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.
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
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