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:
Aug. 05, 2025

Filed:

Dec. 17, 2019
Applicant:

Safran Landing Systems, Velizy Villacoublay, FR;

Inventors:

Florent Fortier, Moissy-Cramayel, FR;

Sébastien Dubois, Moissy-Cramayel, FR;

Florent Dauphin, Moissy-Cramayel, FR;

Assignee:

SAFRAN LANDING SYSTEMS, Velizy Villacoublay, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 25/20 (2006.01); B64C 25/24 (2006.01); F16C 41/00 (2006.01);
U.S. Cl.
CPC ...
B64C 25/20 (2013.01); B64C 25/24 (2013.01); F16C 41/004 (2013.01); F16C 2326/43 (2013.01);
Abstract

A method for protecting the landing gear of an aircraft against stroke-end shocks, the landing gear being manoeuvrable between a retracted position and a deployed position by means of a single electromechanical operating actuator () between these two positions. According to the invention, the method involves the step of equipping the electromechanical operating actuator with an internal damping device () arranged between an output shaft () of the electromechanical actuator coupled to the landing gear and a motor shaft () with a motor () of the electromechanical actuator.


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