B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 3/20 (2006.01) B29D 99/00 (2010.01) B29C 70/08 (2006.01) B29C 70/30 (2006.01) B29D 24/00 (2006.01) B32B 3/06 (2006.01) B64C 3/18 (2006.01) B64C 3/26 (2006.01) B64C 3/28 (2006.01)
Patent
CA 2757910
The invention relates to a composite structuring panel (1) for the trailing edge of an aircraft element, having: an upper surface (3); a lower surface (5); an edge (7) connecting said upper (3) and lower (5) surfaces; the upper surface (3) and the lower surface (5) being connected by transverse stiffeners (9) and the structuring panel being made of a unitary part forming the upper surface (3), the lower surface (5), the edge (7), and the transverse stiffeners (9). The invention also relates to a method for manufacturing such a panel (1), and to an aircraft element comprising such a panel (1).
L'invention concerne un panneau structurant (1) composite de bord de fuite pour un élément d'un aéronef présentant : - une surface supérieure (3); - une surface inférieure (5); - un bord (7) reliant lesdites surfaces supérieure (3) et inférieure (5); la surface supérieure (3) et la surface inférieure (5) étant reliées par des raidisseurs transversaux (9) et le panneau structarant étant constitué d'une pièce monobloc formant la surface supérieure (3), la surface inférieure (5), le bord (7) ainsi que les raidisseurs transversaux (9). L'invention concerne également un procédé de fabrication d'un tel panneau (1) et un élément d'aéronef comportant un tel panneau (1).
Bertrand Arnaud
Francisco Paulo
Millepied Denis
Montagne Valerian
Pacary Jean-Luc
Fasken Martineau Dumoulin Llp
Societe Lorraine de Construction Aeronautique
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