| 摘要 |
<p>A method for purging fuel from a fuel system (28) of a gas turbine engine on shutdown of the engine comprises, in one aspect, terminating a fuel supply (76) 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 (28) used to maintain fuel supply (76) for engine operation, and under the reversed pressure differential substantially purging the fuel (78) remaining in the system (28) therefrom to a fuel source(32).</p> |
