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Mounting of Integrated Combustor Nozzles in a Segmented Annular Combustion System

United States Patent Application

20170276363
A1
View the Complete Application at the US Patent & Trademark Office
A segmented annular combustion system includes integrated combustor nozzles, each of which has a fuel injection panel disposed radially between an inner liner segment and an outer liner segment. An aft end portion of the fuel injection panel defines a turbine nozzle. One or more hook plates attached to the outer surfaces of the liner segments are used to mount the integrated combustor nozzle to an inner mounting ring or an outer mounting ring. A mounting strut or mounting tenon(s) attached to the liner segments may also be employed.
Berry, Jonathan Dwight (Simpsonville, SC), Hughes, Michael John (State College, PA), McMahan, Kevin Weston (Greenville, SC)
15/ 464,443
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.