Double-shell design centre box

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 3/46 (2006.01) B64C 3/18 (2006.01)

Patent

CA 2612590

The present invention relates to a center box (5) for an aircraft wing, as well as to an aircraft comprising such a center box (5). The center box (5) essentially comprises two lateral surfaces (6), which in turn essentially comprise two internal and external skins (2, 1) that are arranged so as to be spaced apart from each other. In order to provide adequate stability to the lateral surface (6), the internal skin (2) and the external skin (1) are interconnected by way of a multitude of profiles (3).

La présente invention concerne une boîte centrale (5) pour une aile d~avion, ainsi qu~un avion comprenant une telle boîte centrale (5). La boîte centrale (5) comprend essentiellement deux surfaces latérales (6), qui à leur tour comprennent essentiellement deux enveloppes interne et externe (2, 1) qui sont agencées pour être espacées l~une de l~autre. Pour offrir une stabilité adéquate sur la surface latérale (6), l~enveloppe interne (2) et l~enveloppe externe (1) sont interconnectées au moyen d~une multitude de profils (3).

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