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:
Aug. 04, 2015

Filed:

Feb. 06, 2014
Applicant:

Nabtesco Corporation, Tokyo, JP;

Inventors:

Toshiaki Ogawa, Gifu, JP;

Koji Itoh, Gifu, JP;

Makoto Nagashima, Gifu, JP;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 13/00 (2006.01); F16H 21/44 (2006.01); B64C 13/28 (2006.01); B64C 13/24 (2006.01);
U.S. Cl.
CPC ...
F16H 21/44 (2013.01); B64C 13/00 (2013.01); B64C 13/24 (2013.01); B64C 13/28 (2013.01); Y02T 50/44 (2013.01); Y10T 74/18888 (2015.01);
Abstract

An actuator-link assembly includes an actuator having first and second opposing ends in order to drive a control surface of an aircraft and a link coupled to the actuator. The actuator has a rod portion having a tip end, located at first end of the actuator, said tip end pivotably attach to a control surface of an aircraft. The link includes a pair of linear portions, each having first and second opposing ends, wherein the linear portions are disposed alongside each other; a coupling portion connecting the first ends of linear portions, a fulcrum shaft attachment portion protruding from the coupling portion configured to pivotably attach to a fulcrum shaft for rotatably supporting the control surface; and an actuator attachment portion configured to pivotably attach to the second end of the actuator. A material constituting the linear portions and the coupling portion contains fiber reinforced plastic.


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