Gas turbine engine assembly and methods of assembling same

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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Details

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

Patent

CA 2606736

A gas turbine engine assembly (10), includes a core gas turbine engine (12), a low-pressure turbine (14) coupled to the core turbine engine, a counter- rotating fan assembly (16) coupled to the low-pressure turbine, and a booster compressor (24) coupled directly to the low-pressure turbine such that the booster compressor and the low-pressure turbine rotate in the same direction.

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