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    Temperature control apparatus and a missile including such apparatus
    1.
    发明公开
    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。

    公开(公告)号：EP0008503A1

    公开(公告)日：1980-03-05

    申请号：EP79301499.4

    申请日：1979-07-27

    申请人： FORD AEROSPACE & COMMUNICATIONS CORPORATION

    发明人： Reisman, Elias ,  Goodsell, David Scott

    IPC分类号： G05D23/10 ,  G12B15/06 ,  F42B15/00

    CPC分类号： F42B15/34 ,  F28F13/00 ,  F28F2013/008 ,  G05D23/01 ,  G12B15/06

    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).

    Heat transfer device and radiation detector apparatus including such a device
    4.
    发明公开
    Heat transfer device and radiation detector apparatus including such a device 失效
    热传递装置和辐射具有这样的设备检测装置。

    公开(公告)号：EP0012564A1

    公开(公告)日：1980-06-25

    申请号：EP79302798.8

    申请日：1979-12-05

    申请人： FORD AEROSPACE & COMMUNICATIONS CORPORATION

    发明人： Reisman, Elias ,  Masino, Fred Silvio ,  Goodsell, David Scott

    IPC分类号： F41G7/22 ,  G12B15/06 ,  G01J5/06

    CPC分类号： F41G7/2253 ,  F25B21/02 ,  F41G7/2213 ,  F41G7/2293 ,  G01J5/061 ,  G12B15/06

    摘要： A thermal conducting path between a relatively movable heat source (24, 20, 14) and a relatively fixed heat sink element (6, 15), is defined as a relatively narrow non-contacting conducting gap (10) between opposing conducting surfaces (12,8). In an embodiment where the heat source (24,20,14) is gimbal mounted, for movement with respect to two orthogonal axes (P, Y), its conductive surface (12) has a convex partial spherical shape while the relatively fixed surface (8) of the heat sink element (6, 15) has a concave partial spherical shape. In order to maintain a constant gap (10), the opposing surfaces have a common spherical centre located at the crossover (30) of said orthogonal axes (P, Y) and the spherical radii dimensions (R 1 , R 2 ) differ by the distance of said relatively narrow non-contacting gap (10) there-between.