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:
Jan. 25, 2022

Filed:

Aug. 12, 2020
Applicant:

Amazon Technologies, Inc., Seattle, WA (US);

Inventors:

Gur Kimchi, Seattle, WA (US);

Dominic Timothy Shiosaki, Seattle, WA (US);

Ricky Dean Welsh, Seattle, WA (US);

Assignee:

Amazon Technologies, Inc., Seattle, WA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 25/26 (2006.01); B64C 17/02 (2006.01); B64C 25/10 (2006.01); B64C 25/52 (2006.01); B64C 27/52 (2006.01); B64C 39/02 (2006.01); B64D 31/06 (2006.01);
U.S. Cl.
CPC ...
B64C 25/26 (2013.01); B64C 17/02 (2013.01); B64C 25/10 (2013.01); B64C 25/52 (2013.01); B64C 27/52 (2013.01); B64C 39/024 (2013.01); B64D 31/06 (2013.01); B64C 2201/027 (2013.01);
Abstract

Aerial vehicles may be configured to control their attitudes by changing one or more physical attributes. For example, an aerial vehicle may be outfitted with propulsion motors having repositionable mounts by which the motors may be rotated about one or more axes, in order to redirect forces generated by the motors during operation. An aerial vehicle may also be outfitted with one or more other movable objects such as landing gear, antenna and/or engaged payloads, and one or more of such objects may be translated in one or more directions in order to adjust a center of gravity of the aerial vehicle. By varying angles by which forces are supplied to the aerial vehicle, or locations of the center of gravity of the aerial vehicle, a desired attitude of the aerial vehicle may be maintained irrespective of velocity, altitude and/or forces of thrust, lift, weight or drag acting upon the aerial vehicle.


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