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:
Mar. 08, 2022

Filed:

Mar. 18, 2019
Applicant:

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

Inventors:

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

Mark Moore, San Francisco, CA (US);

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

Henry Thome Won, Los Osos, CA (US);

Adam Chase, San Luis Obispo, CA (US);

Alex Michael Gary, San Luis Obispo, CA (US);

Cory Seubert, San Luis Obispo, CA (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 23/00 (2006.01); B64C 5/08 (2006.01); B64C 9/00 (2006.01); B64D 11/06 (2006.01); B64D 27/24 (2006.01); B64F 1/36 (2017.01); B64C 3/16 (2006.01); B64C 25/06 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0025 (2013.01); B64C 5/08 (2013.01); B64C 9/00 (2013.01); B64C 23/00 (2013.01); B64D 11/0601 (2014.12); B64D 27/24 (2013.01); B64C 3/16 (2013.01); B64C 25/06 (2013.01); B64C 2009/005 (2013.01); B64F 1/362 (2013.01);
Abstract

A vertical takeoff and landing (VTOL) aircraft, configured to transport passengers and/or cargo, uses propellers during vertical flight and wings during forward flight to generate lift. The VTOL aircraft includes a front wing and a rear wing connected by inboard booms. The rear wing may include a wingtip boom attached to each free end of the wing. A propeller may be attached to each inboard boom and each wingtip boom. The propellers attached to the inboard booms may be stacked propellers including at least two co-rotating propellers. The aircraft can also include a cruise propeller attached to the tail region of the fuselage, where the cruise propeller is configured to rotate in a plane approximately perpendicular to the fuselage to generate thrust during forward flight.


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