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:
Nov. 02, 2021

Filed:

Dec. 18, 2017
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Praveen Sharma, Bangalore, IN;

Shuvajyoti Ghosh, Bangalore, IN;

Narayanan Payyoor, Bangalore, IN;

Tod Robert Steen, Cincinnati, OH (US);

Carl Lawrence MacMahon, Cincinnati, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/26 (2006.01); F02C 7/06 (2006.01); F01D 25/34 (2006.01);
U.S. Cl.
CPC ...
F02C 7/26 (2013.01); F01D 25/34 (2013.01); F02C 7/06 (2013.01); F05D 2220/32 (2013.01); F05D 2260/85 (2013.01); F05D 2270/02 (2013.01); F05D 2270/114 (2013.01); F05D 2270/303 (2013.01); F05D 2270/304 (2013.01);
Abstract

A method of starting a gas turbine engine is generally provided. The engine includes a rotor assembly including a compressor rotor and a turbine rotor each coupled to a shaft. The rotor assembly is coupled to a bearing assembly within a casing enabling rotation of the rotor assembly. The method includes determining, based on a lubricant parameter, a period of time within which a rotational speed of the rotor assembly is maintained within a bowed rotor mitigation speed range; rotating the rotor assembly for the period of time within the bowed rotor mitigation speed range; and accelerating the rotor assembly to the combustion speed to ignite a fuel-oxidizer mixture for combustion.


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