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. 28, 2023

Filed:

Oct. 23, 2020
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Daryoush Mirzahekmati, Kirkland, CA;

Ioan Sabau, LaSalle, CA;

Poi Loon Tang, Montreal, CA;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 21/12 (2006.01); F01D 21/00 (2006.01); F01D 21/14 (2006.01);
U.S. Cl.
CPC ...
F01D 21/12 (2013.01); F01D 21/003 (2013.01); F01D 21/14 (2013.01); F05D 2220/323 (2013.01); F05D 2260/81 (2013.01); F05D 2270/304 (2013.01); F05D 2270/3011 (2013.01); F05D 2270/313 (2013.01); F05D 2270/708 (2013.01); F05D 2270/71 (2013.01);
Abstract

The present disclosure provides methods and systems for determining a synthesized engine parameter of a gas turbine engine. An initial model parameter is obtained from an onboard model associated with the gas turbine engine. A correction factor for the onboard model is determined by modifying a difference between the onboard model and an aero-thermal model of the gas turbine engine using first and second engine parameters and first and second operating conditions, wherein the first and second engine parameters are independent from one another over an operating envelope of the gas turbine engine. The initial model parameter is scaled by applying the correction factor thereto to obtain a corrected model parameter. The corrected model parameter is output as the synthesized engine parameter.


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