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Segmented Annular Combustion System with Axial Fuel Staging

United States Patent Application

20170276369
A1
View the Complete Application at the US Patent & Trademark Office
A segmented annular combustion system includes an alternating arrangement of fuel nozzles and integrated combustor nozzles. The fuel nozzles deliver fuel to the primary combustion zones. The integrated combustor nozzles include an inner liner segment, an outer liner segment, and a fuel injection panel extending between the liner segments. The fuel injection panel includes injection outlets on one or both side walls to deliver a combustible mixture to the secondary combustion zones. Each fuel injection panel, which provides a boundary between adjacent primary and secondary combustion zones, includes an aft end that defines a turbine nozzle. The segmented annular combustion system is part of a gas turbine.
Berry, Jonathan Dwight (Simpsonville, SC), Widener, Stanley Kevin (Greenville, SC), Hughes, Michael John (State College, PA), Flanagan, James Scott (Simpsonville, SC), Citeno, Joseph Vincent (Greenville, SC), McMahan, Kevin Weston (Greenville, SC)
15/ 464,394
March 21, 2017
STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT [0002] This invention was made with Government support under Contract No. DE-FE0023965 awarded by the United States Department of Energy. The Government has certain rights in this invention.