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Title: Radial flow fuel nozzle for a combustor of a gas turbine

Abstract

A combustor for a gas turbine generally includes a radial flow fuel nozzle having a fuel distribution manifold, and a fuel injection manifold axially separated from the fuel distribution manifold. The fuel injection manifold generally includes an inner side portion, an outer side portion, and a plurality of circumferentially spaced fuel ports that extend through the outer side portion. A plurality of tubes provides axial separation between the fuel distribution manifold and the fuel injection manifold. Each tube defines a fluid communication path between the fuel distribution manifold and the fuel injection manifold.

Inventors:
; ;
Publication Date:
Research Org.:
General Electric Company, Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1260244
Patent Number(s):
9,383,098
Application Number:
13/664,705
Assignee:
General Electric Company NETL
DOE Contract Number:  
FC26-05NT42643
Resource Type:
Patent
Resource Relation:
Patent File Date: 2012 Oct 31
Country of Publication:
United States
Language:
English
Subject:
33 ADVANCED PROPULSION SYSTEMS; 42 ENGINEERING

Citation Formats

Means, Gregory Scott, Boardman, Gregory Allen, and Berry, Jonathan Dwight. Radial flow fuel nozzle for a combustor of a gas turbine. United States: N. p., 2016. Web.
Means, Gregory Scott, Boardman, Gregory Allen, & Berry, Jonathan Dwight. Radial flow fuel nozzle for a combustor of a gas turbine. United States.
Means, Gregory Scott, Boardman, Gregory Allen, and Berry, Jonathan Dwight. Tue . "Radial flow fuel nozzle for a combustor of a gas turbine". United States. https://www.osti.gov/servlets/purl/1260244.
@article{osti_1260244,
title = {Radial flow fuel nozzle for a combustor of a gas turbine},
author = {Means, Gregory Scott and Boardman, Gregory Allen and Berry, Jonathan Dwight},
abstractNote = {A combustor for a gas turbine generally includes a radial flow fuel nozzle having a fuel distribution manifold, and a fuel injection manifold axially separated from the fuel distribution manifold. The fuel injection manifold generally includes an inner side portion, an outer side portion, and a plurality of circumferentially spaced fuel ports that extend through the outer side portion. A plurality of tubes provides axial separation between the fuel distribution manifold and the fuel injection manifold. Each tube defines a fluid communication path between the fuel distribution manifold and the fuel injection manifold.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2016},
month = {7}
}

Patent:

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