Safran Landing Systems

Florent Dauphin

Florent Fortier

Sébastien Dubois

Sebastien Dubois

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.

Method for protecting the landing gear of an aircraft against impacts that may affect it

A landing-gear assembly () for an aircraft, the landing-gear assembly comprising: The first secondary damper () is carried by the axle shaft () and comprises:

Landing-gear assembly for an aircraft, the landing-gear assembly including a secondary shimmy damper

Aircraft landing gear () comprising: The first secondary damper () is carried by the first strut part () and comprises:

Growing community of inventors

Velizy Villacoublay, France

Florent Dauphin