ML20117E759

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Verification of CBI Axisymmetric Shell Analysis Computer Program E07811
ML20117E759
Person / Time
Site: 05200003
Issue date: 08/16/1996
From:
WESTINGHOUSE ELECTRIC COMPANY, DIV OF CBS CORP.
To:
Shared Package
ML20117E758 List:
References
NUDOCS 9609030070
Download: ML20117E759 (16)
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Text

._

l

)

1 EbEN AP601 i

f VERIFICATION OF CBI AXISYMMETRIC SHELL ANALYSIS l

COMPUTER PROGRAM 'E0781' l

1 i

PROBLEM NO. 2 j

Non-axisymmetric Loading l

('n 2 0' Fourier Harmonics) i i

August 16,1996 9609030070 960823 PDR ADOCK 05200003 A

PDR cw6ooAnaesistai.coc Page0

~

VERIFICATION OF CBI AXISYMMETRIC SHELL ANALYSIS COMPUTER PROGRAM 'E0781' J

PROBLEM NO. 2t: NON-AXISYb1 METRIC PRESSURE APPLIED TO AP600 CONTAINMENT VESSEL, (n 2 0 FOURIER HARMONICS)

ANALYTICAL METHOD AND MODEL CBI Computer Program 'E0781', " General Shell of Revolution Stress Analysis" based on the method presented by A. Kalnins in the Journal of Applied Mechanics, Vol. 31, September 1964 is used for the analysis.

Model is shown in Figure 1. The stiffeners are modeled as branches. The crane girder is modeled as a closed section using branches and a closed loop.

The radial web plates of the crane girder are considered as the additional orthotropic layers along each of the four sides of the box shaped crane girder. Smeared orthotropic material properties are used with a meridional value for the modulus of elasticity, E equal to Young's modulus factored by the ratio of the radial web thickness divided by the radial web circumferential spacing. The shear modulus is then computed to be one-half the meridional modulus of elasticity and the circumferential modulus of elasticity is zero.

MATERIAL PROPERTIES Properties are at 320 F.

Parts 1 through 3,5 through 10,12,17, and 19 through 22:

6 E = 28.18x10 psi; v = 0.3 Part 4:

9 9

E, = 28.I8x10 psi; Ee = v = 0; G,e = 14.09x10 psi Parts 11,13, through 16, and 18:

Combination oflayers with isotropic and orthotropic properties. The layers representing the radial web plates of the crane girder use the orthotropic properties calculated using the method described earlier.

BOUNDARY CONDITIONS (for each Fourier harmonic loading)

At start of Part 1 (Base):

Fixed At end of Part 22 (Crown):

Q = N,e = 0, N, = An x Rcrown / 2, and M, = N, x t / 2, where An is the nth coefficient of the Fourier series that represents the given pressure distribution - see page 3.

At branch ends:

Free iProblem No. I was for the verification of the program for an axisymmetric uniform pressure (n = 0 harmonic) and was submitted to Westinghouse via CBI Letter No. CBI/NSE0029 dated February 5,1996.

CW600ADRMM81HR1. Doc Page1

4 t=1.625" 2,z

~

j.it

,/

n 44"

=

/

l'

< @l.+'@

j s

a

/

a p15 g.

/

m 18 N/

El. 218*-81/2 T. L O,

,Q(.-.--

g

+

/

g El. 20 5 5 _,,,_,,,,,,,,,,,,,,,,,,,,,,[,',',,

a n,

p

'C Radial Webs

~

/

Q

/

s (80 Ard.)

+

/

l Girder Plates 8':

36"

+n y

/

g t = 1.5"(typ.)

/

[,,,.}

k @ l:

d 30"

+../

EL,1Jg:0 p

9 = 150' hd h

t= 1.625"

=1.75" INSIDE RADIUS, R = 780" g

REFERENCE SURFACE 4

S 9: Meridional (along 's')

'h i

44"

+I.:

0 : Orcumferential El.132'-3

[

'\\

e'C m

g",_,

(._,' /

g

'4 3

h +

.4.

t=0.75" T

/ aper 1:3 (typ.)

El.116*.10 9/32 sr u

'~... e = 79.2116' t=1.75" PART END e

N m

~..

El.104'-1 1/2

. T. L

~ --. ( t 1 J El.100'.0 O e^ar"o.

41

.4 7

'/

g W = u, =, = uG= 0 j

i' FIGURE 1

.(

...,,. /,, /a**"

SHELL OF REVOLUTION 'E0781A' MODEL I

CW600ADRMM811ml. DOC Page 2

COADING Non-axisymmetric normal pressure as shown in Figure 2 is applied on the shell parts above El.

132'-3" through the Fourier harmonics. The shell parts are: 1 through 3, 7,10,14,15, and 19 j

through 22 (see Figure 1). This pressure is applied on the reference surface which is the j

inside surface of the containment vessel.

Applied normal pressure, pn = An, where An is the coefficient of the nth harmonic of the Fourier series representing the given pressure distribution. The distribution is symmetric about 'O - 180*' line. The Fourier series representation for such distribution is given by 3

q=

Z A cos(n0)

(1) n n= 0,1,2,...

Integrating both the sides of Eqn. (1) from 0 to 2n as follows:

i i

2n

.o 2x 2a

.o 2n f q dO =

Z f A cos(n0) dO = Ao jdO + Z J A cos(n0) d0, we get (noting that the n

n 0

n=0,1,2,.. 0 0

n=t2,. O second integral on the right hand side is zero)

"z/2 2x

~

Ao 2x =

f p dO + f p d6 => Ao = p / 2 (2) 0 3s/2 Multiplying both the sides of Eqn. (1) with cos(m0) and then integrating as follows:

2x

=

2x fq cos(m0) d6 =

Z f An cos(ne) cos(m0) d6, we get for n > 0 (noting that the integral on J

0 n=0,1,2,.

O the right hand side is zero when n

  • m and it is equal to An x x when n = m) l An x =

fp cos(n0).dO+ f p cos(ne) d6

> A

si (3) n 0

3s/2 xn 2

l Note that for even 'n' number, An = 0.

The coefficients An in Eqn. (1) determined from Eqns. (2) and (3) using p = 1.0 psig are calculated in the Table 1 (page 6) using Excel 5.0. The given and Fourier distributions using Excel are shown in Figure 3. It can be seen from this figure that the sum of the first 19 terms in the Fourier series of Eqn. (1) adequately represents the given pressure. Therefore, only the first 19 harmonics (actually,11 terms as An = 0 for even 'n' number) are used in the analysis.

l For a given harmonic, 'n', apply normal pressure, pn = An j

(on shell parts 1 through 3,7,10,14,15, and 19 through 22 - see Figure 1).

RESULTS The deflections are summarized in Table 2 and plotted in Figure 4.

The stresses are summarized in Table 3.

1 9

1 CW600ADRWMlHRI. Doc Page 3 1

.a

i 0=0 A

F 4

p = 1 psi over I -90's 0 s 90*

T T

0 NOTE:

y The pressure is applied above elevation 90'

> 270*

s

(.93 132*-3" and to the c.nitainment shell only.

(See Figure 1.)

Containment -

Shell i

180' FIGURE 2: PRESSURE DISTRIBUTION Symfety 1.1 9

1.0,,2 " ; ; " : ; ^ $ ^

3 l

0.9 --

I I

M Given Pressure of 1.0 psi l

0.8 -

I expanded in Fourier Series I

1 0.7 -

I l

6 0.6 -

Fourier Series Sum for the terms: !

I 0.5 -

1 I h 0.4 -

e 1

+ n = 0,1, 3, 5,. 39 1

o,,

0.3 -

g

- -A-n = 0,1, 3, 5,.. 59 0.2-1 0.1 l

l

', M &tsr'h'0;"i2::0;$

0.0

-0.1 --

e O 10 20 30 40 50 60 70 80 90 100 110 120 130 140 150 160 170 180 Angle arourv ' the Circumference, 0, degrees FIGURE 3 GIVEN PRESSURE DISTRIBUTION Vs FOURIER SERIES DISTRIBUTION CMP 600ADRMP781HRI. Doc Page 4

l l

i TABLE 1:

FOURIER COEFFICIENTSt As the coefficients for the harmonics "n = 2, 4, 6,.." are zero, only the harmonics "n = 0,1, 3, 5,.. 19" need to be used in the analysis.

Units: psi.

n

Ani n

LAn n

An -

0

. 0.500 !:

21 0.030:

41

-0.016 1

0.637.--

23

- -0.028 '::

43

. D.015 1

3

-0.212.

25

'0.025 45 0.0144 5

0.127 27

- 0.0244 47

-0.014 7

-0.091 29 10.022?

49

'0.013 9

10.0717 31 40.021 51

-0.01'2'-

11

-0.058 33 10.d19 53

' O.0.12 i 13 0.049 35

<-0.018 ;

55

-0.012 ~

15

-0.042-37

'0.017 57 0.011' 17

0.037 ~

39

-0.016-59 0.'011

~

19

-0.034 I

$ A cos(n0) - see page 4 and Figure 3.

i n the Fourier series equation:

q=

n n = 0,1,3.5...

c:MP600ADRMP781HRt. DOC Page5

TABLE 2:

DEFLECTIONS OF THE CONTAINMENT VESSEL Normal (radial) displacement, '+' is in the direction of 'n' in Fig.1; w:

u,:

Meridional displacement, '+' is in the direction of's' in Fig.1; ue:

Circumferential (hoop) displacement, '+' is in the direction of'0' in Fig. 2.

Due to the symmetry ofload at 0 = 0 and 180*, ue = 0 at these locations.

Shl Prt Coord.

Elev.

fat 0 = 0*4 At 0 = *90*

' At 0 = 180*:

w u,

ue Twl (u,j start /end (Fighl) (Fig.1)

[u,)

(Fig.1) iorini ft Jins

inl in in in iin?

iini 79.2116* 100.000* 0.00000 0.00000 0.00000 0.00000 0.00000 0.00000 0.00000 1sa (s: start) 81.41 100.844 0.00303 0.00024 -0.00095 -0.00007 -0.00088 -0.00492 -0.00039

83.51 101.649 0.00858 -0.00008 -0.00268 0.00003 -0.00177 -0.01394 0.00014 L 85.7 ;

102.489 0.01320 -0.00082 -0.00410 0.00026 -0.00268 -0.02140 0.00134 3 87.8 e 103.289 0.01531 -0.00176 -0.00472 0.00056 -0.00360 -0.02474 0.00288 b

90.00 104.125b 0.01479 -0.00269 -0.00449 0.00085 -0.00453 -0.02378 0.00439 1e,2s (e: end) 1280.1"-

106.675 0.00800 -0.00319 -0.00214 0.00101 -0.00721 -0.01228 0.00521

1310.6 109.217 0.00466 -0.00343 -0.00091 0.00109 -0.00991 -0.00647 0.00562

)1341.2' 111.767 0.00478 -0.00373 -0.00079 0.00119 -0.01269 -0.00637 0.00612 1371.7' 114.308 0.00573 -0.00408 -0.00094 0.00131 -0.01555 -0.00761 0.00670 2e,3s

'1402.3' 116.858 0.00633 -0.00444 -0.00095 0.00144 -0.01847 -0.00824 0.00733 21433.1-119.425 0.00687 -0.00479 0.00093 0.00157 -0.02164 -0.00872 0.00792

1463.9 121.992 0.00757. -0.00515 -0.00098 0.00170 -0.02489 -0.00954 0.00854 1494.7 124.558 0.00606 -0.00551 0.00109 0.00183 -0.02821 -0.01024 0.00916 l

1525.4 127.117 0.00824 -0.00585 -0.00123 0.00196 -0.03159 -0.01070 0.00977

1556.2 129.683 0.00896 -0.00612 0.00081 0.00213 -0.03505 -0.01058 0.01038

. 01092 0

e

1587.0 132.250c 0.01352 -0.00630 0.00165 0.00231 0.03892 -0.01023 3e,7s 1617.2 134.767 0.02081 -0.00677 0.00482 0.00235 -0.04330 -0.01116 0.01146 1647.4' 137.283 0.02348 -0.00734 0.00584 0.00235 -0.04788 -0.01180 0.01204 21677.6 139.800 0.02366 -0.00782 0.00580 0.00239 -0.05213 -0.01206 0.01260 i1707.8' 142.317 0.02368 -0.00827 0.00567 0.00244 -0.05597 -0.01234 0.01315 11738.0 144.833 0.02406 -0.00870 0.00564 0.00249 -0.05940 -0.01278 0.01369

~ 1768.2 147.350 0.02468 -0.00913 0.00564 0.00255 -0.06239 -0.01338 0.01423 L1798.4 149.867 0.02541 -0.00956 0.00565 0.00260 -0.06495 -0.01411 0.01475 11828.6 ~

152.383 0.02826 -0.00998 0.00565 0.00265 -0.06705 -0.01497 0.01527

1858.8, 154.900 0.02723 -0.01038 0.00564 0.00270 -0.06871 -0.01594 0.01578 11889.0 157.417 0.02835 -0.01078 0.00565 0.00275 -0.06994 -0.01705 0.01629 i1919.2 159.933 0.02972 -0.01117 0.00569 0.00281 -0.07076 -0.01833 0.01878 v1949.4 162.450 0.03130 -0.01155 0.00576 0.00285 -0.07120 -0.01978 0.01726
  • BASE bBottom T. L.

' Stiffener Continued on page 7...

1 Page 6 CW600ADRW8mR2. doc 1

1 i

s i

T BLE 2 (Continued)

Shl Prt Coords Elev.

LAt0.= 0' At 0 = 90*

At 0l=
il80*1 w

u, ue (wf y

start /end (Figf1) (Fig.1) 4wl, y (Fig.1) '* 'or in; ft (int Jini in in in lin t

? int 1979.6" 164.967 0.03222 -0.01197 0.00555 0.00289 -0.07128 -0.02111 0.01775

-2009.8 167.483 0.03046 -0.01240 0.00438 0.00292 -0.07111 -0.02170 0.01823 c

2040.0 170.000c 0.02794 -0.01254 0.00299 0.00305 0.07118 -0.02196 0.01863 f

7e,10s 2072.4 172.700 0.03348 -0.01274 0.00463 0.00316 -0.07365 -0.02422 0.01906

-2104.8 175.400 0.03718 -0.01317 0.00566 0.00319 -0.07630 -0.02587 0.01955

2137.2 178.100 0.03833 -0.01355 0.00575 0.00323 -0.07864 -0.02683 0.02002

.2169.7.

180.808 0.03019 -0.01389 0.00567 0.00329 -0.08057 -0.02785 0.02046 2202.1 183.508 0.04039 -0.01421 0.00564 0.00334 -0.08205 -0.02910 0.02000

2234.5' 186.208 0.04187.-0.01453 0.00564 0.00340 -0.08305 -0.03059 0.02132 4

I 52266.9-188.908 0.04358 -0.01483 0.00564 0.00345 -0.08358 -0.03229 0.02173

,2299.3 191.608 0.04559 -0.01511 0.00568 0.00351 -0.08361 -0.03423 0.02213

-2331.8 194.317 0.04799 -0.01539 0.00577 0.00356 -0.08317 -0.03645 0.02251 2364.2.

197.017 0.05011 -0.01569 0.00563 0.00360 -0.08227 -0.03885 0.02289

-2396.6 199.717 0.04941 0.01603 0.00436 0.00363 -0.08101 -0.04070 0.02328 d

2429.0 202.417d 0.04625 -0.01609 0.00255 0.00377 -0.07981 -0.04116 0.02362 10e,14s 2447.0' 203.917 0.04654 -0.01614 0.00261 0.00381 -0.07977 -0.04133 0.02376 14e,15s* ~2465.0 205.417* 0.04683 -0.01618 0.00263 0.00386 -0.07976 -0.04157 0.02390 2483.0 206.917 0.04709 -0.01621 0.00262 0.00391 -0.07977 -0.04186 0.02402 f

2501.0 208.417f 0.04734 -0.01624 0.00257 0.00395 0.07977 0.04220 0.02414 15e,19s 2525.7-210.475 0.05404 -0.01597 0.00394 0.00408 -0.08026 -0.04616 0.02414 r

2550.4 212.533 0.06214 -0.01614 0.00552 0.00411 -0.08066 -0.05109 0.02436

?2575.1 214.592 0.06663 -0.01636 0.00591 0.00410 -0.08085 -0.05482 0.02455

2599.8 216.650 0.06831 0.01653 0.00448 0.00407 -0.08079 -0.05935 0.02466 19e,20ss

_2624.5-218.708s 0.06789 -0.01664 0.00074 0.00408 -0.08050 -0.06641 0.02479 995.0*:

220.611 0.06535 -0.02243 -0.00236 0.00432 -0.08030 -0.07007 0.03107

~ 100.0 e 222.529 0.06336 -0.02798 -0.00339 0.00478 -0.08029 -0.07014 0.03753 E105.0 "

224.475 0.06184 -0.03336 -0.00294 0.00522 -0.08043 -0.06772 0.04381

110.0i 226.465 0.06038 -0.03861 -0.00193 0.00558 -0.08069 -0.06424 0.04978 115.0?

228.513 0.05876 -0.04372 -0.00081 0.00585 -0.08106 -0.06038 0.05541 120.0 >

230.634 0.05697 -0.04866 0.00034 0.00602 -0.08152 -0.05629 0.00070 L125.0 C 232.841 0.05506 4.05341 0.00159 0.00611 -0.08211 -0.05191 0.06563 130.0-' 235.147 0.05318 -0.05798 0.00297 0.00610 -0.08281 -0.04724 0.07017 j

135.0' 237.557 0.05132 0.06235 0.00450 0.00598 -0.08366 -0.04233 0.07430
  • fCrane Girder Bonom, C. L., and Top trop T. L.

Continued on page 8...

Page 7 CW600ADRM8mR2. Doc J

~

i T BLE 2 (Continued)

Shl Prt Coord.

Elev.

fat 0 = 0*,

At 0 = 90*

i At 0 =1180* t l

start /end (Fig.[1) (Fig.1)

(w; fuf w

u, ue jwi

{uf i

(Fig.1)

[dsg) ft fini in in in

$ini hin) i 1140,0*:

240.073 0.04958 -0.06654 0.00617 0.00574 -0.08467 -0.03725 0.07802 l

C145.0 -

242.681 0.04799 -0.07054 0.00795 0.00539 -0.08586 -0.03200 0.08132 20s,21s

!150.01 245.348 0.04657 -0.07437 0.00983 0.00492 -0.08723 -0.02691 0.08421

-152.0-246.418 0.04606 -0.07586 0.01061 0.00470 -0.08783 -0.02t84 0.08525 1154.0 247.481 0.04557 -0.07732 0.01139 0.00446 -0.08845 -0.02280 0.00623 r

. 156.0:

248.532 0.04510 -0.07875 0.01216 0.00420 -0.08910 -0.02078 0.08715

)

158.0:

249.561 0.04465 -0.08017 0.01293 0.00392 -0.08975 -0.01880 0.08801 l

.160.0.

250.560 0.04421 -0.08156 0.01368 0.00362 -0.09042 -0.01685 0.08881 l

.162.03 251.518 0.04375 -0.08293 0.01441 0.00331 -0.09108 -0.01494 0.08955 l

^ 164.0 ?

252.423 0.04328 -0.08427 0.01510 0.00299 -0.09173 -0.01308 0.09025 l

,.168.0 l.

253.264 0.04275 -0.08560 0.01575 0.00265 -0.09234 -0.01125 0.00089 I

168.0J 254.027 0.04214 -0.08690 0.01635 0.00229 -0.09290 -0.00944 0.09149 170.0--

254.700 0.04139 -0.08819 0.01688 0.00193 -0.09340 -0.00764 0.09204 l

'172.0 255.271 0.04051 0.08944 0.01733 0.00155 -0.09381 -0.00586 0.09255 I

J 174.0 255.728 0.03965 -0.00066 0.01769 0.00117 -0.09411 -0.00427 0.09301 21e,22s

176.0 '.

256.062 0.03872 -0.09189 0.01796 0.00079 -0.09430 -0.00281 0.09346 l

E 176.2 >

256.088 0.03864 -0.09200 0.01798 0.00075 -0.09428 -0.00269 0.09349 i

L 176.45 256.113 0.03845 -0.09213 0.01800 0.00071 -0.09429 -0.00246 0.09354 5

i 1176.6?

256.137 0.03822 -0.09225 0.01801 0.00067 -0.09429 -0.00219 0.09359 (176.8 ::

256.159 0.03794 -0.09237 0.01803 0.00063 -0.09429 -0.00187 0.09363 i

r177.01 256.180 0.03759 -0.09250 0.01805 0.00059 -0.09429 -0.00149 0.09368

177.25.

256.200 0.03718 -0.09262 0.01807 0.00055 -0.09429 -0.00105 0.09372 177.4-256.218 0.03669 -0.09274 0.01808 0.00051 -0.09428 -0.00052 0.09377 l

177.6 ~

256.235 0.03610 -0.09286 0.01810 0.00047 -0.09428 0.00000 0.09381 177.8 256.251 0.03542 -0.09298 0.01811 0.00043 -0.09427 0.00080 0.09385 L 178.0 '

256.265 0.03463 -0.09310 0.01812 0.00039 -0.09425 0.00161 0.09388 l-178.2 256.278 0.03373 -0.09321 0.01813 0.00035 -0.09424 0.00254 0.09392 i

F 178.4 k 256.290 0.03271 -0.09331 0.01815 0.00032 -0.09423 0.00358 0.09394 178.61 256.300 0.03159 -0.09340 0.01816 0.00028 -0.09421 0.00473 0.09395 i

! 178.8~

256.309 0.03037 -0.09348 0.01817 0.00024 -0.09420 0.00597 0.09395 22eh C179.0 ^

256.316h 0.02910 -0.09354 0.01818 0.00020 -0.09417 0.00726 0.09394 i

hpolc @ l'0 @

)

i Page8 CW600ADmAM8mM. doc J

m' T

w at 0 = 18,0*.

w at 0 = 0' u, at 0 = 0'

,/

.I. w at 0 = 90*

s 4

,o' u

240 -

i

/l t 0 = 180' 2m-

[,"u, at 0 = 90'

,. *... u, a

,.e

,..v' u

... = ~ ~ ' '

I.

N 220-L P

l f

I I

210-w at 0 = 0*

\\

200-a.

k,.

9 4

f. us t 0 = 90*...*

+

b 190 -

a W

s

+

=

e k

d 180 -

. * 't

,i A

e.

1 r

+

4 g

6, i,

[

170-

+

+ i' 4

ii a.

g, 4

.. I I

o.

w at 0 = 180* '.

1

. = + +

g

-- 6 A.

,4 150-t 1

x

.e

" E.*

140 -

x

+

v.-

- Displacements

'a

, P' w: Normal (radial) 130 -

.ii x

A.

u,: Meridional 120 x

e

'x '

  • g*

u: Cirm.mferential e

'g!L.E.

  • 110
    • w.-..

0.10 4 08 0 06 4 04 4 02 0.00 0 02 0 04 00" 0 de 0.10 OSPLACEMENTS AROUND THE CIRCUMFERENCE, INCHES FIGURE 42 DISPLACEMENTS 7'"TIIE CONTAINMENT VESSEL x

k 3

5 i:

L i

cwso0.memeine >oc Page 9

^

1 s

TABLE 3:

SURFACE STRESSES IN THE CONTAINMENT VESSEL o,:

Meridional stresses; ce:

Circumferential(hoop) stresses; t,e:

Shear @angential) stresses.

Due to the symmetry ofload at 0 = 0 and 180*, t,e = 0 at these locations.

Sh1 Prt Coord.

iElev.:

Face

?At 0 = 0*3 At 0 = *S0*

rat 0H180*::

start /end (Fig.1) k=lj (cf

oe).

o, ce T,0

! o,J; 4003

~

x.

l (Fig.1)

  • or in ift?

Lpm]

fpsii psi psi psi tpm.;.

pm2

~2629

-789-is' 79.2116* 100.000m inside

'1616,

4851

-507

-152

-910 (s: start)

Outside -2383 4715::

747 224

-912 13877! 11163' 81.4 100.844 Inside 1210?

1-106"

-63

-53

-976 t-3351 ?-273 l

Outside E-973+

L-1931 304 58

-852

1580
3091-t l

83.5 101.649 inside 440 a.:.104 :

206

-34

-976 1052:

E-172 :.

OJtside ;C-O #i'2571 35

-85

-837

'189i M-426 '

85.7 102 489 Inside

-1038

143" 333

-47 936

1703 1-238E Outside L2841 K539:

-92

-174

-841 i-466' 4887; 87.8

103.289.

Inside

.-1068 9204:

343

-67

-879

?1754'

-337s T

Outside 321L

621'-

-103

-200

-848 L426.

~-1022 l

1e,2sb 90.0 104.125b Inside f-772L r 270:.

248

-88

-828 11269:: E-446j t

l (e: end)

Outside

30(

65122

-8

-165-

-848 T-47b

?-842' l

1280.1*

106.675 Inside t-1901:

1180:

63

-58 709 2317f

. W 7s i

l Outside i-486-L 92, 160

-29

-742

'806L

(-151;

(

1310.6 109.217 Inside

<-231; 328(

79 9

-717

388-

?-46 ?

Outside

-433r 1 32i 144 10

-711 7225

. 524

'518~

174 1341.2 111.767-Inside

-307?

F 11 s 105 3

-728 Outside

. -3451 420?

118 7

-702

!500c L33:

1371.7

-114.306 Inside 330

115 1

-730 561' t 5 ::.

Outside :-309 f5t 108

-2

-699 J5241

~9J j

  • ),3s 1402.3 116.858 Inside J-305.

E41 109

-2

-781 7522i

?-8 i i

' 22 t j

Outside

, -370 -:;

12s 131 1

-753 16325 1433.1 119.425 Inside

(-328 :

i-74 119 2

-788 L566i 011c Outside

'-332 '
-4=

121 3

-744 15751 7 97 1463.9 1121.992 Inside

?-330::

4i 119 0

-792 (507;

6s "M[

Outside (4161

  • 41 121 1

-733

558(

i-2 L i

1494.7

124.558 Inside

'-326 : '-10:

118

-4

-787 N5611 i2 3

m s 8?

Outside

-304 :-

f2:

122

-3

-722

549 " { 's: s

" BASE bBonom T. L.

Continued on page 11..

i l

'.i, Page 10 cwsooAoneammaoc i

.r.

,,r,.

TABLE 3 (Continued)

Shl Prt Coord.

-Elev.-

Face LAt 0 = 0'

~At0= 90'

-At0.=180*

start /end (Fig.1).(Fig.1) o, ce o,

ce T,e o,

c0 (Fig.1) in fl psi psi psi psi psi psi psi 1525.4*

127.117 Inside

-300

-19 132

-5

-768 564 9

Outside

-314.

-18 108

-12

-733 530'

-6 1556.2

.129.683 Inside

-199

-17 178 24

-778 5551 31-Outside

-398

-40 '

62

-11

-822 523:

19.

c 1587.0 132.250c inside

-102 195 165 109

-1097 431

22 Se,7s Outside

-480-81' 76 82

-898 631 83 1817.2 134.767 Inside

-441 360 49 189

-1323 539-

-18 Outside

-132

.433 191 232 787 515 30 1847.4 137.283 Inside

-342.

494 93 239

-1218

,527'

-16.

Outside

-225.

487 147 255

-847 520-23 1677.6 139.800 Inside

-269 524 120 245

-1061 508- '289 459 120 246

-808

.530 32 Outside 1707.8 142.317 Inside

-251-524 123 242

-931 496~

-40 Outside

-295 439 117 240

-739 530 41 --

1738.0 144.833 Inside

-247 525.

121 240

-814 489-1-45' Outside

-286' 433 119 239

-676 524-46 1768.2 147.350 Inside

-241 528 120 240

-699

'431 48 Outside

-277 431 120 240

-619 5171

- 49 1798.4 149.867 Inside

-234 529-120 240

-585 474.

- Outside

-269

.431 120 240

-566 510-50 1828.6 152.383 Inside

-227-529 120 240

-471 467-

' 49 Outside

.-262 43i-120 240

-512 502..

49 1858.8 154.900 Inside 219 526 120 240

-357 459

-47 Outside

-254 432' 120 240

-457 494 48 1889.0 157.417 Inside 209-524 121 240

-243 451

-43 i

Outside

-248 435 119 240

-396 486 44 1919.2 159.933 Inside

-201 522-121 242

-127 444 Outside

-238 444 119 241

-328 476 38 1949.4 162.450 Inside

-215

'515 114 242

-1 443

-30 Outside

-205 464 126 246

-254

-457 28 1979.6 164.967 Inside

.-271

-464 92 228 138 454-

-7 Outside

-126

.471 148 245

-201 422 19

cfAP600ADR\\AP781HRLDoc Page 11

~

iABLE 3 (Continued)

Shl Prt Coord.

1Eleyh-Face tat 9 = 06

~ At 0 = *90*

?At' 0'= 180' ~

start /end (Fig.1) -(Fig {l);

idel:

o, ce T,0 ::g foe:

(Fig.1) in ift !

j pair psi'I psi psi psi

!psiJ i psit 2009.8' 167.483; inside

?-2501 1334' 97 187 215

'4451 40.

Outside

-121:

'.1360) 143 201

-212 K400?

'421 c

2040.0 170.000*

Inside E3271 1358i; 309 201

-96

?290l

?43:)

7e,10s Outside : 878L J61-

-88 88

-122 L541!

?114-i 2072.4

172.700 Inside L-253.

s355.

90 194

-882

! 432:-
33' Outside

/-831

390

151 212

-542 L384*

L351

~

2104.8 175.400 Inside 0218:

1482s97-234

-777 c413' L-15 :

3 Outside.a108J

4741 143 247

-543

-:3941-

' 20 :<

2137.2

.178.100 Inside F-150 -

519-117 243

-628 53851 1-34.

Outside :::'-164 --

457 :

123 244

-476

-400i e32i 2169.7 180.808 Inside

-127:

L523 122 241

-493 2370i L-40?

Outside ?-1707 i439L 119 240

-395

407:

?411:

2202.1

183.500 Inside

< -119 y o524c 121 240

-366

?3605

{-44:::

Outside $1591 433' 120 240

-320 0390i

'46i 2234.5 186.208 inside

-110,

$251 120 240

-239 1350t 1 46Li Outside :-147f 6432 120 240'

-252

387?
48T 2266.9 188.908 Inside
197f r$251 121 240

-111

338:
T-45 ?

Outside

-138-N432L 119 240

-185 F3777 r47:

1 2299.3 191.608 Inside 1-83 526' 122 242 19 l 326 '.' f-43" Outside J-129 ?

'437:

118 241

-115 366~

!44' q

2331.8 194.317 Inside V-84 ::

525.

116 243 156 i317? M8 '

Outside..-1021

455' 124 246

-41

350' 36; 2364.2 197.017 Inside

.4139:

E486$

92 231 306

-322' T-24 Outside

'-19

,474~

148 248 18 316' 22:

2396.6 199.7.17 Inside

-165 c.345-87 184 406 1340 22 ;:

Outside

. 39 -

380' 153 203 23 206:

26..

10ed 2429.0 202.417d Inside

'410; 300' 331 191 156

251" 83:

Outside

-507

15

-91 65 149

326-1114?

+

~

14sd 2429.0 202.417d Inside

.-41; 164-110 125

-91 260

86 Outside
-51F 1520 113 126

-99 277

100 :.

2447.0 203.917-Inside G31L 134l 111 128

-111

254i i121i Outside

% 331 1251 117 129

-117 4 261a

?.1344

' Stiffener dBottom of the Crane Girder Continued on page 13...

cwaoAoaanslHR3. DOC Page 12

I 4

t 5

4 TABLE 3 (Continued)

Shl Prt Coord.

1Elev.4 Face

.J At 0 ='0*-

At 0 - 90*

i At 0 = 180*:

start /end (Fig.1) (Fig ;l) e, ce e,

ce T,e o,

os (Fig.1)

  • or in

[A[

psi psi psi psi psi psi t

ide,15s* 2465.0*

205.417e inside

-25; 1041 112 129

-114

.249T c153)

Outside ?-24;

951::

118 131

-119 4200i i106L 2483.0 208.917 Inside t-22 ?

' 71

111 123

-106

):2459

i185L j

Outside

-22 ;

62i 117 130

-110 i256--

t196f l

15ef 2501.0 208.417f inside J-23:

-.36 :

110 126

-91

? 242::

'215 Outside

-30, 24' 113 127

-92

2567
229-19sf 2501.0 208.417f inside 919'

.:-319 338 194

-306 r-244)

!:70T Outside '-945'

-250-

-98 63

-308 E7500

<377?

2525.7 210.475 Inside 7-4 L L206:

114 177

-324

232s (147e Outside 171 4195; 126 180

-224

245; s1661 j

2550.4 212.533 Inside 4143;.

F 378 :-

69 220

-239 i281:

62; Outside

.178 L452 171 251

-182 1165:

' 50.

2575.1 214.592 Inside

-75 ^

474-47 228

-119

.169

-19i Outside 143'

515 193 271

-136 243:-

28':1 j

2599.8 216.650 Inside 6 34 :

7451' 14 166 1

162;

< -119 :

Outside

138?

-481; 226 230

-98

?314a

-222 f

ite,20s:

2624.5 218.708s inside i54i L358:

124 64 75

'.194 ?

L-230 j

Outside

88-2356 116-62

-74 144i 4233^

95.0*

220.611:

Inside 1145":

E 264;-

230

-29 54

'::3159 E-323 i-Outside 30 ? i224?

10

-96

-40 G10:-

4-417f 100.0 222.529 Inside

!146:

L1904 187

-95 2

t229-

-3801 Outside 60'-

4162:

55 135

-31 L49s 1-432 105.0 224.475 Inside

.135 1151' 142

-111

-39

?149

-372:

Outside t 98 ?

138 103

-122

-44 1109s 6382?

110.0 226.465 Inside 136-4135 125

-100

-85

?115 :-

1-335-Outside

-123?

130/

125

-100

-65 t126/ ?-329' 115.0 228.513 Inside

!.146 "132t 126

-82

-83 1107h E-298 e Outside

'1384 1128; 129

-81

-83 1121;

-289 120.0 230.634 Inside 1157D
137:L 132

-64

-99 107

  • -264r Outside s150'-

7133s 131

-64

-98 5112)

E-280 125.0 232.841 Inside F169-1148'-

137

-45

-114 1105-

-238.

wn y

outside i164L 6145<

135

-45

-110

'106 '

-234~

  • Crane Girder C. L.

fTop of the Crane Girder sTop T. L.

Continued on page 14...

J CAAP600ADRMMB1HRDOC Page 13

-~

l 9

iABLE 3 (Continued)

Shl Prt Coord.

. Elev~.

Face At 0 = 0* :

At 0 = *90'

At0 ='180*-

start /end (Fig.1).(Fig; 1) 7o,y os o,

ce T,0 0,1 00i (Fig.1) deg

?ft :

psi i i psi-psi psi psi psii psi; l

130.0a 236.1.47 Inside

.181 ;
188

141

-24

-128 L1020 /-215 f

^

Outside 11780

165 ?

140

-23

-121

^1031 '-2111 135.0 237.557' Inside c1945

196.

147 0

-141 h100

-195 Outside 1192i

e 193 :

147 2

-130 b102-

=-189-140.0 240.073 Inside 2071

-231.

153 27

-151 99s

-177::

Outside :207

'2281-154 29 137

102 ::

171; 145.0 242.681 Inside 221:

273-160 55

-159

'1001

' -163 :-

Outside

-221?

!268 162 57

-140

'103:

' 154.-

20s,21s 150.0

'245 348 Inside

-235c 1321:

168 84

-182

.102:

-153 :

Outside

'236 s 1314::

171 86

-137 3106i:

L-141e 152.0 246.418 Inside

241:

341 172 96

-162 103; e-149 !

Outside 241J e333~

174 98

-134 107Ji

-136' 154.0 247.481 Inside

2461

'362.

175 108

-160 n104?

c-147c

.3522 178 110

-130

'109f:

2 -132 c j

Outside : 247:::

156.0 248.532 Inside

!252 384i 179 120

-157 E105J:

4-144.

Outside 2521 372-181 122

-125

'1101

-128 L 158.0 249.561 Inside
257
"405 :

182 131

-152' 107

~ -143 :

' 113 :'

c-125 2 Outside ?-2573 "392' 185 134

-118 160.0 250.560 Inside

-262L 426:

186 142

-145

?109 ; i-142, Outside 261!

413-~

188 145

-110 x115; '-124 162.0 251.518 Inside 1267J 7447' 189 153

-136 1111~

N141<

Outside 265 "4344 191 155 101 118 x-123 -

"141~

164.0 252.423 Inside

270 :-

J467e 192 163

-124

.114 Outside :268:

! 455 --

195 166

-91 1121' i-124 166.0 253.264 Inside 271 485 195 172 111 119

-1411 Outside 272.:

475 198 175

-80 1123.-

126-168.0 254.027 Inside

-:2714 S502i 198 181

-95 124;- :-141i Outside '.' 274 (

'496~

200 183

-68 127::

-129 170.0 254.700 Inside

271!

'518' 200 188

-77 129.

1142i Outside

" 274 ";

5141 203 191

-54

-131;

-132; 172.0 255.271 inside i272; 534-202 194 56 132-

-145 Outside 271 529~

205 197

-39 139 f-135 :

Continued on page 15...

C:%P600ADEM81HRLDoc Page 14

4 4*

3 TABLE 3 (Continued) l Shl Pat Coord.

Elevi Face 1 At 0 = Ok

' At 0 = 90' i At 0 =.180*J i

.. l);

fe,;

[o6g o,

ce T,e

?c,7

06:

j-start /end (Fig.1)

(Fig (. -

l (Fig.1) deg

![fR psi:-

psi..

psi psi psi EpsiV psi 4 j

174.0*

255.728.

Inside (270l

557.

204-199

-36 138

-158 :-

l Outside :2701

. 543 '

207 202

-16 1434 i -139 i I

21e,22s 176.0 256.062 Inside L246.

571L 205 203 1

?1641 166:

Outside '301-i567.:.

208 206

-7 114

-155 i

l 176.2 256.088 Inside 240:

570.

205 203 5

170
-164 a Outside 310

~ 568 ;.

208 206

-6

? 105.:

-156:

I j

176.4 256.113 Inside c' 233 -

~ 569 4 205 203 8

h177c

-162.:

i Outside

321 '

-5681 208 206

-4 95?

4156L t

i 176.6

256.137 Inside

>226i

565J 205 204 12
1841 :-158:i Outside '333i
568 -

208 207

-3 L83i N155:

.l 176.8 256,159:

Inside

2197 1561:

205 204 15

>:192 l

.:::-153 ;

i j

Outside 13464 f 566 -

208 207

-1

70i
-153

]

i 177.0

-256.180 Inside

':2121

. 555 -

206 204 18 199; t-147?

l.

Outside

'360-1564:

208 207 0

56i s-150 177.2
256.200 Inside
206::

E547:

206 204 2?-

t2066

-138f Outside i376L

/ 559 --

208 207 2-140s 9145t l

177.4 256.218 inside

200F 537D 206 205 24

'2121 r-128 j

Outside '393t

-553>

208 207 4

t24%

4139:

i 177.6 256.235 Inside i197?:

5.5252 206 205 27

~215f 6115:

l Outside ::4101

!:5454 208 208 7

'61

-130 >

l 177.8 256.251-Inside 197:"

. 510 ::

206 205 28 c215c 1-101;

' 119*

Outside

-4271

? 534::.

208 208 10

~-11:K s

178.0 256.265, inside i202l e493' 206 205 27 210;L 43; Outside 445L

521-208 208 14 t-281 f-105 178.2 256.278 Inside 215u J4742 206 205 23 l 198l:
43~

Outside :4611 i 506 208 208 18 1-45 E-90.

l 178.4 256.290 Inside 238" J 452 '.

207 205 13 175:

"-41 ::

Outside 14741 7491' 208 209 23 r-581 1-74:

.276r 3430a 207 205

-11 t137J

-194 178.6 256.300 Inside Outsgle L481:

i4801 208 209 27 -62 ':

178.8 256.309 Inside

3359 14141 207 205

-67 79'

'-3.

Outside :472i i487o 208 209 23

<-57 "48-22eh 179.0 256.316h inside

-1408

'424 207 205

-95 7-

-141 i

Outside 408- '552'l 207 210 95

7

. -132 -

hPole (just l' off)

CAAP600ADmAM81HRDoc Pagels

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