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:
Dec. 16, 2025

Filed:

Dec. 29, 2023
Applicant:

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

Inventors:

Joeben Bevirt, Santa Cruz, CA;

Alex Stoll, Santa Cruz, CA (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 11/28 (2006.01); B64C 29/00 (2006.01); B64C 39/06 (2006.01); B64D 27/31 (2024.01); B64D 27/34 (2024.01); B64D 27/357 (2024.01);
U.S. Cl.
CPC ...
B64C 11/28 (2013.01); B64C 29/0033 (2013.01); B64C 39/068 (2013.01); B64D 27/31 (2024.01); B64D 27/34 (2024.01); B64D 27/357 (2024.01); Y02T 50/60 (2013.01);
Abstract

An aerial vehicle adapted for vertical takeoff and landing using a set of wing mounted thrust producing elements for takeoff and landing. An aerial vehicle which is adapted to vertical takeoff with the rotors in a rotated, take-off attitude then transitions to a horizontal flight path, with the rotors rotated to a typical horizontal configuration. The aerial vehicle may have deployment mechanisms which deploy electric motor driven propellers from a forward facing to a vertical orientation. The deployment mechanisms deploy the rotor forward and up as they deploy from a forward flight configuration to a vertical thrust configuration. A single motor may drive two co-axial propellers, with a first propeller driven when the motor spins in a first direction, and a second propeller driven when the motor spins in a second direction.


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