ML18117A376

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4 to Updated Final Safety Analysis Report, Chapter 5, Appendix 5C Figures
ML18117A376
Person / Time
Site: Crane Constellation icon.png
Issue date: 04/06/2018
From:
Exelon Generation Co
To:
Office of Nuclear Reactor Regulation
Shared Package
ML18117A343 List: ... further results
References
TMI-18-047
Download: ML18117A376 (29)
v • d • e


Text

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B-5. for.== r/8 VI. fJPt (capped cylinder),,== 0.3 A.-l for.== 0 VI. fJPt (capped cylinder), * -

O.~

+-....,~-

"OOLE SURFACE I

o-*S. for. -

3 r/B VS. {JPG (capped cylinder), * -

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C-5.. for. - r/4 VI. fJPo (capped cylinder), * - 0.3 NOTE RIEP'ERENCE: "STATE OF STRIESS IN A CIRCULAR CYLINDRICAL SHELL WITH A CIRCULAR HOLE," WELDING RESEARCH COUNCIL au L LET IN 102, 1Ie*.

o 1.0 I.~

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Update -1 7/82 B:imNuclear 1MI Unit-1 Total Stress Concentration Factors for Given Loading Cases MIDDLI 5U,,'ACf I

Ul 1.0 G-Sc at. -

0 for Case III (interna' pressure), *== 0.3 F - s., at. - r/2 for Case II (extension case )vs. {Jpo,,-0.3 o

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p. 5C.FIG-l Fig. 5C-1

a_cl It t r

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......,....,.211 C "".t~

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../2

-1.4030

-1....

-2.4293 S.(M"'~")

  • - 0

./10

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.2.19372 2.29030 2.48768 2.71811 3.02513 3.38629 3.79024 4.23059 4.70107 1.71403 8.79472 7.91827 9.06741

../8 2.33179 2.47978 2.87011 2.89212 3.13783 3.40128 3.87808 3.98608 4.26968 4.86482 5.48212 8.10374 8.72431

  • - 0 2.84701 2.81100 3.03170 3.28670 3.66487 3.83488 4.11911 4.40201 4.87874 6.20121 6.88463 8.0S6I0 8.37120 2.46986 2.86926 2.87286 3.08813 3.26013 3.41823 3.66&81 3.81961 3.81810 4.01661 4.18962 4.29120 4.31120 2.76064 2.14174 3.13210 3.30842 3.46133 3.61032 3.*716 3.72044 3.73868 3.86013 3.441&8 3.01080 2.81198 0.14142 0.21213 0.28284 0.36366 0.42426 0.49497 0.66688 0.83631 0.70710 0.84862 0.98194 1.13137 1.27271 0."14142 0.21213 0.28214 0.36366 0.424.

0.4N1'7 0.66688 0.83831 0.70710 0.14862 0......

1.13137 1.27271 3../8

1. 12040 0.80340 1.36627 0.81807 1.68750 0.83819 1.84227 0.88262 2.08948 0.88118 2.34032 0.91183 2.69828 0.16182 2.86882 0.18618 3.12823 1.02243 3.81078 1.10414 4.28678 1.20142 4.91210 1.31961 1.61731 1.48418 (middle.urface)

NOTK RK~KRKNCK: ".TATK O~.TRKa. IN A CIRCUL.AR CYLINDRICAL aHKL.L. WITH A CIRCUL.AR HOLK."..KL.DI.... RK.IEARCH COUNCIL aUL.L.KTIH loa. 'Me.

r v'Rt The.....0.,..t,e** caneentration factar Sc and the total A

.tre.. caneentration factor Sc are, re.pectively, defined by A

large.t of <<(11, (I 2 )

Sc -

la,**t of <<(I 10, (I 20)

(for fixed r, ~)

where N10, ~O ore the nGlftinal principalstre.. resultants and (110, (120 are the nOMinal flexural.tre..es for the shell uncIer the.0.... loading but without the hole. N1 and N2 denote the principal.tre..,e.ultant., (11 and 02 the principal stre**e.,e.pectively. The.t,e.. caneentration factor is calculated a. a func tion af q,.

1.34374 1.29180 1.29114 1.33988 1.42488 1.54~44 1.89818 1.87983 2.08800 2.17771 3.15842 3.81843 4.1501O

-0.14117

-0.43787

-0.74414

-1.01744

-1.40112

-1.77184

-2.11817

-2.18273

-3.43817

-4.3811I

-1.40137

-8.46127 0.48840 0.28087 0.07888

-0.11723

-0.30964

-0.1008I

-0.89263

-0.88871

-1.08337

-1.48249

-1.88293

-2.27291

-2.83894

../20.48812 0.44170 0.41483 0.37473 0.32403 0.28168 0.18814 0.011I1

-0.11836

-0.38071

-o.eaea

-1.03124

../41.56884 1.86386 1.78710 1.90438 2.08304 2.24180 2.43144 2.86648 2.89277 3.42431 4.03612 4.72369 6.48676 1.08342 1.32121 1.17420 1.81.1 2.01720 2.21480 2.12821 2.711I7 3.201.

3.82821 4.02201 4.317'77 1.79314 2.01190 2.23108 2."09 2.70142 2.93778 3.18071 3.43312 3.89754 4.27107 4.91382 6.83074 8.42C80 0.14142 0.21213 0.28284 0.35366 0.42426 0.49497 0.66668 0.83639 0.70710 0.84862 0.98194 1.13137 1.27271 0.14142 0.21213 0.28284 0.36366 0.42428 0.49497 0.66668 0.83831 0.70710 0.84862 0.98884 1.13137 1.27271 0.21213 0.28284 0.36366 0.42426 0.49497 0.66668 0.63131 0.70710 0.84862 0.18IN 1.13137 1.27211 IaimNuclea, TMI Unit-1 Update -1 7/82

p. 5C.FIG-2 Stress Concentration Factor Variations for Different at Various Angles - Capped Cylinder Fig. 5C-2

STRESS DISTRIBUTION AROUND OPENINGS IN CYLINDRICAL SHELLS o.

1.0 2.0 OUTER (A)

EXTENSION CASE L1KERKKEKER (11)

ERINGEN, NAGHDI AND THIEL (9)

LUR'E (1)

SHEVLlAKOV AND ZIEGEL I (11)

(8)

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CAPPED CYLINDER UNDER INTERNAL PRESSURf laiI!I Nuclea, TMI Unit-1 Update -1 7/82 p.5C.FIG-3 Stress 0istribution around Openings in Cylindrical Shells*

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p. 5C.FIG-4 Fig.5C-4

STEFL

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EXPERIMENTAL THEORETICAL VAN DICKE, ERINGEN lET ALI FINITE ELEMENT SOLUTION

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p. 5C.FIG-6 Member Stresses around Opening Edge (Vessel Subject to Internal Pressure)

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FINITE ELEMENT SOLUTION EXPERIMENTAL THEORETICAL~

VAN DICKE, ERINGEN, lET ALI 123

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EX PERIMENTAL PHOTOELASTICITY HUGGENBERGER TENSOMET ER 0 FINITE ELEMENT SOLUTION 2r

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p. 5C.FIG-9 Axial Stresses along Transverse Axis (Vessel Subject to Internal Pressure)

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p. 5C.FIG-l0 Hoop Stress - Resultant NO along Symmetry Axes (Test problem)

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8il!lNuclear TMI Unit-1 Update -1 7/82 p.5C.FIG-13 Normal Winter Operating Temperature Gradient -

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~R ACCIQ~NI ~ATU~E GRADIENT

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0 10 WALL THIC~NES5 IN INCHES 0L#,3 N

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INTERACTION DIAGRAM FOR AXIAL COMPRESSION/TENSION AN) BENDING 0.85 f~

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p. 5C.FIG-19 Interaction Diagram for Axial Compression/Tension and Bending Fig.5C-19

iQUIP~ ACC'S§'

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  • ---8000=-=--=-:!"----7:-0--::00~----<aOOO::-:-:-:+------=-5--::0-=-O~O----4000-=---+/------3=-O-OO~-.....,..-----=-200-:-=-O~--=~

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19lJ'PMENT Acces9.

SYMBOLS EL~M'NTS 66 o

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p. 5C.FIG-22 Fig.5C-22

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p. 5C.FIG-23 Fig.5C-23

ACCES§ SYMBOL G:L.EMENT DIRECTION 73 HOOP SCALe::

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EgU'PMENT ACCE6S SYMBOLS* ELEMENT DIRECTION 74 HOOP SCALE:

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(-6220) - 25 5)

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roo

(-8140, -145

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~

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p. 5C.FIG-25 Equipment Access Interaction Diagram Element 74 Fig.5C-25

EQUIPMENT ACCE.SG SYMBOL e*

ELEMENT DIRE.CTIO~

MERIDIONAL M ERI 01 ONAL Update -1 7/82 2000

+M IN.*K/I~.*

(1500,-145)

,soo Equipment Access Interaction Diagram Elements 66& 77

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100 so ISO

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100 1000 1500

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~500 3000

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VERT. I'taSO t<AN.

sooo

p. 5C.FIG-26 Fig. 5C-26

..DIRECTION M£RIO,ONAL MER\\O,ONAL Update -1 7/82 (1500, -145)

((il!] Nuclear TMI Unit-1 Equipment Access Interaction 0iagram Elements 44 &55

- COMP~E5SI0N KI'N.

50 100 50 150 + TEN SION

'00

(-2102) -211)

~

HOR. 1"= 500 IN-KIlN*

VERt I'~ 50 ~N-KilN.

(-~'30.-235)

(-4510.-'31)

+MIN-KIlN.*

~5~OO~O:---4'5-0-:-0---4"tO-OO---3-5~OO----=-30t-O~O---2-:5t-:O-O---2"O-:-OO---15:i:OO:-:---~-=-~~~:::::F~.-p~==:::2:;r-':--~---J5~OO:-:---:20~OO=-:

PU,N~

~~tMU)M~

84'

p. 5C.FIG-17 Fig.5C-27

t::.WUIPtv.lii\\j -.f ACC~9~

SYMBOb ELEMENt 01 RECTtON o*

IA 9~

100 101 HOOP HOOP HoOP SCALE:

~OR. III. 1000 IN-~N VERT: 1-. 100 K'/,,,,,

- Co MPRE6SION I</IN.

300 4000

,3000 2000 200 100

(-2102,- 2'7) 2000 3000 4000 5000

-M IN-KIlN.

8000

-+MU,M9 100 200

+TENSlON K'IIN.

£mmNuclea, TMI Unite' Equipment Access Interaction Diagram Elements 99, 100 & 101 Update -,

7/82 Fig.5C-28

p. 5C.FIG-29 SYM. ABOUT t OUTSIDE ELEVAT10N VIEW EL. ~19'*2 7

IS

~R D~

VARIES IT02~

64-118 A.,

~.

MATERIAL SPEC'F ICATION Ie - A516 SR. 10 BiElNuclear TMI Unit-l Sheer Transfer Plates Update -1 7/82 Fig.5C-29

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