Fuel staging system
A fuel staging system for a gas turbine engine has a plurality of fuel injectors each having a mains burner. The system has a mains manifold connected to a mains delivery line and configured to distribute fuel from the mains delivery line to the mains burner of each of the plurality of fuel injectors, and a check valve disposed in the mains delivery line upstream of the mains manifold. The check valve is configured to permit flow of fuel from the mains delivery line to the mains manifold when the pressure of fuel in the mains delivery line exceeds a threshold pressure.
1. A fuel staging system for a gas turbine engine, the fuel staging system comprising:
a plurality of fuel injectors, each fuel injector of the plurality of fuel injectors includes a main burner and a pilot burner;
a main manifold connected to a main delivery line, the main manifold being configured to distribute fuel from the main delivery line to the main burner of each fuel injector of the plurality of fuel injectors;
a pilot manifold connected to a pilot delivery line, the pilot manifold being configured to distribute fuel from the pilot delivery line to the pilot burner of each fuel injector of the plurality of injectors,
wherein both the main manifold and the pilot manifold deliver fuel to each fuel injector of the plurality of fuel injectors; and
a check valve disposed in the main delivery line upstream of the main manifold and all of the plurality of fuel injectors and downstream of a recirculation line connected to the main delivery line upstream of the check valve, such that the recirculation line primes the check valve and the main delivery line upstream of the check valve when the check valve is closed,
the check valve being configured to regulate flow of fuel from the main delivery line to the main manifold and all of the plurality of fuel injectors,
the check valve being configured to open in response to a pressure of fuel in the main delivery line exceeding a threshold pressure.
2. The fuel staging system according to claim 1 , further comprising a splitter valve configured to split a fuel supply between the main delivery line and the pilot delivery line.
3. The fuel staging system according to claim 2 , wherein the splitter valve is configured to variably split the fuel supply between the main delivery line and the pilot delivery line.
4. The fuel staging system according to claim 2 , wherein each fuel injector of the plurality of fuel injectors is provided with a weight distributor valve at the respective pilot burner.
5. The fuel staging system according to claim 1 , wherein the main manifold is in a heat exchange relationship with a secondary fuel line, which is a portion of one of the pilot manifold or the recirculation line.
6. The fuel staging system according to claim 5 , wherein:
the main manifold includes a common main distribution line, and a plurality of feed lines that are configured to direct fuel to the main burner of each of the plurality of fuel injectors, and
the common main distribution line is in the heat exchange relationship with the secondary fuel line.
7. The fuel staging system according to claim 5 , further comprising a pipe-in-pipe arrangement in which a portion of the main manifold is in the heat exchange relationship with a portion of the secondary fuel line.
8. The fuel staging system according to claim 5 , further comprising:
a splitter valve configured to split a fuel supply between the main delivery line and the pilot delivery line, wherein the secondary fuel line is a portion of the pilot manifold.
9. The fuel staging system according to claim 1 , wherein:
each fuel injector of the plurality of fuel injectors is provided with a weight distribution valve at the respective main burner, the weight distribution valve having a variable size opening, through which fuel is permitted to flow; and
a size of each of the variable size openings is a function of an orientation of the respective fuel injector of the plurality of fuel injectors within the gas turbine engine, whereby each of the plurality of weight distribution valves are configured to counteract effects on flow rate of a fuel head pressure through the respective fuel injector of the plurality of fuel injectors which varies around the gas turbine engine.
10. The fuel staging system according to claim 9 , wherein each fuel injector of the plurality of fuel injectors is provided with a weight distributor valve at the pilot burner.
11. The fuel staging system according to claim 1 , further comprising a further check valve disposed in the main delivery line upstream of the main manifold.
12. The fuel staging system according claim 1 , wherein the recirculation line forms part of a main cooling circuit, the recirculation line being configured to receive fuel from the main delivery line when the check valve is closed and recirculate the fuel back into the main delivery line.
13. The fuel staging system according to claim 12 , further comprising:
a splitter valve configured to split a fuel supply between the main delivery line and the pilot delivery line, wherein each fuel injector of the plurality of injectors is provided with a weight distributor valve at the pilot burner, and a secondary fuel line is a portion of the recirculation line.
14. A gas turbine engine for an aircraft, the gas turbine engine comprising a fuel staging system comprising:
a plurality of fuel injectors, each fuel injector of the plurality of fuel injectors includes a main burner and a pilot burner;
a main manifold connected to a main delivery line, the main manifold being configured to distribute fuel from the main delivery line to the main burner of each fuel injector of the plurality of fuel injectors;
a pilot manifold connected to a pilot delivery line, the pilot manifold being configured to distribute fuel from the pilot delivery line to the pilot burner of each fuel injector of the plurality of injectors,
wherein both the main manifold and the pilot manifold deliver fuel to each fuel injector of the plurality of fuel injectors; and
a check valve disposed in the main delivery line upstream of the main manifold and all of the plurality of fuel injectors and downstream of a recirculation line connected to the main delivery line upstream of the check valve, such that the recirculation line primes the check valve and the main delivery line upstream of the check valve when the check valve is closed,
the check valve being configured to regulate flow of fuel from the main delivery line to the main manifold and all of the plurality of fuel injectors,
the check valve being configured to open in response to a pressure of fuel in the main delivery line exceeding a threshold pressure.