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:
Jun. 13, 2023

Filed:

Dec. 13, 2021
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Michel Labrecque, Sainte-Julie, CA;

Kevin Nguyen, Montréal, CA;

Ninad Joshi, Brampton, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/16 (2006.01); F02C 3/04 (2006.01);
U.S. Cl.
CPC ...
F02C 9/16 (2013.01); F02C 3/04 (2013.01); F05D 2220/30 (2013.01); F05D 2240/35 (2013.01); F05D 2270/051 (2013.01); F05D 2270/303 (2013.01); F05D 2270/3013 (2013.01);
Abstract

A method and a system for synthesizing thrust from a turbofan engine are provided. The turbofan engine comprising a compressor section, a combustor, and a turbine section in serial fluid flow communication. The engine is operated and, during the operating of the turbofan engine, a pressure of fluid at an exit of the compressor section and a temperature of fluid at a location upstream of the exit of the compressor section are determined. A synthesized value of thrust from the turbofan engine is determined based on a product of at least a first factor and a second factor, the first factor being a function of the pressure and the second factor being a function of the temperature. The synthesized value of thrust from the turbofan engine is output.


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