Airbus Operations (s.a.s.)

Airbus Atlantic

Airbus Operations Gmbh

Areva Nc

David Chartier

Lionel Diochon

Laurent Lafont

Isabelle Petrissans

Franck Darras

Jean-Michel Cetout

Damien Avril

Jennifer Sanchez-Canet

Michael Sarrato

Yannick Wattiez

Device for machining an end of an elementary panel for its subsequent friction stir welding, the elementary panel comprising a metal body defining two opposite faces, the machining device comprising a chassis, at least two guiding members configured to guide a first face of the elementary panel, at least one machining tool mounted on the chassis, the machining tool being positioned between the two guiding members and at least one pressure member mounted on the chassis and configured to exert a pressure on a second face of the elementary panel so as to press the elementary panel against the guiding members along the horizontal reference direction.

Device and method for the machining of an end of an elementary panel for its friction stir welding

A mount for an aircraft turbojet engine. The mount includes a central box formed by an assembly of two side panels joined via transverse ribs and two side boxes secured to a forward part of the box and arranged either side thereof, each side box including an aft closure frame. One of the ribs forming the box includes two side extensions made in a single piece with the rib and respectively projecting from the two side panels outwardly from the box, the two extensions being fixedly mounted on the frame of each of the two side boxes, respectively.

Turbojet engine mounting structure for aircraft

The invention relates to a turbojet suspension pylon for an aircraft, the pylon being provided with a rigid structure () comprising a longitudinal central box (). According to the invention, the rigid structure also comprises two lateral boxes () fixed to a forward part of said central box (), the pylon also comprising a first () and a second () engine forward suspension designed to resist forces applied along the longitudinal direction (X) of the pylon, these first and second suspensions being arranged on the two lateral boxes respectively.

Aircraft jet engine pylon suspension attachment

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Toulouse, France

David Chartier