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:
Jun. 28, 2016

Filed:

Jun. 25, 2013
Applicant:

Airbus Operations (Sas), Toulouse, FR;

Inventors:

Pierre Tieys, Tournefeuille, FR;

Alain Sagansan, Colomiers, FR;

Laurent Andrieu, Aucamville, FR;

Assignee:

AIRBUS OPERATIONS SAS, Toulouse, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 9/02 (2006.01); B64C 13/28 (2006.01); B64C 3/48 (2006.01); B64C 3/50 (2006.01);
U.S. Cl.
CPC ...
B64C 13/28 (2013.01); B64C 3/48 (2013.01); B64C 3/50 (2013.01); B64C 9/02 (2013.01); Y02T 50/44 (2013.01);
Abstract

A device for mechanically connecting a control surface to a fixed structural element of an aircraft, including a rotary actuator for driving an element that is securely connected to the control surface in rotation in relation to an element securely connected to the fixed structural element, around an articulation axis, as well as articulation elements for articulating this control surface around this axis. These articulation elements are able to support the control surface independently of the rotary actuator. This arrangement permits taking benefit from the advantageous properties of rotary actuators while allowing removal of the rotary actuator without having first to remove the control surface.


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