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. 08, 2020

Filed:

Nov. 01, 2017
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Seiya Sakurai, Seattle, WA (US);

Mark S. Good, Seattle, WA (US);

Lisa Schleuter, Mukilteo, WA (US);

Kelly T. Jones, Snohomish, WA (US);

Gregory M. Santini, Bothell, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 9/06 (2006.01); B64C 9/02 (2006.01); B64C 9/18 (2006.01); B64C 9/32 (2006.01);
U.S. Cl.
CPC ...
B64C 9/06 (2013.01); B64C 9/02 (2013.01); B64C 9/18 (2013.01); B64C 9/323 (2013.01);
Abstract

A system for mechanical operation of an aircraft wing includes a torque tube rotatable at a first rate of rotation to cause a downward rotation of a control surface relative to the aircraft wing. A gearing assembly including an output shaft is coupled to the torque tube. The torque tube is configured to rotate the output shaft, via the gearing assembly, at a second rate of rotation less than the first rate of rotation. A rotational member is coupled to the output shaft, and the output shaft is configured to drive a rotation of the rotational member. A first end of a linear actuator is coupled to the rotational member at a forward attach point, which is eccentric to a rotational center of the rotational member. The rotational member is rotatable to cause a translation of the forward attach point relative to the aircraft wing.


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