| 摘要 |
A wing (10a) of an aircraft provided with a main wing (10) and an arrangement of leading edge lifting bodies (13a), which as seen with reference to the incident flow direction (F) are arranged on the leading edge, which are adjustably arranged on the main wing (10) one behind another as seen in the spanwise direction (S-T) of the main wing (10) by means of respectively two positioning devices spaced apart from one another in the spanwise direction (S-T) of the main wing, wherein the wing (10a) has a connecting device (K), which is coupled to each of two adjacent leading edge lifting bodies (13a), wherein the connecting device (K) is executed such that in the event of a fracture of a positioning device of a positioning body external forces acting on the latter are transferred via the respective connecting device (K) to the leading edge lifting bodies (13a) coupled up via the latter. |
