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:
Nov. 07, 2017

Filed:

May. 21, 2015
Applicant:

Safran Electronics & Defense, Boulogne-Billancourt, FR;

Inventors:

Louis Chavignier, Boulogne-Billancourt, FR;

Marc Lebrun, Boulogne-Billancourt, FR;

Severin Viennot, Boulogne-Billancourt, FR;

Assignee:

SAFRAN ELECTRONICS & DEFENSE, Boulogne-Billancourt, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/28 (2006.01); F16H 25/20 (2006.01); F16H 25/24 (2006.01);
U.S. Cl.
CPC ...
B64C 13/28 (2013.01); F16H 25/205 (2013.01); F16H 25/2015 (2013.01); F16H 25/2454 (2013.01);
Abstract

The invention relates to an actuator () for controlling a flight control surface () of an aircraft, comprising:—a primary route () comprising a first member () for generating a first torque, and a first drive shaft () having an end () able to be connected to the first member () and an end () able to be connected to the control surface (),—a secondary route () comprising a second member () for generating a second torque and a second drive shaft () having an end () able to be connected to the second member () and an end () able to be connected to the control surface (), in which actuator the second drive shaft () is hollow and extends around the first drive shaft ().


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