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:
Jan. 28, 2025

Filed:

Nov. 16, 2023
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Ravindra Shankar Ganiger, Bengaluru, IN;

Kudum Shinde, Bengaluru, IN;

Surender Reddy Bhavanam, Bengaluru, IN;

Weize Kang, Mason, OH (US);

Assignee:

GENERAL ELECTRIC COMPANY, Evendale, OH (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/32 (2006.01); F01D 5/02 (2006.01); F01D 25/34 (2006.01);
U.S. Cl.
CPC ...
F02C 7/32 (2013.01); F01D 5/02 (2013.01); F01D 25/34 (2013.01); F05D 2220/32 (2013.01); F05D 2240/20 (2013.01); F05D 2260/42 (2013.01); F05D 2260/941 (2013.01); F05D 2300/505 (2013.01);
Abstract

A gas turbine engine includes a compressor rotor shaft assembly, an accessory gearbox, and a bowed-rotor mitigation drive device drivingly coupled with the accessory gearbox. The bowed-rotor mitigation drive device is driven during an engine startup phase so as to induce a mechanical load (mechanical energy) to the bowed-rotor mitigation drive device. The mechanical load (mechanical energy) is retained within the bowed-rotor mitigation drive device during operation of the gas turbine engine. The mechanical load (mechanical energy) retained within the bowed-rotor mitigation drive device is periodically released by the bowed-rotor mitigation drive device in a plurality of periods so as to provide, in each period, a driving force to the accessory gearbox, which provides the driving force to the compressor rotor shaft assembly to periodically rotate the compressor rotor shaft assembly.


Find Patent Forward Citations

Loading…