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Title: Variable volume combustor with an air bypass system

Abstract

The present application provides a combustor for use with flow of fuel and a flow of air in a gas turbine engine. The combustor may include a number of micro-mixer fuel nozzles positioned within a liner and an air bypass system position about the liner. The air bypass system variably allows a bypass portion of the flow of air to bypass the micro-mixer fuel nozzles.

Inventors:
; ; ;
Issue Date:
Research Org.:
General Electric Co., Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1343286
Patent Number(s):
9562687
Application Number:
13/760,101
Assignee:
GENERAL ELECTRIC COMPANY
Patent Classifications (CPCs):
F - MECHANICAL ENGINEERING F23 - COMBUSTION APPARATUS F23R - GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
Y - NEW / CROSS SECTIONAL TECHNOLOGIES Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE Y02T - CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
DOE Contract Number:  
FC26-05NT42643
Resource Type:
Patent
Resource Relation:
Patent File Date: 2013 Feb 06
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING

Citation Formats

Johnson, Thomas Edward, Ziminsky, Willy Steve, Ostebee, Heath Michael, and Keener, Christopher Paul. Variable volume combustor with an air bypass system. United States: N. p., 2017. Web.
Johnson, Thomas Edward, Ziminsky, Willy Steve, Ostebee, Heath Michael, & Keener, Christopher Paul. Variable volume combustor with an air bypass system. United States.
Johnson, Thomas Edward, Ziminsky, Willy Steve, Ostebee, Heath Michael, and Keener, Christopher Paul. Tue . "Variable volume combustor with an air bypass system". United States. https://www.osti.gov/servlets/purl/1343286.
@article{osti_1343286,
title = {Variable volume combustor with an air bypass system},
author = {Johnson, Thomas Edward and Ziminsky, Willy Steve and Ostebee, Heath Michael and Keener, Christopher Paul},
abstractNote = {The present application provides a combustor for use with flow of fuel and a flow of air in a gas turbine engine. The combustor may include a number of micro-mixer fuel nozzles positioned within a liner and an air bypass system position about the liner. The air bypass system variably allows a bypass portion of the flow of air to bypass the micro-mixer fuel nozzles.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Feb 07 00:00:00 EST 2017},
month = {Tue Feb 07 00:00:00 EST 2017}
}

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