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Title: Fuel nozzle for a combustor of a gas turbine engine

Abstract

A fuel nozzle for a gas turbine generally includes a main body having an upstream end axially separated from a downstream end. The main body at least partially defines a fuel supply passage that extends through the upstream end and at least partially through the main body. A fuel distribution manifold is disposed at the downstream end of the main body. The fuel distribution manifold includes a plurality of axially extending passages that extend through the fuel distribution manifold. A plurality of fuel injection ports defines a flow path between the fuel supply passage and each of the plurality of axially extending passages.

Inventors:
; ;
Issue Date:
Research Org.:
GENERAL ELECTRIC COMPANY, Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1243327
Patent Number(s):
9,291,103
Application Number:
13/705,443
Assignee:
GENERAL ELECTRIC COMPANY (Schenectady, NY)
DOE Contract Number:  
FC26-05NT42643
Resource Type:
Patent
Resource Relation:
Patent File Date: 2012 Dec 05
Country of Publication:
United States
Language:
English
Subject:
24 POWER TRANSMISSION AND DISTRIBUTION; 33 ADVANCED PROPULSION SYSTEMS; 42 ENGINEERING

Citation Formats

Belsom, Keith Cletus, McMahan, Kevin Weston, and Thomas, Larry Lou. Fuel nozzle for a combustor of a gas turbine engine. United States: N. p., 2016. Web.
Belsom, Keith Cletus, McMahan, Kevin Weston, & Thomas, Larry Lou. Fuel nozzle for a combustor of a gas turbine engine. United States.
Belsom, Keith Cletus, McMahan, Kevin Weston, and Thomas, Larry Lou. Tue . "Fuel nozzle for a combustor of a gas turbine engine". United States. https://www.osti.gov/servlets/purl/1243327.
@article{osti_1243327,
title = {Fuel nozzle for a combustor of a gas turbine engine},
author = {Belsom, Keith Cletus and McMahan, Kevin Weston and Thomas, Larry Lou},
abstractNote = {A fuel nozzle for a gas turbine generally includes a main body having an upstream end axially separated from a downstream end. The main body at least partially defines a fuel supply passage that extends through the upstream end and at least partially through the main body. A fuel distribution manifold is disposed at the downstream end of the main body. The fuel distribution manifold includes a plurality of axially extending passages that extend through the fuel distribution manifold. A plurality of fuel injection ports defines a flow path between the fuel supply passage and each of the plurality of axially extending passages.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2016},
month = {3}
}

Patent:

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