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:
Oct. 25, 2022

Filed:

Dec. 20, 2018
Applicant:

The Texas A&m University System, College Station, TX (US);

Inventors:

Moble Benedict, College Station, TX (US);

David A. Coleman, Bryan, TX (US);

Assignee:

The Texas A&M University System, College Station, TX (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 33/02 (2006.01); B64C 3/18 (2006.01); B64C 3/26 (2006.01); B64C 13/18 (2006.01); B64C 19/02 (2006.01); B64D 27/24 (2006.01); F16H 21/40 (2006.01);
U.S. Cl.
CPC ...
B64C 33/02 (2013.01); B64C 3/185 (2013.01); B64C 3/26 (2013.01); B64C 13/18 (2013.01); B64C 19/02 (2013.01); B64D 27/24 (2013.01); F16H 21/40 (2013.01);
Abstract

A flapping-wing aircraft includes a support frame, a motor coupled to the support frame, a pair of wings coupled to the support frame, and a linkage assembly coupled to the support frame and configured to translate an output torque of the motor into flapping motion of the wings, wherein the linkage assembly includes a first link coupled to a rotational output of the motor, a second link pivotably coupled to the first link at a first pivot joint, a third link pivotably coupled to the second link at a second pivot joint, and a fourth link pivotably coupled to the support frame and slidably coupled to the third link, and wherein the fourth link is coupled to a first wing of the pair of wings.


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