A wing leading-edge device is proposed, comprising a flow body having a front side, a back side and a plurality of ribs arranged in ribs, wherein at least one of the ribs is a load introduction rib comprising at least one first lug for coupling with a drive mechanism, further comprising a second load path component, which comprises at least one second lug, wherein the second load path component isat least connected to the load introduction rib, such that a second opening of the at least one second lug is co-axial with a first opening of the at least one first lug.
提出了一种机翼前缘装置,所述机翼前缘装置包括流动体,所述流动体具有前侧、后侧、以及布置在肋中的多个肋,其中,所述肋中的至少一个肋是载荷引入肋,所述载荷引入肋包括用于与驱动机构联接的至少一个第一凸耳,所述机翼前缘装置进一步包括第二载荷路径部件,所述第二载荷路径部件包括至少一个第二凸耳,其中,所述第二载荷路径部件至少连接至所述载荷引入肋,使得所述至少一个第二凸耳的第二开口与所述至少一个第一凸耳的第一开口同轴。
A WING LEADING-EDGE DEVICE AND A WING HAVING SUCH A WING LEADING-EDGE DEVICE
机翼前缘装置和具有这种机翼前缘装置的机翼
2020-09-29
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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