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:
Sep. 17, 2024

Filed:

Oct. 13, 2022
Applicant:

General Electric Company, Schenectady, NY (US);

Inventor:

Vinod S. Kumar, Bengaluru, IN;

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/02 (2006.01); B64D 27/10 (2006.01); B64D 27/24 (2006.01); B64D 31/00 (2006.01); B64D 35/00 (2006.01); B64D 47/00 (2006.01); F02C 6/00 (2006.01); F02C 7/36 (2006.01);
U.S. Cl.
CPC ...
B64D 27/10 (2013.01); B64D 27/24 (2013.01); B64D 31/00 (2013.01); B64D 35/00 (2013.01); B64D 47/00 (2013.01); F02C 6/00 (2013.01); F02C 7/36 (2013.01); B64D 27/026 (2024.01);
Abstract

An aircraft includes a gas turbine engine, an electric motor, and a propulsion device. The gas turbine engine and the electric motor are configured to provide a target cumulative output to the propulsion device. An electronic control unit is configured to set the gas turbine engine to a first engine mode to provide a first engine output to the propulsion device, set the electric motor to a first motor mode to provide a first motor output to the propulsion device, a sum of the first engine output and the first motor output being within a predetermined range of the target cumulative output, and in response to a speed of the aircraft reaching a target speed and the first engine output increasing to a second engine output, set the electric motor to a second motor mode.


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