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. 03, 2020

Filed:

Nov. 29, 2016
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Fadi S. Maalouf, East Hampton, CT (US);

Matthew E. Bintz, West Hartford, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/27 (2006.01); F01D 19/02 (2006.01); B64D 31/12 (2006.01); F02C 7/26 (2006.01); F02C 7/277 (2006.01); B64D 27/10 (2006.01); B64D 31/02 (2006.01);
U.S. Cl.
CPC ...
F02C 7/27 (2013.01); B64D 27/10 (2013.01); B64D 31/02 (2013.01); B64D 31/12 (2013.01); F01D 19/02 (2013.01); F02C 7/26 (2013.01); F02C 7/277 (2013.01); F05D 2220/323 (2013.01); F05D 2260/85 (2013.01); F05D 2270/114 (2013.01); F05D 2270/304 (2013.01);
Abstract

A system for motoring a gas turbine engine of an aircraft is provided. The system includes an air turbine starter operable to drive rotation of a starting spool of the gas turbine engine and a starter air valve operable to deliver compressed air to the air turbine starter in response to the starter air valve being open. The system also includes a metered orifice coupled in a bypass configuration around the starter air valve to deliver a reduced amount of the compressed air to the air turbine starter while the starter air valve is closed. The reduced amount of the compressed air delivered to the air turbine starter limits a motoring speed of the gas turbine engine below a resonance speed of the starting spool of the gas turbine engine.


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