Counter-rotating gas turbine engine and method of assembling...

Power plants – Combustion products used as motive fluid – Multiple fluid-operated motors

Reexamination Certificate

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C415S068000

Reexamination Certificate

active

10976494

ABSTRACT:
A method for assembling a gas turbine engine includes providing a high pressure turbine, providing a low-pressure turbine inner rotor that includes a first plurality of turbine blade rows configured to rotate in a first direction, providing a low-pressure turbine outer rotor that includes a second plurality of turbine blade rows configured to rotate in a second direction that is opposite the first direction, and coupling a plurality of bearings between the outer rotor and a turbine mid-frame between the high pressure turbine and at least one of the inner and outer rotors such that the plurality of bearings support a forward end of the outer rotor.

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