Cooling ventilation simulation device for testing high-altitude airborne equipment and control method
A technology for cooling ventilation and airborne equipment, applied in aircraft component testing, control/regulation systems, non-electric variable control, etc.
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[0028] In order to enable those skilled in the art to better understand the technical solution of the present invention, the application will be described in detail below in conjunction with the accompanying drawings. The description in this part is only exemplary and explanatory, and should not have any limiting effect on the protection scope of the application. .
[0029] Such as figure 1 Shown is the schematic diagram of the first kind of embodiment of the present application, and in the present embodiment, the high-altitude airborne equipment is tested in the low pressure cabin 8, and the ventilating device of the present application comprises successively connected: air source 1, filter 2, reducer A pressure valve 3 , a flow control unit 4 , a refrigerator 5 , a heater 6 and a back pressure valve 7 , the output end of the back pressure valve 7 is connected to the low pressure chamber 8 .
[0030] The air source 1 is used to output high-pressure air, the filter 2 is used ...
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