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:
Oct. 08, 2024

Filed:

Oct. 28, 2020
Applicant:

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

Inventors:

Thomas Akers, Templeton, CA (US);

Peter Kalogiannis, Tehachapi, CA (US);

Mark Moore, Henderson, NV (US);

Robert Alan McDonald, San Luis Obispo, CA (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 27/52 (2006.01); B64C 29/00 (2006.01); B64C 29/02 (2006.01); B64U 10/25 (2023.01); B64U 30/20 (2023.01); B64U 50/19 (2023.01); B64U 70/80 (2023.01);
U.S. Cl.
CPC ...
B64C 29/02 (2013.01); B64C 27/52 (2013.01); B64C 29/0033 (2013.01); B64U 10/25 (2023.01); B64U 30/20 (2023.01); B64U 50/19 (2023.01); B64U 70/80 (2023.01);
Abstract

An aerial vehicle may have a fuselage, a first wing member, and a second wing member. The fuselage may have a nose end and a tail end. The first wing member may extend from the fuselage and comprise a first drive motor coupled to the first rotor. The second wing member may also extend from the fuselage substantially opposite the first wing member and may comprise a second drive motor coupled to a second rotor. A first motor may be coupled to rotate the first wing member and the first rotor about a first axis substantially perpendicular to a fuselage axis extending from the nose end to the tail end. A second motor may be coupled to rotate the second wing member and the second rotor about a second axis substantially perpendicular to the fuselage axis. A controller circuit may be configured to differentially actuate the first motor and the second motor.


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