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. 23, 2024

Filed:

Jun. 03, 2021
Applicant:

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

Inventors:

Kip Gregory Campbell, Hurst, TX (US);

Kristen Stuart, Fort Worth, TX (US);

Steven G. Hagerott, Wichita, KS (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 31/00 (2006.01); B64C 27/635 (2006.01); B64C 27/68 (2006.01); B64C 39/02 (2023.01); B64D 27/24 (2006.01); B64U 30/20 (2023.01); B64U 50/19 (2023.01);
U.S. Cl.
CPC ...
B64D 31/00 (2013.01); B64C 27/635 (2013.01); B64C 27/68 (2013.01); B64C 39/024 (2013.01); B64D 27/24 (2013.01); B64U 30/20 (2023.01); B64U 50/19 (2023.01); B64U 2201/00 (2023.01);
Abstract

A system can include a flight controller for an aircraft that includes an electric motor that drives blades with a variable pitch, where the flight controller receives a command to change a flight characteristic of the aircraft and creates a torque command and a revolutions per minute (RPM) command. The system can also include a propulsion assembly, where the propulsion assembly creates a current command based at least in part on the torque command and the RPM command, creates a blade pitch command based at least in part on the torque command and the RPM command, communicates the current command to the electric motor to change a mechanical output of the electric motor, and communicates the blade pitch command to blade actuators to control the pitch of the blades. The current command and the blade pitch command cause the blades of the aircraft to rotate at a predetermined RPM.


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