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:
Nov. 21, 2017

Filed:

Jul. 14, 2014
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Abraham J. Pachikara, Bothell, WA (US);

Matthew A. Moser, Marysville, WA (US);

Paul H. Carpenter, Renton, WA (US);

Michael R. Finn, Kirkland, WA (US);

Thomas S. Koch, Seattle, WA (US);

Stefan R. Bieniawski, Seattle, WA (US);

Brian T. Whitehead, Renton, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/16 (2006.01); B64C 9/12 (2006.01); G05D 1/08 (2006.01); B64C 3/44 (2006.01); B64C 9/00 (2006.01); B64D 45/00 (2006.01);
U.S. Cl.
CPC ...
B64C 13/16 (2013.01); B64C 3/44 (2013.01); B64C 9/00 (2013.01); B64C 9/12 (2013.01); B64D 45/0005 (2013.01); G05D 1/0825 (2013.01); Y02T 50/32 (2013.01); Y02T 50/44 (2013.01);
Abstract

Closed loop control of control surfaces is described herein. One disclosed example method includes measuring a flight metric of an aircraft during flight and calculating, using a processor, a deflection of a control surface of the aircraft based on the flight metric. The disclosed example method also includes adjusting the deflection to an effective deflection level based on the calculated deflection to reduce a drag coefficient of the aircraft.


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