Fuel system for a gas turbine engine and operation method therefore

摘要

A fuel system (10) for a turbine engine (16) is provided. The fuel system (10) includes a positive displacement pump (24) driven by an electric motor (26) . The pump (24) is rotated in a first direction to deliver fuel to the turbine engine (16), and a second direction for evacuating fuel from the turbine engine(16). A shut-off check valve (38) is open in a first direction in response to a first differential pressure created by the pump (24) in the first direction. The shut-off check valve (38) is biased to a closed position when the pump (24) is rotating in the second direction. An ecology check valve (46) is biased to a closed position in the first direction and open in the second direction in response to a second differential pressure created by the pump (24). The check valves (38, 46) open and close automatically in response to the pressures generated by the positive displacement pump in each of the first and second rotational directions. In this manner, simple, reliable valves are utilized to regulate the flow of fuel in the fuel system.