Independent temperature and humidity control system for sealed cabin of space aircraft and implementation method
A space vehicle, independent control technology, applied in the direction of heating and ventilation control system, air conditioning system, space heating and ventilation, etc., can solve the problem that it is difficult to meet the air temperature and humidity in the sealed cabin, and the impact of the successful completion of manned spaceflight missions, etc. problems, to achieve precise control, ensure humidity control accuracy, and achieve the effect of secondary adjustment
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[0052] Below in conjunction with accompanying drawing and specific embodiment the present invention is described in further detail:
[0053] Such as figure 1 As shown, the integrated temperature and humidity control system is the temperature and humidity control method currently used in space sealed cabins. After passing through the ventilation regulating valve 105, the air 101 of the main ventilation road is divided into two parts: the dehumidification air branch 102 and the bypass air branch 104, The dehumidification air branch 103 is equipped with a condensing drier assembly 4. The condensing drier assembly 4 cools and dehumidifies the air under the cooling effect of the low temperature circuit 2. After cooling and dehumidifying, the air is mixed with the bypass air, and the temperature and humidity at the mixing point 6 are the control objects. . The low-temperature circuit 2 itself does not have the function of active temperature regulation. The temperature adjustment of...
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