ML20096E941
ML20096E941 | |
Person / Time | |
---|---|
Site: | Summer |
Issue date: | 01/08/1996 |
From: | Don Krause SOUTH CAROLINA ELECTRIC & GAS CO. |
To: | |
Shared Package | |
ML20096E939 | List: |
References | |
DC03050-001, DC03050-001-R00, DC3050-1, DC3050-1-R, NUDOCS 9601230107 | |
Download: ML20096E941 (25) | |
Text
{{#Wiki_filter:. . . - _ . ES 412 Ansch.1, Rev.1 4 SUBJECT CODE SOUTH CAROLINA ELECTRIC AND GAS COMPANY PAGE 30s CALCULATION RECORD 1 W 2.1 1 CALC TTTLE CALC NO. REV STAT l RB TENDON HOOP AND DOME LOSS CALCULATIO95 POR STH DC03080401 0 1 PERIOD SURVELLANCE PARENT DOCUMENT SYSTEM SAFETY CLASS CALC. CLASS l - 60 m M fed OR I U IU IV V VI ORIGINATOR DISC ORGANEATION DATE XREF NO. 3 KRAUSE, D. CS 10/1395 NOfG! A. CALCULATIONINFORMATION j CONTENT DESCRFTION: , THE CALCULATION IDENTIFIES THE RB TEfCON PORCE LOSSE AND THE SURVEILIANCE ACCEPTACE CRITERIA FOR THE l 1 DOME AND HOOP TENDONS. AFFECTED COMPONENTS / ANALYSIS: kM A R. TENDONS Disi, Dm, Dm, Dm, Dm, Dm, Dm, Dm, Dm, $ pC,isAC,i.AC. C ,30C ,2 i . CONTAINS PRELRAINARY DATA / ASSUMPTIONS. s NO O YES, PAGeS 10RINFORMATION_0_NLY COMPUTER PROGRAM USED: O NO I YES, VAUDATION NOT REQ'D. [REF.s.5) C YES,VAUDATED[OTHERS] x YES, VAUDATED [ES-412] O PROGRAMVALIDATIONCALCULATION I B. VERIFICATION i VERIFICATION SCOPE i $ VERIFY CALCULATION METHODOLOGY, INPUT AND ASSLEAPTIOtE. PERFOfRR SPOT CHECK OF MATH. 1 ! VERIFIER: PARSONS, G. ASSIGN BY: WHORTON, R. B. [ M/ LEAD44ENG9DME Ka AG //d$ DEER (DESIGIEEE)/DATE VERIFIER / DATE APPROVAL /DATE
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C. MCORb FE!EL NURABER: FRAME NURABER: 1 TO PRS: NT/DATE ORIQiNAL MAINTAINED BY: . SCE&G DE DISTRIBUTION: CALC PLE [OfuGINAL] DSE /SYSTund ENG /DE FILE 20.4602 [ ATTACH.1 OfLY, COPY] 9601230107 960118 PDR ADOCK 05000395 4 p PDR
ES-412 ATTACHMENT I REVISION 1 PAGE 2 OF 2 - SOUTH CAROLINA ELECTRIC & GAS COMPANY PAGE REVISION
SUMMARY
2 OF ~A I - CALCULATION NO. DC03050-001 REV NO.
SUMMARY
DESCRIPTION O This calculation identifies the predicted forces and acceptance criteria for the RB horizontal and dome tendons that were selected for the fifth period surveillance and the adjacent tendons. l l 3 l I i 0 CONTINUES ON PAGE ES412/ ATTACHMENT LSEVISIC N 1 1
ENGINEERS. Serial 10606 TECHNICAL WORK RECORD Engineer G. F' arsons Date 1/8/96 Project Title . _ RB Horizontal & Dome Tendon Force Page1 of_ Cale: DCO)ofo-oo' R8V 0 J of 21 Page_ , VERIFIER'S COMMENTS The purpose of this TWR is to document the verification performed on DCO3050-001 Rev. O. The verifier has reviewed the calculation methodology,the inputs and the assumptions. A spot check of the math was also performed. This calculation identifies the predicted forces and acceptance criteria for the RB tendons that were selected for the fifth period surveillance, l'revious tendon force predictions were based on subtracting a series of estimated force loss factors from the original lock-off force value. This calculation method replaces these estimated values with graphically derived values. The graphically derived values are extrapolated from previous eurveillance data. This is a more accurate way of deriving the predicted forces since it more accurately defines the unknowns affecting these particular tendons. The calculation inputs include time of original lock-off, original lock-off force, Normalization factors ect.. These values were obtained from previously verified documents and are reasonable and accurate for this application. The primary assumption in this calculation is that if the tendon force vs time is plotted on a semi-log plot,the data points will form a straight line. This assumption is reasonable and is
- shown to be accurate based on previous tendon force data.
I t ._
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Figure 2-1 Dome Tendons Force-Time Curve (Average Of Normalized Surveillance Forces) TIME AFTER AVERAGE DATE OF CONCRETE PLACEMENT (HOURS) 6x10* 8x10* 105 2x105 4x105 6x105 10' 2x10' 4x104 1400 l i j i j i l i ; i i i i i i P I -
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157000IIRS l FORCE =2048.53 - 178.79 x LOG (time) time in hours, force in KIPS --; ; ; y; -
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sId-!- F ! Curve Fit Coefficients: Z z
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" j j __j _ j-_. '_ h Al 21 800 1 3 5 10 15 20 25 30 35 40 ~
YEARS AFTER SITTO 0 SCHEDULED SURVEILLANCE PERIOD
Figure 2-2 Hoop Tendons Force-Time Ccrve (Average Of Nornialized Surveillance Forces) i l TIME AFTER AVERAGE DATE OF CONCRETE PLACEMENT (HOURS) i 2x10' 6x10' 8x108 1 05 2x105 4x105 6x105 ' 10' 4x10' , , , , , , 1000 , , , ,.
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-o YEARS AFTER SITTO s
SCHEDULED SURVEILLANCE PERIOD
'Cald: DC0 2e co-ao / R:v. o Page c- of 2, ENGINEERS Serial TECHNICAL WORK RECORD Engineer D.Krause Date 10-13-95 Project Title Prod!cted Force - Hoop and Dome Tendons Page I of_ 4 FlieID t A:\ TENDON 6. DOC 1.0 OBJECTIVES (1) Develop general methodology for predicted liftoff force for the hoop and dome tendons by using the results from previous surveillances, i.e. h traditional approach based on experience.
(2) Develop the predicted liftoff forces for the hoop and dome tendons for the 5th tendon surveillance (15 years after SIT) planned for April 19% using the traditional approach. 1.1 DESIGNINPUTS 1.1.1 De design inputs consist primarily of previous V.C. Summer Station structural calculations. These are clearly referenced where they are referenced in the body of the calculation. 1.1.2 Other documents referred to in the calculations include: (1) SP 228 Surveillance of the Reactor Building Post Tensioning System. (2) Reactor Building Cnntainment Fourth Period Surveillance Tendon Forces Report. May 1990. 1.2 ASSUMPTIONS Assumptions are identified in te calculation where used. There are no assumptions requiring future confirmation. 1.3 COMPUTER USE The software SigmaPlot for Windows by Jandel Corp. is used to plot the graphs of the data points of group average forces from each surveillance to obtain the force vs. time trend for each group of tendons. The data is also plotted manually on semilog graph paper to verify the results using SigmaPlot. 1.4 CALCULATION ne basic sequence of steps to determine predicted liftoff forces using the traditional approach are:
- 1. Develop the current Group Average Normalized Tendon Force vs. Time graph for each group of tendons.
He curve for each group consists of a straight line fit through the data points for each of the surveillances performed to date. Each data point represents the average of the normalized forces for the tendons in each group for a particular surveillanca. The curves are plotted on a semilogarithmic graph where the force losses versus time are essentially linear over the 40 yearplant design life. SigmaPlot software is used to generate the plots for the dome and hoop tendons. attached as Figures 2-1 and 2-2. The manually drawn graphs on pages si o confirm the accuracy of the SigmaPlot software graphs.
'CaE DC0 7ero-ca l' Rev,'o Page 7 of 2/
ENGINEERS Serial TECHNICAL WORK RECORD Engineer D.Krause Date 10-13-95 Project Title Predicted Force - Hoop and Dome Tendons Page 2 of__ FileID : A:\ TENDON 6. DOC
- - 2. Obtain the tendon force corresponding to the intersection of the time of the surveillance ofinterest and the straight-line projection of group average forte versus time results from previous surveillances.
Figures 2.1 and 2.2 are used to demonstrate the method for the dome and hoop tendon groups for the 5th tendon surveillance period. 4 The time durations from concrete placement to the planned surveillances are given in Table 1 below. Although the difference is minor, the time may be calculated for the actual planned start of the particular surveillare as described below for the 15 year surveillance scheduled to begin on approxunately April 1,1996. As the time since the performance of the SIT increases, the predicted tendon liftoff force becomes less sensitive to the actual time of the surveillance because the losses occur at a logarithmically decreasing rate over time. The majority of the losses occurred in the years immediately following stressing. For example, the hoop tendons at the 15 year surveillance are experiencing losses at the rate of about 0.45 kips per month. At the 20 year surveillance. losses will be occurrmg at the rate of about 0.3 kips per month. Therefore an estimate of the time within 6 months of the actual surveillance for use
- in deemnining the predicted liftoff forces for the 15 and 20 year surveillances will provide an accuracy better than 3 kips.
t An accuracy of 3 kips is acceptable and conservative. For perspective. 3 kips represents about 0.27% of the force in the tendon for a tendon having 1100 kips of force. l These conclusions for the hoop tcudons also apply to the dome tendons because the hoop tendons are experiencing losses i at a faster rate than the dome tendons as shown by a comparison of the slopes of the group force versus time curves (Figures 2-1 and 2 2) for the surveillances completed to date. I For the 25 year, and beyond, surveillances. the use of a time corresponding to the year of the surveillance to determme the t- predicted force will provide an accuracy better than 3 kips.
'CiliiDC0 3eto- ce7 RevN l Pags 8 of 2; ENGINEERS Gerial l TECHNICAL WORK RECORD Engineer D.Krause Date 1013-95 -l Project Title Predicted Force - Hoop and Dome Tendons Page 3 of_ ~
FileID : A:\ TENDON 6. DOC i 1 TABLE 1 PLANNED TIME FROM CONCRETE PLACEMENT TO SURVEILLANCE VERTICAL VERTICAL HOOP HOOP DOME DOME YEAR DAYS HOURS DAYS HOURS DAYS HOURS SIY JAN 1,1981 1,612 38,688 1,612 38,688 969 23,256 1 YEAR JAN 1,1982 1,977 47,448 1,977 47,448 1,334 32,016 3 YEAR JAN 1.1984 2292 64.968 2222 64.968 2Af4 49.536 5 YEAR JAN 1,1986 3,438 82,512 3,438 82,512 2,795 67,080 10 YEAR JAN 1,1991 5,265 126,360 5,265 126,360 4,622 110,928 15 YEAR 3AN 1.1996 2M1 170.184 2M1 170.184 5 448 154.752 20 YEAR JAN 1,2001 8,918 214,032 8,918 214,032 8.275 198,600 25 YEAR JAN 1,2006 10,744 257,856 10,744 257,856 10,101 242,424 30 YEAR JAN 1.2011 12.570 301.680 2 12.E'9 301.680 J.la22 286.248 35 YEAR JAN 1,2016 14,3 % 345,504 14,3 % 345,504 13,753 330,072 40 YEAR JAN 1,2021 16,223 389,352 16,223 389,352 15,580 373,920
Reference:
V.C. Summer Station Structural Calculation Book Z 3D 1 18.3, pages 156 and 157. Examole calculation of dome and hooo aroup averane tendon forte for 15 year surveillance (5th surveillanceh Planned start of surveillance: April 1,19% Total hours in January, February, and March 1996 =
= (2 mo. x 31 days /mo. + 28 days) x 24 hr/ day = 2,160 hours Add 2160 hours to the hours for January 1,1996 shown in Table 1:
Vertical and Hoop = 170,184 hours + 2,160 hours = 172,344 hours (172,400 hours) Dome = 154,752 hours + 2,160 hours = 156,912 hours (157,000 hours) Enter the rounded off hours in the SigmaPlot files for the Dome and Hoop tendon groups respectively and determine the group average force corresponding to the intersection of the hours and the straight line projection of the group average Curve.
'Ibe predicted group average forces at 15 year surveillance are:
Figure 21 Dome Group Average Force = 1120 kips Figure 2-2 Hoop Group Average Force = 1076 kips
. .. ~
[Dal5iDC0 No-#RevN Pcge- 9 of 2s , ENGINEERS Serial TECHNICALWORK RECORD Engineer D.Krause . Date 10-13-95 ProjectTitle Predicted Force - Hoop and Dome Tendons Page 4 of__ I File 10 t A:\ TENDON 6. DOC
- 3. Calculate the predicted liftoff forces for the ladividual selected and adjacent tendons.
The predicted liftoff force is obtamed by subirecting algebraically the normalization factor for the particular tendon from 4 the predicted group average of the namahzed forces for the particular survedlance.The tendon normalization factors are obtained from Table 5 (Enclosure 8) of the current revision of SP 228 " Surveillance of Reactor Building Post-tensioning System" Normalization factors may be calculated for tendons not previously selected using the methodology in V.C. Summer Station Structural Calculation Book Z4-K.1:18.5. starting on page 98. This calculation for normalization factors may be performed manually or by computer using a spreadsheet.
- 4. Tendon group average liftoff force data .
- The data used to develop the group average force versus time plots in attached Figures 2 1 and 2-2 is shown on Tables 2 and 3 below. ! The predicted liftoff forces (Base Values) for the selected and adjacent tendons for the 5th period (15 year) surveillance 4 calculated by the traditional approach are shown in Table 4. i' TABLE 2 - ACTUAL TIME FROM TENDON CONCRETE PLACEMENT TO TENDON SURVEILLANCE (1) (2) (1)+(2) TENDON SURV. PLANNED CONC. EFITCTIVE DELTA CONC. GROUP NUMBER SURV.DATE PLACING SURV.DATE PLANNED PLACING TO TO EFFECT. TO EFFECT.
, PLANNED SURV. DATE SURV.DATE i SURV.DATE (HRS) (HRS) l (HRS)
HOOP 1 Jan.1,1982 47,448 Mar 31,1982 +2160 49,608 i 1 2 Jan.1,1984 64,968 Nov.30,1983 -744 64,224 , 3 Jan.1,1986 82,512 Nov 30,1985 -720 81,792 4 Jan.1,1991 126,360 Feb.28,1990 7080 119,280 4 DOME 1 Jan.1,1982 32,016 Apr. 20,1982 +2640 34,656 2 Jan.1,1984 49,536 Nov.30,1983 744 48,792 3 Jan.1,1986 67,080 Nov.30,1985 -720 66,360
- 4 Jan.1,1991 110,928 Feb.28,1990 -7080 103,848
REFERENCES:
- 1. V.C. Summer Structural Calculations Book Z 3D. calculation 1:183, pages 156.157 for planned surveillance dates and
! hours from concrete placement to plaraed surveillance dates.
- 2. Individual reports for each of surveillances for effective surveillance dates.
I NOTES: ;
- 1. It is sufficiently accurate to use as the effective date of the surveillance either the appmximate midpoint of the actual surveillance work (preferred) or the approximate beginning of the surveillance work.The difference between the two is typically about one month.
'CiliiDC0 D co-o^ r R:v,- o Page /D of 2i l
ENGINEERS Serial TECHNICALWORK RECORD Engineer D.Krause Date 10-13-95
- Project Title Predicted Force - Hoop and Dome Tendons Page r of_
i FileID : A:\ TENDON 6. DOC TABLE 3 - AVERAGE OF THE NORMALIZED TENDON LIFTOFF FORCES a , SURVEILLANCE HOOP TENDON GROUP DOME TENDON GROUP SOURCE
- NUMBER. (KIPS) (KIPS) 1 1238 1236 TABLE 5,3RD PERIOD SURV. REPORT 2 1206 1211 TABLE 5,3RD PERIOD SURV. REPORT 3 1176 1187 TABLE 1,3RD PERIOD SURV. REPORT 4 1123 1151 TABLES 2 2 AND 2 3, l 4TH PERIOD SURV.
REPORT 1
REFERENCE:
V.C. Summer Station Structural Calculation Book Z - 4H. pages 237 to 240. 4 4 I
Cale: DC0 2 orb -oo / Rev. D __ Page 11 of 2/ - ENGINEERS Serial TECHNICALWORK RECORD Engineer D.Krause Date 10-13-95 ProjectTrtle Predicted Force - Hoop and Dome Tendons Page (, of _ FileID t A:\ TENDON 6. DOC 1.5 RESULTS 1.The results of this calculation are shown in Table 4. Table 4 provides the Base Value predcted liftoff force for the selected and adjacent hoop and dome tendons for the 5th tendon surveillance scheduled for April 1996.The values for 0.95 Base and 0.90 Base are also shown.The same approach can be used for the liftoff force prediction for hoop and dome tendons for the surveillances beyond the 5th surveillances.
- 2. When calculating the predicted liftoff forces for a given surveillance, it is recommended that the data point for the nnrman=A group average liftoff force for the tendons in a group from the previous surveillance be added to the plot of data from all previous surveillances and the best fit straight line be reconstructed through all the available data points.
This means that a calculation to determine predeted liftoff forces for each surveillance will be done at any time in the interval following the previous surveillance and prior to the current surveillance. This work could be done at the time the group average curve is replotted during the evaluation of the data from a given surveillance. NOTES FOR TABLE 4 ON THE FOLLOWING PAGE:
- 1. Normalization factors are from Table 5 in SP-228.
- 2. Predicted forces are based on extrapolating the existing surveillance data from the first four tendon surveillances to the planned time for the 5th surveillance, i
ENGINEERS Serial s TECHNICAL WORK RECORD Engineer D.Krause Dats 10-13-95 Project Title Predicted Force - Hoop and Dome Tendons Page 7 of_ FileID : A:\ TENDON 6. DOC , TABLE 4 - PREDICTED DOME AND HOOP TENDON LIFTOFF FORCES 5th TENDON SURVEILLANCE (1) (2) (3) = (1) - (2) TENDON GROUP TENDON GROUPAVE. NORMAL. BASE VALUE 0.95 BASE VALUE 0.90 BASE VALUE NUMBER NORM. FORCE FACTOR PREDICTED (KIPS) (KIPS) FORCE (KIPS) l DOME D111 1120 26 1094 1039 984
" 1040
, Dil2 1120 -36 1156 1098 ;
" 949 D113 1120 65 1055 1002 " 994 D225 1120 15 1105 1049 " 1064 1008 l D226 1120 0 1120 " 1017 D227 1120 -10 1130 1073 " 1078 1021 l D324 1120 -15 1135 .
D325 1120 36 1084 1147 1029 1089 975 1032 Th m
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D326 1120 -27 l o
- HOOP 12AC 1076 25 1051 998 945 O l 13AC 1076 -44 1120 1064 1008 14AC 1076 26 1050 997 945 29CB 1076 -3 1079 1025 971 2*
30CB 1076 28 1048 995 943 31G 1076 -43 1119 1063 1007 S. o s 42BA 1076 59 1017 966 915 uD 43BA 1076 -25 1101 993 990 ~ y 44BA 1076 3 1073 1019 %5 , I D A
l t Figure 2-1 Dome Tendons Force-Time Curve ' (Average Of Normalized Surveillance Forces) TIME AFTER AVERAGE DATE OF CONCRETE PLACEMENT (HOURS) 10' 2x10' 4x10' 6x10' 8x105 1 05 2x105 4x105 6x105 1400 -- , l . ; i ; ,. , i , i i l i I I I I _ _.
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l 6 be= h had w w w in-w 'mmen w w e w ,,,, w l l TABLE 5-1. MEASURED VS. PREDICTED FORCES FOURTH SURVEILLANCE - VERTICAL TENDONS (1) (2) (3) (4) (5) (6) (7) Average Group Predicted % of Predicted % of Liftoff Average Normalizing Liftoff Base Predicted Liftoff Force Base Predicted Force Force Factor Force Force (Kips) Force Tendon No. (Kips) (Kips) (Kips) (Kips) [(1) + (4)] 100 (2) - (3) 1(1) + (6)l 100 Method 2 g_{g) Method 1 98.4 4'i V1 1170 1190 +1 1251 93.5 1189 V2 1161 1190 +23 1228 94.5 1167 99.5 94.1 1200 98.9 4'8 V3 1187 1190 -10 1262
#'8 V4 1188 1190 +12 1242 95.7 1178 100.8 99.2 8 V5 1193 1190 -13 1264 92.4 1203 94.7 1204 99.4 4'l V7 1197 1190 -14 1264 1190 -9 1258 95.3 1199 100.0 k'l VS1 1199 101.4 4e6 V63 1216 1190 -9 1259 96.6 1199 100.8 8 V90 1187 1190 +12 1239 95.8 1178 1190 -12 1264 96.4 1202 101.3 44 V94 1218 ave.= s.19.
_Hotes:
- 1. Fourth period surveillance tendons experiencing jack stressing adaptor rotation during liftoff as W cf well as previously retensioned tendons are excluded from this comparison. $S !R."
- 2. Method 1 - Method used for predicted forces for fourth surveillance. -
Method 2 - Proposed method to predict liftoff forces for future surveillances. 8 J bO 8
-e M 3 O
W bed heel bed bema ha J lemm4 bas 4 immed immed head and W u w d amas fW humul TABLE 5-2. MEASURED VS. PREDICTED FORCE 5 FOURTH SURVEILLANCE - DOME TENDONS (4) (5) (6) (7) l (1) (2) (3) % of Average Group Predicted % of Predicted l Average Normalizing Liftoff Base Predicted Liftoff Force Base Predicted Liftoff Force Force Force Factor Force Force (Kips) (Kips) (Kips) (Kips) [(1) + (4)] 100 (2) - (3) [(1)Method
+ (6)1 Tendon No. (Kips)
Method 1 2 100 bN 1213 95.4 2.5 0116 1157 1151 -62 1245 92.9 98.5 1136 101.3 2.B 0119 1151 1151 +15 1168 99.5 1119 102.3 2. 6 D211 1145 1151 +32 1151 0 1182 96.9 1151 99.5 2/o D226 1145 1151 1178 97.4 1143 99.7 2.3 ' 0303 1147 1151 +8 98.8 1167 101.5 2.1 D332 1185 1151 -16 1200 NE = 2.G . $o Notes:
- 1. Fourth period surveillance tendons experiencing jack stress adaptor rotation during liftoff as well as previously retensioned tendons are exc Nded from this comparison.
- 2. Method 1 - Method used for predicted forces for fourth surveillance. '
Method 2 - Proposed method to predict liftoff forces for future surveillances. [d' W$O O N a O
- s A
I; 2 , at
-s a
O C-
U W 6J 6- J 6J n- J 61 W 6 mi bei 6A b-J 6J 'emed W y '
.- d famed W TABLE 5-3. MEASURED VS. PREDICTED FORCES FOURTH SURVEILLANCE - Il00P TENDONS (3) (4) (5) (6) (7)
(1) (2) % of Average Group Predicted % of Predicted Liftoff Average Normalizing Liftoff Base Predicted Liftoff Force Base Predicted Force Force Factor Force Force (Kips) Force Tendon No. (Kips) (Kips) (Kips) (Kips) [(1) + (4)] 100 (2) - (3) 1(1)Method
+ (6)]2100 U\,bg)
Hethod 1 101.4 61 8 7AC 1172 1123 -33 1218 96.2 1156 101.8 E3 12AC 1118 1123 +25 1159 96.5 1098 4'N 1123 -44 1228 92.9 1167 97.8 13AC 1141 96.9 E 1123 -53 1241 91.9 1176 ISBA 1140 1123 +7 1179 91.7 1116 96.9 16BA 1081 1123 +15 1171 94.1 1108 99.5 32AC 1102 1123 -10 1195 93.8 1133 98.9 33AC 1121 1123 +50 1136 92.7 1073 98.1 34AC 1053
+58 1128 97.4 1065 103.2 34CB 1099 1123 100.9 6'3 43AC 1167 1123 -34 1221 95.6 1157 105.5 6'b 46AC 1141 1123 +41 1145 99.7 1082 Notes:
- 1. Fourth period surveillance tendons' experiencing jack stressing adaptor rotation during liftoff as $ p well as previously retensioned tendons are excluded from this comparison. O
- 2. Method 1 - Method used for predicted forces for fourth surveillance, o Method 2 - Proposed method to predict liftoff forces for future surveillances. ;
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ES-412 ATTACHMENT I REVISION 1 PAGE 2 OF 2 SOUTH CAROLINA ELECTRIC & GAS COMPANY PAGE REVISION
SUMMARY
2 OF Y ! CALCULATION NO. DC03050-001 . REV NO.
SUMMARY
DESCRIPTION 1 The purpose of revision 1 of this calculation is to correct an error in revision 0 of this calculation. The error in the
; original calculation is contained on page 12 of 21. The j corrected page follows this page. This revision corrects the 95% base value for hoop tendon 43BA. This was simply a mathematical error I
1 I i 1 0 CONTINUES ON PAGE ES-412/ATTACHMENTI/ REVISION 1
.- _ = . - - . . . _ - _ . _ . - - _ -- . .
ES412, AttachJ,Rev.1 SUBJECT CODE SOUTH CAROLINA ELECTRIC AND GAS COMPANY PAGE 305 CALCULATION RECORD 1.e af ,. CALC TITLE CALC NO. REV STAT CORRECTED 98% BASE PREDICTION FOR 43BA DC03060401 1 /A lL6usissIs PARENT DOCUMENT SYSTEM SAFETY CLASS STP0140.001 BS NN QR SR ORIGINATOR DISC ORGANIZAllON DATE XREF NO. PARSONS, G. P. CS SCE&G DE 1/18/96 DC03060401 3 et CALCUMTIONINFORMATION CONTENT DESCRIPTION. THIS CALCUMTION REVISION CORRECTS THE 96% BASE VALUE PREDICTED TENDON FORCE FOR HOOP TENDON 43BA FOR THE FIRTH PERIOD SURVEILLANCE. AFFECTED COMPONENTS / ANALYSIS: HOOP TENDON 43BA .
.FORINFORMATION ONLY CONTAINS PRELIMINARY DATA / ASSUMPTIONS: @ NO O YES, PAGES
, COMPUTER PROGRAM USED: @ NO O YES, VALIDATION NOT REQ'D. [REF. 3.5] O YES, VALIDATED [OTHERS]
- 0 YES, VALIDATED [ES.412] O PROGRAM VALIDATION CALCULATION 2
B. VERIFICATION VERIFICATION SCOPE YERIFY THE MAIli.lS_CDBRECT. VERIFIER: WHORTON, R. B.
- ASSIGN BY
- WHORTON, R. B. ///p/f(,
~ ~ M ENGINEER (DESIGNE@ATI!
I APPROVAL /DATE VERIFIER / DATE 1 RJhp il 16 / 9 <, Rah ilis /% i C. RECORDS REEL NUMBER: 1 f FRAME NUMBER: 4 TO PRS: INIT/DATE ORIGINAL MAINTAINED BY: SCE&G DE : I DISTRIBUTION: CALC FILE [ ORIGINAL] PDE / SYSTEM ENG /DE FILE 20.6602 [ ATTACH.1 ONLY, COPY)
ENGINEERS Serial 10606 TECHNICAL WORK RECORD Engineer G, Pamons Date 1/18/9 6 ProjectTitle RB Hooo and Dome Tendon Force Calculations Pagel of_ Cale: DC0 3cre- oo i Rev. ' A. PURPOSE: Page 3 of y . The purpose of revlolon 1 of this calculation le to correct an error in revielon O of this calculation. The error in the original calculation le contained on page12 of 21. The corrected page follows this page.
- B. DESIGN INPUTS
- ,
The revlelon to thle calculation le a correction to the previous revision. This revielon has no inpute. This reviolon elmply correcte a calculation of the previous revielon. 2 > C. COMPUTER CALCULATIONS: There are no computer calculatione in thle revielon. D. ASSUMPTIONS: - 4 There are no assumptione in thle revlolon which require future conformation. i E. METHODOLOGY: l The methodology used in making thle revielon is identical to the methodology used in the base i calculation. F. CALCULATION DOCUMENTATION: Calculation documentation le contained in the following page. G.
SUMMARY
This reviolon corrects the 957. base value for hoop tendon 43BA. This was simply a mathematical error. Note: These values are rounded down to the nearest whole number.
T l l I l ENGINEERS Serial TECHNICAL WORK RECORD Engineer D.Krause Date 10-13-95 Project Title Predicted Force - Hoop and Dome Tendons Page 7 of_ FileID : A:\ TENDON 6. DOC , l TABLE 4 - PREDICTED DOME AND IlOOPTENDON LIFTOFF FORCES Sth TENDON SURVEILLANCE (1) (2) (3) = (1) - (2) GROUP AVE. NORMAL. BASE VALUE 0.95 BASE VALUE 0.90 BASE VALUE TENDON GROUP TENDON I NUMBER NORM. FORCE FACTOR PREDICTED (KIPS) (KIPS) FORCE (KIPS) 26 1094 1039 984 DOME Dill 1120 1156 1098 1040 Dil2 1120 -36 Dil3 1120 65 1055 1002 2h 949
'a E D225 1120 15 1105 1049 g 994 D226 1120 0 1120 1064 g 1008 " -10 1130 1973 1017 D227 1120
{ D324 1120 -15 1135 1078 0 1021 . y[k
" 36 1084 1029 ?' 975 D325 1120 " -27 1147 1089 o 1032 9, .
D326 1120 R ' 0 g 945 IlOOP 12AC 1076 25 1051 998 1008 Q 13AC 1076 -44 1120 1064 D 14AC 1076 26 1050 997 ,q $ 945 - 29G 1076 -3 1079 1025 - 971 $*
" 28 1018 995 943 30CD 1076 1076 -43 1119 1063 1007 R o 31CD s 42BA 1076 59 1017 915 MD r -993- l oV F 990 ,$ i 43BA 1076 -25 1101 " 3 1073 ~1019 965 f 44BA 1076 D
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