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:
May. 30, 2023

Filed:

Feb. 12, 2021
Applicant:

Bell Textron Inc., Fort Worth, TX (US);

Inventors:

Guy Bernard, Kirkland, CA;

Jeffrey Epp, Bedford, TX (US);

William K. Heironimus, Dallas, TX (US);

Assignee:

Textron Innovations Inc., Providence, RI (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 31/06 (2020.01); B64D 27/24 (2006.01); B64D 35/02 (2006.01); B60L 50/60 (2019.01); B60L 3/00 (2019.01);
U.S. Cl.
CPC ...
B64C 31/06 (2013.01); B60L 3/0061 (2013.01); B60L 50/60 (2019.02); B64D 27/24 (2013.01); B64D 35/02 (2013.01); B60L 2200/10 (2013.01);
Abstract

A propulsion system for providing propulsion of an aircraft includes a plurality of electric motors coupled with a rotor of the aircraft to drive the rotor and a propulsion motor control. The propulsion motor control includes at least one processor electrically connected with at least one electric motor to actuate the at least one electric motor and at least one battery electrically connected with the at least one processor and at least one electric motor to provide power to the at least one processor and the at least one electric motor. The propulsion motor control actuates the plurality of electric motors based on a desired torque level to drive the rotor to provide propulsion of the aircraft.


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