Counter-rotating turbine engine and method of assembling same

Power plants – Reaction motor – Including counter rotating rotors

Reexamination Certificate

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C060S039080, C060S226100

Reexamination Certificate

active

10976526

ABSTRACT:
A method for assembling a gas turbine engine that includes providing a first fan assembly configured to rotate in a first rotational direction, rotatably coupling a second fan assembly 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, coupling a first shaft to the first fan assembly and to a first turbine rotor that is configured to rotate in a first rotational direction, coupling a second shaft coupled to the second fan assembly and to a second turbine rotor that is configured to rotate in a second rotational direction that is opposite the first rotational direction, and coupling a lubrication system to the gas turbine engine such that a lubrication fluid is channeled through the first shaft to lubricate at least one of the first and second fan assemblies.

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Great Britain Search Report; Ref. No. 13DV132284/11050; Application No. GB0521903.5; Mar. 21, 2006; 3 pgs.

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