[특허]Fuel system for a gas turbine engine

Woodward Governor Company

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Fuel system for a gas turbine engine

국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F02C-007/22
미국특허분류(USC)	060/039.094; 060/039.281; 060/734
출원번호	US-0461205 (2003-06-13)
발명자 / 주소	Baryshnikov,Dmitriy Smith,Douglas P.
출원인 / 주소	Woodward Governor Company
대리인 / 주소	Reinhart Boerner Van Deuren P.C.
인용정보	피인용 횟수 : 15 인용 특허 : 3

초록
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A system for automatically transferring the fuel from one or more engine fuel manifolds directly to the engine fuel tank(s) during engine shutdown using an ejector pump has been presented. A checkvalve, which may be integrated with the ejector pump, is also used. A metering valve initiates fuel flow shutoff and is used in the draining of the fuel manifolds, thereby eliminating the need for an additional solenoid dedicated mainly to the shutoff function. The shutoff and pressurizing valve provides flow division between manifolds and manifold drain for sys...

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What is claimed is: 1. A system for transferring fuel from at least one engine fuel manifold of a gas turbine engine to a fuel tank comprising: a fuel metering and shutoff valve configured to provide high pressure fuel to the at least one engine fuel manifold; a bypass valve in fluid communication with the fuel metering and shutoff valve; an ejector having an inlet port for receiving fuel from the bypass valve during engine operation, an outlet port in fluid communication with one of the fuel tank and a fuel tank ejector, and a suction port, the ejector defining a nozzle extending between the inlet port and the outlet port for increasing the velocity of high pressure fuel flowing therethrough so as to create suction at the suction port; a checkvalve in fluid communication with a drain port of a manifold drain valve and one of the suction port and the inlet port, the manifold drain valve having an inlet port in fluid communication with an output port of the fuel metering and shut off valve, at least one manifold port in fluid communication with the at least one engine fuel manifold, a port connected to the checkvalve, and the drain port, the manifold drain valve configured to connect the at least one manifold port to the high pressure fuel during engine operation and to the drain port when the metering valve and shutoff valve inlet port is switched to low pressure. 2. The system of claim 1 wherein the fuel metering and shutoff valve comprises an electro hydraulic servo valve. 3. The system of claim 1 further comprising an electronic engine controller in communication with the fuel metering and shutoff valve. 4. The system of claim 1 wherein the manifold drain valve includes a first manifold and a second manifold and wherein the manifold drain valve is further configured to supply fuel to the first manifold when the fuel pressure of fuel flowing in the inlet port of the manifold drain valve is above a first pressure and to supply fuel to the first manifold and the second manifold when the fuel pressure is above a second fuel pressure. 5. The system of claim 1 wherein the gas turbine engine has a high pressure pump supplying high pressure fuel to the metering and shutoff valve and wherein the bypass valve is configured to maintain an approximately constant pressure drop across the metering and shutoff valve by bypassing excess fuel flow from the high pressure pump back to the inlet of the high pressure pump. 6. The system of claim 5 wherein the bypass valve is further configured to supply fuel to the inlet port of the ejector. 7. The system of claim 1 wherein the bypass valve is configured to supply fuel to the ejector pump as a function of excess fuel flow. 8. The system of claim 7 wherein the bypass valve is further configured to drain the at least one manifold as a function of engine speed. 9. The system of claim 1 wherein the fuel metering and shutoff valve is adapted to initiate a shutoff sequence of the system such that the manifold drain valve moves to a position where the at least one manifold port is connected to the drain port in response to the fuel metering and shutoff valve closing, thereby draining fuel from the at least one manifold. 10. The system of claim 1 wherein the ejector and the checkvalve are integrated into a single component. 11. The system of claim 10 wherein the single component comprises: a housing having a bore along a first axis and a first radial passage from an outer surface of the housing to the bore defining a suction port, the bore defining an inlet port at a first end of the housing; an ejector piston mounted within the bore, the ejector piston having at least one second radial passage along a second axis from an outer surface of the ejector pump to a nozzle extending from a first opening to a second opening of the ejector piston, and wherein the ejector piston moves along the first axis as a function of the pressure of the medium flowing through the nozzle such that the at least one radial passage provides a flow path from the suction port to the nozzle at a pressure range of the medium flowing through the nozzle and does not provide a flow path outside the pressure range.

이 특허에 인용된 특허 (3)

이 특허를 인용한 특허 피인용횟수: 15

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Fuel system for a gas turbine engine

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이 특허에 인용된 특허 (3)

이 특허를 인용한 특허 피인용횟수: 15

IPC 상위 출원인

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Fuel system for a gas turbine engine

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이 특허에 인용된 특허 (3)

이 특허를 인용한 특허 피인용횟수: 15

IPC 상위 출원인

상세정보조회

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IPC 상세정보(version : 201201)

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