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Integrated Combustor Nozzle for a Segmented Annular Combustion System

United States Patent Application

20170299187
A1
View the Complete Application at the US Patent & Trademark Office
The present disclosure is directed to an integrated combustor nozzle for a segmented annular combustion system. The integrated combustor nozzle includes an outer liner segment, an inner liner segment, and a fuel injection panel extending radially between the outer liner segment and the inner liner segment. The fuel injection panel includes a first side wall, a second side wall, and a plurality of premixing channels between the first and second side walls, each of the premixing channels having an outlet on one of the first and second side walls. The aft end of the fuel injection panel defines a turbine nozzle.
Berry, Jonathan Dwight (Simpsonville, SC), Widener, Stanley Kevin (Greenville, SC), Hughes, Michael John (State College, PA), Hafner, Matthew Troy (Honea Path, SC), Citeno, Joseph Vincent (Greenville, SC)
15/ 464,419
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.