An aircraft wing

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 3/28 (2006.01)

Patent

CA 2591895

The invention relates to an aircraft wing panel, for example, a trailing edge upper panel'1 which is joined to the wing skin (20) by means of spigots (19) which project and engage with slots (13). Preferably, the slots are provided in lips (10, 11, 12) which extend from the leading edge (5) of the panel and the spigots (19) are fastened to and extend from the wing skin (20).

Cette invention concerne un panneau d'aile d'aéronef tel qu'un panneau supérieur de bord de fuite (1) qui est rattaché au revêtement de l'aile (20) au moyen de tenons (19) qui dépassent et s'emboîtent dans des encoches (13). Ces encoches sont de préférence situées dans des lèvres (10, 11, 12) qui s'étendent depuis le bord d'attaque (5) du panneau et les tenons (19) sont fixés au revêtement de l'aile (20) et s'étendent depuis celui-ci.

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