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 2607042

A turbine engine assembly (10) is provided. A turbine engine assembly (10) includes a core gas turbine engine (12) includes a high-pressure compressor (18), a combustor (20), and a high-pressure turbine (22). A turbine engine assembly (10) further includes a booster compressor (30) coupled upstream from the core gas turbine engine. A turbine engine assembly (10) further includes an intermediate- pressure turbine (32) coupled to the booster compressor, the intermediate-pressure turbine disposed downstream from the core gas turbine engine. A turbine engine assembly (10) further includes a counter-rotating fan assembly (16) disposed upstream from the booster compressor, the counter-rotating fan assembly includes a first fan assembly (50) configured to rotate in a first direction and a second fan assembly (52) configured to rotate in an opposite second direction. A turbine engine assembly (10) further includes a low-pressure turbine (14) disposed downstream from the intermediate- pressure turbine, the low-pressure turbine configured to drive the counter- rotating fan assembly.

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