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Title: Apparatus for mixing fuel in a gas turbine

Abstract

A combustor nozzle includes an inlet surface and an outlet surface downstream from the inlet surface, wherein the outlet surface has an indented central portion. A plurality of fuel channels are arranged radially outward of the indented central portion, wherein the plurality of fuel channels extend through the outlet surface.

Inventors:
;
Issue Date:
Research Org.:
General Electric Company, Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1178278
Patent Number(s):
9,010,083
Application Number:
13/020,156
Assignee:
General Electric Company (Schenectady, NY)
DOE Contract Number:  
FC26-05NT42643
Resource Type:
Patent
Resource Relation:
Patent File Date: 2011 Feb 03
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING; 33 ADVANCED PROPULSION SYSTEMS

Citation Formats

Uhm, Jong Ho, and Johnson, Thomas Edward. Apparatus for mixing fuel in a gas turbine. United States: N. p., 2015. Web.
Uhm, Jong Ho, & Johnson, Thomas Edward. Apparatus for mixing fuel in a gas turbine. United States.
Uhm, Jong Ho, and Johnson, Thomas Edward. Tue . "Apparatus for mixing fuel in a gas turbine". United States. https://www.osti.gov/servlets/purl/1178278.
@article{osti_1178278,
title = {Apparatus for mixing fuel in a gas turbine},
author = {Uhm, Jong Ho and Johnson, Thomas Edward},
abstractNote = {A combustor nozzle includes an inlet surface and an outlet surface downstream from the inlet surface, wherein the outlet surface has an indented central portion. A plurality of fuel channels are arranged radially outward of the indented central portion, wherein the plurality of fuel channels extend through the outlet surface.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2015},
month = {4}
}

Patent:

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