Counter-rotating turbine engine and method of assembling same

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

Patent

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F02C 7/06 (2006.01) F01D 25/20 (2006.01)

Patent

CA 2516752

A method for assembling a gas turbine engine (10) includes providing a first fan assembly (12) configured to rotate in a first rotational direction, rotatably coupling a second fan assembly (14) to the first fan assembly, wherein the second fan assembly is configured to rotate in a second rotational direction that is opposite the first rotational direction, and coupling a lubrication system (150) to the gas turbine engine such that a lubrication fluid is channeled through at least a portion of the second fan assembly.

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