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:
Jul. 15, 2025

Filed:

Mar. 31, 2021
Applicant:

University of Florida Research Foundation, Inc., Gainesville, FL (US);

Inventors:

Subrata Roy, Gainesville, FL (US);

Sarthak Roy, Gainesville, FL (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 21/00 (2023.01); B64C 21/04 (2023.01); B64C 21/06 (2023.01); B64C 21/08 (2023.01); B64C 23/06 (2006.01); F15D 1/12 (2006.01); H05H 1/24 (2006.01);
U.S. Cl.
CPC ...
B64C 21/08 (2013.01); B64C 21/04 (2013.01); B64C 21/06 (2013.01); B64C 23/06 (2013.01); F15D 1/12 (2013.01); H05H 1/2439 (2021.05);
Abstract

The present disclosure presents systems, apparatuses, and methods of active flow controls for dissipating tip vortices. In this regard, a method comprises positioning one or more fan-shaped plasma actuators on an end surface of a tip of one or more airfoils of an aircraft, wherein the fan-shaped plasma actuators are surface compliant with the surface of the tip of the one or more airfoils; and activating the one or more fan-shaped plasma actuators during a flight of the aircraft, wherein at least one tip vortex generated by a flight of the aircraft is reduced by an introduction of one or more vortices generated by the one or more fan-shaped plasma actuators on the end surface of the tip of the one or more airfoils of the aircraft. Other systems, apparatuses, and methods are also presented.


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