Lubrication system for a counter-rotating turbine engine and...

Details Lubrication system for a counter-rotating turbine engine and... Lubrication system for a counter-rotating turbine engine and...

2004-10-29

2008-12-02

Rodriguez, William H (Department: 3746)

Power plants

Reaction motor

Interrelated reaction motors

C060S039080, C060S039162

Reexamination Certificate

active

07458202

ABSTRACT:
A method for assembling a gas turbine engine 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, and coupling a lubrication system 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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International Search Report; London Patent Office; Place of Search GB; Ref. No. 13DV-126857; Application No. GB0515220.2; Date Nov. 23, 2005; 3 pgs.

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