Device and method for testing airplane tank system
A technology of aircraft fuel tanks and equipment, which is applied in the direction of fluid tightness testing, machine/structural component testing, and measuring devices, and can solve problems such as inattention, discomfort, and time-consuming aircraft fuel tank systems.
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[0025] Apparatus 10 for testing an aircraft fuel tank system 12 includes a fuel supply 14 in the form of a refueling cart including a fuel reservoir 16 . A fuel supply reservoir 16 is connected to a first end of a fuel supply line 18 . A second disconnect of the fuel supply line 18 is connected to a fuel outlet 20 of the fuel supply device 14 .
[0026] A first isolation valve 22 is provided in the fuel supply line 18 which, in the closed state, interrupts the supply of fuel from the fuel reservoir 16 to the fuel outlet 20 of the fuel supply 14 . Conversely, in the open state, the first isolation valve 22 allows fuel to be supplied from the fuel reservoir 16 to the fuel outlet 20 of the fuel supply 14 . A fuel pump 24 is provided in the fuel supply line 18 downstream of the first isolation valve 22 for delivering fuel from the fuel reservoir 16 .
[0027] A fuel outlet 20 of the fuel supply 14 is connected to a first end of a fuel delivery line 26 via a suitable coupling mem...
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