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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Figure CN122014420A_ABST
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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