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:
May. 09, 2017

Filed:

May. 01, 2014
Applicant:

Airbus Helicopters, Marignane, FR;

Inventors:

Boris Grohmann, Munich, DE;

Thomas Buro, Marseilles, FR;

Assignee:

Airbus Helicopters, Marignane, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 13/00 (2006.01); B64C 13/50 (2006.01); F16H 3/72 (2006.01); B64C 13/42 (2006.01); B64C 27/82 (2006.01);
U.S. Cl.
CPC ...
B64C 13/50 (2013.01); B64C 13/42 (2013.01); B64C 13/503 (2013.01); F16H 3/724 (2013.01); B64C 2027/8281 (2013.01);
Abstract

A control system () for controlling pitching stabilizer means of an aircraft, said system () being provided with at least one outlet shaft () and with a first actuator () and a second actuator (). The first and second actuators (and) are different, and the first actuator () is a slow actuator having a first driving portion that moves at a first speed, the second actuator () being a fast actuator having a second driving portion that moves at a second speed faster than the first speed, said control system () comprising a control device () connected to the first actuator () and to the second actuator () in order to cause said outlet shaft () to be driven either by the first driving portion () and/or by the second driving portion ().


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