Safran Landing Systems

Alexandre Daulny

Thierry Blanpain

Nicolas Nguyen

Yves Courtois De Lourmel

Aurélie Soula

Patrice Palazzoli

Arnaud Caraty

The invention relates to a bar () for a braked aircraft wheel (), the bar being for fitting to a rim () of the wheel in order to drive rotor brake disks () in rotation. The bar comprises a substantially rectilinear body () having at least one segment () including two wings () connected together by a core () and intended to co-operate with the rotor disks. At least one brace element () connects a free edge of each of the wings to a central portion of the core.

Bar for a braked aircraft wheel

A landing gear includes structural parts arranged to connect a wheel to a structure of an aircraft, each structural part including two or more interfaces for connection to one or more other of the structural parts or to the structure of the aircraft and two or more webs which extend so as to face one another while delimiting between them a free space and which connect the two interfaces in order to transmit the forces from one to the other.

Landing gear with reinforcing web

Growing community of inventors

Moissy-Cramayel, France

Alexandre Daulny