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.

Patent No.:

US 10875626 B1

PDF
Full Text
Expired
Date of Patent:
Dec. 29, 2020

Filed:

Oct. 01, 2018
Applicant:

Textron Innovations Inc., Providence, RI (US);

Inventors:

Levi Charles Hefner, Wichita, KS (US);

Dakota Charles Easley, Dallas, TX (US);

Danielle Lynn Moore, Fort Worth, TX (US);

Assignee:

Textron Innovations Inc., Providence, RI (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/56 (2006.01); B64C 11/48 (2006.01); B64C 29/02 (2006.01); B64C 39/02 (2006.01); B64C 39/00 (2006.01); F16H 1/06 (2006.01);
U.S. Cl.
CPC ...
B64C 3/56 (2013.01); B64C 11/48 (2013.01); B64C 29/02 (2013.01); B64C 39/006 (2013.01); B64C 39/024 (2013.01); B64C 2201/021 (2013.01); B64C 2201/042 (2013.01); B64C 2201/088 (2013.01); B64C 2201/102 (2013.01); B64C 2201/108 (2013.01); B64C 2201/146 (2013.01); B64C 2201/165 (2013.01); F16H 1/06 (2013.01);
Abstract

A foldable wing system for an unmanned aerial system having a fuselage includes a left wing frame having an inboard gear rotatably coupled to the fuselage, a right wing frame having an inboard gear rotatably coupled to the fuselage and a wing actuator coupled to a linkage point on at least one of the wing frames. The wing frames are movable between a plurality of positions including a deployed position and a stowed position. The inboard gear of the left wing frame is engaged with the inboard gear of the right wing frame such that the wing frames move symmetrically between the plurality of positions in response to movement of the linkage point by the wing actuator.


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