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. 29, 2019

Filed:

Nov. 30, 2017
Applicant:

The United States of America, As Represented BY the Administrator of Nasa, Washington, DC (US);

Inventors:

Michael D. Patterson, Yorktown, VA (US);

Jesse R. Quinlan, Yorktown, VA (US);

William J. Fredericks, Williamsburg, VA (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 37/02 (2006.01); B64C 39/02 (2006.01); B64C 29/00 (2006.01); B64C 3/00 (2006.01); B64D 37/04 (2006.01); B64C 9/00 (2006.01);
U.S. Cl.
CPC ...
B64C 37/02 (2013.01); B64C 3/00 (2013.01); B64C 29/0033 (2013.01); B64C 39/024 (2013.01); B64C 9/00 (2013.01); B64C 2201/021 (2013.01); B64C 2201/042 (2013.01); B64C 2201/104 (2013.01); B64C 2201/108 (2013.01); B64C 2201/128 (2013.01); B64C 2201/146 (2013.01); B64C 2201/165 (2013.01); B64C 2211/00 (2013.01); B64D 37/04 (2013.01);
Abstract

A modular Unmanned Aerial System (UAS) includes an Unmanned Aerial Vehicle (UAV) parent module and UAV child modules. A main wing extends from a respective fuselage of the modules. The UAS includes docking mechanisms coupled to wingtips of the main wings. The child modules dock with the wingtips of the parent or an adjacent child module. Docking forms a linked-flight configuration, with undocking and separation from the parent or adjacent child module achieving an independent-flight configuration. The modules have booms arranged transverse to the main wings and parallel to the longitudinal axis, as well as front and rear rotors/propellers. The front and rear propellers have axes of rotation that are normal to a plane of the longitudinal axis in a vertical takeoff and landing (VTOL) configuration, with the axis of rotation of the rear propellers parallel to the longitudinal axis in a forward-flight configuration.


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