B - Operations – Transporting – 32 – B
Patent
B - Operations, Transporting
32
B
B32B 5/02 (2006.01) B32B 1/00 (2006.01) B32B 7/00 (2006.01) B64C 1/00 (2006.01)
Patent
CA 2735953
The invention relates to a composite sandwich panel (1) comprising at least a web (2) provided between an inner skin (3) and an outer skin (4), each skin being made of a composite material from a plurality of fibrous plies (5, 6, 7, 8), characterised in that a portion of the plies of the inner skin and/or of the outer skin each extends at least partially through the web at an uninterrupted area thereof in order to form together a through-reinforcement (9) extending from the inner skin to the outer skin of the composite sandwich panel. The invention further relates to an aircraft element including such a composite sandwich panel.
La présente invention se rapporte à un panneau sandwich composite (1) comportant au moins une âme (2) comprise entre une peau interne (3) et une peau externe (4), chaque peau étant réalisée en matériau composite à partir d'une pluralité de plis fibreux (5, 6, 7, 8), caractérisée en ce qu'une partie des plis de la peau interne et/ou de la peau externe s'étendent chacun au moins partiellement à travers l'âme, au niveau d'une zone interrompue de cette dernière, de manière à former ensemble un renfort (9) traversant s'étendant de la peau interne à la peau externe du panneau sandwich composite, ainsi qu'à un élément d'aéronef comprenant un tel panneau sandwich composite.
Francisco Paulo
Pacary Jean-Luc
Norton Rose Or S.e.n.c.r.l. S.r.l./llp
Societe Lorraine de Construction Aeronautique
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