Airbus Operations (s.a.s.)

Jacques Demange

Michael Berjot

Rémi Lansiaux

Germain Gueneau

William Bras

Sébastien Van Arendonk

Sébastien Commenge

A linking device connecting an aircraft engine and a primary structure of an aircraft pylon, comprising a support connected to the primary structure, a spreader having a central part connected to the support and a first and a second end that are connected to thrust rods, at least one limiting system for limiting the travel of the spreader having an upper and a lower stop between which is positioned the first or second end of the spreader, the upper and the lower stop being connected to one another so as to form a single part connected to a fitting secured to the support.

Device for connecting an aircraft engine and a primary structure of an aircraft pylon comprising a rudder and a system for limiting the displacement of the rudder incorporating a double stop, aircraft comprising such a device

Growing community of inventors

Toulouse, France

Jacques Demange