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. 11, 2022

Filed:

Jul. 01, 2020
Applicant:

Aerovironment, Inc., Simi Valley, CA (US);

Inventors:

Christopher E. Fisher, Simi Valley, CA (US);

Phillip T. Tokumaru, Thousand Oaks, CA (US);

Marc L. Schmalzel, Simi Valley, CA (US);

John Peter Zwaan, Simi Valley, CA (US);

Jeremy D. Tyler, Thousand Oaks, CA (US);

Justin B. McAllister, Seattle, WA (US);

Gabriel E. Torres, Seattle, WA (US);

Pavel Belik, Simi Valley, CA (US);

Assignee:

AeroVironment, Inc., Simi Valley, CA (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 39/00 (2006.01); B60K 1/04 (2019.01); B60K 1/00 (2006.01); B64D 27/00 (2006.01); B63H 21/17 (2006.01); B63G 8/08 (2006.01); B60K 7/00 (2006.01); B60K 17/356 (2006.01); A63H 27/00 (2006.01); B64C 27/00 (2006.01); B64C 39/02 (2006.01); B64D 27/24 (2006.01); B63B 35/00 (2020.01); B63G 8/00 (2006.01);
U.S. Cl.
CPC ...
B60K 1/04 (2013.01); A63H 27/12 (2013.01); B60K 1/00 (2013.01); B60K 7/0007 (2013.01); B60K 17/356 (2013.01); B63G 8/08 (2013.01); B63H 21/17 (2013.01); B64C 27/00 (2013.01); B64C 39/024 (2013.01); B64D 27/00 (2013.01); B64D 27/24 (2013.01); B60K 2007/0092 (2013.01); B60Y 2200/52 (2013.01); B63B 2035/008 (2013.01); B63G 2008/005 (2013.01); B64C 2201/027 (2013.01); B64C 2201/042 (2013.01); B64C 2201/108 (2013.01);
Abstract

A quadrotor UAV including ruggedized, integral-battery, load-bearing body, two arms on the load-bearing body, each arm having two rotors, a control module mounted on the load-bearing body, a payload module mounted on the control module, and skids configured as landing gear. The two arms are replaceable with arms having wheels for ground vehicle use, with arms having floats and props for water-surface use, and with arms having pitch-controlled props for underwater use. The control module is configured to operate as an unmanned aerial vehicle, an unmanned ground vehicle, an unmanned (water) surface vehicle, and an unmanned underwater vehicle, depending on the type of arms that are attached.


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