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. 06, 2019

Filed:

Jun. 02, 2017
Applicant:

Aerovironment, Inc., Monrovia, CA (US);

Inventors:

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

Quentin Lindsey, Canoga Park, CA (US);

Assignee:

AEROVIRONMENT, INC., Monrovia, CA (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 39/02 (2006.01); B64C 27/26 (2006.01); B64C 29/02 (2006.01);
U.S. Cl.
CPC ...
B64C 27/26 (2013.01); B64C 39/02 (2013.01); B64C 39/024 (2013.01); B64C 29/02 (2013.01); B64C 2201/088 (2013.01); B64C 2201/104 (2013.01); B64C 2201/108 (2013.01); B64C 2201/165 (2013.01);
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. (2019). Vertical take-off and landing (vtol) winged air vehicle with complementary angled rotors (U.S. Patent No. 10370095). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10370095

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

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