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:
Aug. 12, 2025

Filed:

Mar. 31, 2023
Applicant:

Beta Air Llc, South Burlington, VT (US);

Inventors:

Kyle Brookes, Richmond, VT (US);

Collin Freiheit, Burlington, VT (US);

Nicholas Moy, Burlington, VT (US);

Daniel Spira, Beaconsfield, CA;

Assignee:

BETA AIR LLC, South Burlington, VT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 31/06 (2024.01); B64C 11/34 (2006.01); B64D 27/24 (2024.01); B64U 50/19 (2023.01); B64U 10/20 (2023.01);
U.S. Cl.
CPC ...
B64D 31/06 (2013.01); B64D 27/24 (2013.01); B64C 11/34 (2013.01); B64U 10/20 (2023.01); B64U 50/19 (2023.01);
Abstract

A system and a method for controlling a propulsor assembly of an electric aircraft. The system may include an electric motor, wherein the electric motor may include a rotor and a stator, a propulsor driven by the electric motor configured to propel an electric aircraft. The propulsor may include a propeller. The propeller may include a blade. The system may include a cyclic control assembly configured to deflect the blade. The cyclic control assembly may include an actuator and a push rod mechanically connected to the actuator and the propulsor. The system may include a flight controller. The flight controller may be configured to receive sensor datum from at least a sensor communicatively connected to the electric aircraft, generate a deflection command as a function of the sensor datum and actuate the cyclic control assembly as a function of the deflection command.


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