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Combustor with non-circular head end

United States Patent

September 29, 2015
View the Complete Patent at the US Patent & Trademark Office
The present application provides a combustor for use with a gas turbine engine. The combustor may include a head end with a non-circular configuration, a number of fuel nozzles positioned about the head end, and a transition piece extending downstream of the head end.
Kim; Won-Wook (Simpsonville, SC), McMahan; Kevin Weston (Greer, SC)
General Electric Company (Schenectady, NY)
13/ 437,954
April 3, 2012
This invention was made with government support under Contract No. DE-FC26-05NT42643 awarded by the U.S. Department of Energy. The Government has certain rights in this invention.