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There is intense pressure shock in the boom refueling system because of the fuel receptacle shutting down suddenly and the fuel flow decreasing to zero soon when the refueling process finished, which the aerial refueling system even flight security will be damaged. In this paper, the software, AMESim will be applied to establish the model of the boom refueling system of a certain type of aircraft,...
In order to realize performance test and experimental research for the accessories of aircraft fuel system, a type of integrative testing system is designed in this paper. It can accomplish function and performance tests for accessories of aircraft fuel system, and also can execute fault detection experiments. The simulation model of the system is established by using the software of AMESim, and the...
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