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. 18, 2022

Filed:

Feb. 26, 2019
Applicant:

James Thomas Pike, Waterloo, CA;

Inventor:

James Thomas Pike, Waterloo, CA;

Assignee:

Other;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/26 (2006.01); B64C 27/08 (2006.01); B64C 25/32 (2006.01); B64C 39/02 (2006.01);
U.S. Cl.
CPC ...
B64D 27/26 (2013.01); B64C 25/32 (2013.01); B64C 27/08 (2013.01); B64C 39/024 (2013.01); B64C 2025/325 (2013.01); B64C 2201/024 (2013.01); B64C 2201/042 (2013.01); B64C 2201/108 (2013.01); B64C 2201/165 (2013.01); B64C 2201/20 (2013.01);
Abstract

The unmanned aerial vehicle (UAV) includes detachable motor arms. In this way, the UAV may be conveniently stored and transported, rapidly assembled in the field, and repaired in the event of a crash. The motor arms are also configured to separate from the fuselage in the event of a crash. An example unmanned aerial vehicle comprises: a fuselage and two motor arms. Each motor arm is detachably secured to the fuselage by two mechanical connectors and comprises a tube having a rotary wing propulsion system on each end and an electrical connector, positioned between the two rotary wing propulsion systems, configured to conductively interface with an electrical connector in an underside of the fuselage. The two mechanical connectors detachably securing each motor arm to the fuselage are configured to facilitate the separation of that motor arm from the fuselage during a crash.


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