Invention Grant
- Patent Title: Fuel nozzle for use in a turbine engine and method of assembly
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Application No.: US13687103Application Date: 2012-11-28
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Publication No.: US09677766B2Publication Date: 2017-06-13
- Inventor: Bassam Sabry Mohammad Abd El-Nabi , Gregory Allen Boardman
- Applicant: General Electric Company
- Applicant Address: US NY Niskayuna
- Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee Address: US NY Niskayuna
- Agent John P. Darling
- Main IPC: F23R3/28
- IPC: F23R3/28 ; F23D14/64 ; F23D14/62
Abstract:
A fuel nozzle for use in a turbine engine is provided. The fuel nozzle includes a fuel injector configured to discharge a flow of fuel therefrom and a premixer tube coupled in flow communication with the fuel injector. The premixer tube is configured to receive the fuel flow and a flow of air at an upstream end of the premixer tube, wherein the fuel and air are progressively mixed as the fuel and air are channeled through the length of the premixer tube.
Public/Granted literature
- US20140144150A1 FUEL NOZZLE FOR USE IN A TURBINE ENGINE AND METHOD OF ASSEMBLY Public/Granted day:2014-05-29
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