发明公开
EP0008503A1 Temperature control apparatus and a missile including such apparatus
失效
温度控制装置,以及具有这种装置提供格斗导弹。
- 专利标题: Temperature control apparatus and a missile including such apparatus
- 专利标题(中): 温度控制装置,以及具有这种装置提供格斗导弹。
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申请号: EP79301499.4申请日: 1979-07-27
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公开(公告)号: EP0008503A1公开(公告)日: 1980-03-05
- 发明人: Reisman, Elias , Goodsell, David Scott
- 申请人: FORD AEROSPACE & COMMUNICATIONS CORPORATION
- 申请人地址: 300 Renaissance Center P.O. Box 43339 Detroit, Michigan 48243 US
- 专利权人: FORD AEROSPACE & COMMUNICATIONS CORPORATION
- 当前专利权人: FORD AEROSPACE & COMMUNICATIONS CORPORATION
- 当前专利权人地址: 300 Renaissance Center P.O. Box 43339 Detroit, Michigan 48243 US
- 代理机构: Crawford, Andrew Birkby
- 优先权: US934439 19780817
- 主分类号: G05D23/10
- IPC分类号: G05D23/10 ; G12B15/06 ; F42B15/00
摘要:
A solid state temperature gradient cooling system in which thermal energy is, under a first condition, carried from a heat source to a heat storage device (20) and under a second condition is carried from the heat source and storage device (20) to a heat dissipator (2). The change in conditions is responsive to changes in the temperature of the heat dissipator above and below a predetermined value. Bimetallic disc elements (16) are employed, which respond to temperature changes about the predetermined temperature, and snap from a first condition concave/convex surface configuration to a second condition convex/concave configuration. The disc elements (16) are supported about their outer peripheries so that the change in configuration will cause the centre of the disc (16) to move along an axis normal to the disc. This movement is used to respectively open and close a low resistance thermal path (10, 12, 8) between the heat dissipator (2) and a first thermal conducting path (24, 10, 22) defined to transmit thermal energy between the heat source and the heat sink (20).
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