The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Nov. 29, 2022

Filed:

Nov. 12, 2020
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Narayanan Payyoor, Bangalore, IN;

Peeyush Pankaj, Bangalore, IN;

Richard Schmidt, Loveland, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/06 (2006.01); F02C 7/36 (2006.01); F16C 13/02 (2006.01); F16C 19/49 (2006.01);
U.S. Cl.
CPC ...
F02C 7/06 (2013.01); F02C 7/36 (2013.01); F05D 2220/32 (2013.01); F05D 2240/24 (2013.01); F05D 2240/52 (2013.01); F05D 2240/54 (2013.01); F05D 2240/60 (2013.01); F16C 13/02 (2013.01); F16C 19/49 (2013.01); F16C 2360/23 (2013.01);
Abstract

An interdigitated turbine assembly for a gas turbine engine, the interdigitated turbine assembly including a first turbine rotor assembly interdigitated with a second turbine rotor assembly. A first static frame is positioned forward of the first turbine rotor assembly and the second turbine rotor assembly. The first turbine rotor assembly is operably coupled to an inner rotatable component of a gear assembly. The second turbine rotor assembly is operably coupled to an outer rotatable component of the gear assembly. The static structure is connected to the first static frame. A driveshaft is operably coupled to the outer rotatable component. A first bearing assembly is operably coupled to the driveshaft and the first static frame. A second bearing assembly is operably coupled to the first static frame and first turbine rotor assembly. A third bearing assembly is operably coupled to the first turbine rotor assembly and the second turbine rotor assembly.


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