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. 17, 2021

Filed:

Jun. 14, 2018
Applicant:

Wing Aviation Llc, Mountain View, CA (US);

Inventors:

Kevin Jenkins, Dixon, CA (US);

Jacob Huffman, Cupertino, CA (US);

Nicolas Renold, San Jose, CA (US);

Cameron Fitchener, Mountain View, CA (US);

Assignee:

Wing Aviation LLC, Mountain View, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 39/04 (2006.01); B64C 39/02 (2006.01); B64D 31/06 (2006.01); G05D 1/04 (2006.01); G05D 1/08 (2006.01);
U.S. Cl.
CPC ...
B64C 39/024 (2013.01); B64C 29/0025 (2013.01); B64C 39/04 (2013.01); B64D 31/06 (2013.01); G05D 1/042 (2013.01); G05D 1/0808 (2013.01); B64C 2201/021 (2013.01); B64C 2201/024 (2013.01); B64C 2201/108 (2013.01); B64C 2201/162 (2013.01);
Abstract

An aerial vehicle includes an airframe; vertical propulsion units, and a controller. The vertical propulsion units are mounted to the airframe and include propellers oriented to provide vertical propulsion to the aerial vehicle. The vertical propulsion units are physically organized in quadrants on the airframe with each of the quadrants including two or more of the vertical propulsion units. The controller is coupled to the vertical propulsion units to control operation of the vertical propulsion units. At least two of the vertical propulsion units in each of the quadrants are adapted to counter-rotate from each other during flight of the aerial vehicle.


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