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Title: Turbine combustor with fuel nozzles having inner and outer fuel circuits

Patent ·
OSTI ID:1111479

A combustor cap assembly for a turbine engine includes a combustor cap and a plurality of fuel nozzles mounted on the combustor cap. One or more of the fuel nozzles would include two separate fuel circuits which are individually controllable. The combustor cap assembly would be controlled so that individual fuel circuits of the fuel nozzles are operated or deliberately shut off to provide for physical separation between the flow of fuel delivered by adjacent fuel nozzles and/or so that adjacent fuel nozzles operate at different pressure differentials. Operating a combustor cap assembly in this fashion helps to reduce or eliminate the generation of undesirable and potentially harmful noise.

Research Organization:
General Electric Company, Schenectady, NY, USA
Sponsoring Organization:
USDOE
DOE Contract Number:
FC26-05NT42643
Assignee:
General Electric Company (Schenectady, NY)
Patent Number(s):
8,613,197
Application Number:
12/850,763
OSTI ID:
1111479
Country of Publication:
United States
Language:
English

References (14)

Gas turbine combustor patent June 2009
Low-cost dual-fuel combustor and related method patent June 2009
Methods and apparatus for low emission gas turbine energy generation patent June 2009
Flame Holding Tolerant Fuel and Air Premixer for a Gas Turbine Combustor patent-application April 2010
Toroidal Ring Manifold For Secondary Fuel Nozzle of A DLN Gas Turbine patent-application March 2009
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Combined pilot and main burner patent December 1981
Main stage fuel mixer with premixing transition for dry low No.sub.x (DLN) combustors patent March 2000
Reduced center burner in multi-burner combustor and method for operating the combustor patent March 2007
Flashback resistant fuel staged premixed combustor patent August 1993
Gas turbine combustor of the completely premixed combustion type patent August 1994
Premixed secondary fuel nozzle with integral swirler patent March 1993
Low NOx combustion patent November 1993
System and method for supporting fuel nozzles in a gas turbine combustor utilizing a support plate patent January 2004