,1.50@4, 0.0, 6, 120.3, 299 0, 0.9 35: % -39 (22),11.540. 1. 07, 47 6,1. 9 & 4, 0.0, 1,124.7. M,M 36: 39 -40 (23),10 114. 1, 02, 11.1.1.50@4, 18.8, 1, 127.2, M,M 37: 40 -41 124),12.5M. 1. 1.2, 70.9.1.50@4, 15.7, 1, 129.6, M,M
% : 41 -42 (25),14.312. 1, 09, 40.1.1.5000-4, 3.7, 1, 1 33.6. M,M 39: 42 -43 C6).21.542. 1, 00, 6.2.1. 9 & 4, !!.1, I,1%.6, M,M 40: 43-44(27)21.562. 1, 0 0. 25,1.50@4, 4.5, 1, 138.2, M,M 41: 44-fil G6),14 OfA, l. 0.52, 12.9,1.5000-4, 13.0, 1, 168.5, M,M 42:FTI-FT2G9a),9562.
13:FT2-fi3Gib), 7 652.
- 1. 0.34, 13.6,1.5000-4, 6.0, 1, 198.6. M,M 1, 0.52, 8.7,1.5000-4, 0.0, 1, 198.6, M,M 44: V-52593 ,7652, 1. 00, 0.0,1.50@4, 0.0, 6, 198.8,4 E3.0, 1.0 45: b','-5252 ,7652. 1, 0.0, 0.0,1. 9 & 4, 0.0, 6, 198.9,3040.0, 1.0 46: FT3-FT4 ,7.561, I, 0.47, 18.7,1.50@4, 1.6, 1, 198.9, M,M 47: FTA-fi5 .11.938. 1, 0.6, 14.1.1.5000-4, 0.0, 1, 198.9, M,M 48: FTS-FT5A .11.338, 2, 1.0, 0.0,1.50@4, 0.0, 1,198.9, M,M
FLG = 1143 6M AT 1(N cncE2 O Uq FW (16E (C6 ENTER FFEi51.EE] (yin):Y? FIRE WTER(:1), Cf)SMTE(:2) f.R IAW:3) FW: 1 ? N, _ g3 FWtS) AR%.%EMENT (TR 0 - FT6ALLEL:1 - SERIES 2): 0? P 23 8" FELTW M EL FLOW = 125 F M? FLW 6 FW 1149.00 FM AT 100F FW Ele : 102.41 FT/STA3E FILE:EE5ti.(LTAT - N0. OF SF.TI0tes: 48 - TFrFMiE SECT!WS'0!VIDER: 10 SECilm 10 k FLW F(IN) F(0VT) 1: 1-4 10.020 14.0 574,500 144.5 141.5 2: 4-6 6.065 80 574.500 141.5 121.5 3: 6-7 7.961 1.9 574,500 121.5 120.8 4: 7-8(1) 7.670 54 574,500 120.8 118.5 5: 8-9(2) 9.516 38.7 574,500 !!8.5 109.7 6: 9-10(3) 9.172 3.1 574,500 109.7 135.1 7 : 10 -11 (4) 9.172 2.0 317,403 115 1 135.1 8 : 11 -12 (5) 3.152 12.3 f5,750 1351 IM.0 9 : 12 -18 W ) 3.150 0.6 95,750 1 M .0 125.8 10:18-19(Eb) 3.346 1.1 95,750 125.8 127.4 11: 19 -20 (7) 06161166 5,319 127.4 91.6 12: 20 -21 W ) 0674 0.3 5,319 91.6 91.2 u F%E55 (CR) TO W, TIE u SECTlW 10 K FLOW F(IN) F W T) 13:21-22(Et) 0.898 07 1.773 91.2 91.1 i 14: 72 -23 (Sc) 0724210.3 1.773 91.1 793 15: 23 -73A(9) 0 724 34.5 1,773 79.3 76.6 16: 2M-24 (10) 0.724 37 1 1,773 76.6 73.6 17:24-25(11) 0 550 45.2 1,773 73.6 65.4 18: 25 -3 (12) 0590 4.9 1.773 65.4 62.8 19: 26 -27 (13) 0.590 38 0 1,773 62.8 59.8 20:27-28(14) 0.5M 7.9 1,773 59.8 63.6 21:28-23t15a) 0.765 0.4 5,319 63.6 63.8 22:29-30115b) 0.969 12.6 5,319 63.8 73 6 23:30-31(16) 3.803 1.1 95,750 73.6 71.4 24:31-32(17) 5.63 51 55,750 71 4 502 25:32-32A(184) 9.5FA 3.0 55,79 50.2 50.2 26:32A-r5(16b) 9.5FA 06 151,500 50.2 50.2 27:328-33 (16c) 9.FA 0.1 057,250 50.2 50.1 28: 33-3M(19a) 10.620 0.3 287,250 50.1 50.1 23:3M-34 (19b) 10.820 03 ;&3,000 50.1 50.1 30:34-344(20a)10E0 0.3 333,0)0 50.1 50.1 31:34A-348 20b) 10.820 0.5 478,750 50.1 50.1 32:348-35 (20c) 10.820 0.6 574,500 50.1 50.0 33:35-36(21) 5.826 2.7 237,250 50.0 49.1 u FSESS (CR) TO CrATIE u
!ECTIS'; lC k FLOV .F(IN) .Ft0VT) <-
(n c.. $]- 10
' 34: Fv-2227 5.826 I
- is: 36 -39 (22) !!.540' l.40) 2%7,250 574,500 45.449.1 45.3454Wcr: 922,074 -
M: 39 -L) (23) 10.114 0.4 574,500 45.3 37.2 ATT, g f. 7 j OF g I 37: 40-Al(24)12.500 2.2 574,500 37.2 3).3 ! 38: 41-42(25)14.312 1.5 574,500 30.3 28.7 39: 42-43(26)21562 0.1 574,500 28.7 23.9 40: 43 -44 (27) 21.562 00 574.500 23.9 22.0 41: 44-FT! (28) 14 000 0.7 574,500 22.0 16.5 42:Fil-FT2(23a) 95f2 05 574,500 16.5 13.9 43:FT2-FT3(290) 7652 06 574.500 13.9 13.6 44: V-52389 7.652 0.0 574,500 13.6 13.5 Wcr=3,713,357 15: W-5252 7.652 00 574,500 13.5 13.4Vcr=2,546,677 46: FT3-FT4 7.951 07 574,500 13 4 12.4 47: FTA-FT5 11.9M 1.0 574,500 12.4 12.4 48: FTS-FT5A 11.9% !.0 257,250 12.4 12.3
** FRE59AE AT END CF SYSTEM = 12.3 FSIA REFEAT WITH EV C00171Cf;5 tynm
EA(f 2 ~f C Tit'E: 770 Secs: 12.&) ly::; ( gr,q: 1(47 6 6/:1-ig;-244:4F] ME 'l: T- VIR: 80 0( ) K: 80 5 INT: 2.40+01EIT:0.0M0 ATT, b f .22 # 20E 2: T- M: 60.0( ) K: 601 thT: 5.70+03EIT=0.0MQ IGE 3: T- WTE: 60.0( ) E: 60 2 INT = 2.10+04 EXT = 0.0M0 D M 4: T- b7R: 601( ) Lt= 60.5 INT: 3.90+04EIT:0.0M0 M.E 5: T- biR= 801( ) t= 60.2 thT= 7.00+03 EIT: 0.00+0) ZGE 6: T- G: 80.l( ) R : 60 2 - Q- Iki: 1.70+03 EIT: 0.00+00 20E 7: T- M: 60 2( ) R : 60 2 thT: 6.5M3EIT:0.0M0 D M 8: T- VIR: 60.2( ) R: .60 2 INT = 6.10+02 EIT= 0.0M0 ME 9: T- G: 62.3( ) R: 62.3 INT: 1.10+06 EXT = 1.10+06 M E 10: T- G : 84 7( ) K : 64 7 thT= 1.D06 EIT= 1.D06 ZGE 11: T- W: 69.5( ) E= 89 5 IhT: 2.6M6 EIT= 1.50+06 ZGE 12: T- WiR: 89 8( ) L : 90 5 thT: 1.70+05 EIT= 0.00+00 D M 13: T- m : 93 1( ) R : 931--Q-INT:4.40+06EIT=1.70#/, DM 14: T- b7R= 99.5( ) Lt= 101.2 INT = 7.90+05 EIT= 0.00+00 ME 15: T- WTR= 100.6( ) E= 101.5 thT= 5.90+05 EIT= 0.00+00 FRESS KU TO M.TINVE. ZGE 16: T- VIR: 100 6t ) R= 105.1 thT= 9.6M4 EIT= 0.0M0 ME 17: T- WiR: 107.2( ) E: 148.3 IhT: 3.40+06 EIT= 0.00+00 ME 18: T- m= 110.6( ) ht: 162.5 IhT= 1.60+06 EIT= 0.0M0 ME 19: T- VTR= 111.6( ) R= 205.3 INT = 5.50+05 EIT= 0.0M0 ME 20: T- bTR= 116.2( ) K= 209.4 INT = 3.5M6 EIT= 0.00+00 ZGE 21: T- WTE: 122.4( ) E= 164.7 - INT = 2.D06 EIT= 0.00+0) ME 22: T- b7R= 116.9i ) R= 159.4 IkT= 2.40+06 EIT= 0.00+00 ME 73: T- E= 127 5( ) R= 152.3 INT = 3.10+05 EIT= 0.0M0 DM 24: T- VIK: 131.7( ) R= 146.0 - Q- INT = 2.20+06 EXT = 0.0M0 20E 25: T- G: 135.5( ) R= 155.6 - Q- IhT: 2.10+06 EXT:0.0M0 DM 26: T- WTR= 137.7( ) Lt= 173.5 INT = 1.20+06 EIT= 0.00+00 20hE27:T-biK: 138.6( ) t= 175.4 IhT= 4.70+05 EIT= 0.0M0 ME 3: T- VIR: tir3.38. ) V.= 346 9 INT: 3.20+07EIT=0.00+00 ZGE 29: T- WTR= 158 9i ) E= 214.2 INT: 3.00+05 EIT: 0.00+00 R0W FATE (ffM): 1(47 6 ? !!A9 SATIAATil) TEN. (&g F): 244.4?203 1 lEAT OF EVEffATION (BTME4); 949.3?976 { S
s . (qc p2.;C ii"E:67.; iici: 14 g ,y y ( [gg. ggg3 g ,7 7 , . ZrM 1: T- VIR= 80 Os ) R= (0 0.-- Q- thT: 410+00 EXT: 0 00@ ZGE 2: T- WTR= 60 0( ) R: 60 0 - Q- INT: 1.40+03 EXT: 0.00@ ATT, f b ira 3: T- VI;= 60 0( ) R= 80.0 - Q- IE: 4 20+03 EIT= 0.00+00 ZGE 4: T- Wi;= 60 0( ) R: 60.1 IE: 7.90+03 EIT: 0.00+00 D M 5: T- WTR= 80 0( ) R : 60.0 14= 1.20+03 EXT = 0.00@ ZiR 6: T- V!;= 60 0( ) R 60 0 INi: 3.00+02 EXT = 0.00+00 ZGE 7: T- VT;= 80 0( ) R: 60.0 - Q- li.T= 1.2D+03 EIT= 0.00+00 ZGE 8: T- biR= 80 Of ) R= 80 0 - Q- INT: 1.10+02 EIT= 0.00+00 F1E 9: T- VTR= 619( ) R: 01.9 - Q- In: 1.1046 EIT= 1.10+% ZGE 10: T- VIR: 64.0( ) R= SL O - Q- INT: 1.20+06 EIT= 1.20+% ZGE 11: T- bTR= E4 61 ) R= 66 8 thT= 1.60+06 EIT: 1.50+% ZGE 12: T- WIK % Si ) R= 66.8 INT: 1.30+04 EIT= 0.00+00 Zi/E 13: T- VIR= 90 il ) R= 90.2 - Q- INT: 2.00+M EIT= 1.80+% DM 14: T- biR: 90 il ) V.= 9).5 IhT: 6.E0+04 EIT= 0.0M0 ZGE 15: T- WiR 90.5f ) R= 90.5 - Q- IE: 5.00+04 EIT= 0.00+00 FREis <CD TO CGJTIMI ZGE 16: T- WTR= 90 5f ) R= 90.9 - Q- INT: 8.60+03 EIT= 0.00+00 DM 17: T- b7R= 92.2( ) E= 104.0 - Q- IE: 9.E0+05 EIT= 0:00+00 DM 18: T- UR= 93.5f ) R= 124.5 - Q- thT: 7.7045 EXT:0.00+00 ZGE 19: T- WiR: 94 Of ) R= 141.8 - IE: 2.80+05EIT:0.00+00 ZrR 20: T- WIR: 97.2( ) R: 144.8 - Q- INT: 1.80+06 EIT: 0.0040 D M 21: T- VTE: S8.6( ) R= 113.2 IhT: 7.7045 EXT: 0.00+00 D M 22: T- b7R: 99.9f ) E= 110.3 - Q- INT: 7.70+05 EIT= 0.00+00 ZGE 23: T- VTE: 1001( ) R= 107.3 - Q- thT= 9.10+04 EXT = 0.00+00 ZiR 24: T- kiR= 101.l( ) R= 105.7 - Q- INT: 6.20+05 EIT= 0.00+00 irk 25: T- bi;= 102.2( ) V.= lii5 - Q- IhT: 6.1045 EXT:0.00+00 ZGE 26: T- 47;= 102.9f ) R= 115 6 - Q- INT = 4.10+05 EIT= 0.00+00 ZGE 27: T- VTR= 103 2( ) R= 115.5 - Q- Iki: 1.70+05 EXT = 0.00+00 ZGE 28: T- biR: 147 2< ) V.= 26 7 - Q- INT: 2.50+07 EIT: 0.00+00 ZGE 29: i- biK: 147 Ji ) R= 154.4 - Q- IhT: 1.30+05 EIT= 0.0040 CASE VUEi fia SA'd OLO GEi (N/Y)? l l
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