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

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I- I<br />

Let us fIind the safety coefficient <strong>of</strong> the plate:<br />

tax<br />

We should select n = .1.3-1.5.<br />

Peculiarities in analyzin~g pl~ates braced<strong>and</strong><br />

flexiller-eactor<br />

'<br />

In certain cases, it is immediately apparent that a plate, if<br />

,it is not braced, will either be 'very heavy or will have an extremely<br />

large~deflection under loading. A defl6ction is called large when<br />

it exceeds the thickness <strong>of</strong> the plate.. In order to avoid this,<br />

we can rigidly connect, by welding the rods, the load-bearing plate<br />

- with the end plate, which has great rigidity due to its shape <strong>and</strong><br />

lower heating temperature (Fig. 2.53).<br />

Two end plates connegted thus are analyzed as follows.<br />

elliptical end plat'e to which rods are braced we shall consider<br />

absolutely rigid. Only' the 'plate <strong>and</strong> the bracing rods are deformed<br />

in<br />

operalion. *We shall assume thlat the rods are placed axisymmetrically<br />

iorming a continuous force ring for a plate attachment.<br />

An<br />

'<br />

(<br />

+<br />

(a)<br />

I Fig. 2.53.<br />

P a<br />

(b)<br />

Diagram <strong>of</strong> a braced plate.<br />

I<br />

<strong>The</strong> problem'is statically jndeterminate. We shall solve it<br />

by the structural mechanics method <strong>of</strong> forces. Let us cut the<br />

qystem at the spot where the rods join the plate; we compensate<br />

for the effect <strong>of</strong> the rods by force R. An equation is set up using<br />

the method <strong>of</strong> forces (see Fig. 2-53).<br />

'II.<br />

176<br />

A

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