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. 09, 2024

Filed:

Aug. 29, 2022
Applicant:

The Boeing Company, Chicago, IL (US);

Inventor:

Neal Van Huynh, Bellevue, WA (US);

Assignee:

The Boeing Company, Arlington, VA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 13/40 (2006.01); B64C 9/00 (2006.01); B64C 9/04 (2006.01); B64C 13/18 (2006.01); B64C 13/50 (2006.01); B64D 45/00 (2006.01); G05D 1/00 (2024.01);
U.S. Cl.
CPC ...
B64C 13/503 (2013.01); B64C 9/04 (2013.01); B64C 13/18 (2013.01); B64C 13/40 (2013.01); B64C 13/505 (2018.01); B64C 13/506 (2018.01); B64D 45/00 (2013.01); G05D 1/101 (2013.01); B64C 2009/005 (2013.01);
Abstract

Systems, methods, and apparatus for controlling aircraft roll operations are disclosed. An example system includes an aileron actuator including a mode selector valve to control fluid flow through the aileron actuator, and a valve spring coupled to the mode selector valve, the valve spring to adjust the mode selector valve from the active position to a block position, the block position to prevent fluid flow through the aileron actuator, a wing cable system coupled to the aileron actuator, a wing actuator coupled to the wing cable system, the wing actuator to control displacement of the aileron of the aircraft in response to the mode selector valve being in the block position, and a differential linkage coupled to the wing actuator and the aileron, the differential linkage to translate the displacement of the wing actuator into rotational movement to adjust the aileron from a first position to a second position.


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