Improved injectors for gas turbine combustion chamber
AssigneeSafran Helicopter Engines
InventorsGuillaume TALIERCIO, Nicolas SAVARY, Olivier LAMAISON
Life of this patent
Estimating the term…
Loading patent…
AssigneeSafran Helicopter Engines
InventorsGuillaume TALIERCIO, Nicolas SAVARY, Olivier LAMAISON
Estimating the term…
An injector for a gas turbine combustion chamber, includes a fluid feed system; an injector body extending along a longitudinal axis; an injection head arranged on the injector body and configured to spray the fluid in a direction that is inclined relative to the longitudinal axis; and an actuator configured to turn the injector selectively about the longitudinal axis so as to vary the direction in which the fluid is sprayed; wherein the actuator is configured to enable the orientation of the injector to be varied by turning about the longitudinal axis through an amplitude less than or equal to 90°.
An injector for a gas turbine combustion chamber, the injector comprising:
Dependencies are inferred from the claim text.