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:
Dec. 22, 2015

Filed:

Jun. 25, 2015
Applicants:

Gaofei Yan, Hallandale, FL (US);

James Dees, Sunrise, FL (US);

Inventors:

Gaofei Yan, Hallandale, FL (US);

James Dees, Sunrise, FL (US);

Assignee:

Other;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/08 (2006.01); B64C 1/08 (2006.01); B64C 1/06 (2006.01); B64C 17/00 (2006.01); A63H 27/00 (2006.01);
U.S. Cl.
CPC ...
B64C 1/08 (2013.01); A63H 27/12 (2013.01); B64C 1/061 (2013.01); B64C 17/00 (2013.01);
Abstract

An aeronautical vehicle that rights itself from an inverted state to an upright state has a self-righting frame assembly has an apex preferably at a top of a central vertical axis. The apex provides initial instability to begin a self-righting process when the vehicle is inverted on a surface. A lift and stabilization panel extends across an upper portion of said frame to provide lift, drag and/or stability. A propulsion system can be located within a central void of the frame assembly and oriented to provide a lifting force. An electronics assembly is also carried by the self-righting frame for receiving remote control commands and is communicatively interconnected to the power supply for remotely controlling the aeronautical vehicle to take off, to fly, and to land on a supporting surface. The frame provides self-righting functionality and protection of elements carried therein.


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