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Title: Combustor and combustor screech mitigation methods

Patent ·
OSTI ID:1133625

The present application provides for a combustor for use with a gas turbine engine. The combustor may include a cap member and a number of fuel nozzles extending through the cap member. One or more of the fuel nozzles may be provided in a non-flush position with respect to the cap member.

Research Organization:
General Electric Co., Schenectady, NY (United States)
Sponsoring Organization:
USDOE
DOE Contract Number:
FC26-05NT42643
Assignee:
General Electric Company (Schenectady, NY)
Patent Number(s):
8,733,108
Application Number:
12/833,237
OSTI ID:
1133625
Country of Publication:
United States
Language:
English

References (16)

Movable combustion system for a gas turbine patent June 1992
Flashback resistant fuel staged premixed combustor patent August 1993
Staged fuel delivery system with secondary distribution valve patent June 1994
Gas turbine combustor patent November 1998
Multiple venturi ultra-low nox combustor patent July 1999
Dynamically uncoupled low NOx combustor having multiple premixers with axial staging patent August 1999
Dynamically uncoupled low nox combustor with axial fuel staging in premixers patent December 2000
Gas turbine combustor patent September 2001
Gas turbine combustor patent December 2001
Gas turbine combustor patent May 2005
Methods and systems for combustion dynamics reduction patent August 2009
Axially staged combustion system for a gas turbine engine patent December 2009
Gas turbine combustor patent-application September 2003
Gas turbine combustor and operating method thereof patent-application March 2004
Gas Turbine Combustor and Ignition Method of Igniting Fuel Mixture in the Same patent-application July 2008
Swirler, Fuel and Air Assembly and Combustor patent-application December 2011

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