ML20138J152
| ML20138J152 | |
| Person / Time | |
|---|---|
| Site: | Davis Besse  |
| Issue date: | 08/28/1995 |
| From: | Osting S TOLEDO EDISON CO. |
| To: | |
| Shared Package | |
| ML20138J127 | List: |
| References | |
| C-CSS-100.03-01, C-CSS-100.03-013-R01, C-CSS-100.03-1, C-CSS-100.03-13-R1, NUDOCS 9705080052 | |
| Download: ML20138J152 (48) | |
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ATTACHMENT A SHEET
- 0F 9 4 f' PAGE NO. 1 C-C5 5 -lo b 0 3- C43 CALC.N0. ID: Toledo Edison I
- 8 T A A D - III *
!
- Revision 20.0b *
- Proprietary Program of *
- Research Engineers, Inc. *
!
- Date= APR 20, 1995
- d
- Time = 9:51:29 *
- USER ID: Toledo Edison *
- 1. STAAD SPACE
- 2. UNIT INCH KIPS
- 3. JOINT COORDINATES
- 4. 1 0. O. O.
- 5. 2 0. 22. O.
- 6. 3 0. 36.5 0.
- 7. 4 0. 54. D.
- 8. 5 O. 62.5 0.
- 9. 6 0. 76.5 0.
- 10. 7 0. 98. O.
- 11. 8 -20. 22. O.
- 12. 9 -20. 54. O.
- 13. 10 20. 36.5 0.
- 14. 11 20. 62.5 O.
- 15. 12 20. 76.5 0.
- 16. MEMBER INCIDENCES
- 17. 112
- 18. 22 3
- 19. 3 3 4
- 20. 4 4 5
- 21. 5 5 6
- 22. 667
- 23. 78 2
- 24. 89 4
- 25. 9 3 10
- 26. 10 5 11
- 27. 11 6 12
- 28. MEMBER PROPERTIES
- 29. 1 TO 6 PRIS AX 1.95 IX .1 IY 1.107 YD 4.875 IZ 4.062 ZD 1.625
- 30. 7 TO 11 PRIS AX 1.11 IX .1 IY .478 YD 3.25 IZ .93 ZD 1.625
- 31. SUPPORTS
- 32. 1 FIXED BUT MY MZ
- 33. 7 FIXED BUT FY MY MZ
- 34. CONSTANTS
- 35. E 29000. ALL
- 36. DEN .000283 ALL
- 37. LOAD 1
- 38. SELF X .96
- 39. SELF Y -1.
- 40. JOINT LOAD
- 41. 8 TO 10 FX 216
- ._ . - - - . .- .~ . - .. _ -. - _.. - .. - - _ _ . - . - . ._ - -. . _= . _ .--
i 1 STAAD SPACE ATTACHMENT- ^ -- PAGE NO. 2 i SHEET 3 Of 9 ID: Toledo Edison [l f
- 42. 8 TO 10'FY .225 L CALC.N0. c -c 5 5-too .0 2-o t2
- 43. 11 FX .325 j 44, 11 FY .338 4
- 45. 12 FX .432 ~ ~ ~ ~ ;
l'
- 46. 12 FY .45 !
- 47. LOAD 2
- 48. SELF X .96 !
, 49. SELF Y -1.0 !
- 50. JOINT LOAD ;
i 51. 8 TO 10 FX .216 1 l 52. 8 TO 10 FY .225 {
1
- 53. 11 FX .325 i s 54. 11 FY .338
- 55. 12 FX .432 j
. 56. 12 FY .45 !
l 57. PERFORM ANALYSIS ,
e i
- PROBLEM STATISTICS ,
a l NUMBER OF JOINTS / MEMBER + ELEMENTS / SUPPORTS = 12/ 11/ 2 i
- ORIGINAL / FINAL BAND-WIDTM = 7/ 3 I TOTAL PRIMARY LOAD CASES = TOTAL DEGREES OF FREEDOM =
2, 65 i SIZE OF STIFFNESS MATRIX = 1560 DOUBLE PREC. WORDS REQRD/ AVAIL. DISK SPACE = 12.04/ 156.5 MB, EKMEM = 12.90 MB
) ++ PROCESSING ELEMENT STIFFNESS MATRIX. 9:51:32 2
++ PROCESSING GLOBAL STIFFNESS MATRIX. 9:51:32 l j ++ PROCESSING TRIANGULAR FACTORIZATION. 9:51:32 [
i 4
00$ WARNING - IMPROPER LOAD WILL CAUSE INSTABILITY AT JOINT 12 i j DIRECTION = MY PROBABLE CAUSE MODELING. PROBLEM 0.455E-12 !
++ CALCULATING JOINT DISPLACEMENTS. 9:51:32 l f ++ CALCULATING MEMBER FORCES. 9:51:32 l j
1 l 58. PRINT MEMBER FORCES i
1 I
k i
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0 J
f
STAAD SPACE .IIACHMENT A SHEET H OF T -- PAGE NO. 3 l C. NO. C- CSI- f oo 0 3 -o G MEMBER'END FORCES STRUCTURE TYPE.= SPno" ALL UNITS ARE -- KIPS INCH '
i
- MEMB LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
! 1 1 1 1.55 -0.77 0.00 0.00 0.00 0.00 2 -1.54 0.76 0.00 0.00 0.00 -16.78 2 1 1.55 0.54 0.00 0.00 0.00 0.00 2 -1.54 -0.53 0.00 0.00 0.00 11.70 a
2 1 2 1.31 -0.54 0.00 0.00 0.00 21.35 3 -1.30 0.53 0.00, C.00 0.00 -29.05
- 2 2 1.31 0.30 0.00 0.00 0.00 -7.14 l
3 -1.30 -0.30 0.00 0.00 0.00 11.49
! 3 1 3 1.07 -0.31 0.00 0.00 0.00 24.49
! 4 -1.06 0.30 0.00 0.00 0.00 -29.75 2 3 1.07 0.07 0.00 0.00 0.00 -16.05 4 -1.06 -0.06 0.00 0.00 0.00 17.27 4 1 4 0.82 -0.07 0.00 0.00 0.00 34.31 5 -0.82 0.07 0.00 0.00 0.00 -34.92 l 2 4 0.82 -0.16 0.00 0.00 0.00 -12.71 5 -0.82 0.16 0.00 0.00 0.00 11.35 5 1 5 0.48 0.26 0.00 0.00 0.00 28.10 l 6 -0.47 -0.27 0.00 0.00 0.00 -24.38 2 5 0.48 -0.49 0.00 0.00 0.00 -18.18 6 -0.47 0.50 0.00 0.00 0.00 11.23 6 1 6 0.01 0.71 0.00 0.00 0.00 15.32 7 0.00 -0.72 0.00 0.00 0.00 0.00 2 6 0.01 -0.94 0.00 0.00 0.00 -20.29 7 0.00 0.95 0.00 0.00 0.00 0.00 7 1 8 -0.22 -0.23 0.00 0.00 0.00 0.00 2 0.22 0.23 0.00- 0.00 0.00 -4.56 2 8 0.22 -0.22 0.00 0.00 0.00 0.00 2 -0.22 0.23 0.00 0.00 0.00 -4.56 8 1 9 -0.22 -0.22 0.00 0.00 0.00 0.00 4 0.22 0.23 0.00 0.00 0.00 -4.56 2 9 0.22 -0.23 0.00 0.00 0.00 0.00 4 -0.22 0.23 0.00 0.00 0.00 -4.56 9 1 3 0.22 0.23 0.00 0.00 0.00 4.56 10 -0.22 -0.22 0.00 0.00 0.00 0.00 2 3 -0.22 0.23 0.00 0.00 0.00 4.56 10 0.22 -0.22 0.00 0.00 0.00 0.00
..e, ,
l 1
! A SHEET C OL9-'
STAAD SPACE 'll: a ACHMENT -- PAGE NO. 4 4
(.i '.C. N0. c-us-tod,o3-o o _ _ ID: Toledo Edison MEMBER END FORCES STRUCTURE TYPE - 6? ACE - - - -
i ALL UNITS ARE -- KIPS INCH MEMD LOAD JT AXIAL SHEAR-Y SHEAR-Z TOPSION MOM-Y MOM-Z 10 1 5 0.33 0.34 0.00 0.00 0.00 6.82 11 -0.33 -0.34 0.00 0.00 0.00 0.00 2 5 -0.33 0.34 0.00 0.00 0.00 6.82 11 0.32 -0.34 0.00 0.00 0.00 0.00 11 1 6 0.44 0.46 0.00 0.00 0.00 9.06 12 -0.43 -0.45 0.00 0.00 0.00 0.00 2 6 -0.44 0.46 0.00 0.00 0.00 9.06 12 0.43 -0.45 0.00 0.00 0.00 0.00
- 0*********** END OF LATEST ANALYSIS RESULT **************
- 59. PRINT SUPPORT REACTIONS 1
I I
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I
~ !ACHMENT A SHEET 0 0F 9 i STAAD SPACE -- PAGE NO. 5 C. NO. c-CSS- 00 0-ot3 ID: Toledo 'dison E
i SUPPORT REACTIONS -UNIT KIPS INCH 61huvivaE lire - APACE '
JOINT LOAD FORCE-X FORCE-Y FORCE-Z MOM-X MOM-Y MOM Z ;
l' 1 0.77 1.55 0.00 O.00 0.00 0.00 I 2 -0.54 1.55 0.00 0.00 0.00 0.00 7 1 0.72 0.00 0.00 0.00 0.00 0.00 '
2 -0.95 0.00 0.00 0.00 0.00 0.00 l
l
- END OF LATEST ANALYSIS RESULT ************** ]
- 60. PRINT MEMBER STRESSES
)
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i
f STAAD SPACE -- PAGE NO. 6 ATTACHMENT - A SHEET 7 0F A ID: T led Edison
~
MEMBER STRESSES ALL UNITS ARE KIPS /SQ INCH 1
MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z l 1 1 .0 0.8 C 0.0 0.0 0.8 0.4 0.0 1.00 0.8 C 0.0 10.1 10.9 0.4 00 2 .0 0.8 C 0.0 0.0 0.8 0.3 0.0 j ' :L . 0 0 0.8 C 0.0 7.0 7.8 0.3 0.0 j
! 1 2 1 .0 0.7 C 0. Ct 12.8 13.5 0.3 0.0 1.00 0.7 C 0.0 17.4 18.1 0.3 0.0 2 .0 0.7 C 0.0 4.3 5.0 0.2 0.0 1.00 0.7 C 0.0 6.9 7.6 0.2 0.0 l 3 1 .0 0.5 C 0.0 14.7 15.2 0.2 0.0 l 1.00 0.5 C 0.0 17.9 18.4 0.2 0.0 2 .0 0.5 C 0.0 9.6 10.2 0.0 0.0 1.00 0.5 C 0.0 10.4 10.9 0.0 0.0 4 1 .0 0.4 C 0.0 20.6 21.0 0.0 0.0 l
1.00 0.4 C 0.0 21.0 21.4 0.0 0.0 2 .0 0.4 C 0.0 7.6 8.0 0.1 0.0 1.00 0.4 C 0.0 6.8 7.2 0.1 0.0 f 5 1 .0 0.2 C 0.0 16.9 17.1 0.1 0.0 1.00 0.2 C 0.0 14.6 14.9 0.1 0.0 2 .0 0.2 C 0.0 10.9 11.2 0.3 0.0 1.00 0.2 C 0.0 6.7 7.0 0.3 0.0 6 1 .0 0.0 C 0.0 9.2 9.2 0.4 0.0 1.00 0.0 C 0.0 0.0 0.0 0.4 0.0 2 .0 0.0 C 0.0 12.2 12.2 0.5 0.0 1.00 0.0 C 0.0 0.0 0.0 0.5 0.0 7 1 .0 0.2 T 0.0 0' 0. 0.2 0.2 0.0 1.00 0.2 T 0.0 8.0 8.2 0.2 0.0 2 .0 0.2 C 0.0 0.0 0.2 0.2 0.0 1.00 0.2 C 0.0 8.0 8.2 0.2 0.0 i 8 1 .0 0.2 T 0.0 0.0 0.2 0.2 0.0 1.00 0.2 T 0.0 8.0 8.2 0.2 0.0 2 .0 0.2 C 0.0 0.0 0.2 0.2 0.0 1.00 0.2 C 0.0 8.0 8. 2 . 0.2 0.0 1 l
9 1 .0 0.2 C 0.0 8.0 8.2 0.2 0.0 1.00 0.2 C 0.0 0.0 0.2 0.2 0.0 2 .0 0.2 T 0.0 8.0 8.2 0.2 0.0 1.00 0.2 T 0.0 0.0 0.2 0.2 0.0 l 10 1 .0 0.3 C 0.0 11.9 12.2 0.3 0.0 I 1.00 0.3 C 0.0 0.0 0.3 0.3 0.0 l 2 .0 0.3 T 0.0 11.9 12.2 0.3 0.0 l 1.00 0.3 T 0.0 0.0 0.3 0.3 0.0 ,
l
. _ . _ _ _ . ~ - . _ _ _ _ . . . _ . _ . . _ _ . . . _ _ _ _ . . _ _ _ _ _ . . . . _ . . . _ _ . _ _ _ . . _ _ . _ . _ __
1
~'
STAAD SPACE -- PAGE NO. 7 ATTACHMENT- A SHEET 2 O' q ID: Toledo Edison i CI L C. No. C- C 5.5 -00.0 3_--09 4
MEMBER STRESSES f j
' ~ ~ ~ ~
ALL UNITS ARE KIPS /SQ INCH j MEMB-
^
LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAP-Z l
11 1 .0 0.4 C 0.0 15.8 16.2 0.4 0.0 i i 1.00 0.4 C 0.0 0.0 0.4 0.4 0.0 l l 2 .0 0.4 T 0.0 15.8 16.2 0.4 0.0 I 9 1.00 0.4 T 0.0 0.0 0.4 0.4 0.0 J l
- 00*********** END OF LATEST ANALYSIS RESULT **************
l
- 61. PRINT JOINT DISPLACEMENTS i
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W ACHMENT- A SHEET _3_ b . 9 STAAD SPACE -- PAGE NO. 8
,i Cl LC. N0. C -C CHoo 03 -o 13. - ID: Toledo Edison j I '
JOINT DISPLACEMENT (INCH RAurans; ornvu2vns 1YPE = SPACE l
JOINT LOAD X-TRANS Y-TRANS Z-TRANS .X-ROTAN Y-ROTAN Z-ROTAN l 1 1 0.00000 0.00000 0.00000 0.00000 0.00000 0.00779 l 2 0.00000 0.00000 0.00000 0.00000 0.00000 -0.00420 l 2 1 -0.15983 -0.00060 0.00000 0.00000 0.00000 0.00622 l 2 0.08443 -0.00060 0.00000 0.00000 0.00000 -0.00311 3 1 -0.22865 -0.00093 0.00000 0.00000 0.00000 0.00312 ;
2 0.12182 -0.00093 0.00000 0.00000 0.00000 -0.00196
~
4 1 -0.24904 -0.00126 0.00000 0.00000 0.00000 -0.00092 2 0.13471 -0.00126 0.00000 0.00000 0.00000 0.00052 5 1 -0.23067 -0.00139 0.00000 0.00000 0.00000 -0.00341 2 0.12655 -0.00139 0.00000 0.00000 0.00000 0.00139 6 1 -0.16054 -0.00150 0.00000 0.00000 0.00000 -0.00653 I 2 0.09395 -0.00150 0.00000 0.00000 0.00000 0.00313 7 1 0.00000 -0.00150 0.00000 0.00000 0.00000 -0.00793 2 0.00000 -0.00150 0.00000 0.00000 0.00000 0.00499 8 1 -0.15997 -0.14744 0.00000 0.00000 0.00000 0.00790 2 0.08457 0.03907 0.00000 0.00000 0.00000 -0.00142 ;
9 1 -0.24917 -0.00544 0.00000 0.00000 0.00000 0.00077 '
2 0.13484 -0.03408 0.00000 0.00000 0.00000 0.00220 10 1 -0.22878 0.03889 0.00000 0.00000 0.00000 0.00143 2 0.12195 -0.06261 0.00000 0.00000 0.00000 -0.00364 11 1 -0.23088 -0.10330 0.00000 0.00000 0.00000 -0.00594 2 0.12676 -0.00733 0.00000 0.00000 0.00000 -0.00114 12 1 -0.16081 -0.17689 0.00000 0.00000 0.00000 -0.00989 2 0.09423 0.01644 0.00000 0.00000 0.00000 -0.00022 1
000*********** END OF LATEST ANALYSIS RESULT **************
- 62. FINISH
- END OF STAAD-III ***************
- DATE: APR 20,1995 TIME = 9:51:35 ****
- For questions on STAAD-III, contact: *
- Research Engineers, Inc at
- Ph: (714) 974-2500 Fax: (714) 921-2543 *
. - . ~ . _ . . . _ _ _ _ _ . ~ . . - . _ . _ _ . _ . . . . _ . _ _
(tm) 7.4 L IT- 53 @ .11 % .
b
, r n -- u e 2o ~ 3 36 RACEWAY INQUIRY REPORT g,4 g r TJ3 - I b
- Dawls-Besse Nucteer Power Station gg_g g ,e3 W 000 Ltf- 23 $ e il ---) 3. (3 Raceway ID Status Serv Layout Length Card Last Rev BLFA12 PSC Lvl Drawing No. Eng Act Rev 11/22/88 L C 7. ' 6 b' O' Rwy Code: T3 C 7 L E356 45 50 12:01 L4 P-l3 @ 'M '3M ;
Rwy type: Tray SU-Sys: SG: B SC: Fac: Revision: g_4 .f: ,g 5gg FCR/ MOD t DCN No Iso Dwg : g __
g Inct cab Pct filt Avail Space Overfill Wt/ unit xP- u
' 'M Design: 150 33.30 28.843 0.00 L11 - $ $ IM "
Const : 150 33.29 28.843 0.00 g_g g ,3 - y Z . 7,4
- l. L Q - 4 0
- i I4 -> O # (o l Included Cables ,
BLCOA502A(1-L1T)C BLC0A503A(1-L1T)C BLC0A504A(1-L1T)C LYP-I k '" ~
BLCC*505A(1-L17)C BLCOA506A(1-L1T)C BLC0A507A(1-L1T)C g4 - 1 g ,13 '? O
- N BLC0A508A(1-LIT)C BLCOA509A(1-L1T)C BLC0A510A(1-LIT)C BLCOA511A(1-L1T)C BLCOA512A(1-L1T)C BLC0A513A(1-L1T)C D. 9 [ hi t.
- BLC0A514A(1-LIT)C BLCCA515A(1-LIT)C BLC0A516A(1-L1T)C BLCCt.517A(1-LIT)C BLCOA318A(1-LIT)C BLC0A522A(1-L17)C C % 24" T M Y W O C. E gA BLC0A523A(1-L1T)C BLC0A324A(1-LIT)C BLC0A525A(1-L1T)C f gf g g L ,4 7,g y $ q g, 3 4 44jt BLCOA526A(1-L17)C RLCOA527A(1-LIT)C BLCOA535B(1-LIT)C BLC0A550A(1-LIT)C BLC0A603A(1-L1T)C BLC0A604A(1-L1T)C BLCC*.605A(1-L1T)C BLCOA613A(1-L1T)C BLC0A619A(1-L17)C 55 % Dr#, l BLC0A624A(1-L1T)C BLC0A627A(1-L17)C BLC0A628A(1-LIT)C ,
BLCOA637A(1-LIT)C BLCOA638A(1-L17)C BLC0A639A(1-L1T)C f BLC0A640A(1-L1T)C BLCOB504A(1-TJ2)C BLCOB505A(1-TJ2)C A
Q BLCOB506A(1-TJ2)C BLCOB510A(1-TJ2)C BLCOB507A(1-TJ2)C BLCOBS11A(1-TJ2)C BLCOB508A(1 TJ2)C BLCOB512A(1-TJ2)C
- E y %>b l 2
CLCOB513A(1 TJ2)C BLCOB514A(1-TJ2)C BLCOB533A(1-TJ2)C . P E BLCC0535A(1-TJ3)C BLCOB542C(1-TJ1)C BLCOB542D(1-TJ1)C I BLCOB542E(1 TJ1)C BLCOB542F(1-TJ1)C BLCOB543D(1-TJ1)C q g BLCOB546A(1-TJ1)C BLCOE538A(1-L4P)C BLCCF520A(1-L4P)C '
BLC0J503A(1 i1P)C BLC0J505A(1-L4P)C BLC0J508A(1-L1P)C. U g BLC0Y101A(1-LC2)C BLC0Y102A(1-LC2)C BLC0Y103A(1-LC2)C Y BLC0Y104A(1-LC2)C BLC0Y124A(1-LC4)C BLC0Y126A(1-LC4)C BLC0Y142A(1-LC2)C BLC0Y143A(1-LC2)C BLC0Y144A(1-LC2)C , y f' BLC0Y145A(1 LC2)C BLCV1 B(1 L1T)C BLCV1 C(1-L1P)C O BLCV2 B(1 L17)C BLCV2 C(1-L1P)C BLCV3 B(1-L1T)C % .c { y f BLCV3 C(1-L1P)C BLCV4 B(1-L1T)C BLCV4 C(1-L1P)C h 9 -
BLDESTf.01(1-L58)C BLICS183M(1-L1P)C BLMY4532C(1-L1P)C BLISV1 B(1-L17)C BLICS183D(1-L1P)C BLISV2 B(1-LIT)C h(-a 61 W
'1 BLISV3 B(1-L1T)C BLISV4 B(1-LIT)C BLIV1 B(1 LIT)C og EtlVI D(1-L1P)C BLIV2 8(1 L1t)C BLIV2 D(1-L1P)C l
Bllv3 8(1 L17)C SLIV4 B(1-L1T)C SLL3401A(1-L58)C 8LL34018(1-L58)C BLME510 A(1-LXP)C BLME512 A(1-L4P)C BLME513 A(1-LXP)C BLME514 A(1 L4P)C BLME518 A(1-L&P)C BLME521 A(1-L&P)C SLME522 A(1-L1P)C BLME523 A(1-L1P)C i
' 8LME525 A(1 L1P)C 8LME548 A(1-L1P)C BLME548 C(1-L1P)C ,
BLME548 D(1-L1P)C BLME550 A(1-L&P)C BLME551 A(1-L4P)C BLME569 A(1-L4P)C BLME576 A(1-LXP)C SLME640 A(1-L1T)C BLME641 A(1-L1P)C BLN41121(1-L21)C' BLNN1122(1-L21)C 8LN41123(1-L21)C 8LN4113E(1-L20)C BLNul13G(1-L20)C ,
SLNN113N(1-L20)C 8LN41141(1-L20)C BLNN1143(1-L20)C BLN11144(1-L20)C 8LNN1145(1-L20)C BLNN1146(1-L20)C ,
8LN41194F(1-L1P)C 8LSPARE21(1-L1P)C BLSPARE25(1-L1P)C BLSPAREA1(1-L10)C BLSPAREA2(1-L10)C BLSPAREA3(1-L10)C SLSP"REf.4(1-L10)C BLSPAREE4(1-LTP)C BLSPAREG5(1-L58)C ;
SLT02 C(1-L4P)C BLT09 A(1-L1P)C BLT09 B(1-L4P)C 8LT09 C(1-L1P)C SLT09 D(1-L1P)C BLT09 E(1-L1P)C BLT09 F(1-L1P)C BLT09 G(1 L1P)C BLT09 1(1-L1P)C.
BLT09 J(1-L1P)C BLT10 A(1-L1P)C BLT10 B(1-L1T)C BLT10 C(1-L1P)C BLT10 J(1-LIT)C BLT11 A(1-L1T)C t BLT11 8(1 L1P)C 8LY11 C(1-L1P)C CLNF5878(1-L4P)C Recency Links..: 27079A 47180A 47181A BLP77A BLWD11 T-BLPA11/8LPA21 T BLPA13/BLWD11 Wrap / Zone /Lgth.: N/422A/0
- END OF REPORT -- NORMAL TERMINATION ** j__g > ' I 5ho lli!C 2:
l 5
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C Cn T__
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. . _ - . . . _ . . _ . - _ _ _ _ _ _ _ _ _ . _ _ _ _ - _ . _ . _ _ _ _ _ . _ _ _ _ _ _ _ _ . _ .__ _ _. _____ _ _ _ ____ ,-__.__.m. - -.-c _ _ _ - _ _ _ __ - _. ._ - - ,_ - - _ r_.- _ _ _ _ . _ _ _ _ _ _ _ _
Cable ACSPARC0100 cannot be routed through Recewey ACPG52' . .j .
because the Raceway is Sep Grow incespotibts ~~
GA*(e) DETECTED DURING ROUTING CJ CABLE ACSPARE0100 BETWEEN:
"FROM" equipment (MA01) and first recewey (ACPG52*)
Lett Racewey (ACPG52*) and "To" e gipment (C57618)
Included cables for Racewey ACPG52*
CABLE ID DWG NO ACSPIRE010D E488
'"*'"' (t-MD ' IT@ .34%r =- 5.to"/rz Included cables for Raceway ACPG52* [f - Ec 1) ? IO @ .IL -- 1. (c o CAM E ID M NO { g _ g7_, , j @ 43 ,,~ *f '
ACSPARE010D E488 END LIST (l-(og ) * @ h .M r 3. 2 O 04-16-95 (I'CIO) 15
- 1\ =
2.53 %$
S:troute(tm)'(.4 {y_{q e, g @ ,ZG _
[g b-Cll) i 7bei0
~
RACEWAY INOUIRY REPORT b OO o
Davis-Besse Nucteer Power Station o-cos) : 7 @.43 = M3 g t
Status Serv Layout Length Card Lost Rev (1- C.2 O) ". i @ 09 -
- ,O9 0 1
Receway ID ACPG51 PSC Lvl Drawing No. Eng Act Rev 11/22/88 h - C2.2.] ; I h ,2.2. O , 7 2. $ l Rwy Code: T3 C 7 C E356 15 14 12:01 ~~ b Fac: Revision: C ! ' (2O) 4 @
- 2G /* W Rwy type: Trey SU-Sys: SG: A SC: L FCR/ MOD : DCN No : Iso Dwg : ,
_ ,g h
(,a Inct cab Pet filt Avell Space Overfill Wt/ unit u ;
Design: 95 31.88 30.375 6.70 g _ Lj p ') ,
( @ ,d -
, ll ;
31.88 30.375 6.70 Q r const : 95 Ci- L4e) : 2 G,zo = .sc ,
included Cables Act::AM A(1-C10)C ' AC1PAM A(1-C10)C ' AC1PNAM A(1-C10)C'
~~
I) - Ik ' If ~~
ACAACC2 C(1-C12)C ' ACAACC2 M(1*C10)C - ACAC2031A(1-C01)C -
ACAC2032A(1-Cf"C ' ACAC205 B(1'-C12)C - ACAC205 C(1-C01)C - 22. 9 $'[l:p ACAC206 B(1-C .)C ' ACAC206 C(1-C13)C ' ACAC208 8(1-C01)C -
ACAC208 C(1-C13)C ' ACAC211 G(1-C12)C ' ACAC211 M(1-C01)C - g g y,g dg ACAC211 J(1-C01)C - ACC02172A(1-L4P)C / ACC02176B(1-LSTjC ' ,
ACC0Z188a(1-L4P)C ' ACD1AM A(1-C01)C ACD1AM 8(1-C01)C - og t j,34- g ACD1NVM A(1-C10)C ' ACD1PVM A(1-C10)C - ACD1VM A(1-C10)C ' Q ACMA01 M;1-C13)C - Acta 03 M(1-C13)C ' sb- 5 ACDAP22A(1-807)C /
h.
+
ACHA0501C(1-C11)C / ACHA05010(1-C11)C ' ACMA0501E(1-C10)C '
ACMAAC A(1-C12)C ' ACMAAC B(1-C01)C '
N ,
ACHA10028(1 C10)Ce ACMAAE2 L(1-C01)C / 53 ACMAAE2 G(1 C01)C / ACMAAE2 M(1-C12)C ' '
ACMAAE3 G(1-C01)C / ACMAAE3 M(1-C12)C ' ACMAAE3 L(1 C01)C' l ACMAAE4 D(1-C12)C / ACMAAE4 F(1-C01)C ' ACHAAE4 L(1-C01)C e y ACMx01A J(1-C10)C/ ACM).01A M(1 C10)C ' ACMx02A G(1-C13)C /
i 5
ACMX11A D(1-C10)C e ACMX110 E(1-C10)C - ACL1526 A(1-C20)C '
ACPSRC22C(1-C23)C / ACPSRC22G(1-C23)C ' ACPSRC23C(1-C23)C '
ACSPARE43(1-C10)C e ACSPARE45(1-C10)C ' ACSPARE4' Sit-807)C '
ACSPARE64(1 807)C ' ACSPARE6A(1-C23)C ' ACSPARE8A(1 L1P)C '
' ACVSP7A1G(1-C11)C /
ACSPACEAM(1-C13)C ' ACT01v(1 CS3)C ACVSP7ASE(1-C11)C - ACVSP781G(1 C11)C ' ACVSP7BSE(1-C22)C '
ACY1vM A(1-C10)C / ACY3VM A(1-C10)C / ACY45115A(1-825)C '
ACTAR12 A(1-807)C ' ACTARVM A(1-C10)C - ACTAU14 B(1-C10)C '
ACYAU14 C(1-C10)C - ACYAU28 A(1 807)C - ACYAU32 A(1-807)C -
ACYAU43 A(1-807)C - ACTAU45 A(1-807)C e ACYAU47 A(1-807)C '
ACYAU40 A(1 807)C - ACYAuvM A(1-C10)C ' CCAN3J014(1-ANN)C -
CCAN3M015(1-ANN)C - CCAN3M016(1-ANN)C - CCAN3VL11(1-AM)C -
CCAN3VL12(1-ANN)C ' CCA43VL13(1-ANN)C e CCAN4XX19(1-ANN)C-CCCNSF022(1-ANN)C ' CCAM5F023(1-ANN)C' CCAMSF024(1-ANN)C-CCAN5cP25(1-ANN)C ' CCAN50P26(1-ANN)C' CCAN5T017(1-ANN)C '
CCT5T018(1-ANN)Ce CCAN60E27(1-ANN)C -
RCtetoy liras..: ACPG50 TRAY ACPG50 TRAY ACPG52 Wrap / Zone /Lgth.: N/422A/0 O* END OF REPORT -- NORMAL TERMINATION ** ,_
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Cable ACSPARE010D cemet be routed through Receway ACPG52' because the Recewey la Sep Group incompatiblo
] ,j 04-16-95 Setreute(tm) 7.4 RACEWAY INQUIRY REPOR7 Davis-Besse Nuclear Power Station d i O - M cS) 'S @ ,% glPT = 5.\o lpr ,
R2cewey ID
- f. CPG 52 Status Serv Layout P$C Lvt Drawing No.
Length Card Last Rev Eng Act Rev 04/16/95
()_6(f g Q ,@ = gg ; Rwy Codes T3 C 7 C E356 43 43 23:01 b- DLh f @ 4b C .b ; Rwy Type: Tray SU-Sys: SG: A SC: Fac: Revision: _ y j DCN No : FCR/ MOD : Iso Dwg : Inct cab Pct fitt. Avall Space Overfilt Wt/tmit D: sign: 95 31.74 30.526 6.38 ({ -Clo] 7,qQ,}{ "
- 2,(c4 P Z I const : 95 31.74 30.526 6.38 b ~b I h Yh M
- Included Cables Q-Cid 7 @ *90 2*00 P .
Act:AM A(1-C10)C ' AC1PAM A(1-C10)C - AC1PNAM A(1-C10)C - h-C \ b ) ] ,49 ' p ACAACC2 C(1 C12)C / ACAACC2 M(1-C10)C ' ACAC2031A(1-C01)C - c _
,Og v.
( I'C2-0) {@ Ot ACAC2032A(1-C01)C - ACAC205 s(1-C12)C ' ACAC205 C(1-C01)C - . l {\-C2 ACAC206 8(1 C01)C - ACAC206 C(1-C13)C ' ACAC208 B(1-C01)C - , Q C ,Q ? g ACAC208 C(1 C13)C - ACAC211 G(1-C12)C - ACAC211 HC1-C01)C - O T ACAC211 J(1-C01)C - ACA41106A(1-LP1)C / ACC0Z172A(1-L4P)C ' bbD) 4 h '2 b !' ACC0Z176B(1 LS1)C. '" ACC0Z188A(1-L4P)C ' ACD1AM A(1-C01)C - ACD1AM 8(1-C01)C - ACD1NVM A(1-C10)C r ACD1PVM A(1-C10)C - (l-C3h }
' - '4 o
ACD1VM A(1 C10)C - ACDAP22A(1-807)C e ACHA01 M(1-C13)C - ACHA0501D(1 C11)C ' I_ g *gg _ *gg ' ACHA03 M(1 C13)C ' ACHA0501C(1-C11)C ' y Q 36 ; I% 4 ACHA0501E(1-C10)C ' ACHA1002B(1-C10)C / ACHAAC A(1-C12)C ' { } _ Q p) - ACHAAC B(1-C01)C / ACHAAE2 G(1-C01)C ' ACHAAE2 H(1-C12)C - ACHAAE2 L(1-C01)Cf ACHAAE3 L(1-C01)C ' ACHAAE3 G(1-C01)C - ACHAAE4 D(1 C12)C ' ACHAAE3 M(1-C12)Cf ACHAAE4 F(1-C01)C ' ((-(_fI) { @ ,gl 0 - i ACHAAE4 L(1 C01)C/ ACHXO2A G(1-C13)C - ACHX01A JC1-C10)C r ACMX02A Jt1 C10)C / ACMX01A M(1-C10)C - ACMXO2A M(1-C10)C ' (l- Ol)
~
l Q .Ik e
-~ ~~~~~
ACMX11A A(1-C13)C / ACMX11A D(1-C10)C ' ACMX11A E(1-C10)C e g* ACL1526 A(1-C20)C ' ACPSRC22C(1-C23)C ' ACPSRC22G(1-C23)C - b.5 f ACPSIC23C(1 C23)C ' ACSPARE43(1-C10)C ' ,
% % SPARE 45(1 ]-C10) g" g ACSPAIE49(1-B07)C ' ACSPARE6A(1 C23)C / ACSPARESA(1-L1P)C ' Q ACS7ARE9U(1 C10)C -
ACVSPTA1G(1-C11)C - ACSPAREAM(1-C13)C " ACVSP7ASE(1-C11)C ' ACT01V(1-CS3)C ACVSP7B1G(1-C11)C - g [l !* tt[ ACVSP7BSE(1 C22)C ' ACT1VM A(1-C10)C / ACY3VM A(1-C10)C ' y i,CY45115A(1-825)C ' ACYARVM A(1-C10)C ' ACTAU14 B(1-C10)C - 30.(g9gb y& ACYAU14 C(1 C10)C - ACYAU28 A(1-807)C ' ACYAU32 A(1-807)C - ACTAU43 A(1 807)C ' ACYAU45 A(1-807)C ' ACYAU47 A(1 807)C ' O ACYAU49 A(1-837)C / ACYAUvM A(1-C10)C / CCAN3J014(1-ANN)C / 9 CCA23M015(1-ANN)C ' CCAN3M016(1-ANN)C / CCAN3VL11(1 ANN)C ' -D - - - -mm= , _ _ _ '- - _ _ _ _ _ _ _ _ _- --w- : _--P s a--__+ _& -n a - _
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m_. . .. _ .. . . . . . . . _ . . ~ . . _-- . . - _ . . m ...m_.... . . _-- ._. b CCAN5F022(1 ANN)C e CCAN5F023(1 ANN)C - CCAWSF024(1-ANN)C e CCAN5cP25(1-A44)C - CCAN50P26(1-ANN)C - CCAN57017(1-ANN)C - g CCANST018(1-ANN)C f CCAN60E27(1-ANN)C - i Recewey Lir*s..: 5712A1 57742A 579941 CCP22A T-ACPG31/ACPG32 ; CCP21C i TRAY ACPG51 Notes..........t RRRR 1 i G END OF REPORT ** NORMAL TERMINATION ** s k I t P i t O M k r H , O > O 2 Z P Krn , 2 ! H p' i i O w D1 I48
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,ld is*f 6 q .Z4 FCR/ MOD : DCN No : Iso Dwg : gg g lg inct cab Pct fill Avail Space Overfill Wt/ unit ,h% h .
Design: 155 49.34 11.499 0.64 6Q] q f -lb g ' const : 147 47.80 13.176 0.48
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** END OF REPORT -- NORMAL TERMINATION ** f r
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; ; ATIACHMENT- o SHEET 2- O d t PAGE NO. 1
- '"4 C. NO. L- c 5 r-too.o3. oq ID
- toledo edison t i.
- S T A A D - III *
>
- Revision 19.0a * '
j'
- Proprietary Program of *
- RESEARCH ENGINEERS, Inc.
- 2
- Data = APR 21, 1995 *
- Time = 11: 7:40
- 4
- USER ID: toledo edison *
- *******************+******************************
] 3 1 j 1. STE%D SPACE ,
- 2. UNIT INCH KIPS
! 3. JOINT COORDINATES I 4. 1 0. O. O.
- 5. 2 0. 12. O. :
! 6. 3 0. 28. O. !
- 7. 4 0. 44. O.
! 8. 5 O. 60. O. i , 9. .6 0. 76. O. j 10. 7 0. 98. O.
- 11. 8 46. O. O.
- 12. 9 46. 12. O.
4- 13. 10 46. 28. O. ~~ l i' 14. 11 46. 44. D. l
- 15. 12 46. 60. O.
- 16. 13 46. 76. O.
i 17. 14 46. 98. O. i 18. MEMBER INCIDENCES
- 19. 112 i '20. 22 3
- i. 21. 3 3 4 l 22. 4 4 5
- 23. 55 6
- 24. 6 67 '
4
- 25. 78 9 l
- 26. 8 9 10
{ 27. 9 10 11 [ 28. 10 11 12
- 29. 11 12 13 i 30. 12 13 14 l 31.-13 2 9
- 32. 14 3 10 l 33. 15 4 11
- 34. 16 5 12 .
4 35. 17 6 13
- 36. MEMBER PROPERTIES t< 37. 1 TO 12 PRI.9 AX 1.95 IX .1 IY 1.107 YD 4.875 IZ 4.602 ZD 1.625
- 38. 13 TO 17 PRIS AX 1.11 IX .1 IY .478 YD 3.25 IZ . 93 ZD 1.625 j 39. SUPPORTS i 40. 178 14 PINNED
!. 41. CONSTANTS j -42. E 29000. ALL i 1 l f f 3
l. ( OTAAD SPACE ATIACHMENT ' SHEET 3 bi 9
* -- PAGE NO. 2 ID: toledo edison
- 43. DEN .000283 ALL CALC.N0. C -OS2 'oo 63 -oG [
44.-LOAD 1
- 45. SELF X .96 .. . l
- 46. .SELF Y -1. (
4
- 47. MEMBER LOAD ;
- 48. 13 TO 17 CON GY .45 23. I i' 49. 13 TO 17 CON GX .43 23. '
- 50. PERFORM ANALYSIS PROBLEM STATISTICS NUMBER OF JOINTS / MEMBER + ELEMENTS / SUPPORTS = 14/ 17/ 4 l ORIGINAL / FINAL BAND-WIDTH = 7/ 4 :
TOTAL PRIMARY LOAD CASES = 1, TOTAL DEGREES OF FREEDOM = 72 ! OIEE OF STIFFNESS MATRIX = 2944 DOUBLE PREC. WORDS , REQUIRED DISK SPACE = 12.06 MB, TOTAL EXMEM = 6.75 MB
++ PROCESSING ELEMENT STIFFNESS MATRIX. 11 7:43 l ++ PROCESSING GLOBAL STIFFNESS MATRIX. 11: 7:43 ' ++ PROCESSING TRIANGULAR FACTORIZATION. 11: 7:43 : ++ CALCULATING JOINT DISPLACEMENTS. 11: 7:44 ! ++ CALCULATING MEMBER FORCES. 11: 7:44 f
- 51. PRINT MEMBER FORCES i
t l i I f I
7
' ulACHMENT C SHEET _3.. b i STAAD CPACE -- PAGE NO. 3 t' N O. c-c. ss- ro o .o 3 - 33 ID: toledo edison
'~
MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ARE -- KIPS INCH HEMD LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 1 1 1 0.35 0.58 0.00 0.00 0.00 0.00 2 -0.35 -0.58 0.00 0.00 0.00 6.96 2 1 2 0.39 0.29 0.00 0.00 0.00 -3.22 3 -0.38 -0.28 0.00 0.00 0.00 7.78 3 1 3 0.32 0.06 0.00 0.00 0.00 -6.35 4 -0.32 -0.05 0.00 0.00 0.00 7.28 4 1 4 0.13 -0.17 0.00 0.00 0.00 -8.72 5 -0.13 0.18 0.00 0.00 0.00 5.95 5 1 5 -0.19 -0.42 0.00 0.00 0.00 -10.48 6 0.20 0.43 0.00 0.00 0.00 3.72 6 1 6 -0.65 -0.51 0.00 0.00 0.00 -11.30 7 0.66 0.52 0.00 0.00 0.00 0.00 7 1 8 0.98 0.79 0.00 0.00 0.00 0.00 9 -0.97 -0.78 0.00 0.00 0.00 9.40 8 1 9 0.47 0.62 0.00 0.00 0.00 -0.45 10 -0.46 -0.61 0.00 0.00 0.00 10.36 9 1 10 0.05 0.39 0.00 0.00 0.00 -3.71 11 -0.04 -0.38 0.00 0.00 0.00 9.88 ; 1 10 1 11 -0.24 0.16 0.00 0.00 0.00 -6.09 12 0.25 -0.15 0.00 0.00 0.00 8.59 11 1 12 -0.40 -0.05 0.00 0.00 0.00 -7.90 13 0.41 0.06 0.00 0.00 0.00 7.02 12 1 13 -0.42 -0.42 0.00 0.00 0.00 -9.42 14 0.44 0.43 0.00 0.00 0.00 0.00 13 1 2 -0.29 -0.04 0.00 0.00 0.00 -3.74 9 -0.16 0.51 0.00 0.00 0.00 -8.95 14 1 3 -0.22 0.06 0.00 0.00 0.00 -1.43 10 -0.22 0.41 0.00 0.00 0.00 -6.65 15 1 4 -0.22 0.18 0.00 0.00 0.00 1.44 11 -0.22 0.28 0.00 0.00 0.00 -3.78 16 1 5 -0.24 0.32 0.00 0.00 0.00 4.53 12 -0.20 0.15 0.00 0.00 0.00 -0.69
ATTACHMENT c- 5 SHEET ' 0F.S_ - STAAD SPACE -
-- PAGE NO. 4
"!1. C. NO. _C - CS S -lo o 03 -0 9 - ID: tol'd 'di8 "
MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ARE -- KIPS INCH MEMD LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 17 1 6 -0.08 0.45 0.00 0.00 0.00 7.58 13 -0.36 0.02 0.00 0.00 0.00 2.40 600*********** END OF LATEST ANALYSIS RESULT **************
- 52. PRINT SUPPORT REACTIONS i
I 4 e i
1 m 4
' ATTACHMENT c- - SHEET _L Of :i !
STAAD SPACE -- PAGE NO. 5
' c NO. c-C SS- too. o3-o #3 ID: toledo edison i SUPPORT REACTIONS -UNIT KIPS INCH STRUCTURE TYPE = SPACE i JOINT LOAD FORCE-X FORCE-Y FORCE-Z MOM-X MOM-Y MOM Z 1 1 -0.58 0.35 0.00 0.00 0.00 0.00 7 1 -0.52 0.66 0.00 0.00 0.00 0.00 8 1 -0.79 0.98 0.00 0.00 0.00 0.00
- 14 1 -0.43 0.44 0.00 0.00 0.00 0.00 1
###*********** END OF LATEST ANALYSIS RESULT **************
- 53. PRINT MEMBER STRESSES
STAAD SPACs -- PAGE NO. 6 MMCHMUE C- SHfH 7 0F f ID: toledo eaison CALC.NO. c-c 5 I-too os -oss MEMBER STRESSES ALL UNITS ARE KIPS /SQ INCH M'JMB LD SECT- AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z ; l 1 1 .0 0.2 C 0.0 0.0 0.2 0.3 0.0 1.00 0.2 C 0.0 3.7 3.9 0.3 0.0 2 1 .0 0.2 C 0.0 1.7 1.9 0.1 0.0 l 1.00 0.2 C 0.0 4.1 4.3 0.1 0.0 I 3 1 .0 0.2 C 0.0 3.4 3.5 0.0 0.0 ; 1.00 0.2 C 0.0 3.9 4.0 0.0 0.0 ; i 4 1 .0 0.1 C 0.0 4.6 4.7 0.1 0.0 ! 1.00 0.1 C 0.0 3.2 3.2 0.1 0.0 5 1 .0 0.1 T 0.0 5.6 5.7 0.2 0.0 f 1.00 0.1 T 0.0 2.0 2.1 0.2 0.0 ! 6 1 .0 0.3 T 0.0 6.0 6.3 0.3 0.0 ; 1.00 0.3 T 0.0 0.0 0.3 0.3 0.0 } 7 1 .0 0.5 C 0.0 0.0 0.5 0.4 0.0 1.00 0.5 C 0.0 5.0 5.5 0.4 0.0 i l 8 1 .0 0.2 C 0.0 0.2 0.5 0.3 0.0 1 1.00 0.2 C 0.0 5.5 5.7 0.3 0.0 ! 9 1 .0 0.0 C 0.0 2.0 2.0 0.2 0.0- l 1.00 0.0 C 0.0 5.2 5.3 0.2 0.0 l 10 1 .0 0.1 T 0.0 3.2 3.4 0.1 0.0 l 1.00 0.1 T 0.0 4.6 4.7 0.1 0.0 l 11- 1 .0 0.2 T 0.0 4.2 4.4 0.0 0.0 l 1.00 0.2 T 0.0 3.7 3.9 0.0 0.0 , 12 1 .0 0.2 T 0.0 5.0 5.2 0.2 0.0 l 1.00 0.2 T 0.0 0.0 0.2 0.2 0.0 ! 13 1 .0 0.3 T 0.0 6.5 6.8 0.0 0.0 . 1.00 0.1 T 0.0 15.6 15.8 0.5 0.0 j
. i 14 1 .0 0.2 T 0.0 2.5 2.7 0.1 0.0 !
1.00 0.2 T 0.0 11.6 11.8 0.4 0.0 l f 15 1 .0 0.2 T 0.0 2.5 2.7 0.2 0.0 l 1.00 0.2 T 0.0 6.6 6.8 0.3 0.0 i 16 1 .0 0.2 T 0.9 7.9 8.1 0.3 0.0 1.00 0.2 T 0.0 l'2
. 1.4 0.1 0.0 l 17 1 .0 0.1 T 0.0 13.2 13.3 0.4 0.0 l 1.00 0.3 T 0.0 4.2 4.5 0.0 0.0 l h
l l
_ - _ _ _ . _ . _ . _ _ _ _ _ . _ _ _ _ _ _ _ = - - . CTAAD SPACE ATTACHMENT f. SHEET f 0F T ID ed edison
. .o 3 -oG _ , , _ .
MEMBER STRESSES , ALL UNITS ARE KIPS /SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z o+e*********** END OF LATEST ANALYSIS RESULT ************** I
- 54. PRINT JOINT DISPLACEMENTS I
J l 3 2 i 4 i' l
ADACHMENT c- SHEET 9 OfA
- STAAD SPACE c-tsS-to .o 3- i3 -- PAGE NO. 8 E 0*
{ID: toledo edison 1 4 JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN 1 1 0.00000 0.00000 0.00000 '0.00000 0.00000 -0.00215 2 1 0.02458 -0.00007 0.00000 0.00000 0.00000 -0.00184 3 1 0.04945 -0.00018 0.00000 0.00000 0.00000 -0.00118 4 1 0.06190 -0.00027 0.00000 0.00000 0.00000 -0.00036 5 1 0.06017 -0.00031 0.00000 0.00000 0.00000 0.00052 6 1 0.04393 -0.00025 0.00000 0.00000 0.00000 0.00137
- 7 1 0.00000 0.00000 0.00000 0.00000 0.00000 0.00231 8 1 0.00000 0.00000 0.00000 0.00000 0.00000 -0.00220
- 9 1 0.02467 -0.00021 0.00000 0.00000 0.00000 -0.00177 2
10 1 0.04945 -0.00034 0.00000 0.00000 0.00000 -0.00112 11 1 0.06191 -0.00035 0.00000 0.00000 0.00000 -0.00031 12 1 0.06020 -0.00028 0.00000 0.00000 0.00000 0.00057 13 1 0.04373 -0.00017 0.00000 0.00000 0.00000 0.00147 14 1 0.00000 0.00000 0.00000 0.00000 0.00000 0.00225 1 660*********** END OF LATEST ANALYSIS RESULT ************** 2 l 55. FINISH
*************** END OF STAAD-III ***************
1
**** DATE= APR 21,1995 TIME = 11: 7:46 ****
i
- For questions on STAAD-III/ISDS, contact: *
- RESEARCH ENGINEERS, Inc at *
- Ph: (714) 974-2500 Fax: (714) 974-4771
- 1 4
E \ I
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- . - - - _ _ - . . . . 1 a.flACHMENT o SHEEL._2. 7 PAGE NO. 1 l Ci10. N0. C- CE- ioo o 3 -o \3- ID: Toledo Edison l
***************(Af********************A***********
- S T A A D - III *
- Revision 20.0b *
- Proprietary Program of *
- Research Engineers, Inc. *
- Date= APR 20, 1995 *
- Time = 7:27:25 *
*
- l
- USER ID: Toledo Edison * ,
************************************************** I I
i
- 1. STAAD SPACE
- 2. UNIT INCH KIPS
- 3. JOINT COORDINATES
- 4. 1 0. O. O.
- 5. 2 0. 22.5 O.
- 6. 3 0. 38.5 O.
- 7. 4 0. 79. O.
- 8. 5 0. 98. O.
- 9. 6 71. O. O.
- 10. 7 71. 22.5 0.
- 11. 8 71. 38.5 0.
- 12. 9 71. 79. O.
- 13. 10 71. 98. O.
- 14. MEMBER INCIDENCES
- 15. I 12
- 16. 2 2 3 i
- 17. 3 3 4
- 18. 4 4 5
- 19. 567
- 20. 678
- 21. 7 8 9 I
- 22. 8 9 10
- 23. 9 2 7
- 24. 10 38
- 25. 11 4 9
- 26. MEMBER PROPERTIES
- 27. 1 TO 8 PRIS AX 1.95 IX .1 IY 1.107 YD 4.875 IZ 4.602 ZD 1.625
- 28. 9 TO 11 PRIS AX 1.11 IX .1 IY .478 YD 3.25 IZ .93 ZD 1.625
- 29. SUPPORTS
- 30. 1 5 6 10 PINNED
- 31. CONSTANTS
- 32. E 29000. ALL
- 33. DEN .000283 ALL
- 34. LOAD 1
- 35. SELF X .96
- 36. SELF Y -1.
- 37. HEMBER LOAD
- 38. 9 10 11 CON GY .15 20.
- 39. 9 10 11 CON GX .144 20.
- 40. 10 11 CON GY .275 50.
- 41. 10 11 CON GX .264 50.
l I
STAAD'DPACE ATTACHMENT D SHEET __3_ U 7 -- PAGE NO. 2 ID: Toledo Edison
- 42. PERFORM ANALYSIS " ' !f.. N O. M S S - Wo.o s - o! 3 l
t PROBLEM STATISTICS ___________________________________ i l NUMBER OF JOINTS / MEMBER + ELEMENTS / SUPPORTS = 10/ 11/ 4 ORIGINAL / FINAL BAND-WIDTH = 5/ 4 TOTAL PRIMARY LOAD CASES = 1, TOTAL DEGREES OF FREEDOM = 48 SIZE OF STIFFNESS MATRIX = 1152 DOUBLE PREC. WORDS ' REQRD/ AVAIL. DISK SPACE = 12.04/ 373.5 MB, EXMEM = 12.90 MB
++ PROCESSING ELEMENT STIFFNESS MATRIX. 7:27:30 ++ PROCESSING. GLOBAL STIFFNESS MATRIX. 7:27:30 ++ PROCESSING TRIANGULAR FACTORIZATION. 7:27:30 l ++ CALCULATING JOINT DISPLACEMENTS. 7:27:31 l ++ CALCULATING MEMBER FORCES. 7:27:32 i
- 43. PRINT MEMBER FORCES l
l I 4 1
1 c i I AnACHMENT D- SHEET _1 bi . 7 CTAAD SPACE -- PAGE NO. 3 f c-tss-I r/!C.N0. . 3 - c7J3 ID: Toledo Edison i MEMBER END FORCES STRUCTURE' TYPE f SPACE ~~~'~~ ALL UNITS ARE -- KIPS INCH MEMB LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z I 1 1 1 0.23 0.26 0.00 0.00 0.00 0.00 2 -0.22 -0.24 0.00 0.00 0.00 5.64 i 2 1 2 0.15 0.01 0.00 0.00 0.00 -5.00 j 3 -0.14 0.00 0.00 0.00 0.00 5.14 j l 3 1 3 -0.03 -0.12 0.00 0.00 0.00 -7.18 4 0.05 0.14 0.00 0.00 0.00 1.87 4 1 -0.31 -0.37 0.00 0.00 I 4 0.00 -7.11 5 0.32 0.38 0.00 0.00 0.00 0.00 1 5 1 6 0.31 0.29 0.00 0.00 0.00 0.00 1 7 -0.30 -0.27 0.00' O.00 0.00 6.30 l 6 1 7 0.20 0.34 0.00 0.00 0.00 -3.26 8 -0.19 -0.33 0.00 0.00 0.00 8.64 7 1 8 -0.09 0.03 0.00 0.00 0.00 -4.29 9 0.11 -0.01 0.00 0.00 0.00 4.95 0 1 9 -0.30 -0.20 0.00 0.00 0.00 -3.82 10 0.31 0.21 0.00 0.00 0.00 0.00 l 9 1 2 -0.23 0.07 0.00 0.00 0.00 -0.64 l 7 0.07 0.11 0.00 0.00 0.00 -3.04 10 1 3 -0.12 0.17 0.00 0.00 0.00 2.03 8 -0.30 0.28 0.00 0.00 0.00 -4.35 11 1 4 -0.23 0.26 0.00 0.00 0.00 5.23 9 -0.20 0.19 0.00 0.00 0.00 -1.13 000*********** END OF LATEST ANALYSIS RESULT **************
- 44. PRINT SUPPORT REACTIONS
I D SHEET _E 't 7 ! STAAD SPACE l ATIACHMENT -- PAGE NO. 4 r p;), c -t S 5 - t 00,03 - O o ID: Toledo Edison SUPPORT REACTIONE -UNIT KIPS INCH STRUCTURE TYPE = SPACE JOINT LOAD FORCE-X FORCE-Y FORCE-Z MOM-X MOM-Y MOM Z 1 1 -0.26 0.23 0.00 0.00 0.00 0.00 5 1 -0.38 0.32 0.00 0.00 0.00 0.00 6 1 -0.29 0.31 0.00 0.00 0.00 0.00 10 1 -0.21 0.31 0.00 0.00 0.00 0.00 ; i
************** END OF LATEST ANALYSIS RESULT *****r******** '
- 45. PRINT MEMBER STRESSES I
4 I
1 l l STAAD SPACE -- PAGE NO. 5 ATTACHMENT D SHEET Co 0F__7_. ID: Toledo l: Edison L-CSS-'00.07-00 1 ' . " C. NO. MEMBER STRESSES '
- ALL UNITS ARE KIPS /SQ INCH
! MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z i 1 1 .0 0.1 C 0.0 0.0 0.1 0.1 0.0 4 1.00 0.1 C 0.0 3.0 3.1 0.1 0.0 2 1 .0 0.1 C O.0 2.7 2.7 0.0 0.0 1 1.00 0.1 C 0.0 2'7
. 2.8 'O.0 0.0
] 3 1 .0 0.0 T 0.0 3.8 3.8 0.1 0.0 1.00 0.0 T 0.0 1.0 1.0 0.1 0.0 l I 4 1 .0 0.2 T 0.0 3.8 3.9 0.2 0.0 a 1.00 0.2 T 0.0 0.0 0.2 0.2 0.0 } 5 1 .0 0.2 C 0.0 0.0 0.2 0.1 0.0 4 1.00 0.2 C 0.0 3.3 3.5 0.1 0.0 6 1 .0 0.1 C 0.0 1.7 1.8 0.2 0.0 j 1.00 0.1 C O.0 4.6 4.7 0.2 0.0 i 7 1 .0 0.0 T 0.0 2.3 2.3 0.0 0.0 l 1.00 0.1 T 0.0 2.6 2.7 0.0 0.0 1 8 1 .0 0.2 T 0.0 2.0 2.2 0.1 0.0 l 1.00 0.2 T 0.0 0.0 0.2 0.1 0.0 l 9 1 .0 0.2 T 0.0 1.1 1.3 0.1 0.0
- 1.00 0.1 T 0.0 5.3 5.4 0.1 0.0
- 10 1 .0 0.1 T 0.0 3.6 3.7 0.2 0.0 i 1.00 0.3 T 0.0 7.6 7.9 0.3 0.0
! 11 1 .0 0.2 T 0.0 9.1 9.4 0.2 0.0 ,
1.00 0.2 T 0.0 2.0 2.2 0.2 0.0 l i i
************** END OF LATEST ANALYSIS RESULT **************
- 46. PRINT JOINT DISPLACEMENTS i
_ ~ . . STAAD SPACE ATTACHMENT D SHEET._.10' 7 __ p3gg 3g, , oc go, __.c d u -too.03-013 ID: Toledo Edison l JOINT DISPLACEMENT (INCH RADIANS)
. STRUCTURE TYPE = SPACE d
JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN 1 1 0.00000 0.00000 0.00000 0.00000 0.00000 -0.00151 2 l' O.03026- -0.00009 0.00000 0.00000 0.00000 -0.00103 3 1 0.04183 -0.00013 0.00000 0.00000 0.00000 -0.00042 l 4 1 0.02502 -0.00010 0.00000 0.00000 0.00000 0.00098 5 1 0.00000 0.00000 0.00000 0.00000 0.00000 0.00149 t 6 1 0.00000 0.00000 0.00000 0.00000 0.00000 -0.00154 7 1 0.03052 -0.00012 0.00000 0.00000 0.00000 -0.00100 8 1 0.04168 -0.00018 0.00000 0.00000 0.00000 -0.00029
- 9 1 0.02510 -0.00010 0.00000 0.00000 0.00000 0.00114 10 1 0.00000 0.00000 0.00000 0.00000 0.00000 0.00141 a
************** END OF LATEST ANALYSIS RESULT ************** +
- 47. FINISH
*************** END OF STAAD-III ***************
**** DATE= APR 20,1995 TIME: 7:27:37 ****
4
- For questions on STAAD-III, contact:
- j
- Research Engineers, Inc at *
)
t
- Ph: (714) 974-2500 Fax: (714) 921-2543 * '
I \}}