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. 26, 2019

Filed:

Mar. 11, 2015
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Janusz Fiedler, Oakville, CA;

Tatjana Pekovic, Saint-Lambert, CA;

Dave Sellors, Burlington, CA;

Amandeep Singh Chahal, Brampton, CA;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/46 (2006.01); G05B 9/03 (2006.01); F01D 21/00 (2006.01); F01D 21/02 (2006.01); F02C 9/26 (2006.01); F02C 9/28 (2006.01); F02C 9/44 (2006.01); B64D 31/10 (2006.01);
U.S. Cl.
CPC ...
F02C 9/46 (2013.01); B64D 31/10 (2013.01); F01D 21/00 (2013.01); F01D 21/02 (2013.01); F02C 9/263 (2013.01); F02C 9/28 (2013.01); F02C 9/44 (2013.01); G05B 9/03 (2013.01); F05D 2270/021 (2013.01); F05D 2270/051 (2013.01); F05D 2270/62 (2013.01);
Abstract

An overthrust protection system for an aircraft engine. The system comprises an engine overspeed protection unit comprising overspeed logic and an overspeed solenoid valve controlled by the overspeed logic, the overspeed logic configured to energize the overspeed solenoid valve for removing fuel flow to the engine upon detection of an overspeed condition of the aircraft engine; and an overthrust controller coupled to the overspeed protection unit and configured to measure engine thrust and to detect an overthrust condition when an engine thrust threshold has been exceeded, and configured to trigger energizing of the overspeed solenoid valve upon detection of the overthrust condition and an aircraft-on-ground condition.


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