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US09033263B2 Fuel injection nozzle with film-type fuel application 有权
燃油喷嘴采用薄膜式燃料应用

Fuel injection nozzle with film-type fuel application
Abstract:
A fuel injection nozzle for a gas turbine combustion chamber with a film applicator (1) is provided with several fuel openings (2). Center axes (5) of the fuel openings (2) through the film applicator (1), with regard to their radial orientation, are essentially parallel to the main flow direction (6) of the air.
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