Aircraft front undercarriage steering pressure relief valve moment tester
A technology of pressure relief valve and front landing gear, which is applied in the direction of aircraft component testing, etc., can solve the problems of high failure rate, short service life and low work efficiency of the pressure relief system, so as to reduce the maintenance time, low cost, and improve the The effect of efficiency
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[0013] The aircraft nose landing gear steering release valve torque testing machine provided by the present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.
[0014] like Figure 1 to Figure 2 As shown, the aircraft nose landing gear steering release valve torque testing machine provided by the present invention includes a testing machine main body 1 equipped with movable universal wheels and brakes, a pressure release valve torque test installation platform 12, and a hydraulic oil circuit control system for testing. 10. Pressure sensing test system 4, oil leakage test pipeline for oil inlet circuit 5, oil leakage test pipeline for oil return circuit 6 and leakage oil collection plate 11, where the pressure release valve torque test installation The platform 12 includes an oil inlet circuit 2 for installing a pressure relief valve, an oil return circuit 3 for installing a pressure relief valve test, and a torqu...
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