Turbine engine with fuel nozzle

CN122014420APending Publication Date: 2026-05-12GENERAL ELECTRIC CO
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
GENERAL ELECTRIC CO
Filing Date
2025-09-28
Publication Date
2026-05-12

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Abstract

A turbine engine can burn fuel to drive a turbine, and the turbine drives the engine. The fuel nozzle may supply fuel for combustion or ignition of the fuel. The fuel nozzle may include a center body defining a first fuel passage terminating in a first orifice. The annular first wall circumferentially surrounds and is spaced apart from the center body to define a first airflow passage therebetween. A set of first swirler vanes are spaced circumferentially around the center body and disposed within the first airflow channel. The fuel nozzle may supply a mixture of fuel and air for combustion.
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