Cooling ventilation simulation device and control method for high-altitude airborne equipment testing
A technology for cooling ventilation and airborne equipment, applied in aircraft component testing, control/regulation systems, non-electric variable control, etc., can solve problems such as uncontrollable temperature and flow, affecting test results, and failing to meet simulation requirements
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[0028] In order to make those skilled in the art better understand the technical solutions of the present invention, the present application is described in detail below with reference to 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 present application. .
[0029] like figure 1 Shown is a schematic diagram of the first embodiment of the application. In this embodiment, the high-altitude airborne equipment is tested in the low pressure chamber 8. The ventilation device of the application includes: an air source 1, a filter 2, a The pressure valve 3 , the flow control unit 4 , the refrigerator 5 , the heater 6 and the 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 to filter out particles and oily impurities in the h...
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