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

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I<br />

the additional surface depends on its geometric s!pe, the heat<br />

conductivity <strong>of</strong> the material, <strong>and</strong> the method <strong>of</strong> jotning elements<br />

to the main surface.<br />

a, I<br />

a) (a)c0(b<br />

Fig. 4.25. Jacket-<strong>and</strong>-pipe heat exchangers with bent pipes:<br />

a - with U-shaped pipes <strong>and</strong> a common pipe panel; b - with<br />

U-shaped pipes <strong>and</strong> a U-shaped Jacker; c - with fl-shaped<br />

pipes; d - with sinusoidal bend.<br />

For this purpose there are installed longitudinal <strong>and</strong> lateral fins <strong>of</strong><br />

various shapes (Fig. 4.24b, 4.29) or pipe covers which increase the<br />

path <strong>of</strong> the heat exchange agent in the interpipe space (in the first<br />

case) or increase the rate <strong>of</strong> flow <strong>of</strong> the pipes with the heat carrier<br />

<strong>of</strong> another loop.<br />

In order to ensure the normal operation <strong>of</strong> a heat exchanger under<br />

weightless conditions during space flight, devices for twisting the<br />

heat carrier are found in<br />

each tube.<br />

All these measures in,'.rease the heat transfer coefficient <strong>and</strong><br />

reduce the size <strong>and</strong> weight <strong>of</strong> the heat exchanger.<br />

469

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