| 摘要 |
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 ).
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