Counter-rotating turbine engine and method of assembling same

Rotary kinetic fluid motors or pumps – Plural runners supported for relative motion or on separate... – Interdigitated – oppositely extending – coaxial – axially...

Reexamination Certificate

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Details

C415S068000, C415S069000, C415S229000

Reexamination Certificate

active

10976496

ABSTRACT:
A method for assembling a gas turbine engine that includes providing a low-pressure turbine inner rotor configured to rotate in a first direction, providing a low-pressure turbine outer rotor configured to rotate in a second direction that is opposite the first rotational direction, and coupling at least one foil bearing to at least one of the inner and outer rotors to facilitate improving clearance control between a first rotating component and at least one of a second rotating component and a non-rotating component.

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International Search Report; European Patent Office; Place of Search Munich; Ref. No. 130556/10897; Application No. 05255228.8-2315 PCT; Date Oct. 19, 2005; 8 pgs.

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