Duct burning mixed flow turbofan and method of operation

Details Duct burning mixed flow turbofan and method of operation Duct burning mixed flow turbofan and method of operation

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 1/06 (2006.01) F02C 9/18 (2006.01) F02K 1/40 (2006.01)

Patent

CA 2613777

A gas turbine engine (10) includes a turbomachinery core (28) operable to generating a first flow of pressurized combustion gases, the core (28) having an exit plane (E); a fan (14) disposed upstream of the core (28) adapted to extract energy from the core (28) and generate a first flow of pressurized air; a bypass duct (30) surrounding the core (28) which receives a portion of the flow of pressurized air from the fan (14); a duct burner (32) disposed in the bypass duct (30), upstream of the exit plane (E), for receiving the first flow of pressurized air and generating a second flow of pressurized combustion gases; and an exhaust duct (38) disposed downstream of the core (28) and operable to receive and the first and second flows of pressurized combustion gases and to discharge the combined flows downstream.

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