logo

For the Inventor, By the Inventor

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 11851173 B1

PDFFull Text
Date of Patent:
Dec. 26, 2023

Filed:

Jan. 11, 2022

Vertical take-off and landing (vtol) winged air vehicle with complementary angled rotors

Applicant:

Aerovironment, Inc., Arlington, VA (US);

Inventors:

Henry Thome Won, Simi Valley, CA (US);

Quentin Lindsey, Canoga Park, CA (US);

Assignee:

AEROVIRONMENT, INC., Arlington, VA (US);

Attorneys:

Concept IP LLP

Michael Zarrabian

Eric Aagaard

Primary Examiner:

Philip J Bonzell

Int. Cl.
CPC ...
B64C 27/26 (2006.01); B64D 27/06 (2006.01); B64C 29/02 (2006.01); B64C 39/02 (2023.01); B64U 30/10 (2023.01); B64U 30/20 (2023.01); B64U 50/13 (2023.01); B64U 70/80 (2023.01);
U.S. Cl.
CPC ...
B64C 27/26 (2013.01); B64C 29/02 (2013.01); B64C 39/02 (2013.01); B64C 39/024 (2013.01); B64D 27/06 (2013.01); B64U 30/10 (2023.01); B64U 30/20 (2023.01); B64U 50/13 (2023.01); B64U 70/80 (2023.01);
Abstract

Systems, devices, and methods for an aircraft having a fuselage; a wing extending from both sides of the fuselage; a first pair of motors disposed at a first end of the wing; and a second pair of motors disposed at a second end of the wing; where each motor is angled to provide a component of thrust by a propeller attached thereto that for a desired aircraft movement applies a resulting torque additive to the resulting torque created by rotating the propellers.

Find Patent Forward Citations

Quick Actions:

Won, Henry. (2023). Vertical take-off and landing (vtol) winged air vehicle with complementary angled rotors (U.S. Patent No. 11851173). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/11851173

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

Loading…