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. 05, 2026

Filed:

Jun. 29, 2023
Applicant:

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

Inventors:

Mark Moore, San Francisco, CA (US);

John Conway Badalamenti, San Francisco, CA (US);

Ian Villa, San Francisco, CA (US);

Adam Warmoth, San Francisco, CA (US);

David Josephson, Santa Cruz, CA (US);

Assignee:

JOBY AERO, INC, Santa Cruz, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 17/02 (2006.01); B64C 17/08 (2006.01); B64D 9/00 (2006.01); B64D 11/00 (2006.01); B64D 11/06 (2006.01); G01G 19/07 (2006.01); G06Q 10/08 (2024.01); G06Q 50/47 (2024.01);
U.S. Cl.
CPC ...
B64C 17/08 (2013.01); B64C 17/02 (2013.01); B64C 29/0016 (2013.01); B64D 9/00 (2013.01); B64D 11/003 (2013.01); B64D 11/0639 (2014.12); B64D 11/0649 (2014.12); G06Q 10/08 (2013.01); G06Q 50/47 (2024.01); G01G 19/07 (2013.01);
Abstract

Vertical take-off and landing (VTOL) aircraft can provide opportunities to incorporate aerial transportation into transportation networks for cities and metropolitan areas. However, VTOL aircraft can be sensitive to uneven weight distributions, e.g., the payload of an aircraft is primarily loaded in the front, back, left, or right. When the aircraft is loaded unevenly, the center of mass of the aircraft may shift substantially enough to negatively impact performance of the aircraft. Thus, in turn, there is an opportunity that the VTOL may be loaded unevenly if seating, luggage placement, and/or positions of internal components are not coordinated. This application describes systems and methods for dynamically assigning payloads and adjusting components of the VTOL aircraft.


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