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.:
Date of Patent:
Mar. 04, 2025
Filed:
Aug. 30, 2023
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:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/26 (2006.01); B64C 3/10 (2006.01); B64C 3/32 (2006.01); B64C 27/08 (2023.01); B64C 27/22 (2006.01); B64C 27/52 (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 27/08 (2013.01); B64C 27/22 (2013.01); B64C 27/52 (2013.01); B64C 29/0016 (2013.01); B64C 39/06 (2013.01); B64C 39/068 (2013.01); B64C 2027/8236 (2013.01); B64C 29/0025 (2013.01);
Abstract
A vertical take-off and landing aircraft which uses fixed rotors for both VTOL and forward flight operations. The wing rotors are tilted forward and provide some forward propulsion during horizontal flight. The rotors are positioned to achieve a high span efficiency. The rotors are positioned to even out the lift across the span of the synthetic wing. The synthetic wing may also have airfoils which may provide structural support for the rotors as well as providing lift during forward flight.