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:
Aug. 25, 2026

Filed:

Dec. 30, 2025
Applicant:

Archer Aviation Inc., San Jose, CA (US);

Inventors:

William Martin Waide, Central Point, OR (US);

Abraham Karem, Santa Ana, CA (US);

Assignee:

Archer Aviation Inc., San Jose, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 3/10 (2006.01); B64C 3/16 (2006.01); B64C 5/02 (2006.01); B64C 9/18 (2006.01); B64C 13/18 (2006.01); B64C 39/12 (2006.01); B64D 27/34 (2024.01); B64D 35/021 (2024.01); B64F 5/00 (2017.01);
U.S. Cl.
CPC ...
B64C 29/0033 (2013.01); B64C 3/10 (2013.01); B64C 3/16 (2013.01); B64C 5/02 (2013.01); B64C 9/18 (2013.01); B64C 13/18 (2013.01); B64C 39/12 (2013.01); B64D 27/34 (2024.01); B64D 35/021 (2024.01); B64F 5/00 (2013.01);
Abstract

'Apparatus, systems, and methods are contemplated for electric powered vertical takeoff and landing (eVTOL) aircraft engineered to carry safely carry at least 500 pounds (approx. 227 kg). It is contemplated that one or more rotors generate a significant amount of lift (e.g., 70%) during rotorborne flight (e.g., vertical takeoff, hover, etc), and tilt to provide forward propulsion during wingborne flight. The rotors preferably employ individual blade control, and are powered by electric motors supplied by dedicated batteries. The aircraft may include a fuselage, at least one wing, and a nacelle assembly comprising a static portion and a tilting portion. The tilting portion supports multiple electric motors and a rotor, all configured to tilt together for transition between flight modes. Separate batteries are positioned within the wing and nacelle to power respective motors.'


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