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:
Sep. 18, 2012

Filed:

Apr. 27, 2011
Applicants:

Mehul Patel, Chandler, AZ (US);

Thomas C. Corke, Granger, IN (US);

Inventors:

Mehul Patel, Chandler, AZ (US);

Thomas C. Corke, Granger, IN (US);

Assignees:

Orbital Research Inc., Cleveland, OH (US);

University of Notre Dame du Lac, Notre Dame, IN (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 23/00 (2006.01); B64C 21/00 (2006.01); F42B 15/01 (2006.01);
U.S. Cl.
CPC ...
Abstract

A method of controlling an aircraft, missile, munition or ground vehicle with plasma actuators, and more particularly of controlling fluid flow across their surfaces or other surfaces which would benefit from such a method, includes the design of an aerodynamic plasma actuator for the purpose of controlling airflow separation over a control surface of a aircraft, missile, or a ground vehicle, and a method of determining a modulation frequency for the plasma actuator for the purpose of fluid flow control over these vehicles. Various embodiments provide steps to increase the efficiency of aircraft, missiles, munitions and ground vehicles. The method of flow control reduces the power requirements of the aircraft, missile, munition and or ground vehicle. These methods also provide alternative aerodynamic control using low-power hingeless plasma actuator devices.


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