Gas turbine engine assembly and methods of assembling same

Details Gas turbine engine assembly and methods of assembling same Gas turbine engine assembly and methods of assembling same

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 3/067 (2006.01) F02C 7/36 (2006.01) F02C 9/16 (2006.01)

Patent

CA 2563482

A method for assembling a gas turbine engine (10) includes providing a core gas turbine engine (12) including a high-pressure compressor (26), a combustor (28), and a turbine (30), and coupling a counter-rotating fan assembly (16) to the core gas turbine engine such that air discharged from the counter-rotating fan assembly is channeled directly into an inlet (104) of the gas turbine engine compressor.

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