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. 31, 2022

Filed:

Nov. 19, 2019
Applicant:

Joby Aero, Inc., Santa Cruz, CA (US);

Inventors:

Robert Alan McDonald, San Luis Obispo, CA (US);

Mark Moore, Henderson, NV (US);

Ian Andreas Villa, San Francisco, CA (US);

Assignee:

Joby Aero, Inc., Santa Cruz, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 27/26 (2006.01); B64D 27/24 (2006.01); B64D 9/00 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0025 (2013.01); B64C 27/26 (2013.01); B64D 9/00 (2013.01); B64D 27/24 (2013.01);
Abstract

An aerial vehicle that uses motor pulsed-induced cyclic control is provided. In example embodiments, the aerial vehicle comprises a fuselage incorporating a battery system and a payload bay for operatively receiving and holding a payload and at least one mono-blade rotor coupled to an electric motor and an electric motor control system. The electric motor control system controls the electric motor using pulse-induced cyclic control. The aerial vehicle further includes at least one wing, at least one cruise propeller, and an avionics system. The avionic system is configured to transition the aerial vehicle between a vertical take-off and landing mode in which the at least one mono-blade rotor is primarily engaged to propel the aerial vehicle vertically and a cruising mode in which the at least one cruise propeller is primarily engaged to propel the aerial vehicle horizontally.


Find Patent Forward Citations

Loading…