NRC-94-0050, Design Calculation, Qualification for Qai Duct Supports in Stress Rept 2848-1
ML20069F162 | |
Person / Time | |
---|---|
Site: | Fermi |
Issue date: | 07/20/1984 |
From: | Chuang C, Raju Patel HOPPER & ASSOCIATES, ENGINEERS |
To: | |
Shared Package | |
ML20069F099 | List: |
References | |
CON-NRC-94-0050, CON-NRC-94-50 2806, NUDOCS 9406080155 | |
Download: ML20069F162 (191) | |
Text
{{#Wiki_filter:, Attachment 16 to r ! NRC-94-0050 D.C. No. [80& Page h t Table of Contents , 1 Title Page No. L Introduction / Purpose 1 i Sumary of Results 1 e Calculation References 3 General Nomenclature 0 Support Index Sheet 7 Calculations: Part I - Support Load Determination h Support Design Load Table lh ; Part II - Bounded Support Load Assessment 29 Part III - Structural Support Calculations 2.1 Other PAhT E- Ad+ Pxmv A%E%aEF bb k-i List of Attachments 7) 9406080155 940603 PDR ADOCK 05000341 P PDR e %
T D.C. No. ill?O4. Page / Op b INTRODUCTION The responsibility for HVAC ductwork and associated support design was originally with the Fluor Pioneer Co. for all QA Level I/ Seismic Cat. I duct in the Reactor and Auxiliary Buildings, excluding the drywell. The original duct design was based upon a computer analysis of the systems between structural anchors to establish support system design loads and duct adequacy. This duct analysis was performed assuming the supports as being rigid attachments to the building. This assumption yields a high system frequency response and consequently artificially low support design loads. The support structures were designed using an established stan-dard and by Engineering judgement. The seismic support loads calculated by Fluor are based typically on zero period accele-ration ( 50 Hz response) for the OBE case at 2% damping. 1 l l 1 I l l l I I
F i D.C. No. 28Cb ! Page 2. Of N ! 1!
~
i PURPOSE This calculation establishes a conservative support design load ; by methods established in the reference design calculation 2935. ! The method provides increased loads to account for shifts in l system frequencies due to support flexibility. Structural cal- l i culations of the subject supports noted on the index sheet for ; the Fluor Stress Report No.2649-/ are contained in this design calculation based on the newly established loads. l r
# E
SUMMARY
OF RESULTS ( All support calculations contained here comply with the govern-
- ing codes and standards addressed in reference design calcula-tion 2935. Member stresses are within limits expressed in the ,
AISC Manual as established in Section 3.9.2.2.4.1 of the FSAR. i The support designs cre censidered adequate to resist the stated t design loads. i i i
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D.C. No. E00b
?A his b Of HVAC DUCTWORK SUPPORTS CALCULATION REFERENCES Ref. No. TITLE 1 Design of Welded Structures, Blodgett-1972.
2 Manual of Steel Construction - AISC, Seventh Edition-1970, or 8th Edition as noted. 3 S6W Paper, EMTR-612, Design and Analysis of Base Plates. 4 S&L Report SL-2682, Seismic Analysis of the Reactor-Auxiliary Building Complex. 5 EF2-46,027 - Allowable Load for Phillips Flush Anchors. 6 Design Calculation 2935 , Design Methods - Standard Ductwork Supports. 7 Mechanical Engineering Design - Shigley, Second Edition. 8 Supplement No. 3 to the Specification for the Design, Fabrication
& Erection of Structural Steel for Buildings - AISC, June 12, 1974.
9 EF2-19,726 - Load Carrying Capability Derating of Continuous (Gateway) Inserts. 10 ITT Phillips Drill Division - Spacing, Edge and End Distance Recommendations - Red Head Engineering Bulletin, 7/17/73. 11 Red Head Engineering Report No. 1372 - Minimum Embedment Depth. 12 Edison Specification 3071-226, Rev. D - Purchase & Installation of Concrete Anchors. 13 Formulas for Stress and Strain, Roark, Fourth Edition. I
1 D.C. No. 2 80$o 1 fA 6s k of $ I GENERAL NOMENCLATURE Term = Definition and Units a Acceleration (g) i i A Cross Sectional Area of One Anchor Bolt (in2 ) 2 A, Total Area of Anchor Bolts in Tension (in ) ; B Length of Plate, (in) Total Compressive Force in Concrete (Ib) C e D Length of Base Plate (in) l d Distance from Extreme Concrete Compression Fiber to the Centroid j of the AnchorBolts in Tension, Diameter of Drilled Hole, (in) ; 6 p, g) . E, Modulus of Elasticity of Steel (29 x 10 E M d lus f Elasticity of Concrete (3.0 x 106 p,g) c e Direct Force Eccentricity, (in) fa Computed Axial Stress (psi) F, Axial Stress Allowed (psi) F Bending Stress Allowed (psi) b Fg Allowable Tensile Stress (psi) Fy Allowable Shear Stress (psi) L F Specified Minimum Yield Stress (psi) [ Y r FX,FY...MZ Forces and Moments Applied to the Base Plate and Reacted by I the Concrete and Anchor Bolts, Ib and in-lb. j j freq. Frequency (hz.) i I Moment.of Inertia of Section (in ) -l K Effective Length Factor Kg Fatigue Stress Concentration Factor j
,i L Span Length (ft) ,
i M Moment (in-lb). i 1 j g 3
D.C. No. 2806
?A 6E S~ o f N GENERAL NOMENCLATURE (cont'd.)
Term Definition and Units P Concentrated Load (1b) ' i R Reaction Applied to Beam (Ib) S Section Modulus (in ) S, Section Modulus of Weld Treated as a Line (Blodgett, page 7.4-7) T Anchor Bolt Tension i V, Shear Load at Weld Location V Shear Load (1b) ! W Width of Plate
/
C Distance from N.A. to the Point at which Stress is Desired (in) 1 d Nominal Bolt Diameter (in) I f Allowable Force on Fillet Weld (1b/in) f I Force on Weld Due to Uniform Distribution of Load over Total Weld Length (Ib/in) f 2 Vertical Force on a Weld at a Specified Location Due to Moment (Ib/in) f 3 Horizontal Force on a Weld at a Specified Location Due to a Moment (Ib/in: , f b Computed Bending Stress (psi) f Compressive Stress in Concrete (psi) fI Compressive Strength of Concrete (psi = 3000) f Actual Bearing Pressure p f g Computed Tensile Stress (psi) f y Computed Shear Stress (psi) l k Distance from Extreme Concrete Compressive Fiber Stress to the Nuetral d I Axis Location of the Base Plate, (in) i 1 Length of Each Weld (in) Length of Vertical Weld (in) N Total Number of Anchor Bolts Ng Number of Fasteners in Tension i
D.C. No. 7, dSO 6, F%s se 6 or 17:33 CENERAL NOMENCLATURE (cont'd.) Term Definition and Units n Ratio of Es/Ec - 9 r, Least Radius of Gyration with Respect to the Principal Axis (in) T, Total Tensile Force in Anchor Bolts, (Ib) t p Thickness of Plate (in) X, Y, Z Coordinate Axis 21 Perpendicular Deflection (in) O Leg Size of Fillet Weld (in) T Allowable Shear Stress on Throat of Weld (psi) l I l 1
D.C. No. 2fCh Date 7 20-N Fermi 2 Power Plant Page *7 o f M
Subject:
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D.C. No. $$d3Oba Page $.0 CF b-Part II - Bounded Support Load Assessment The structural calculation for supports within this calculation have been performed based on the design load determined within Part I of this design calculation. This load is based on calculation methods established in reference Design Calculation 2935 utilizing OBE and DBE spectra data. Subsequently, a duct capability evaluation was made by the Engineering consulting firm of Hopper & Associates. This analysis was necessary to assure the integrity of the ductwork itself, and was based on the site specific earthquake data. This duct assessment yielded bounded support loads based on duct size and support stiffness. Pertinent data from the analysis can be found attached to this design calculation. This part of the calculation is an evaluation of the subject duct sup- - ports for the bounded load established by Hopper & Associates. The table found on the next page compares the design load used within the structural calculation and the bounded load. Conclusions relative to the adequacy of the support based on support member and weld stresses and anchor systems are stated in the table. OBE allowable stresses , and allowable anchor bolt pullout have been maintained unless otherwise noted. Calculations required to substantiate these conclusions are referenced in the comment section of the table. For vertical system frequencies determined to be greater than or equal to 33 Hz, the ver-tical duct loading is the same as the values calculated within Part I. t h
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ACTIVE UNITS INCH LS DEG. F&MR SEC LeM O O 'O ; O INTERNAL MEMBER RESULTS
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M FORCE Y FORCE 2 FORCE M MOMENT V MonENT 2 MORENT 4.8309488 0.0837718 0.4839281 O 1 GLOBAL 0.023351: 499.528074 -0.1129905 10 CLP'4AL -0.0233511 500.471480 0.1429905 1.7748841 0.2431437 -0.4839281 9 , S LOAF 4NG - 2 O 9 g unsER FcaCES LOAs NG - 2 g MEMBER JOINT /- - - ----- ------ FORCE --------------------//- -
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to 4 352.079590 -851.551584 -840.997559 -72.1140594 -5239.54250 5160.39042 ' 11 3 2451.75098 -1063.420e5 -1033.47583 4.6144514 10439.4005 -11071.7773 *
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AX1AL SHEAR 1 SHEAR I' TORSI,0NAL BENDING'T BENSING 2 6 -30.5180444 -9018.20312 8971.01953 O 12 9 -2438.21631 991.559082 974.289795 2 2438.21631 -991.559002 -974.289795 30.5180444 -10271.7422 10440.8398 12 O e G SUPPORY JOINT REACTION LOADS LOADING - 2 , g JOINT /-----*- - == *---- FORCE ---------~~--------//-----***----*- MO M E N T --~~~~---------*- # x FORCE Y FORCE 2 FORCE M M0 MENT Y MONENT I M0 MENT g 3 , GLOSAL -11.3231621 -7048.08984 147.481137 -5787.02734 -54.6354944 *1453.02444 1 GLOBAL 11.3231421 7068.08984 832.318848 -14259.4758 -103.888550 1453.02444 4D 10 0 PAGE - 13 g g G LIST DISP 5 4 7 3 g PAGE = 14 g 6e O g esseeeeeeeeeeeeeeeeeeeeeense O eRESULTS OF LATEST ANALYSE 8e seeeeeeeeeeeeemeneeeeeeeeeen b e g PR0aLEM - SilFFNES TITLE - MWAC SUPPORT en-2850-H-31 g g ACTIVE uMITS INCH LB DEG. FAHR SEC LBM g N
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PROFILE EDUALS Y JulNTS _ _ _ . . _ _ _ _ _ . _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ m -__2 ._1 s,- _- - .-r.- . . - , . = - , , - - - - - y
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MEMBER MAN NORMAL .AT SECTION LOAD MIN NORMAL AT SECTION LDAD 1 2386.02271 0.0 FR 3 ' .207929E+04 0.0 FR 3 2 1353.39232 1.000 FR 3 .121979E+04 1.000 FR 3 ' MOO 3 1331.12999 0.0 FR 3 .122663E+04 0.0 FR 3 yyQ 4 1222.06201 0.0 FR 3 .129207E +04 0.0 FR 3 J qq 5 2181.19312 1.000 FR 3 .237749E+04 1 000 FR 3 6 2002 97427
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-----FORCES------- ---//--------= -----MOMENTS----- ----- -/
MEMPER MOMENT Z AX1AL SHE AR Y SHEAR Z TORSION MDMENT Y m 3 1 649.599111 -25.0065309 22.3729249 9.5551577 -500.693350 -753.469019 16.6797720 -14.0451794 -9.5551577 -276.114259 -135.679429 i _ 2 -665.624269 ,
- 9 1027.92397 950.510799 3 9 -977.356934 90.2646637 -77.6310425 16.5160990 10 999.129639 -85.9594513 93.2259301 -16.5160990 1277.25391 1530.03992 11 0.0706000' 1121.25659 -1176 99693 3 3 257.611094 -105.921136 -101.637756 9 -259.994521 112.210724 109.027359 -0.0706000 930.005371 -956 121094 ,
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PAGE - 10
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EXECUTE PR00 RAM '000LOBAL'
. STRUDL MESSAGE - MEMBER FORCES AND MOMENTS HAVE BEEN ROTATED TO THE OLOBAL COORDINATE ^
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LIST FORCE REACTION
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AMIAL SHEAR Y 9 HEAR 2 TORBION MOMENT Y MOMENT 1
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-0.9454641 32.1363373 -25 9036499 s#
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8 3 9 -2 0097153 -507.763194 -3.6154795 -251.390065 12.0313740 43.0596619 %# 9 2.9097191 529 940430 19.1693726 -390.450439 -12.0313740 115 239746 9 -
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# PAGE - 12 ^ ^
MEMBER FORCES
, MEMPER LOADINO JOINT /= FORCES // MOMENT 9------ - -/ ^
AXIAL SHEAR Y SMEAR Z TORSION MOMENT Y MOMENT-Z 10 1 9622294 999.129639 119.541325 -1995 05542 -16.5160990 179.745341 g 3 7 0.5079193 106.494064 44.4697195 947.599977
- 2 4726542
- -9.1720734 . 4 -0.5079346 -101 231720 -42 6036997 604.491201 -4.6394277 9.1720734 ,
3 3 -2 75912?? -294.932129 91.9327179 1625.11035 -20 2500000 -27.4955757 9 2.7591146 292 297109 -76.4309092 1333.69239 -13.1635742 - -12.7519043 12 , 3 ? -0.9474792 349.416016 92.4796904 1719.63770 -4.4943750 10.1335449
, 2 0.9474792 -340.973977 -97.0136971 1950.63943 17.7475117 -23.3996916 BUPPORT JOINT REACTION LOAD 9 -
JOINT LOADING / -FORCES - -- //- - ---~ MOMENTS -- / X MDMENT Y MOMENT 2 MOMENT S X FORCE Y FORCE Z, FORCE 1 OLOBAL " 3 -1 9622331 -447.599111 33 5023346 -996 919336 -9.5551577 -179.745575 10 OLO94L 3 1 9422332 999.12?a37 119.561340 -1995.05566 -14.5160990 179.745422' s PAGE - - 13 4 . LIsf DISPLACEMENT S & t iPAGE - 14
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- PAGE - 9 e3 t) seestesseestesseestessetteet eRESULTS OF LATEST ANALYSESe .,
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.I PR09LEM - 6M-2949- TITLE - MONE 01VEN ACTIVE IMITS INCH LB DCO. FAHR SEC LDM V) O Q I>O - d ~4 FI OZ INTERMAL MEMKR RESULTS ')D),4 -~
a mN I - 4 O> gs
. MENKR MAXIMUM STRESS nN /
AT SECTION LOAD STRESS - MIN WORMAL AT SECTION LOAD
/ 'g MEMBER MAX NORMAL * - 1 *2579 90462 1 000 FR 3 .213923E404 1.000 FR 6 .
2 7507 51172 1 000 FR 3 .706971E404 1.000 FR 6 3 9523 96719 1 000 FR 6 .923254E404 1.000 FR 6
-e . 4 0.129915E405 1 000 FR 3 .132964E405 1.000 FR 6 5 0 126963E405 00 FR 3 .110067E 405 00 FR 6 6 3613 44971 1 000 FR 3 .192615E404 1 000 FR 6 . 7 4621 46592 1 000 FR 3 .443900E404 1.000 FR 3 -
9 -260 215332 00 FR 3 .294670E404 0.0 FR 3 __.____m - _ ___m._ s^ -u _ -Tw- e -----"---*'m T-- w ew- m- iw - ---m ----ieuw _--_a_- v- % - _a -.*_m.m. - - - . - ___a
PAGE - 10 EXECUTE PROGRAM '0GGLOPAL*
~ ^
STRUDL MESSADE - MEMDER FORCES AND NOMENTS HAVE BEEN ROTATED TC THE CLOBAL C00RDINATE SYSTEM FORALL ACTIVE MEMPERS AND LDADS. LIST FORCE REACTION PAGE - 11 setettetsteststeset**ttetste ' 9RESULTS OF LATEST ANALYSES $ 3
$$$tetts****S$$$$$$$$$ststet 3
PROPLEM - 6M-2949- TITLE - NONE O!VEN ACTIVE UNITS INCH LB DEO. FAHR SEC LBM MEMBER FORCES MEMPER LOADING JOINT / -FORCES -//J------- -
---MOMENTS ------- / >
AXIAL SHEAR Y SHEAR Z 70RS10N MOMENT Y MOMENT 2
/
I , 1 1 3 1 -7.9103699 -3.4699436 -520.412354 92.9903359 -173.933029 -3 4479971 l 2 3 2900001 29.6320343 515.904766 436.735352 -3 9135601 3.4479971 l 6 1 -7.9141046 -4.9722910 10.2955704 110.077274 -177 154738 -3.6771499 J l 2 3.3046139 31 1353912 -5.7679992 458.845459 -3 6561279 3.6771489 gg 3 2 -1 2119141 166.192932 -454.611572 -1350.02715 6.0279320 20.4411163_ _s I# 3 -1.3349541 -151.476101 452.064697 -1500.19434 -4.9213n67 -20.4411163 d a 2 -1.2249290 166.067591 63.0231629 -1352.95605 5.9757324 20.512:070 . 2 3 -1 3218231 -151.350815 -6Q.4763947 -1503.B0933 -5 0041504 -20.5122070 J 9 3 3 1.3340541 151.476212 -197.065040 1500.19430 4.9211397 20.4409190 Dh y I 6 4 3
-3.0016:23 1 3210231 -136.759460 151.350061 194.519200 -194.523544 2016.0549.1 1503.00900 -4.9211397 5.0039663 26.5073242 20.5122070 s
O~- (g l 4 4 -3.0605760 -136.634109 197.070312 2020.53491 -3 0039663 26.2011719 J qg t q 3 4 3.0816223 -336.240479 60.4816509 -2016.05519 4.9211426 -26.5072021 S -3.9624420 347.606760 -62.4624796 -2771.43604 -73 1293945 26.5072021 h
& '4 3.0605760 -336 365723 -452.070069 -2020.53491 5.0039062 -26.2012377 -
5 -5.0493005 347.012012 454.051025 -2760.71069 -73.0295410 26.2012177 l' 5 g 3 5 6 5466309 669.450252 1106.02637 2432.09063 35 3000594 8.8903360 a 6 -7.1123047 -666.107744 -110%.59229 109.194672 -62 69n2269 -0.R903360 6 5 6.532714n 672 219402 506.100099 2506.90649 36.5249023 7.9112244 6 -7.0906329 -669.949463 -505.534100 175.432663 -63 7966050 -7.9112244 ., 1 A l l . ..
PADE - 12 MEMPER FORCES MEMBER LOADING J01MT / -FORCES-- - --//---- --
-MOMENTS /
Alt!AL SHEAR Y SHEAR Z TORSION MOMENT Y MOMENT 2 3 6 7 5001392 -17.3534546 1047.96572 -355 099145 60.4939325 -0.4995540 7 -12.1077175 43.5165710 -1052.39331 -619.922510 -375.490234 0.4995540 4 6 7.4935711 -15.9699402 525.732422 -334.935937 41 5669499 -0.2991624 7 -12.0111313 42.1330261 -521 204034 -594.011279 -373 492179 0.2991624 7 3 4 -0.4670650 210.541794 59.7263499 165.903939 2 2140627 9 3999926 2 -2.0799079 -195.925027 ~61.2731019 914.091309
-2 2140627 -23.9993602 '4 6 -0.3951013 211.919795 59.9019104 159.403595 2.2196274 9.2003794 2 -2.1616669 -197.203019 -37.2551575 994.110107 -2 2196274 -24 1992090 g n 3 5 -0.6930999 -1017.14502 -1043.54349 299.337159 37.7495909 -35.3975525 9 -4.5194244 1050.77051 1034.36035 -217.194509 -142.797949 140.436905 4 5 -0.6931303 -1020.03199 -1040.15112 - 241.903955 36 5050659 -34.1124725 8 -e.5202036 1081 65723 1047 35449 -157.113069 -141 572144 139 179535 9
SUPPORT JOINT REACTION LOADS
" /
JOINT LOAD 1M9 /- - FORCES -----//- - -----MOMENTS----+ =/ X FORCE Y FORCE Z FORCE X MOMENT T NOMENT - Z MOMENT (* 1
- OLOBAL 3 -7.9193719 -3.4699436 -520.412354 92.9903711 -173.933014 -3.4479971
. 6 -7.9141945 -4.9722919 10.2955704 119.977274 -177.154709 -3.67714B9 %>
7 OLOBAL , 3 -12.1077347 43.5165963 -1052.39331 -619.922517 -375 490234 0.4995540
- 6 -12,0111523 42.1330414 -521.204934 -594.911523 -373.492422 0.2991624 >
8 GLOBAL . 3 -4 5194349 1059.77075 1034.3&O40 -217.196707 -142.799071 140.437042
- 6 -e.5202036 1061.65771 1047.35474 -157 113251 e141.572250 139 179657 /
PAGE - 13
*E .e O LIST DISPLACEMENT 3 4 ? g PAGE - 14 s %o 't i l N ti ~
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*il h D . ............................ s i N th db .RE.SU.L.T.S..O.F .. . .. . . L.AT.E.S.T. ... . ANAL.Y.S.E.S..
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- PROBLEM - eM 2949- TITLE - NOME O!VEN -
ACTIVE UNITS INCH LD l'EO. FAHR SEC L9M - --.----------m- - -- -- - , - - - - , . - - - , . - - - - - - - w e ~~ -v, -..,--e- -n- e- - - - - - - - - . - - - - - - - ,
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sur_ DATE.31 0F_13 :---I
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i i D.C. Ms. Q2:cGo f Page No. bb af )) l e l PART IV l ANCHOR BOLT ASSESSMENT AS-BUILT RECONCILIATION o r This section of the calculation addresses noted deficiencies in i the anchor system installation; see Non-Conformance Report 84-1606. : i The following table identifies the supports affected, change documents, duct loading and reference derivation, and the anchor bolt margin of safety. The stated loading is the maximumL of the ' OBE or DBE load case. The allowable for the anchor bolts is , limited to 25% of the avdrage ultimate espacities as determined by . Pittsburgh Testing Laboratories as published in the Phillips Drill [ Company Catalog F-1000. I ; As an aid in determining the effect of misplacing the support attachment from the base plate mid point a study has been per-formed by Hopper & Associates. The resulta noted in correspondence
- BA-10/84-347 dated 10/4/84 state a maximum bolt load amplification [
of 4.5 and plate bending stress amplification of 1.1 due to support member ~ eccentricity. This study assumes that a standard base plate ( and bolting system has been used as well as a standard member size. Cases which cannot meet this 4.5 criteria or are odd cases have been justified by a specific calculation. This calculation can be found within this section, see the table for the specific page. , l l l
PART IV - ANCHOR BOLT ASSESSMENT TABLE Duct
*EN '
Sup ort g , y,, 88 Duct Loading F (Lbs.) M (In.-Lbs.) Load Ref. See As-Built Change Anchor Bolt Margin * @ Calc. Cosaients dk i i Height Fx/Mx Fy/My Fz/Mz Legend Notice Ref. Load Fage # h.k o - q P. O. >>an = 'Jo *1 '% < N E u 2o s d si toxico -
%6 1(o6 A Ben os54 -
4 i 344* = Auoo . cw- ? :: ud649445 itox t'J. IS2 c: A 6 - A 46m-cuer4 S, J S %$QQL coM4649 4 44 Itaxt2 I62. 596 - A 4EM-Oss7 9.6 (o . c,M 2849 4 4s leo as 12. I 3 '2- S96 - A '1BN 055+ 5 % A T ia % ceo I e:> 7 ,, wnb49 4 A1 sto x i?. Ib2 s96 - A nm oxs+ 5.j b ocr u c4ea A m G ii'
- N tS50 4 9 tox6 -
34 l(o b A A7N-055V l3 ~) ii! 'm P4 O W 1650-411 LOX (o 1"l 1 coo - A 68V0s#4 - 7 $'EIMS$ . F' n a A tb50-4 % l1
- b GH-2650 4 Tl 118 8 tb'L ISS (o O (o o b
b ABN0354-BBM-4559 b S ,o) Y y l k'j' y olTro (4m 4 %) G y {j [p
- a. n M 2850 5 30 11x6 -
13 3 (o o D //BM-#554- - 8 ,10 onto (We W 2G) = w h W 1650-d bl 1186 - 1S4 '(o O D //dh 055f- - 8 ,10 Dirro(We 4 10) II i 9N*
- 2:
7
% = -
b 3 (P N O h n I i A o a' eh
,D E t
i' <k
- Anchor bolt margins assuming plate attachment @ baseplate ( is allowable bolt pull-out/ actual calc. value. h
Forni 2 Fowsr F1cnt D.C. N >. 7 6 0 45 A D2to to '5c>- 8 4 F:s2 bd # U
Subject:
_ Qualification for QAI Duct Supports in Stress Report No. 'Z. 6 48). ] t FART IV I ANCHOR BOLT ASSESSMENT AS-BUILT RECONCILIATION i ASSESSMENT TABLE LEGEND , FCR LOAD DERIVATION REFERENCES i t Designation Description l
)
A Feak bounded lateral support loads by Hopper & Associates ' per HA-10/84-351. B Reduced bounded lateral support loads by Hopper & Associates. C Specific anchor loads supplied by Hopper & Associates due f to duct system flexibility. (~ D-H Dynamic analysis results supplied by Hopper & Associates. D-D , Dynamic analysis results by Edison. f E Fluor loads modified by a system frequency factor
- Maximums of OBE/DBE load case.
F Fluor analysis loads used directly for OBE load case and modified to DBE case @ ZFA. t G Static analysis by Edison at system frequencies derived , by computer analysis. ; E i I
oc de- ?.6oe A to '2.9 84 E.FE?vA1 E (ksE % og 75 Adc M6 bolt ASSEssu sr4T Ch @cd eLTeh R. S . Purc L Mt->A M- 51 occ7 LDb 05Eo tW coM FoTEh Ard AL.YSIS - PA AT E : t. Fy = 8460 % Fs= blo* bocWDEo Doc T LOS A F7 E : Fy = 29b N i F, = l co b
- co815EF,VATIVE LY PAoP, ATE 6 ALE R. P,5 ACTierdS 6Y A FecTo h oP (796 /9 4,) = . b 4 C6 tTic A L. 6ASE R 6EAGTioWS - PsoA ATEC - AF15 '
4 F.
- 105 5'/ 64 ) b8 5 k= (o 19 (
D r 52c/'f JT 7, LDc, 5 V >' = 3 9 u f
) = b l (o " T i .A, L2/ +g= cd /.e2S" = >.6 >8 c ,w c =g .-<>---
i - G q' E HTh . c,
"
- P'o4
. . L. P. = l. S (54 1PLIF IED McMoD ) *e _,# - = 1 ~
U ~ ~ ~ ~ Foh *b" P4tLLIF5 ArJcM AS OSED'- l' : 3" Rc. Actoc = 1 S44 gg
. b' (@ JT.7 ) ___ _
S20 sm F.o._ ASS 4 + g,3)+y3)ble 3764 EFF. MAX R C). D'lO [ I, b) = SG7 154M ,*. C)h Mcdos co. T eo. e onJ 6 E use e5 , ' A' 4 'c.' e Ju I 6 6 f1ESPECTivELY A6E LESS Nr4 @ f:ASE Ft 'Ed , JT.7 6Y IN'5fECT-tord oF AS-boiLT5 d ST60DL. o L>T pot . l
o c. ed 2. 7. S o e A 10 10).84 a Feh Al H PL, H oF 73 AtJcdon e:ot T ASSE55u EdT ! A5A b lEL.T % RA.MTEb F4c,h A 4 2, Ab i 4b n4sse >Jc>AS AAs toEtJTical. 9/ 3 Is. s e < e s o orJ o s. o ! L os , . ords Ardat.vs ts alt L cousA T>Ise alt. ! boodoEO ocx T LoS A AE: , Fx = l b 2.bi Fy = 59b
- occ.T L.oS o s so ar4 c.ou P. AW AL. . - fb67 E - ML0.6 51 A6E' Fy = 94c/ 4 F,g.= Sto Y cow 5 E6vATivE LY' FAo AATE 6ASE R_ 6E ACTio45 6Y P FAc.To6 oF ( 5% /9 4 La ) = .co b '2.
c6TicAL BASE R. 6E ACTier45 - PAomATso - A hs.: P, = to sB( .c,32 3 = eee
- 4= Sw( "
)= 2 5 6" + J T. 7,, LCr.o 3 m ,= st9 ( " ) = b => \ " h acne: c,w as eoiuvs ros e.1c'(ears)asne Nioso FoA MESE bh5 30dlCd ,
P(M MAD 4 g's 4/td dE bolt ibTrkhd . DOE To IM ACCE55Abit. TTY Wo AS 60tL"C wese woeo sx e.> wiVcsaTs to msfECTiVELY)/.ME P.o, AMAt.ysts IS bAMC l OA de ATIKE>AEh oF% To 4.oF ff. PER 09. WETCdE%. l bxse n. s"<5"nc" 5 of 4 3s" + rMass (m == 1s AA% l l 4 66- S Max Po, = + ( 2 bb + 3871 ) = 'D 1 4 4 gg y t.1/te= .ffs= b
...L.F.= 1,o A1T O
- Adcdos dour uawa = (S4 4 /'2. ll = 5,7 > 4 . .,OK 48 I 1
I l l
Ct IdGL 2.8 o(o d t o 2.0) b 4 F FEhM \ 1T. Pe to8 0F
- E ArJcdon e= c.r ASSE.S$ ugd T oc h Sed eers.h R.s.eere.A d L,h d 44 d
bo0MDED DOCT LDb , e F7 = 6 >bE 4 f-i = 1 b 2.8 1 _ c,e4 : co BEAcricWS @ JTl 5 IN LIEO oF STA.) o -- i 1" 16' tod Adat.Y$15; OSE WE py ,w Fattooisit uoo E L. ' 1 S::o* bco* To DEustoF JT l me xTioWS 5 h= ee4 sw 754 w % ec-wsw) u = 'xo(z Xio) 66+ 20)
$N5 i "
e au" 2.(2ot sm =bscis5 ISO [E.ZU , n_ Ul r ^ oinow y
- i4 5 = gg4 4 uA >t Ro.= [ + 3
'><o L/*t 2
D/<Fl6 # b #- LF* !* O (SIMPL1FIED HETMoo) EM T8bi P6 4 hEACTioWS @ JT. b i h = 60 4 sw M= S co"* Max Ro. = Y + % = 1564 c6 mat g o, ut.t.o.a . e.o. ( s e' + nacdas) = 1 s 4 4 0 A4c4# eat.T u+neid = i S44 / 156 = o).6 > 4 eud. 4 g c3 is <diW eocr earrena eos mJis re ..on 4 6
1 O c rd e 7. b o ro A to - 2.9 b4 E FEhMI E. Pa se 69or 73 Ark. dom bot.T A55s55usr4T Ch $cMELTEh R - S - P AT U. . IMCoh N-9 00CT Los osso i9 coMPoTEh Ar4 ALY SIS - PAhT E Fy : So* 6 P.g = 18e8 l D o vedo E D D0C.T LDS
- F=
y 34 E & F, = l (o6E-Gord5EhvATiv e tY. 05s t4od pac:> HATED DASE fE. 6 E - ACTiordS . Fy = 14 4 E M x = 46 5'* Hg= 14"* - JT.1 (c A men t.) l
+ Asc + n A lM wax Fo.=. 4 sc3) = ile + Lt/+.g= b/ss=6 .'. LF = l ALloc Po. ( b"& Adcdoec) = IS44 E i
t A Wcelon bour Maat,tra = 15244 = 15 7 4 ..Oh Appsce j
, ,q #6 :
Oco n N - 1'). pao-hATeo 6 Ass ft. hs Ac.Tiot45 To. 6EFLECT bourJOED LD5 AhE -PEh b 19 CALCS "- P= y 17 4 4 4 84 t= lo '2.co *
- Ro. allee (Foh '--
Lz / t g = 7,5 / G Z 5 = l '2. .- L P = 1. 5
" 'A,Y--4>- L_A e
l'2 " J '1' Ma P.o,= 174 /'2. + lo 2(o /4.S = SIS EFF.' M Ax P.O. = 315(l,S) = 47 2.5 4< '2.61 ^
..oh uggg',,$
F;W g,
oc do 2boe, A so . 2nb4 e FEhui E. P6 '2D op '/.3 A WcJo n eau.T Assessusa r oh fedeuveh R.s.eArct i l dt,h d '2. ro ,1 1, So 6 Sl occr Los oseD IW Cou PoTEh ANALYS]S - PAAT E l'y = l lo E & F, = (oro d l hE FINED booMDED LOAD PEh MoPPEh 6 assoc, exI i 47 i Fy=lbA4 6 Pg = .<o(tooN)= took %1 l t TdESE VALoEs AS E APPhak.. EctOn t. 4 SidcE A dohlt. ML,b iWEhTIA LOAD toAS iMPoTTED 4W THE ST600L Rod i TdE 6ASE it., AEACTioWS SWootD ACTO ALLY BE I SLic::>dTLY dord5ERVAT1VE 714EhE FohE 05E TN E. 6 ASE ft. h E AC.TioWS Phovtoso oW P6 4ci oF PA6T E. l AWcdos eo. = Sa 2.4 (Pt, w ce PAAT m.) AMcdca bou-r ua66tW = 1544/58,2.
- 2.,(o b .
codsAs Attoo P.o, FoA A. g'96 ArdcdoA : 1544k ! de,h d -2(o it.As DOitT AdaL.Y5tS (beso a 4 c.g.) ' N o srd !? ~ 8= =,54S T= 'k = . l') l l heob A. 6. A.MPLIFlcATiod t- f. <. 7.. to 5 /. o h i
. .8 42 soot 14 ft. - Y = 992. 2. =. b x = 1 = . 4 21 Arrac4 ; *b !
Pe.so A.D. AMPLIFicATiod t 2. l 4. 1. (o S . . o h 61 { i Mc h M-27 ft.AS botLT AWALYstS
- Wasn4 e
- Y= S BS = .8c) x = $6= .62e l l
l 65C D A, b. AMPLIFlcATioW t 'l . 6 > 2 ,(o S .*. W . L ,. ; i l t
D C. rdo 2.606 A 11-1 5 - 8 4 5 FEhMI E S rne 7I of 73 Adcdo6 A5tessueWT Ch ScdE LTE h R.5 P ArE.t ! M6h M 26 , 7.~7 , do 4 S } (cod T.)
- 1. C.53 scand E : Y=2 = .85 x= .76S_
1 . 'dA P,asa A.b. e M PttFic ATio W 't 7. 6 ') 2. 6 5 . W.6. er iw sPecTiW6 As- bOi tT5 ., e_ ' A' APFeAns Tc) Eb e. c AiTic e t. 4 o t. t be AW e, t i seo Foh ACTOF_ P. O . PEfm A b - BOI LT D 1Mb . I of 4 . 50) '), l' 4 l$% E-b . 4
- 2. e- ne "-
wi
>y' y 4 l.b'o' +
S. 2 + e p .oF 4 bout _i . bA'os E AE NTio45
- F=6664 y W = 196.5* Mg= 1 19 8 cr-se I - A.e.'l' het:575 ALL oF Mg L . !tP : 2.IS 379:~).6<Ot.LF=l 2
- 800 (I- IP = 1R.f5N<lS4M..oh g,0, = hk+4,d 2.,, + IDSI ( 7.7 6 ) + 1 (1. 6 1 $)
gg i c ASE E - 6.b. '1' 4 ' b' e>EttSTS 4 L./tL: i t 5.16/375 =b.(/7)bt.LF=l.5 00D b R#S -t
=- M14 P.o.
e2 = k nick + 2('s.23) i 20.cou A 2 er go. = sn (i.e) = es v < ie w ..on
DG de 2600 A 1 0 0 *; o b4 ! E FEhMI I. P4 m 7 2,:gy 73. l AMCdoh tbtT A SSES$MEWT' Oh idELTEh R . S . P ATE L. ; idcoh d - 2.(o, 2. 7, bo 4. S 1 Cot 4T' Id t, P, d - bo FE. A 5 bon LT A r4 ALY Slb SitJ45 bot 1J I* W ave nde L2.x2.xQ MeMSEA f VIATo* LLY CEtJ7E6eo ord ME 6ASE ft. ME A 6. ATracd - A MFt. I Flc ATaos! < 2. to 5 6Y i r45P E cT to M. . o h 46 ; Pt, 2 dt,h id -b l FE. A5' B olLT ArJALY6tb i r WohTd D Y= " 19e x = kDD = .2(47 heQt) A. 6, AMPLIFicATiod
- 2.0 < '2..co b ..c> h !
,o92.
sound it.: Y: 1.59 2.= ,'796 ><.= 7, =,oS : 1 i hEQD A , 6. A M PLlFicpTioW e 2.2.4. 2. e 5 . . oh h i i
- i
l D.6. 2 & c 6 10 8 4- l Feami 2 Pount /21sr % Tb e 7.3 G%uncwon ;& Q4.I Dxr Svers. InSker&n zm l Soens-reo-r n. s. es,et I ATT AC HMsWT Lis T I. FLO OR'4 S TI= E S 5 R e f o R. T 2- 4%ETdHLS OF dhtdfj&R. . e V pc f d o. T 4 t o 2 - M o I :
- 4. PGR de. bl6 '
R&V & ; I t tj o. T 4to ?- M o Z 77 C f im NOPPGK bovNO6O lcAo5 lLe r-re12 lc,as e H ,
- 7. McFFEh BE F1WE D E:o0N DE D LOADS / LETT6 h O- I-!oPPEh Adcdoh bot.T LOAD AMPLIFlGATiord d FAc.Toh cde, AT / LET766
- 9. As Satur , Asm- oss 4 Res4 i
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[ Y. N ,' T, DOCT SUPPORT DESibt SHEET ; , b .*, . A 3-9-11 -- Analysis Pt.*No. JroS- .a ;; Date ^ Client The Robert'Irsay Co. _ Hanger Mk. Ilo. [N- Uf0"N- 9 Project Enrico Feral Atomic Power Plant #2 Hanger Deg. No.h-'/tr8-MO '#-h -9 Project No. 1D-4221 Duet sire- /0N ~ ~ ~ ~ --- 5ystem CCWW {6NE$. WG. Computed by D* MADN$
- E , *'
r . , - . 1. . '(
.-....ay, ':. - --.s ,.
y - -~ - 1 k , 7 . . . - - . . . _ . . . Support Type . Eang'cr ~ LaGral'-~~ ~~ Axial ~ .,.,
. i .- ...):k"a +.a a - ~
Direction VEE.T- N ,9 - .
=~-_:--- /
Coordinate Axis [ f., - u .. p n - 3 :g= . g y O -- L Max. Force Weight Setemic lead (f): z,y .s, Dir. Cobained Ixx Equiv.. Cylinder l yy E.quiv. Cylinder ' lead (1bs.) load Fx r, gj o . ,o .. . 18 Tx
~ j ' 'J r ~ , ,'k ; . ; Of.+ t. - . . . 3 . . ,
The m.aximum load is^ weight load plus seismic load. ' iU The larger sciente load from eithey fxx or tyy.. is used.
.s .. , .' l' 3' . --c ;.g Af ~ . g"? :
N -
*a+.*
7 v'm*- 'o -
/ r,. % '* - al.n . .k.i.k. .~.,' , ;i: - g -3 _
E
$ support design drawing is ' included in this report.
gRemark: c support ta for .uittple ducts, ts. deide .. a desvios is v.m
't '. . O - - includedin"reht566 'h b ' ,l . /.ddMfM$$h$$NT N @ $ h !f M df N N I ,.
l
l ~D C, '".. DU d ' . f [-_-_-__--_-__-__ ,,.,.s-_._.. _(P3. 6P - - _ - _.- IM
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- g. . .
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t SHT; 1.. OF_ %k-
, .%* ;: f
[ bh '. h I ,l.1 - r'8,'bk * * , .*, ' ?g ...e k*a' . . .. 4 . k. l >y. . ' ' .. }4..<^. y !y : *<-* ..u,t.,f .3 ary[ ., + .. e ,.. . g
'. .7 ' f. g. d. M E4C, .
a.- _; - .
.p p - .- g . . .,
mq 4 .- - ,
~: 1-DUC - 'P- s .,T i.% . ;,SUPPORT DESIGN SHF.ET o r ..
r , y. .:; gp ~ (. r - ~ - -
.. g . y y .- . a. m 2 , .u...~.
Analysis Pt. No,.
,- Date Clicat The Robert Irsay b[' '
HanaerMk.No.[M-2ffC-8-N ,_
#2 Hanger Dwn. No./04221-N-M-4_@_-M Project .-- _ _ Enrico Termi Atoute Power Plant- .___._ __. _
10-4221 Duet size . . ./U8 $, _ , Project No. ' System [o_NIEtt CEMit1JVAC. ____ computed by T) map 4 M w- . .. . wa. .:;2.,a .. . . , _ .
.:e-:- ~. . ;,c , i ~ C;i ;. (( ;,Qi_.ld;; .-_.:, . ,. ;;_.._. , ..~.. , .
_..---,.m_ , . _-~_..~ Support Type,* m ' *- : Manger IAteret- Axial. ,--
.t:; ._ _ . -. D_irection_ . _ _ . _ _ _ __ V. ETT1 . . E-N ~~
i
,,. , Coordinate Axis , g . . . y .. ,, _ X- ,,-- , ;;. . 7
- i. . . .
.. . u~_ < ., .g 3,.
e*
.~.. .
Max. I Torce Weight Selenic load (i): n.y s. Dir. Codined las Equiv. Cylinder 1 Equiv. Cyli,oder 14ed load
'h.5 a. . (1bs.) 77 /, . - r, - o 7 7 p:
4y .. rr 97 . o. o 's7 i.- :
- r, 1 . ' ':, -"'O. .- ; ,-
- p The maximum load'is weight load plus seismic load., ,
A[ The Israer seismic load from either las or tyy is used. f,. , , p 'i.J' ." ' - >s . . - .fi.. -l _ , ,
. 3, c.r , .. ,:g .-
L
, v.5- . # . , t . . 4 ,
P, g. t.' 5* *
? % ,' e I
8 . . 7 F . r . A
@ Support design drawing is included in thin report.
f',hRemarks - . . .42, support i. ror. Itiet.' e ct., th. de.i.n dr i i.- '.-
. 2c :
g.;t. .'ye- .. O ps;;+p,jj p,*. -- m . included is;t. port.50.f'M...
!)i.e t.s,.. . Li.a m N.: :s.A*A .c .m. .v. n e c,',e n :,. y :s .v~C " c.< W 'g ,
4 .
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* ~
lN[f,. Wi&SW 'f .* y Y __k,_f g _ .9*] gy.;;, JJ f f.,6 4 ' f[1-- y n.:' . ,'~'f. f. f.., + . p .'g s += _.. 4 s
~> s .'s',. ' ; 1 :-
- 3. , ,;. ' l. .i , ,_ , 7 :.
gL'.$'( ( f" .ll,,a[*~, .y ,. R; y,a,,,x . . ,.y .., .'3 ii. 4, as. .
.,c,c .,= . j, +,.. , . , - , . , . - , . y, -.,'t s . s. + - . ;. .w , - n. . :; , ' -
- f M M y@C, N'f.o. . 1 { ,. .
w;- ( . . e. w <. y,. - . .,
- n. . . *
. :,r . . y . . t. ., t v7,
- 3. , , .
9
. .ooc..7 _- y,2,7 , >," ,d ' if .; i . _ ,>, ; .?. f. * ; *4 . . DUCT SUPPORT DESIQI SHF.ET c s .v.7;M. .- .s. , ,, 3 27'- '
1 .; , .$.- _
.f- , . . . ' j .' -; - . .- ,g I. , .Date _ b- h~f*7.m... bE E D ^
Analysis Pt'. No, b80 -
~, ., y Hanger Mk. No. [N-2I N 2S Client The Robert Irsa'y'Co. J k '. .
Project Enrico Fermi Atomic ower Plant #2 _HangerDwA.No.!O 22#" W O' M " O'2S n, e Project No. --- 422f ~ - Duet Size -- - - [2A 8 - System 00MRol Ce' meg. WAc computca by - D.MADA3/
. L. ;. * - . , ,.. c . - '.:.: wh4'-...d-blu,.r:. .. i. a. <.r..: -w ~ . : . . . . . . . . , .. . ,n. n . ,.a . ,. ,. :
n,,..a...,.,..,-.
.~ , w n.. - . ~*
L.:--%. stDJMii. - -i.- - c -.: w mEms ;. e.q =. v.._Gm.ni.%+%.;= =.: - - - . . -
.a . > : uy ;c ... ,.. . - . . - . . .~==.mo-. = . .- .- - . . . ~ - - , ~ . - l Support Typ... e n,. Hanger-- -1.ateral -. - Axi al - ----- - - - - . - -
- 1. ,,
.r..r.
Mf~ jf ". b
Direction,$[." ' .' - 7' ~ * .T' -
Coordinate ~ Axis = -'7 iY * ' ' ~2:: - '
.: . c _ & = x , w m t.,.. ~.. _.r._.,.
o . . . e.m,.s~t -.u. e. , .3 . . a.,_ . ,. v.:g,., m .m
~-,:.,.. .n,, . , . _,. , ..
r. 3._ , - ., ,n..
. . . . . . . . ~ , . . _. , 2 - -Q 2 :. _ . . '~}".- .
Force Weight selspie load (i): w y,z. Dir. Coniped Max. (1bs.) load Igx Equiv., Cylinder 1 Equiv. Cylinder Imad 77 r, -- , - .! < ' _ l
.. r, - 82. i9 x I Z- . % . ~ . . . - - - . . T.. x . . . .... ~ . _ . . :a - x, f ,- ;., . ..
f . z . ._ ~f
, r.. . . . . .- . ., The maximum load is weight load alus seismie load.
The larger seismic load froe either !xx or t yy.is used. . . '
.d..^ ~N. . [, ,- jgM ( [ , j, " , b Ij U' , , *
(. ..-.wv 3
/.- ".w*- -y* :'.&. . ,+f... . . . * * ~'
p- - p.
,.>4--3, - ., - . . .r . , ,,t =pw. 3( 8 , , , ? *;.* e.*. ~lm's { 7, m , . ,. . ,
- l~~ -
- e ._,g*j 4' ,,
e_
- c. .
w :: .. Z , O.
, ; g ,,,,,a E support desian arawlos is incioded in thi. r., ore. '
a . . sopport s. rse .ulti,1 4.c'es, the.4. sten ar i W.r q
^
4't$...?:.. M. n.gltsej& ' Y r & So $ & S $} W Y & . $ $ h% 5 :; i s ,
' ^
- m;
- gs. g,' g= gy )
., 4 g..
- W ; eg ,
4 f La g 48 .p' e,
, 9g.<
q.n , .' 6
. . :.m ,, . , , 6 t".' w .e .+
f y n . .,
^ .( q ;e: .$ h.
h .y?
.; . 7 - . _, ., y ,_ ,c _ . . . - -
2 ,
... g u .c . . . u ,. c.t' 3. . ,,t.>, .. , g,. , . 2.,.3 ,. .**-[.~,.-4...,}..., .]# ..s gg . e .. ~ %" ;s. ' ,'f a =* ,. L . , *. .'r}/. d. aj. T } ,(/9] [ ,. y .v ~'
v , - . , ,:_..$. - '.O5 A3 ~~-*~~". i !, l 1 a 'l
.. , .g . . . , , . ,. *t;:,- -> , .5 -, *.. . .; 7, p j .;. ..'- .. . / ? .m., . . g . ,., 9.j. * . j c i, ., e 'y 'a rt. - - ,. ..- 1.ppro 24 ; , z.
p .
-u . . . .c ...4 .m.siyp 4;^i . . s, ' '4 's ,' ~-,"
is .. ' Q . . , t - - U. Y ,1 _ ,, , . e DICT SUPP, ORT DESICH SHEET - . .-
! $ , 11, . , . *[ $ * ~5 ,'5.- . t .[ ^ ' --4 .i.. . , , ap g, - .L 3. 9.-77 -
to,1,,1, ,,, ,,, 57o , Cilent Tbe Robert Irsay Co.' Hanger Mk. No. [Ilf-2870-N-27 Project Enrico Teral Atomic Power Plant #2 Hanger tw. No./O-422/-tm /M-283 -27
. t k Pro, ject No.2-- 4221 ~ - ---
Duet Size ~~ f2 I~~ --~~~~~ ~ ~ - '
~
Systen QJ)] el C6NTtd /h/NC ' ' Computed by 9 AIND.IM
. . . .:.a. a u.1:_.: m:2m: .. ; u . :..t .:_ 2 ;_. _..J._.. '
- a. c %, . .
- 5 I'bi$
< :. r. -
3$hu'5I* N4N'-%N $
- s. h :.,- -'
* ' . ~ ih . ^ .m:, -
_ . . . . . . ...._.._-..,,J._ ...w = :.- .a , . . - _ . - .. Support Type - -; j ___
- - Hanger - - Lateral - - Axial ~~- ' --- ' - - -- - ~
- Dir'ection't ' '
NRi ' W .,. 9 i
,. _ . ~ - hdime Axis ~ -h-- "~$~'~~ ~~~ ~~ ~' ~" - ~ ~' I i
I '* n'. Q : . %: 4%.;i.i .,~ ?l \ %V k . .::.. .. -
=--
i . . . P l Torce Weight Seisnie Load (f): z,y,s, Dir. Cob &tned Max. l i (1bs.) , load , Ixx Equiv. Cylinder 1 77 Equiv. Cylinder Imad -'
- F, -
~. - -
r r 83 - et t .. 10 lof a > c:
. } . .. . , . _
Fs ~. * " ' "
.' 6' ~ \ ,' . I', ~ i '-
[ - . - - . . n. . .
. .. e ,f..,... .The maxisca load is weight load plus seienic load. ' i the larger seismic load from either fxx or t yy is used. .. < ,h. t N.
, .,q
~
sg:c . f
.p; ..j ., e v . ..;. n.9.-....f. , , 4, .g.. 4 ..j r.-
- a. .
-g.- . ,s .+
y ,. Remark: $ Support design drawing is included in this report. O Support is for multiple ducts, the design draw'r.g is i . ,. _ ^
...c.. ..s 4??; lre.W. -. . a. .
- included in report 30.1( **' *6-**.'
. Nf' .::t ~ 'ic >4' W f.'
ic
; .' ,, . .! : ] . h. ..c'>$k'.htcw,ff' k r r<
pl ,;;y.-
.. . .r. m.. . ., w n 1 .
i a
'g mm-
. . yg - . , n .- x.--,-- . . , ... ; ,,- _ _3._ _ M#4 _ . - 'J:i . q;.dy3.' ' ' " #: . ,d.k DATSHT W
_tGC k, , , i W.. ^ OFd.'h "
' > ~'
s 's s t.~ , =.."~ ( % ' ,,.. ':r*' n . ; s; .A , .
.'f.. '*'* . .m ..., 3,.,,,,.
- ,l
. y ~. . ?*
w..,-. [*
' , '. ,;,,p e.&. <
a;, - 7'Q2. . . p,
- w. ,. ,
- ~.
- c. .,r k M. N. E'
?
- e. ..
I.
; o .- . ., ~ . DUCT SUPPORT DESIGN SilEET '.~
1 {5.,' j'_ - ,
^
f85'
; _ Date 3"<f~7) '
AnalysisP'b.No. :;
~
Client The Robert Irsay'Co. Hanger Mk. No. f Af Wo -h-30 'l Froject. Enrico Fermi Atomic Power Plant #2 Hanger. Dwn.' Mo./04271-OOO -/./5f. 2851c-3(* Project No. - -.- 10-4221. ..- - --- - Duet S' ire - ID0 4 Computed by .D. AlijpA A/ ! Systen OOMik'st. CEM{CC. SV4C
~- . . . . . . L ,, . - _ . 3.._ - _ _ , ,, ,_ ...~.. .. , ; ,. ..... u, . g ,. _ . , . . . .2 . _. _ . , . . ~
Sup po r t Type._ .-. -.- -
. .. Hanger.
f : ~~~'.a*.-1 t e'.~T Axial . '_'.*_~' ' Z Z". !.'"T._"'* *", : ral'?.'Z'. 3 9 - ~- - , .U . in
' Direction gf, N.' . . Coordinate Axis - T - . + ,l.: - .m..* - - m . r m . .~ . .. .m . ,a. . . . .-- y. :i . e .: ...;,.
_,a,, x r. ;.f l u._ Force Weight Scismic lead (f): x.y,s Dir. Cobained Mez, (1bs.) . Ioad Ixx Equiv. Cylinder l yy Equiv. Cylinder Load F, . Ty 83 03 ),l l06
.. Es. . l . 6. . q~ .c a 7..
- e. P The maximum load is weight load plus seismic load. '
The larger seismic load from either Ixx or tyy,1s used.- *
,~ ..- .x. ? . , p, . .. .
- . . v. < .
s; . ., gf. . :g:g; ; ,- . .,
? %. . ;; 3 -. ,. -
l
- . , ~+ - .u l -.h. . .r. . .b i i /Y 4 'r ~ '
hg,,g, % Support design draying is included in'this report.
, C Support is for multiple ducts, the design dra'ving is * ** . . G ly .s.*. Q n .': ~inc1'uded in report No.:.'..,.6. ,.
p.e.;.;.,%
- N " . r, ' 2 N 9 -@ y .- .7 " -M l~ . i .,:.. , , ? . .. - n ., p . . w. .a irr D' % *
- 3. a - ~** '; *e r..
y .,. .2 l {.g
- 3i -; .) * >";, ,,. Q.'
4' = , ).. , , l ;*i.g '- f L_________________________ _ _ _ _ _ _ _ _ _ _ _ _ . _ _ _ _ . _ _ . _ _ ._ . J
_ m.. . . _ . . _ . _ , , ._ ....-4 _ _ _ _ _ _ _ ... ._ ___ _ _ Tf f kA * ' y, -
. p- .N, .
o -
,e s , i. ..c m,g. .t. , .-S. . ).b.' * .. .c .
n
'fi* r ? :, - -
Q3 . 4 ,w o__,n,,,, ,,;. ,, ,,:. .
~.- -
I,,2, . . - . - . . a. b; , [*- .
.?
DUCT StfPPokT DESICN SHEET !y;_
. , ' !'.Eg .t- .- xJ c.. . :;t . .r. .2 - Date ,9 77 -
Analysis Pt. No.~ [O;. m W: 'W : $' '
. ~~ -.._'_'~ a Hange' Mk. No [N-288'd-3/AS/ T i~'T ~ ~
Cliens The' Robert Iraay Co. r
, Project Enrico retal Atomic Power Plant #2 Hanger fug. No./O 3/22/*CDO-0N-28, *3I ~ ~ u Project No.
10-4221 Duct Sire -- NX0 '
. . . .: -..s; .7t
- System OMTfDL bd7tI N V C. ' Computed by -
O
- N/lD.4 N ']* -
i
. v . . .c' -
- s.,. .]+j_,-i.g-; h r L
..e... ,...._..__.~.u.. , .ss :. .4 c
i j
-- - / . ,f. --. - .v, - .,et , .t., . . . ,;: ., * ,. , , . A. ,;;,
Support Type. _ _ , ._ j!angt r . _ L.ateral. ... Axial,,.. ,
._ . 1 21,__ ;
Direction pg72T". g ,y ~ e--u ce. _ . . .a v-Q -kWJvM 4 sa,/ow. %4%
% w-. .
Coordinate Axis . . _ _ _3_ ..,. . . . _' .
.a1.%;.. ...... . . - . , .., m ... .y ,,, , 3 u,,,.;;, . , ,g.g, .n .~-.7._q.,.._..- , , g, ;.; 7 a',, , , , . .
r - .- .r:? m t%=,, ,- r,,. ,. .;1; .ur:n, .1. n- - V force Weigh"t Seisste toad (i): r,y,s, Dir. Cobained - Mas.
- (1bs.). Icad Ixx Equiv. Cylinder l yy Equiv. Cylinder lead ,
r, -- __ - u ! l
.z:
l _ Fy Sc/ - S$ 31 - lib ** j f y ,,,,,, g- - . . ,. u - .,,
. , .. x .m ; 4y 3 5 f ~; ' .n'yjl }f s
The maximum load is weight load plus' seismic load. . , - Thelargerscissteloadfromeither*Ixx or tyy is used..',. .. ,. ..T.,1 'f1i . ,f./3 i
\ .c .. c: . ,n: . . .o y f . , l J;v. .. 5; _.:.~x 's 's ~ gnlQ j Q n . s:
N, ., 9;
- , . a x- - vy
- 1';
.<, 'i
- G,Qq4, ya . .s n' ,;' .&,g,ue. T f.H-yo.
, . . y@j.p. O gig .. ..yr, n.s u e a.v ,ypu ,e g ~ ~ ' ".T :; .r ... ., m.u. y n , #.w:w 2' . + . v. / , ; . _ e .;.y 3 3.
- ~. ..a.,.
,- . .m> t 4 ' Support design drawing is included in this report.
C' f,. [p gg,,,,g, % C Support is for multiple ducts, the design drawing is y_
, included La report No.', I [ ' . ,wbNk -ha - b'kN - ,w w - s .I.3 '<mw%Li.w$ sc:. . . .i , . .
v .:. s -n. . u - i
; . ara':e.w a ,.a. m. :, , * 'l.. ~ :.
rw.. :~r-. : t
~} ~ 'lh.I' % :<*Y.;.*$$a*
i - . . . .. .- --
l .
,. g i. . uGNuggpf1 .n.;
l
-($1 I l
LDATE DATE,k7//.g. LEHT'. SHTs 012aop/pg ' Vi '
,,.9.5 i l
y ,]t .I - d , I*.hs, ' 8"g,,,g ' ,y,':; , . , pp , y
, . ', i j g;,y,,*; .g ~
j
' . .{,Js. . n ., . ~ 8% , t [g p,4.@
- t'-
o
, e, '.di '. - . k Pil)OR WC. U. . s. ' .s ;, :.....'. / f ,
DUCT SUPPORT DES!Cil SIIEET ' c , ,, i Date Analysis t. No. MM-
. . , . . . . . ,, . MJ Client The Robert Irsay Co. Ilanger Hk. No bi- 28(/9-N- 41 i
Project _ Enrico Fermi A'tomic Power Plant #2 Hanger Dwg. No.h *il72/-4'b /M-7F<N (/2 2
= ,. - '
Project No. 10-4221 Duet Site - l(-K if. 31 System I_ CUT Ctf CENR$ #VAC. computed b' D M404/ , r.r- - .Y .>; ..t
.... , . f.;.u.. :,.a, .e :. .:.7 3, ,, . .,
Support Type.. - Hanger 4teral .<. . .~ Axial. . . ,h w-, . . ~ v Direction - $f g f. . E IV . . '~,~"w' -_ ;Im _:-
,_ w ..._.C t
Coordinate Axis y_ )( . r
~ ~ .*~ -.: c , g: :z .~ ..; g%g;,3.p' l {_- ..._ ;
4k . 4 - . ;
~ )
rorce Weight Setssic Load (tit z,y ,s, Dir. Cobalnad Man.~ - (1bs.) load Irx Equiv. Cylinder l yy Equiv. Cylinder , lead ,
, F, & g .y fg 4..
Y
- r. 19 7 'll lY
~
ZIS F, - - . -_ , -
, .. 7 wr o. - \ r; the maxleum load is weight load plus seisale lead. . . . .,4 . . ,L . - . . l The 1stger seismic load from either fra or f yy is used. s, '..h37] . ,., , . _ ;.- . . p ;Ny r. t: - -
- s.
j [ i '3 j :- y dj -
'ef , . }l, l g ') .* . *y ' . :?.g ,':: -fg^ .1 ; ,. qp (C- ,., . . . I 5 , ~ 7.,. s . E'.? .? ' $. ,i h . w e,t,y . .
4,T . i
~
g.' . . g Rema rk t % Support design drawing is includedi in tkis' report $ '
- i N 4.' ~
p C Support is for multiple ducts, the design drawing to included ik reporh [lo. kkh.k3 .i $ N $ b'eb N W ifhh h h h ' hfEdhh, fh:*i M.-;y .y ;7766-{;{ y
- 6h. .W,,, .--
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[ ^, DUCT SUFPORT DE51CN SHEET
. y .y' . 3 ~ "
r , . . h .,
" *;M*%
Date 3 1'l . .i . Analysis Pt. 380.
. MJO '- . m <;,-L Client The Robert Irsay Co.
Hanger Mk. No. [N-2ft/9'-//-MJ . Project _ Enrico Fermi Atomic Power Plant #2 Hanger Dwg. No./O-t/tti-O@ -6Af.7]</9./j , se 3, - Project No. 10-4221 _ . . _ . Duct Size /6A l f --- - -- - ~-~h 5 System CUTDt CEWd pVAC Computed by D.M/ID.N
. . . ..i. t . naz ..u nq . .. . -......~^L...,.-,...-..l',.T..~. .w.~.., . . n.. :. , .
4 ...s.h % M &i2.YLM.Ii.A __.x :EdE5
......_.-.-.._.s+ w~.-....c.... . . ., _. . . ,. .m -
Support Type. -. t.ateral _,.. _ Axia.l,. , _ _ _.. Hanger.- ,, ,. Direc tion' - gy. '< - - -E-W ~= + ",. A" * *W. . . . . n#.~.' ' .
.s . w Coordinate Axis- -T . -g...- -, ..! .f-; -J : . y .. . ; s . . : . , gp:.3.t:;qq1g'i j.;7. ';ggy.;ql,:h.,gQ .
p; hh O *
-~ . ; *. . T p - .' e ., . . ~ .1.:: 2,1., g Torce Weight Seismic toad (i); x.y s$ Dir. Cobalmed' ' > Max. .i[
(Ibs.) load Ixx F,quiv. Cylinder, 1 77 Equiv. Cylinder load y 4 r, - 33 y*- ,: 33- }
~
r, So6 'f4 .- ItfL % S20 r 0;
- g. . e .s..y- .w. , h(b.
3 ..
*"" ..**"dr.,,s . a . . . . EA .', * ., <r A a? .e, i . ". j d'. ,; .% ,.
'l s : 's t m- . . .? ;"% -';;,i...: C L f... ,, . _l , The maximum load is weight load plus seismic load."'C .'i'iW J.E' C . % j A ^, '? g 3 The larger seismie load from either Ixx or 1 77 isused.yff'sf2"i W.'. N;d '
. . . qfF .s . . . J'!& kWh; .. cgf.l- . W.. 'y- q.j' Mlk,)f:.f . K; , L-2,-s.;y;,~t . ; 4.'*-; ' "1 , .& D,};$)@i?rh..SIilA&5?'.h s .u -
y ^ 4 .* d ,.:j,7c. a& h 6, ....aj}.d.1Q(
'l .y. . Q . . sp .4% 3 :,p;; w. ..p . . : .;.w 4 . , n,. .~ .- .s v
, . ,g . . , J 1 .' > #
,;fc"..
u . - &gcy :
;~
s<
. a,. , .y. . :.u. . . p., , o. , . , . ,- . ...< . .. ' .,g,.. % Support design drawing is included in this re'hrt'. p .. %
- gRemarb Q Support is for multiple ducts, the design' drew'ing is r* - '\ ' .
~includedlareporYNo.'lRN. -
Nh $ -
'D-;
j,g.::q M " M U M & W if
i?;*# ' W/1)
.3 , ' ' it rA ,,,731E -
h
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. ; f, ,, ' ' , ) , . g . , , , .a . - . 1 s.. < . . , ITjp ' ,. , . ,, e:j_t'y yk (h ..,y.. l l.
t t;PLUOft M NC. r
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DUCT SUPPORT DESIGN SHEET 'i - { , . 31-7 7.. _, . .
.)_., i._ , , , , ,, , (, ,
Client The Robert Irsay Co. Ranger Hk. No.6M- 2.#44-/f-# Project Enrico Teral Atomic Power Plant #2 Hanger Dws. No./C-#f 21-M bM 28Q t((
= ,,
Project No. 10-4221'~
~ ~ ' ' ~ ~ ~ ~ ' ~ ' ' ~ ~
Duet Size ~ ~ I6A l2, ' _.~~ Systenff&1l?tt CENTER }lVAC Computed by .D Af A r>t d _ .'. ..6.'A. -* . . _ -.
. s . . - p M ...-.4. ,:./ N.i d . $ z u ; f,a .!d-.h ; ~.s+ ; .',;', ^- - - r . . ~ . . .. *- : a r- . . .a-Support Type ~ ~ ~ ~ ~ ~ ~ ~ ~ ' " ~ ' ~
Hanger ^~ 1.ateral~~~' ~TAxial Direction
' MD . E-W" ~ --. E' Coordinate Axis T: ' )( - . . . :v s -
- . . e . .e . . , . .,..-:=.n: - - - - ~^ -
.?
9 I
.m .
j e
,
- _. -.s Force Weight Setssic toad (i): z,y,s. Dir. Cobained Max. -
(1bs.) load Ixx Equiv. Cylinder 1 77 Equiv. Cylinder lead r, I g 23 .
#7 .
Ty jjf, jf , - r: l.T - 4 2N r, -- - - -
- --- r - .%." . S ',.s.r* ' d The maximon load is weight load plus seismic load. '. 't r
f. The larger seismic 16ad from either,1xx or l yy isused{^ . - - y:
. ~ . . ?
5;..
- k f 3: ; 2f ~ , ;
y
.' , 4.;,j . 4.: b W.' . * . s
_', , ;, ~.r s'
~. ^ ,, .. . -. ~ . ? . . , ~
hRewrh E support design drawing is focluded in th1s report'l' O' support is for tittile' ducts;.th. dess e n ar rio i. # . ... ; imeluded'in$ehrt
~
Ididh ~
.,- m b .. ~... 'b u f's p4*
3,.. b4 .. t v. . . -.,
$g , ..a. j 4* i i * '; C, ; f, ji&R*- Qh *~
vv . m _- - - - -
- .--y=~.- , .. ;,. -, _....,t .
08I ]/Y,b4
;', 1 h'~
t l'- S H T .__ 1 $ D JO F _.1 1 }. ., V :. , , -
;Ty3*f.3 g. . , .g,('.4-j , ,9..p. w m 4.c a , q. % x,p ,*) -
3, f. ".Ig M ?hM ,.i.,iik
. . ..e . .i..A Q.?, * ',1., 7 : . ~ '
k M . M.. E : i 1 l DUCT SUPPORT DESICH SHEET s . V' 3-9-17 Date Analysis Pt. No. MO - , 1 Client The Robert Irsay Co. Hanger Mk. No.(>Al-2N9-//-Yi" Project,,, Enjco retai Atomic Power Plant f2 Hanger Dwg. No./O-922I"@ IM 2M/-Y.7 I Project No. _ 10-4221 " ~ ~~~~
~~~
Duet Size /6Kl[ i
~
Syatcm .M[ot . k&JQfl}/A C.. Cosiputed by J). AMDh/ L - : .a. 3::w . . __
.a . _ - ~ '- - " - - ":0?*ii _ . ' = ?M.5 . .. . . . . , , , , _ . . , , , .m-.. . . . , . , ,
- Support Type ~
11an ge r--' - 1.ateral ~ Axial -- - - - - - - - - - Direction -~ VERT^ E-W -
~ f ~ ~' - ~ '-- ~~- - - ~ ~ ~ ^ - --
Coordinati~ Ails ~ ;"J ~
~
v.e r- m. . s..:. x , - r .;.a. . : ..~ ,. ... . . . O . . . - _, ., rorce Weight Seismic load (t) z,y I, Dir. Cobained Max.- ~~ (Ibs.) load Ixx Equiv. Cylinder 1 77 Equiv. Cylinder Iesd r, - j9 2.2. 29 : r, - ASo ato . . I7 950 r, -. _, . _:. .:. ( . - . . . _., The maximum load is weight load plus seismic load.'
~ ' ' '
1he large'r _ seismic load from either 1xx,or yt y is used. . a 40,..
'.3 r y'I.r:., ., v i : < ., , .1, -*~--
N . v.
,8 % m ;r - < ~
3 ;.
.y - s ;., n . c. - .c . v, . ,e-3 ,
g , ;-
.,' . 'n, - ~
Remark t h Support desig drawing is included in this report. O ' 5=rPore 'is'ror .uiti,i. ducts.. ts. 4..is. 4ravi
- 1. - . 5 l
~ . v .. ~
1.e1.d.4 L re w e % W ri; A $ M.... .. . W. . ...% W eh W && W akikNkbh$$$?bhhh hkN'Y ^. UAQhh l
. g. . . - - .
NO7 ~ h 0f5E...1 HON ' 4
....,_.e~..-_. '.',
S' H T.l'.'g f ~ d p?? } y .~-
.. - g .,-.. . .-r------- -
y.r.?.3 e ".31 J;
,_ ?.; . ,.y '.& , %. >. . .* 6. , , ._ :3 y _, ,g' - ~. ~ . .' ? l 3- # ,','. ~,*
q g . 50. DUCT SUFFORT DESIGN SHEET
- .L*.1"Y.-
3 ... Date M Analysis Pt. No. Client The Robert Irsay Co. Manger Mk. No.SM-7I8/9 -#- % Project _ Enrico Fermi Atomic Power Plant #2 Hanger !%,g. No. h-V221-O@-SN f8W.8/6
- e. ;
Project No. '10-4221 ~ _ Duet sire k (f. systemh07Rct. OEsprR, M4C computed by D AfADAM w,
.l 4.:v r s - i e.. , - ~ . . _ . . - , . -. , , , _ _ _ ._ . _ . . . _ . . - - - ~ ~ . . .- ~~ , _ _ _ , , _ _ _ . .
Support TYPE Hanger Lateral Axial l3 . _ . . _ . . _ . Direction __ __. . Mf; _ . E-W .. - - -l----- 1 Coordinate Axis , f,- @ q _. ..,-)("" ~~
~ ~ ~V -
O . .
~
i .', r. l Force ' Weight Seissie lead (2): x.y,s. Dir. Cobained
..;. k-Max.
(1bs.) load Ixx Equiv. Cylinder I yy Equiv. Cylinder 14ad N > ['. - i . r, -~ 4D S3 53 ' i .
~ .- ,936' 'A.
T,
$$ $3 & )t; y, _
9,d.
- The maximum load is weight load plus seismic load. .
2 The larger seismic load from either Ix, or lyy is used. '
.r A * - , ;.p' . 1 + . .
1
..e .~ . , -
t4 Z . i hFemark: @ Support design drawing la included in this report. . C Support is for multiple' ducts, the design dreving is.- .-*'9- , g, w *.W.sr included in report No.' 1:y;f:,.; t4 . tsS'f..r :%4$%'.yW
.f; i.i:i . . 4 [..i.Q. % 9 .. r. . .h '* * *- --
i h' "i - -
~ . .. t< -
_~. _ _ - _ _ _ _ _ . _ . _ . . _ _ _ . _ . _ _ . . _ _ _ _ _ _ .
- ' ,j., ..%-y ' h" ; i k< *" ," ; . _, _ . , ,
V- j
, Y7*0)7-Y "
- l . W:$ ' & Q 7} N. &p >.,,_~
l OkT% aAl
... a, _mem . . se_ _p z . .. #
i i: i . .
.. T- ?
f ' '. f'-J'[;;$ %f1'6uI'$x,%'h'$iI..*diaT'[/*'j[E. ' ~~* S , T 4
!.3 3 W- , p.[ & y f a ~' '
f,,. . gc . .
~ }g t . . v- . ; s. ~ .
3 e , y ; DUCT SUPPORT DESICN SHEET h d'.. . . :E.
~
i Date $" #I* 7 7 Analysis Pt. No. 880 i Client The Robert Irsay Co. Hanger Mk. No.0 M'lI O */f-9 7 l Project Enrico Fermi Atomic Power Plant #2 Hanger Dwg. No.h.V22f.000 4M 2JW 8// -- Project No. 10-4221 Duet Site /0El6 5ystes h lylftsL (CAJTf_L' //t /40. Computed by D IIII)D4A/ 1
,.,, , - , , - , - - . - . -- - . - - - ~ -
4,,, , . . .
,J.,. m ee e<> ...-...~._..--=-.~.~*~=--.=~-*~~~~.-----.-------J. -*---~--Am.- - - - + - + - .. Support Type'- ~
Hanger t.ateral Axial
. _ _ . . . - - - - . - Direction - -ygRT - L .bl - - - - - - - - - - - - - - -
p*. . .- Coordinate Axis f g ' - - i Porce Weigh.: Selenic toad (i); x,y ,s, Dir. Cobained Max. (1bs.) load Iza Equiv. Cylinder 1 77 E.quiv. Cylinder toad . Ts - 50 52 El F. y M'l to Sa* 'i.*ll .:
- i. F, . , - - - -
r ,. The maximus loa'd is weight load',plus seismic load. .-, ,
. The larger seismie load from either 1xx or Iyy is used. ' ;~ r .- .
{[, , 9- , N . 2' . er
- Remarkt @ Support design drawing' is included in this report.
* ~
Q Support.is for multiple ducts, the design drewing is N '
$ ' ....,'-t_. : L f;pi' ..~' 5 ",*jz.q-A +: L : / ai] - .t . -
e e .-!.* , ; P- . included la. report <k.c . - No < .4, - :.:ts ; . ,
..a__,___.._ . -
4_ % .. y .. :t mp.:,' g .5:.6#4{ ' ~ ~ ,
.U.; 'Wt **' ? % '** M *. 4. ., . ,t b . ?. . ! 4' C. . - it @,,', .4 -- -, d;,, .-
____ ___ _ . . _ _ _ . 4- - - , , --e. -y - - -
i ' ' * < l
-fpt)7 N/ {yif f.NO_gO $ ' - ~ lf MTr -Tf l - - : SHTu.Jf.MOF - G -
l I
;.$'s ? * . h? . " . s.; l ?;.b.
f N'~Y' b .
.h,, A ,.** ' -
t gh , * < 3.u .c r.gl . f M M NC. r- 1 i, ,
,'l , . . - <W ,, y . DOCT SUPPORT DESlQt SHEET we. .
e' , Date 3}~l) Analyste Pt. No. 8l[O Client The Robert Irssy Co. . Hanger Mk. No./M 2$'U/f-8" /8 Project Enrlco Fermi Atomic Power Plant #2 Hanger Dwg. No.h-Y22/'8V' *dN'78'/7"f8
~ e. '.. Project No. 10-4221 Duct Size /SX16 __
Systea Oh)1998. (UnstrID }WAC. _ _ . Computed by j). tllAp4N 5- =. .... , . , . , , . 6 6___...._
.~ . _ . _ _ _ . . _ _ . _ . . . . _ _ _ . ". . Support Type Hanger t.ateral ' Axial .
Direction yg?r. N ,# --______ . _ , _ _ _ _ _ _ _ _ _
,ry-Coordinate Axis [ , ~d:: - -
t . Q. Seissie lead (i): x,y.s. Dir. Cobaloed Max. 7 rorce Weight (1bs.) load Ixx Equiv.' Cylinder 1 Equiv. Cylinder 77 lead g.: r, - -- - - ry 96 16 87 . l13 R. .
- 6,.. rs l _
ITS l82. 185 T (3 *. The maximum load is weight load plus seirsic load. . 1
*g . The larger seismic load from either fxx or l yy is used.
( 4 ..c ' 1 llJ N &. - . a
.i . '
Remarkt @ Support design drawing is included in this report. 4[; '
.y.
- .O Support is 'for smaltiple ducts, the design' d swing is rk? ' jfegg y d .,"eport ho 'M
'i. 3 I IIbI $E H- ??M$'SkCb$kYh 5h hh k ! , $h:- !
W. N $ 9 $.3 6 '= .1 fk$ l
~ , /" T/7/ 7 - ~'
ONd//.k 8Hk)h._;_QF__j.%-s:m ~f 1 l I I
.. r' .. ..t. ,,*]7 ,o ., .' ' . ? J f;- ~.... ,. y".p e *fm;'a ,,3 ^' ;~ ~
s rx, -
.y o : < ,q1y p} p g a.,,, . y WWC, ; $[
- y. '$ @'.t @.p',: g :, , y j- ,. &
. 7t.* ; ')
[ *
'" ~- 4 .$j DUCT SUPPORT DESIGI $HEET - ~ .w. - - - ..e..
. Date Analysis Pt. No. 380 CIlent The Robert Iraay Co. Ranger Mk. No.[N 2FC/9-//-l/9 7 , Froject Enrico Termi Atomic Power Plant #2 Nanger Dwg. No./tF-Vl#-Cet' -MNWf . -
. , . i Froject No. 10-4221 Doct Site /dXila System b0lVII'I-[GUR/d/IVAC. Computed by h M494d m,
g.. ,. . , _,y
, - . ~. . ..__,,,.,.m__;__ . ,,4 i ^
j Support Type Hanger Lateral Antall - -
- d. .
I - Direction y0,ET.._. g.,g. .._--_._ .- l Coordinate Axis 7 A - n'=-
- : - . ', . d.
w -.s s,
-c Force WetS ht Setsaic toad (+): x.y s, Dir. Cobained Max.
(Ibs.) load Ixx Equiv. Cylinder 1 77 Equiv. Cylinder , teed .
,:. ~. 4 y, .,,.
Fy j& ' *
)4 fl +
1.03 - < r, - ts' Is . JW s.i 7.3
'l . .- -,r p' . .
- n . . g : .1 . ;, '
-* The marious load is weight load plus seismic load.' ,, -
r e%2
' (( e n.: ." -', . . [.
- h. The larger seismic load from either fxx or tyy is used.,.4 .f i
d -{f"- [&
. ry . . :. . .* . ,p, .,
ky ir,9; l Q ^ *. ;^. . y.h..'.+q
. ,..; ; sp.f, , l ' , . ?, . ; ,s. .q. , , . -. .7- - ., ~,r I '
hy,,,,g % Support design drawing is included in this report. [ C Support is, for multiple ducts, the design dravias is . a' ' l .
- inelhed[idrehrt ebNU' *. . N fka ~~ "
L. -
, . J' ,;@n..x:.ni -
x k v r- - n . :. s .;4d
- ' ((
, [..\ ;
.....g . ~ ~ , , . . ~_.. ' - ~ ~
n ;.y .., , ,_ : DCi % _'l.82P6 ._JJ$ ll. ? ! hT7MT Yl
. ,- L .
hkTGC 2fts/s4..n. G': . !
-g g _
f
.,__ {
l l I r , .' - }J -
,J.. . .1. . F . ,, .. . g , .4J J 'd !
5.q . % ' ' . y v.a. . .
~ /I';h . "f Y . s g o , . ., t , . . . . . .. . .-g e- .t.c;. p .. . . ,
n .) , .
- g.:e
.' DUCT SUPPORT DESIQl' SHEET ' ' '9 'J ~i. j . , _ ., : . a . , ~ . . . - 7 i Date Analysis Pt. No.
i Client The Robert Irsay Co. Ranger Mk. No.d M .)$ @ . N f0 t Hanger Dwg. No. M N " M M ' N I 88 __
. Project Enrico Fermi Atoute Power Plant #2 = . '
i Froject No. 10-4221 Duct Sise fSXEe l System [CNJRrl. l'GLik"fi NVAC. Computed by D.MAMd l ;
- .. . - , . -.-L.
. 9 ., 5.+ . .h . . ,; .J. g-LEH r . 7y. . . . ..~.n :-- < -
l -1
, . , . .w.-_.
i ..- Support TyP' Ranger Lateral - Axial ,s.y' 3.. ; A ;A . -
.- o
) , , 7 Direction . . _ . -
/66.__. _ Af,5. - - :
i \
'.. Coordinste Axis Y: g , .e . #
m w+# ? - ~.__. . 5' . . . . . . . a
- .s
.~
1 :: . . ..
.; Force Weight Seisele Load u): x.y ,s, Dir. Cobained Man'. .
i X (ibs.) . Ioad Izz Equiv. Cylinder I yy Equiv. Cy11aser imod
....y . F, - - .g ;*
Yy $90 b . k' -
~
- 5. & , 8,
[,,;. Fs "
.3 s- O' ~ ' U Ui/1 bl=I fb 'h E.. . . -d .~ t e: c . O !? ~
The maximum toed is weight load plus seismic loed. .-T W,, I T.e,a ;,f. ' 3 J. The larger seismic load from either tax or t yy is used.. .P.1
&y,. *.- . , < . . ^ ' .% .,
3
. . =Ite.n. -*s P : #.n/.$...'
y, w . :,. . . y . ln . ;L,k . . Q+ :f._ } x n,,h.- .$::
- Np*..f.,. ..*( ?
fE ; c'
.N .. ; m, +. .
p g. wg ' - . m,y ; f.g: . t si .
, r.q. ,,.3 9 3,,.y.. -
1 9 g* *. < ; 4 y - y ,
,y . .e .e 1 s. .
- u. . .r. .
l
.. . . -? @ Support design drawing is included in this Ireport. ..
\
;' .. Remarks . e . . . : ~n g ,:- : .~ ,r.w -
m It1,1e 4uete, in. destoo dr.y;;. c. .,- - . svies i.x WD
.- ;/.y '. O s., port i. c., '. } ~ .)f' Ujs&&&h$h'kh&hhlh$&i,h'N .
L .fc1:.u.j:.:q.1. .. r . : br.c.z.
- k. mn v .
~.en 4 y wr e > > ;
c g. y,<.a.j .
.r . on.. ::
-'x g 1
i
; ; ': '. y g, g : :; + 3,- .j [N;:' .
Y ~1 TI4*f =,.. OAT 5wi1n- Aif../24 5. ~,,
,f;-_ - ,.,,w ,1 eh Q g _ 3 Q y .g $ q ..,.p. -. $..,: _- ~~---,.-,..-..n ,. -
t,:
*S a..
b 'F .a . *
.n J s f'
g ub,q< ., ' 3',;- Y. (y i ;r. .g P', {~mg.f y..;.;g;;(N,4p,%* .,3 , ' ' , ,
' ..% < , 7p ) a . .<.,,.,._....3 , ~ q . t v_. F a.
- , s.v .e<
g*-. p;m,,y.,. .:
> 4 O;.+ ,; . A. . ;. . ,;, ; _
- u.'
. . . . a:. . . ^
u..- DUCT SIFFORT DESIGl SMEET , ? .
,3, -.,'..- 'A*
- . . :;.:-r. ,
.;;_ :. g 2.u._.; . . .. ,_ *; Date 3 " 9 'II Analysis Pt. No. '3F# ~
Hanger Mk. No.[W-2fM9-N*[I
~
Client The Robert Irssy Cs. Froject Enrico Fermi Atomic Power Plant #2 Hanger Dwg. No./0 4/111-000 M28V9 4'/_
*. s Project No. 10-4221 "
Duct Site NX16
- Syaten biRol. CEMTcR #dC Computed by . FAN A AA Il
, , ._ . , . - . . .. : . . . . w. . ., g.1 - - . - ..g .yg . . .. .s. ..o. +, .
4.
- - . _ , . , _ . . , _ _ _ w . . . %. . % _ _ _ _ . . . _ - > Support Type -
C's Hauger1 1.ateral-
- Axial l' N -.
Direction . - (ERC - N -# n- - ---= S- Coordinate Axis .G *f.;L'ly; ;2- *'
*"& '$K ~ ? ;~q:-' 7 ,?;p .'. s a w
Y* .: Force Weight Seismic tood(ilt w.y,s. Dir. Cobaimed Max.
. (1bs.) load Imx Equiv. Cyli,nder I yy Equiv. Cylinder toad a ).g,n '
y, - - - - A.n l.
~~ '
509
.,,.+-. . Yy 30[ . . '., . Sa.' ' .
i
'g l,. F, -. j .,
j ' f - (p -l O .
~- - '. 2 -
1' The maximum load is weight toed plus seismic load.' - ,
,3 lThe larser seismic load from either fxxo ,r. yy .
I is us.ed., u... ...
;- . ~ '; p , .;. :- < ' ~ .5 .'s L. '~..t-.. i< ,
s 4
.,. g7 ., .D zw , u : - . ge 1 . . - 4 . t , . .:; +m _ ~ : ,
l u. ' ~;he l
= .-
- m. ; m,._. v . s .
e 4 Z .
;9 % Support design drawing is ine'luded in this report. ; Remarks 'h,.p ' . c ~
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