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:
Mar. 15, 2022

Filed:

Nov. 27, 2019
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Peeyush Pankaj, Bangalore, IN;

Narayanan Payyoor, Bangalore, IN;

Shashank Suresh Puranik, Bangalore, IN;

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/10 (2006.01); F01D 25/16 (2006.01); F02C 7/06 (2006.01); F01D 5/03 (2006.01); F01D 5/06 (2006.01);
U.S. Cl.
CPC ...
F01D 5/10 (2013.01); F01D 5/03 (2013.01); F01D 5/06 (2013.01); F01D 25/164 (2013.01); F02C 7/06 (2013.01); F05D 2240/50 (2013.01); F05D 2260/96 (2013.01);
Abstract

A gas turbine engine includes a rotatable drum rotor having a plurality of blades secured thereto. The blades extend radially inward of the rotatable drum rotor. The gas turbine engine also includes a support frame mounted radially outward of the rotating drum rotor and a rotor support system having a bearing assembly positioned between the rotatable drum rotor and the support frame. The bearing assembly includes, at least, a stationary component and at least one rotatable component. Further, the gas turbine engine includes a damper assembly for securing between the support frame and the rotatable drum rotor. Moreover, the damper assembly includes at least one damper secured between the support frame and the stationary component of the bearing assembly or to a surface of the rotatable drum rotor. As such, the damper(s) is configured to provide damping to the rotatable drum rotor during operation of the gas turbine engine.


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