Invention Grant
US09261025B2 Fuel system of gas turbine engines 有权
燃气轮机发动机燃油系统

Fuel system of gas turbine engines
Abstract:
A method for purging fuel from a fuel system of a gas turbine engine on shutdown of the engine comprises, in one aspect, terminating a fuel supply to the fuel system and using the residual compressed air to create a reversed pressure differential in the fuel system relative to a forward pressure differential of the fuel system used to maintain fuel supply for engine operation, and under the reversed pressure differential substantially purging the fuel remaining in the system therefrom to a fuel source.
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