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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.

Patent No.:

US 12202595 B1

PDFFull Text
Date of Patent:
Jan. 21, 2025

Filed:

Dec. 01, 2023

Vtol aircraft using fixed forward canted rotors

Applicant:

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

Inventors:

Gregor Veble Mikic, Santa Cruz, CA (US);

JoeBen Bevirt, Santa Cruz, CA (US);

Alex Stoll, Santa Cruz, CA (US);

Assignee:

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

Attorney:

Michael A. Guth

Primary Examiner:

Nicholas McFall

Assistant Examiner:

Marisa V Conlon

Int. Cl.
CPC ...
B64C 27/26 (2006.01); B64C 3/10 (2006.01); B64C 3/32 (2006.01); B64C 27/22 (2006.01); B64C 29/00 (2006.01); B64C 39/06 (2006.01); B64C 27/82 (2006.01);
U.S. Cl.
CPC ...
B64C 27/26 (2013.01); B64C 3/10 (2013.01); B64C 3/32 (2013.01); B64C 27/22 (2013.01); B64C 29/0016 (2013.01); B64C 39/06 (2013.01); B64C 39/068 (2013.01); B64C 2027/8236 (2013.01);
Abstract

A vertical take-off and landing aircraft and method which uses fixed rotors for both VTOL and forward flight operations. The rotors are positioned to achieve a high span efficiency. The rotors are positioned to even out the lift across the span of the wing. The wing may also have narrow front and rear airfoils which may provide structural support as well as providing lift during forward flight, or may have a single center wing. The wing rotors are tilted forward and provide some forward propulsion during horizontal flight.

Find Patent Forward Citations

Quick Actions:

Mikic, Gregor. (2025). Vtol aircraft using fixed forward canted rotors (U.S. Patent No. 12202595). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12202595

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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