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:
Mar. 22, 2016

Filed:

Feb. 17, 2012
Applicants:

Jayant Ratti, Atlanta, GA (US);

Emanuel Jones, Atlanta, GA (US);

George Vachtsevanos, Marietta, GA (US);

Inventors:

Jayant Ratti, Atlanta, GA (US);

Emanuel Jones, Atlanta, GA (US);

George Vachtsevanos, Marietta, GA (US);

Assignee:
Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 33/00 (2006.01); B64C 33/02 (2006.01);
U.S. Cl.
CPC ...
B64C 33/025 (2013.01); B64C 33/02 (2013.01);
Abstract

Multi-wing hovering and gliding flapping Micro Air Vehicles ('MAV') are disclosed. The MAV can have independent wing control to provide enhance energy efficiency and high maneuverability. Power to each wing can be controlled separately by varying the amplitude of the wing flapping, the frequency of the wing flapping, or both. The flapping frequency can be controlled such that it is at or near the natural frequency of the wings for improved energy efficiency. The wings can be controlled by a gear train, coil-magnet arrangement or many other actuation systems that enable variable frequency flapping, variable amplitude flapping, or a combination of both. The gear train mechanism provides gyroscopic stability during flight. The wing flapping can include a rotation, or feathering motion, for improved efficiency. The wings can be transitioned between flapping flight and fixed wing flight to enable gliding and hovering in a single configuration.


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