Fairing for an aircraft structure

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 3/18 (2006.01) B64C 1/00 (2006.01) B64C 3/00 (2006.01) B64C 3/28 (2006.01)

Patent

CA 2560978

The invention relates to nose parts of the fairing of vertical and horizontal tails and wings of an aircraft with a skin and a support structure, the skin (2) being disposed on the support structure (4, 6). The support structure is provided with a plurality of ribs (6) and a plurality of stringers (4), the plurality of stringers being arranged on the plurality of ribs to support the skin. Advantageously, an improved deformation behavior can be obtained, e.g. in the event of an impact of a bird, while the weight and cost are minimized by providing the stringers.

L'invention concerne des pièces des bords d'attaque du revêtement de l'empennage vertical et horizontal et des ailes d'un avion, présentant une peau et une structure support, la peau (2) étant disposée sur la structure support (4, 6). La structure support présente une pluralité de nervures (6) ainsi qu'une pluralité de traverses (4). La pluralité de traverses est disposée sur la pluralité de nervures en vue de supporter la peau. Avantageusement, le fait de prévoir des traverses permet d'obtenir un comportement amélioré à la déformation, par exemple, en cas d'impact d'un volatile, tout en minimisant le poids et le coût.

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