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:
Oct. 22, 2019

Filed:

Jul. 18, 2017
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Neal Van Huynh, Bellevue, WA (US);

Matthew Alexander Moser, Everett, WA (US);

Patrick Joseph McCormick, Mukilteo, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/16 (2006.01); B64C 13/50 (2006.01); B64C 9/20 (2006.01); B64C 9/00 (2006.01); B64D 45/00 (2006.01); B64C 5/02 (2006.01); B64C 5/06 (2006.01);
U.S. Cl.
CPC ...
B64C 13/16 (2013.01); B64C 9/20 (2013.01); B64C 13/50 (2013.01); B64C 5/02 (2013.01); B64C 5/06 (2013.01); B64C 9/00 (2013.01); B64C 2009/005 (2013.01); B64D 2045/001 (2013.01);
Abstract

Methods, apparatus, and articles of manufacture for a distributed aircraft actuation system are disclosed. An example apparatus includes a collection engine to obtain first monitoring information corresponding to a first set of control surfaces of an aircraft, the first set including a first control surface on a first side of the aircraft and a second control surface on a second side of the aircraft, the second side opposite the first, and obtain second monitoring information corresponding to a second set of control surfaces of the aircraft, the second set including a third control surface on the first side and a fourth control surface on the second side. The example apparatus further includes a non-responsive component detector to determine if one of the control surfaces is non-responsive based on the first and the second monitoring information, and a command generator to deactivate the first set when the non-responsive component detector determines that the first control surface is non-responsive while the second set remains active.


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