| 摘要 |
<p>A component having a box structure for an airplane, in particular, a wing, a flap or an aileron and so on, comprises a plurality of C-pro files (31-34). The C-profiles (31-34) are subsequently inserted into one another. One of the C-profiles (31-34) with its connecting portion is inserted into an opening end of another adjacent C-profile (31-34) and is fixed thereto in the region of being inserted into one another.</p> |
