Testing device and method for aircraft fuel system in simulated high altitude environment
A technology of fuel system and testing device, which is applied in the direction of aircraft component testing, ground equipment, aircraft parts, etc., and can solve problems such as complex system, high cost, and accuracy error
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[0025] In order to overcome the shortcomings of the prior art, the present invention provides a test device and method for simulating the fuel system of an aircraft in a high-altitude environment. By adjusting the working pressure and temperature of the fuel system, a low-temperature and low-pressure (such as plateau or high altitude) environment is simulated. , To record the working parameters of the fuel system for analysis and testing.
[0026] Such as figure 1 Shown is the schematic diagram of the test device for the aircraft fuel system in the simulated high altitude environment, including a low temperature air supply system connected to the fuel system and a vacuum exhaust system connected to the pressure-resistant fuel tank of the fuel system.
[0027] The low-temperature gas supply system includes a gas storage tank 11, a first regulating valve 12, an expansion turbine unit 13, an electric heater 15 and a plate heat exchanger 17 which are sequentially connected through a ga...
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