| 摘要 |
A structural arrangement (200), in particular for an aircraft or spacecraft (100), comprising a box structure (202), comprising a first fibre portion (212) which extends in a first plane (XY), comprising a second fibre portion (214) which extends in a second plane (XZ) which intersects the first plane (XY), the first and the second fibre portion (212, 214) being interconnected at a crossing point (216) thereof, the first fibre portion (212) comprising a first portion (218) on one side of the crossing point (216) and a second portion (220) on the other side of the crossing point (216), the first portion (218) of the first fibre portion (212) being connected to a first portion (232) of the box structure (202) and the second portion (220) of the first fibre portion (212) being connected to a second portion (233) of the box structure (202), the second fibre portion (214) forming, on one side of the crossing point (216), an inner web (222) inside the box structure (202) and, on the other side of the crossing point (216), an outer web (224) outside the box structure,
comprising a supporting element (234) which is connected to the inner web (222), and comprising an attachment point (226) for introduction of a first load (230) into the outer web (224), the second fibre portion (214) guiding the first load (230) which is introduced at the attachment point (226) from the attachment point (226) into the supporting element (234), and the first fibre portion (212) simultaneously transferring a second load (235) between the first and the second portion (232, 233) of the box structure (202). |
