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:
Aug. 06, 2019

Filed:

Jun. 14, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Nicholas Adam Descamps, Cincinnati, OH (US);

David Alexander Hiett, Cincinnati, OH (US);

John Thomas Lammers, West Chester, OH (US);

Robert Charles Hon, Fort Mitchell, KY (US);

Thomas Charles Swager, Maineville, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 19/00 (2006.01); F02C 9/00 (2006.01); F01D 21/06 (2006.01); F02C 7/262 (2006.01); F02C 9/46 (2006.01);
U.S. Cl.
CPC ...
F01D 19/00 (2013.01); F01D 21/06 (2013.01); F02C 7/262 (2013.01); F02C 9/00 (2013.01); F02C 9/46 (2013.01); F05D 2220/32 (2013.01); F05D 2260/80 (2013.01); F05D 2260/85 (2013.01); F05D 2270/092 (2013.01); F05D 2270/304 (2013.01); F05D 2270/334 (2013.01); Y02T 50/671 (2013.01);
Abstract

Systems and methods for shutting down a gas turbine engine in response to a severe mechanical failure include determining a rate of change of one or more process conditions. If the rate of change of the one or more process conditions exceeds a respective predetermined failure threshold, a potential severe mechanical failure of the gas turbine engine may be determined. Steps may be taken to confirm the potential severe mechanical failure of the gas turbine engine. In response, an engine restart is prevented.


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