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:
Feb. 18, 2025

Filed:

Oct. 28, 2022
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Jeffrey Poissant, Brossard, CA;

Robert Pontarelli, Brossard, CA;

Cristina Crainic, Longueuil, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/16 (2006.01); F02C 9/28 (2006.01); F02C 9/44 (2006.01);
U.S. Cl.
CPC ...
F02C 9/28 (2013.01); F02C 9/16 (2013.01); F02C 9/44 (2013.01); F05D 2220/323 (2013.01); F05D 2270/051 (2013.01); F05D 2270/304 (2013.01); F05D 2270/311 (2013.01); F05D 2270/313 (2013.01); F05D 2270/708 (2013.01);
Abstract

A method and system for correlating engine thrust and engine thrust lever angle (TLA) during operation of a gas turbine engine powered aircraft is provided. The method includes: a) providing current flight conditions including a Mach number of the aircraft, altitude of the aircraft, and a TLA; b) determining a corrected fan speed value based on a sensed fan speed and flight conditions; c) determining a first corrected net thrust value based on the corrected fan speed value and the Mach number; d) determining a compensation factor using the corrected fan speed value, the Mach number, and the corrected net thrust value; e) determining a second corrected net thrust value as a function of the TLA; and f) correlating an engine fan speed to the TLA using the second corrected net thrust value as a function of the TLA and the compensation factor.


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