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:
Mar. 26, 2019

Filed:

Jun. 16, 2016
Applicants:

Safran Electronics & Defense, Boulogne-Billancourt, FR;

Safran Electrical & Power, Blagnac, FR;

Inventors:

Serge Roques, Blagnac, FR;

Francois Guillot, Boulogne-Billancourt, FR;

Assignees:

SAFRAN ELECTRONICS & DEFENSE, Boulogne-Billancourt, FR;

SAFRAN ELECTRICAL & POWER, Blagnac, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 25/24 (2006.01); B64C 25/40 (2006.01); B64C 25/34 (2006.01); B64C 25/42 (2006.01); B64C 25/12 (2006.01);
U.S. Cl.
CPC ...
B64C 25/24 (2013.01); B64C 25/34 (2013.01); B64C 25/405 (2013.01); B64C 25/42 (2013.01); B64C 2025/125 (2013.01); Y02T 50/823 (2013.01);
Abstract

The invention relates to an aircraft landing gear () comprising: —a leg () that can be pivotably connected to a load-bearing structure of the aircraft () in order for the landing gear () to be deployed and retracted; —a wheel () that is rotatable in relation to the leg (), and an electric motor () that can rotate the wheel () in relation to the leg (); —a transmission mechanism () designed to selectively transmit torque generated by the electric motor () to the wheel () in order to rotate the wheel in relation to the leg () or to the leg () in order to rotate the leg () in relation to the load-bearing structure of the aircraft () in order to deploy or retract the landing gear ().


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