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. 20, 2016

Filed:

Jul. 01, 2008
Applicants:

Donald V. Drouin, Jr., O'Fallon, IL (US);

Scott Lee Schwimley, Foristell, MO (US);

Inventors:

Donald V. Drouin, Jr., O'Fallon, IL (US);

Scott Lee Schwimley, Foristell, MO (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G06F 17/00 (2006.01); B64C 21/00 (2006.01); B64C 23/00 (2006.01); H05H 1/24 (2006.01);
U.S. Cl.
CPC ...
B64C 23/005 (2013.01); H05H 1/2406 (2013.01); B64C 2230/12 (2013.01); Y02T 50/166 (2013.01);
Abstract

Systems and methods for alleviating aircraft loads with plasma actuators are disclosed. A method for operating an aircraft in accordance with a particular embodiment includes receiving an input corresponding to an aircraft component structural response to an aerodynamic load. The method can further include, based at least in part on the input corresponding to the aircraft component's structural response, reducing the structural response to the aerodynamic load by activating at least one plasma actuator carried by the aircraft, in accordance with one or more activation parameters.


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