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:
Feb. 09, 2021

Filed:

Sep. 20, 2017
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Peeyush Pankaj, Bangalore, IN;

Shashank Suresh Puranik, Bangalore, IN;

Darek Tomasz Zatorski, Fort Wright, KY (US);

Christopher Charles Glynn, Clearwater Beach, FL (US);

Richard Schmidt, Loveland, OH (US);

Bhaskar Nanda Mondal, Bangalore, IN;

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/16 (2006.01); F01D 5/30 (2006.01); F02C 3/04 (2006.01); F02K 3/04 (2006.01); F01D 5/03 (2006.01); F02C 7/06 (2006.01); F02C 3/067 (2006.01); F01D 1/26 (2006.01); F02C 7/36 (2006.01);
U.S. Cl.
CPC ...
F01D 25/16 (2013.01); F01D 1/26 (2013.01); F01D 5/03 (2013.01); F01D 5/30 (2013.01); F01D 25/164 (2013.01); F02C 3/04 (2013.01); F02C 3/067 (2013.01); F02C 7/06 (2013.01); F02C 7/36 (2013.01); F02K 3/04 (2013.01); F05D 2240/24 (2013.01); F05D 2240/50 (2013.01); F05D 2260/4031 (2013.01); F05D 2260/40311 (2013.01);
Abstract

A turbomachine includes a spool and a turbine section including a turbine rear frame, a turbine, and a support member. The turbine includes a first plurality of turbine rotor blades and a second plurality of turbine rotor blades, the first plurality of turbine rotor blades and second plurality of turbine rotor blades alternatingly spaced along the axial direction and rotatable with one another. The support member extends between the first plurality of turbine rotor blades and the spool and couples the first plurality of turbine rotor blades to the spool. The turbomachine also includes a bearing assembly including a bearing, the bearing rotatably supporting the support member and supported by the turbine rear frame, the bearing spaced apart from the spool along the radial direction.


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