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:
Jul. 09, 2019

Filed:

Oct. 25, 2017
Applicant:

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

Inventors:

Pragyana K. Mishra, Seattle, WA (US);

Dushyant Goyal, Seattle, WA (US);

Assignee:

AMAZON TECHNOLOGIES, INC., Seattle, WA (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
G06Q 10/08 (2012.01); B64D 1/12 (2006.01); G05D 1/10 (2006.01); H04B 7/185 (2006.01); B64C 39/02 (2006.01); B64D 47/08 (2006.01); G08G 5/00 (2006.01);
U.S. Cl.
CPC ...
B64D 1/12 (2013.01); B64C 39/024 (2013.01); B64D 47/08 (2013.01); G05D 1/105 (2013.01); G06Q 10/0832 (2013.01); G08G 5/0021 (2013.01); G08G 5/0034 (2013.01); G08G 5/0069 (2013.01); G08G 5/0086 (2013.01); G08G 5/0091 (2013.01); H04B 7/18506 (2013.01); B64C 2201/128 (2013.01); B64C 2201/141 (2013.01);
Abstract

Directed fragmentation of an unmanned aerial vehicle (UAV) is described. In one embodiment, the UAV includes various components, such one or more motors, batteries, sensors, a housing, casing or shell, and a payload for delivery. Additionally, the UAV includes a controller. The controller determines a flight path and controls a flight operation of the UAV. During the flight operation, the controller develops a release timing and a release location for one or more of the components based on the flight path, the flight conditions, and terrain topology information, among other factors. The controller can also detect a disruption in the flight operation of the UAV and, in response, direct fragmentation of one or more of the components apart from the UAV. In that way, a controlled, directed fragmentation of the UAV can be accomplished upon any disruption to the flight operation of the UAV.


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