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Title: Variable volume combustor with an air bypass system

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:
OSTI Identifier:
1343286
Assignee:
GENERAL ELECTRIC COMPANY NETL
Patent Number(s):
9,562,687
Application Number:
13/760,101
Contract Number:
FC26-05NT42643
Resource Relation:
Patent File Date: 2013 Feb 06
Research Org:
GENERAL ELECTRIC COMPANY, Schenectady, NY (United States)
Sponsoring Org:
USDOE
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING

Other works cited in this record:

Variable Geometry Combustors
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System for damping thermo-acoustic instability in a combustor device for a gas turbine
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