A Reversible Locking Radiation Thermal Control Mechanism
A technology of locking mechanism and radiant heat, which is applied in the direction of the device for controlling the living conditions of aerospace vehicles, etc., can solve the problems of large power consumption, increase the quality and complexity of the thermal control system, achieve enhanced heat dissipation, improve high temperature conditions, Improve the effect of low temperature conditions
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[0017] The preferred embodiments of the present invention will be further described in detail below in conjunction with the accompanying drawings.
[0018] Such as figure 1 and figure 2 As shown, this example provides a reversible locking radiation heat control mechanism, including: a support plate 1, a truss 2 and a moving cover 3, the supporting plate 1 is fixedly connected to the temperature control target cabin 4, and the moving cover One end of 3 is movably connected with the support plate 1 , and the other end of the moving cover 3 is movably connected with the temperature control target cabin 4 through the truss 2 .
[0019] The temperature control target cabin board 4 described in this example refers to the cabin board used to realize temperature control or to set a thermal control mechanism of the spacecraft, and the reversible locking radiation thermal control machine is set on the temperature control target of the spacecraft The outer side of deck 4.
[0020] Su...
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