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:
Jul. 08, 2025

Filed:

May. 07, 2024
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Harry Kirk Mathews, Jr., Clifton Park, NY (US);

Stefan Joseph Cafaro, Chapel Hill, NC (US);

Brendon Leeker, Cincinnati, OH (US);

Kevin Graziano, Liberty Township, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/26 (2006.01); F02C 6/00 (2006.01); F02C 9/28 (2006.01); F02C 9/48 (2006.01); F02C 9/56 (2006.01);
U.S. Cl.
CPC ...
F02C 9/26 (2013.01); F02C 6/00 (2013.01); F02C 9/28 (2013.01); F02C 9/48 (2013.01); F02C 9/56 (2013.01);
Abstract

Systems and methods for high bandwidth control of thrust response for turbofan or turboprop engines are provided. Such systems and methods include an engine control system that processes a rate command and a feedback signal from an engine to generate separate fuel and electric machine control signals that respectively control fuel and electric machine dynamics of the engine to produce engine dynamics that result in desired thrust response.


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