Low emission, fixed geometry gas turbine combustor

Details Low emission, fixed geometry gas turbine combustor Low emission, fixed geometry gas turbine combustor

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 3/14 (2006.01) F23R 3/28 (2006.01) F23R 3/34 (2006.01)

Patent

CA 2124069

ABSTRACT OF THE DISCLOSURE A fixed geometry combustor for a gas turbine comprising at least one combustion chamber, a dilution chamber disposed downstream of said combustion chamber and in communication with said combustion chamber, at least one primary inspirator for introducing a fuel/air mixture into said combustion chamber in communication with said combustion chamber, and means for introducing dilution air into the dilution chamber.

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