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:
Jul. 21, 2020

Filed:

Dec. 15, 2017
Applicant:

General Electric Company, Schenectady, NY (US);

Inventor:

Charles Stanley Orkiszewski, Cincinnati, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 19/02 (2006.01); F04D 29/66 (2006.01); F01D 25/34 (2006.01); F01D 5/02 (2006.01); F04D 29/52 (2006.01); F16D 43/30 (2006.01); F16D 43/04 (2006.01); F01D 19/00 (2006.01); F02C 7/268 (2006.01); F02C 7/26 (2006.01); F02C 7/277 (2006.01);
U.S. Cl.
CPC ...
F01D 19/02 (2013.01); F01D 25/34 (2013.01); F04D 29/668 (2013.01); F01D 5/02 (2013.01); F01D 19/00 (2013.01); F02C 7/26 (2013.01); F02C 7/268 (2013.01); F02C 7/277 (2013.01); F04D 29/522 (2013.01); F05D 2220/32 (2013.01); F05D 2260/42 (2013.01); F05D 2260/85 (2013.01); F05D 2260/96 (2013.01); F05D 2270/304 (2013.01); F16D 43/04 (2013.01); F16D 43/30 (2013.01);
Abstract

Embodiments of systems and methods for operating a gas turbine engine defining a bowed rotor condition are generally provided. The systems and methods include rotating a rotor assembly defining a bowed rotor condition from approximately zero revolutions per minute (RPM) to within a bowed rotor mitigation speed range, in which the bowed rotor mitigation speed range is defined by a lower speed limit greater than zero RPM and an upper speed limit less than or equal to an idle speed condition of the gas turbine engine; applying a load at the rotor assembly via an energy storage device; adjusting the load to limit rotational speed or acceleration of the rotor assembly to within the bowed rotor mitigation speed range for a period of time; and removing the load to enable rotation of the rotor assembly to the idle speed condition following the period of time.


Find Patent Forward Citations

Loading…