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:
Apr. 28, 2020

Filed:

Dec. 06, 2016
Applicant:

Aai Corporation, Hunt Valley, MD (US);

Inventor:

Neal H. Willford, Andover, KS (US);

Assignee:

AAI Corporation, Hunt Valley, MD (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/50 (2006.01); B64C 39/02 (2006.01); B64C 25/34 (2006.01); B64C 29/02 (2006.01); B64D 17/80 (2006.01); G05D 1/00 (2006.01); G05D 1/08 (2006.01);
U.S. Cl.
CPC ...
B64C 39/024 (2013.01); B64C 25/34 (2013.01); B64C 27/50 (2013.01); B64C 29/02 (2013.01); B64D 17/80 (2013.01); G05D 1/0055 (2013.01); G05D 1/0816 (2013.01); G05D 1/0858 (2013.01); B64C 2201/021 (2013.01); B64C 2201/042 (2013.01); B64C 2201/088 (2013.01); B64C 2201/104 (2013.01); B64C 2201/108 (2013.01); B64C 2201/162 (2013.01); B64C 2201/165 (2013.01);
Abstract

A technique is directed to operating an unmanned aerial vehicle (UAV) having a fuselage defining a flight direction of the UAV and wing-plate assemblies that propel the UAV in the flight direction defined by the fuselage. The technique involves providing, while the flight direction defined by fuselage of the UAV points vertically from a takeoff location on the ground, thrust from propulsion units of the wing-plate assemblies to fly the UAV along a vertical takeoff path. The technique further involves maneuvering, after the UAV flies along the vertical takeoff path, the UAV to align the flight direction along a horizontal flight path that is perpendicular to the vertical takeoff path. The technique further involves providing, after the UAV flies along the horizontal flight path, thrust from the propulsion units of the wing-plate assemblies to land the UAV along a vertical landing path that is perpendicular to the horizontal flight path.


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