Turbofan engine assembly and method of assembling same

Details Turbofan engine assembly and method of assembling same Turbofan engine assembly and method of assembling same

F - Mech Eng,Light,Heat,Weapons

02

C

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

Patent

CA 2606860

A turbofan engine assembly (10) including a booster compressor (30) coupled to an upstream end of a core gas turbine engine (12), an intermediate- pressure turbine (32) coupled to the booster compressor, the intermediate-pressure turbine disposed downstream from the core gas turbine engine, a first fan assembly (50) coupled to a low-pressure turbine (14), a second fan assembly (52) disposed downstream from the first fan assembly, and a gearbox (100) coupled between the second fan assembly and the low-pressure turbine.

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