发明名称 |
Mechanical heat transfer device |
摘要 |
A unidirectional heat transfer device for use between an electronic assembly on an aircraft and the skin and/or pod on the aircraft. The device includes a thermal decoupler mechanism which operates to disengage a retractable interface heat transfer surface when the skin on the aircraft reaches a predetermined elevated temperature caused by the high speed of the aircraft. In the decoupled mode, the heat from the electronic equipment passes to a phase change material heat absorber to provide a limited capability cooling function during extended high speed aircraft operation.
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申请公布号 |
US4273183(A) |
申请公布日期 |
1981.06.16 |
申请号 |
US19790062592 |
申请日期 |
1979.07.31 |
申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE |
发明人 |
ALTOZ, FRANK E.;WINN, WILLIAM H. |
分类号 |
B64D43/00;F28F27/00;(IPC1-7):F28F27/00 |
主分类号 |
B64D43/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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