Air modulated carburetor with axially moveable fuel injector tip and swirler assembly responsive to fuel pressure
AssigneeGeneral Electric Company
InventorStephen J. Howell
Life of this patent
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AssigneeGeneral Electric Company
InventorStephen J. Howell
Estimating the term…
A gas turbine engine carburetor includes a fuel injector and a cooperating air swirler for injecting fuel and air into a combustor. The fuel injector includes a hollow body joined to a supporting stem for receiving fuel therein for flow through an injector tip slidingly mounted to the injector body for movement relative thereto. The air swirler surrounds the injector tip and is spaced form the injector body to define an air inlet, and is spaced from the injector tip to define an air outlet. A spring operatively engages the injector body and the injector tip and is preloaded for biasing the injector tip to an initial position. The spring is sized so that increasing pressure of the fuel in the injector body further loads the spring for moving the injector tip from the initial position to a displaced position, with movement of the injector tip modulating airflow through the swirler for in-turn modulating the ratio of discharged fuel and air.
A carburetor for discharging fuel and air into a gas turbine engine combustor comprising:
A carburetor for discharging fuel and air comprising:
A carburetor for discharging fuel and air comprising:
A carburetor for discharging fuel and air into a gas turbine engine combustor comprising:
Dependencies are inferred from the claim text.