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:
Oct. 15, 2019

Filed:

Feb. 12, 2016
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Frederick M. Schwarz, Glastonbury, CT (US);

Amy R. Grace, Ellington, CT (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/00 (2006.01); F01D 21/00 (2006.01); F01D 25/34 (2006.01); F01D 25/36 (2006.01); F02C 7/32 (2006.01); F02C 7/268 (2006.01);
U.S. Cl.
CPC ...
F02C 9/00 (2013.01); F01D 21/00 (2013.01); F01D 25/34 (2013.01); F01D 25/36 (2013.01); F02C 7/268 (2013.01); F02C 7/32 (2013.01); F05D 2220/323 (2013.01); F05D 2260/20 (2013.01); F05D 2260/85 (2013.01); F05D 2270/114 (2013.01); F05D 2270/54 (2013.01); Y02T 50/676 (2013.01);
Abstract

A bowed rotor prevention system for a gas turbine engine of an aircraft is provided. The bowed rotor prevention system includes a bowed rotor prevention motor operable to drive rotation of a starting spool of the gas turbine engine through an engine accessory gearbox. The bowed rotor prevention system also includes a controller operable to engage the bowed rotor prevention motor and drive rotation of the starting spool until a bowed rotor prevention threshold condition is met or a bowed rotor prevention shutdown request to halt rotation of the starting spool is received.


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