| 摘要 |
<p>The present invention provides a composite (1), particularly in the aerospace sector, comprising a O-stringer (3) having a rib section (6), and a connecting element (8), which on one end (9) thereof is connected to the rib section (6) of the O-stringer (3) and on the other end (24) can be connected to a standard coupling element (26). The object of the present invention is to provide a O-stringer (3) with a connecting zone which is coupled to the rib section (6) of the O-stringer (3), thus allowing for the transfer of comparatively high loads, and which can be connected to a standard coupling element (26) in order to utilize the advantages of such standard coupling elements (23) when connecting O-stringers (3) to other stringers, for example T- or other O-stringers.</p> |
