Pressure Control System of Aircraft Air Source Vehicle
A technology of pressure control and air source vehicle, which is applied to aircraft parts, pipeline systems, mechanical equipment, etc., can solve the problems of high operating cost and complex system, and achieve the effect of low operating cost, simple system structure, and fewer control components
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[0011] See figure 1 and figure 2 , the pressure control system of the aircraft air source vehicle of the present invention, which includes an air supply pipeline 1 and a state selection switch SA, a pressure control valve 4, a first electromagnetic valve 3, a second electromagnetic valve 5 and an overflow valve 6, wherein the first electromagnetic valve Valve 3 is a two-position two-way solenoid valve SV2, and the second solenoid valve 5 is a two-position three-way solenoid valve SV1. The two-position two-way solenoid valve SV2 is set forward, and the two-position three-way solenoid valve SV1 is set reversely. SA is equipped with "aircraft start" status contacts and "air conditioning" status contacts, and the air supply pipeline 1 is provided with a control air output interface a and an overflow valve interface b, and the output interface a of the air supply pipeline 1 passes through the pipeline respectively. It is connected with the air inlet 3-1 of the first solenoid valv...
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