Gas turbine fuel injector with metering cavity
AssigneeSolar Turbines Incorporated
InventorsChristopher Zdzislaw Twardochleb, James Gregory Roesch
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AssigneeSolar Turbines Incorporated
InventorsChristopher Zdzislaw Twardochleb, James Gregory Roesch
Estimating the term…
A fuel injector for a gas turbine engine may include a flow path for a fuel-air mixture extending longitudinally through the fuel injector, and a fuel gallery extending circumferentially around the flow path. The fuel gallery may be adapted to inject a liquid fuel into the flow path. The fuel injector may also include an annular casing positioned circumferentially around the fuel gallery to define an insulating chamber around the gallery. The fuel injector may also include an annular cover extending around the fuel injector to define a metering chamber. The fuel injector may further include one or more purge holes fluidly coupling the metering chamber to the insulating chamber, and one or more metering holes fluidly coupling the metering chamber to a volume exterior to the fuel injector.
A fuel injector for a gas turbine engine comprising:
A method of operating a gas turbine engine including a fuel injector, the fuel injector including a fuel gallery extending circumferentially around the fuel injector, an annular casing positioned circumferentially around the fuel gallery to define an insulating chamber around the fuel gallery, and a metering chamber spaced apart from the insulating chamber and circumferentially extending around the fuel injector, the insulating chamber and the metering chamber being fluidly coupled together by one or more purge holes, and the metering chamber being fluidly coupled to a compressed air space external to the fuel injector by one or more metering holes, the method comprising:
A gas turbine engine, comprising:
Dependencies are inferred from the claim text.