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:
Sep. 14, 2021

Filed:

Jul. 04, 2018
Applicant:

Aerhart, Llc, Malibu, CA (US);

Inventors:

Kevin Burns, Malibu, CA (US);

Diana Brehob, Dearborn, MI (US);

Assignee:

Aerhart, LLC, Malibu, CA (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/605 (2006.01); B64C 29/00 (2006.01); B64C 39/02 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0033 (2013.01); B64C 39/024 (2013.01); B64C 2201/02 (2013.01); B64C 2201/14 (2013.01); B64C 2201/165 (2013.01);
Abstract

An aeronautical apparatus is disclosed that has two pairs of wings. Each wing has a thrust-angle motor. A propeller and propeller motor are coupled to each thrust-angle motor. Propeller pitch is controlled by a propeller-pitch motor. The thrust-angle motor allows the propeller axis of rotation to be parallel to the fuselage's longitudinal axis; vertical (perpendicular to longitudinal axis, as in well-known fixed-position, four-propeller drones); and any position between as well as a given range exceeding these bounds which is used for control. An electronic control unit is electronically coupled to the thrust-angle motors, propeller motors, and propeller-pitch motors, which can be independently controlled, to provide the desired thrust and trajectory. Such an apparatus can provide efficient operation in vertical take-off/landing (hovering) and forward (translational) flight modes. Control surfaces, such as ailerons, which are provided on airplanes, are unnecessary due to the many degrees of freedom in control.


Find Patent Forward Citations

Burns, Kevin. (2021). Aeronautical apparatus (U.S. Patent No. 11117657). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/11117657

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

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