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

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Plastic deformations in the latter case can, achieve such<br />

significant values that we can not disregard them where it Is<br />

important to conserve the geometric dimensions <strong>of</strong> an it'em.<br />

To evaluate the supporting power <strong>of</strong> material operating for a<br />

long time under elevated temperatures, it would be best to take<br />

the deformation diagram <strong>of</strong> this material under conditions <strong>of</strong> actual<br />

operating time <strong>and</strong> temperature. However, machines for experiments<br />

under such conditions would have to be built. <strong>The</strong> conditions themselves<br />

cannot be a limitless quantity; some tests cannot be set up at all.<br />

<strong>The</strong>refore, tests are carried out on the simplest niachines. Constant<br />

pull P is applied to a sample <strong>and</strong> elongation <strong>and</strong> rupture stress ar(<br />

measured as a function <strong>of</strong> time <strong>and</strong> temperature. As a result <strong>of</strong> svch<br />

tests: we can plot curves a = f(T) at t = const or a f(t) at T =<br />

= const (Fig. 125a, b).<br />

60 F<br />

S• ~~~=C~llst ' •gt~<br />

Kt<br />

'C-<br />

\ L<br />

P'1<br />

-1>-pI<br />

S~c)<br />

a) b)<br />

Fig. 1.25.<br />

Typical creep dlt;,.;am.<br />

However, it is best to obtain the function e f(T), wihich we<br />

call the creep curve (Fig. 1.25c).<br />

If stresses are low <strong>and</strong> the i:kme for taking the deformation<br />

diagram is short, relative el.ongatin :f a rod will be deterviined<br />

from formula e = a/E = P/EF.<br />

"i

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