| 摘要 |
<p>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).</p> |
