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:
Oct. 31, 2017

Filed:

Oct. 07, 2015
Applicant:

Messier-bugatti-dowty, Velizy Villacoublay, FR;

Inventors:

Pierre-Yves Liegeois, Velizy-Villacoublay, FR;

Thierry Blanpain, Velizy-Villacoublay, FR;

Edouard Campbell, Velizy-Villacoublay, FR;

Assignee:

MESSIER-BUGATTI-DOWTY, Velizy Villacoublay, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 25/34 (2006.01); B64C 25/50 (2006.01);
U.S. Cl.
CPC ...
B64C 25/505 (2013.01); B64C 25/34 (2013.01); Y02T 50/54 (2013.01);
Abstract

The invention relates to an aircraft landing gear equipped with a steering device () for orienting the wheels (), the steering device () comprising a body () in which is incorporated an electromechanical actuator () equipped with an electric motor (). The landing gear is further equipped with damping means intended to limit the transmission of vibration from the wheel () to the rest of the landing gear () when the aircraft is on the ground. The body () of the steering device () is mounted with the ability to rotate with a limited amplitude of rotation. The damping means are mounted between the body () of the steering device () and the strut assembly () of the landing gear to damp the vibration between the body () of the steering device () and the strut assembly ().


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