Invention Application
US20150253009A1 GAS TURBINE ENGINE FUEL INJECTOR WITH AN INNER HEAT SHIELD 有权
燃气涡轮发动机燃油喷射器内置热风罩

GAS TURBINE ENGINE FUEL INJECTOR WITH AN INNER HEAT SHIELD
Abstract:
A fuel injector for a combustor of a gas turbine engine is disclosed. The fuel injector includes a gas outer tube, a gas inner tube, a liquid tube, and a heat shield. The gas outer tube and the gas inner tube form a gas fuel annulus. The gas inner tube and the liquid tube form a liquid fuel annulus. The liquid tube forms an air cavity. The heat shield extends within the liquid tube forming an insulating gap between the heat shield and the liquid tube.
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