Airbus Operations (s.a.s.)

Thomas Le Hetet

Jérôme Colmagro

Philippe Blot

Julien Guillemaut

Denis Soula

Dominique Guittard

Frédérick Cavaliere

Jerome Colmargo

Florian Musseau

A method for producing a central wing box having an upper panel, a lower panel, a front spar and a rear spar, the upper edges of said spars approximately parallel to an axis Y being connected by the upper panel, and the lower edges of said spars approximately parallel to the axis Y being connected by the lower panel. The method includes producing at least one panel and at least one spar from composite material in one piece.

Method for producing a central wing box

A process for the production of a structural part of an aircraft, whereby the part is made of composite material that includes a thermosetting resin and that has a section profile that can be stamped, whereby the process includes:

Method of producing a structural part made from a thermosetting resin by drawing

A process for the production of a core that can be used for the manufacturing of a part that is made of composite material, whereby the core consists of at least one powdered and/or granular product (), includes introducing the at least one powdered and/or granular product () by vibrating it in an outer envelope () placed in a device () having a cavity that is delimited by a wall () whose geometry is adapted to that of the core to be produced and flattening the outer envelope () against the wall (), characterized in that vibrations are emitted slightly above the fill level during filling.

Method of making a core comprising an envelope containing granular and/or powdery products, device and core obtained

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La Chevroliere, France

Thomas Le Hetet