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Design and Stress Analysis of Extraterrestrial ... - The Black Vault

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I"<br />

Table 2.2. (Cont d)<br />

(1) V(. )3 (4)_ ,_ "1y,,11_ ,,IMP<br />

CTpC- cI'vll•,,•uls E 1 ' \R =,5. .1t3.i,; .% R: . 0 .75.10- 3 .;r<br />

27 0,5(4) 10-3 1,17 1,-42 1 2,47<br />

28 (5)+(27) 10-3 41795 5,2 8,87 8,97<br />

29 (4) [(17)'( 15)](2S,)=e: 107 ,32,03 31,52 32,71 32,C0<br />

3() (20) h 104 -34,67 ý-34,02 -33,41 -34,13<br />

3 (2) h,415 43 44<br />

32 (30)+(32) 104 i 638 8,98 9,79 10,51<br />

33 (2)h' 10-1 -31,6 -32.,11 -32,28 -28,5<br />

34 (29) I' 104 48,05 .17,28 49,07 J 49,9I<br />

35 (33)+(34) 104 18,19 15,17 20,57 10,17<br />

36 0,5 (.r) 104 8,09 7,.59 10,2."9 10,09<br />

37 (32)-(3T'-)=A 0% -1,71, 1,39 --0,5 0,42<br />

38 p=(Q5)!R 10S 17,59 16,49 22,33 21,92<br />

<strong>Stress</strong> analysis <strong>of</strong> the load-bearing plate <strong>of</strong> a react~or ,<br />

In the design <strong>of</strong> reactors <strong>and</strong> lother engine units we frequently<br />

encounter single-layer <strong>and</strong> multi-layer plates, as i•ell as disks,<br />

which operate in a bend from the forces <strong>of</strong> fluid pressure <strong>and</strong><br />

concentrated loads.<br />

Support plates <strong>and</strong> end pieces are usually 'found tohave a<br />

constant thickness <strong>of</strong> asymmetric form with asymmetrically located<br />

openings <strong>and</strong> bracing rods. <strong>The</strong>y 'can be greatly or moderately heated<br />

<strong>and</strong>, in certain cases, there can be a temperature gradjent alone the<br />

radius <strong>of</strong> a disk <strong>and</strong> some va'iati6n in its thickness. <strong>The</strong> latter,<br />

case can include two-layer plates shield~ed from hot fluids by a<br />

thin wall. <strong>The</strong> support plate has openings for the passag, <strong>of</strong>. fluids;<br />

the openings are used for attaching pipes which connect both plates.'<br />

<strong>The</strong> perforations in the support plate lead to the fact that in a<br />

radial direction it usually has variable i'igidity, particularly at<br />

its bracing point to the walls <strong>of</strong> the cylinder part <strong>of</strong> the shell.<br />

161

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