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

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

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Total operating time <strong>of</strong> the sample before -ruptureowas<br />

Let us designate in terms <strong>of</strong> TlpS t2p, ... , skp the time<br />

intervals necessary for rupture under stresses a, c ""I .2 ak"<br />

<strong>The</strong>se quantities are determined from the stress-rupture strength<br />

curves at various temperatures tl, t 2 , ... , tk. We shall call the<br />

ratios T i/Tlp, T 2 /T2p, ... , Tk/tkp material damage in first, second,<br />

etc., modes,.<br />

Experimental studies on stress-rupture strength <strong>of</strong> samples<br />

operating under nonstationary stresses <strong>and</strong> heating have enabled us<br />

to establish the fact that total damage for a given material is equal<br />

to one:<br />

£ s-L-l.(1-31)<br />

This assumption Is called the law <strong>of</strong> linear damage summation.<br />

Under continu6us stress variation<br />

•P d- .<br />

-- 1,<br />

(1.32)<br />

Where a <strong>and</strong> t are, subscript <strong>and</strong> superscript indicating that rupture<br />

time T- i•s determined for •a glvenh dress a <strong>and</strong> a given temperature<br />

t.<br />

Let us find-the coefficient <strong>of</strong> operating time reserve,<br />

which, as before, we shall designate nT.<br />

7,7

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