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:
Apr. 23, 2024

Filed:

Jun. 21, 2022
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Arthur William Sibbach, Boxford, MA (US);

Brandon Wayne Miller, Liberty Township, OH (US);

Erich Alois Krammer, West Chester, OH (US);

Douglas Scott Jacobs, Boston, MA (US);

Joseph Alfred Iannotti, Glenville, NY (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 21/02 (2006.01); F02C 9/28 (2006.01); F02C 9/46 (2006.01); F02C 9/50 (2006.01);
U.S. Cl.
CPC ...
F01D 21/02 (2013.01); F02C 9/28 (2013.01); F02C 9/46 (2013.01); F02C 9/50 (2013.01); F05D 2270/021 (2013.01); F05D 2270/304 (2013.01); F05D 2270/335 (2013.01);
Abstract

A method for providing overspeed protection for a gas turbine engine having an engine shaft includes monitoring, via an overspeed protection system, a torque of the engine shaft. The method also includes determining, via the overspeed protection system, at least one additional condition of the engine shaft. Further, the method includes determining, via the overspeed protection system, an overspeed condition of the gas turbine engine when the torque of the engine shaft drops below a torque threshold and the at least one additional condition of the engine shaft is indicative of the gas turbine engine being in an operational state. Thus, the overspeed condition is indicative of an above normal rotational speed of the engine shaft. In addition, the method includes initiating a shutdown procedure for the gas turbine engine in response to the determined overspeed condition to reduce the rotational speed of the engine shaft.


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