An aircraft wing assembly is disclosed. An aircraft wing assembly includes a wing box comprising: an upper surface; a lower surface; and a leading edge structure connecting the upper surface to the lower surface and fixed to the upper surface at a connection point. The aircraft wing assembly further includes a drive mechanism secured to the wing box; and a high lift device mounted to the driving mechanism. The drive mechanism is configured to, in use, move the high lift device between a retracted position and an extended position, and wherein the high lift device is configured to overlap the connection point when in the retracted position.
公开了一种飞行器机翼组件。飞行器机翼组件包括机翼盒,该机翼盒包括:上表面;下表面;以及前缘结构,该前缘结构将上表面连接至下表面并且在连接点处固定至上表面。飞行器机翼组件还包括:驱动机构,该驱动机构固定至机翼盒;以及高升力装置,该高升力装置安装至驱动机构。驱动机构构造成在使用中使高升力装置在缩回位置与伸出位置之间移动,并且其中,高升力装置构造成当处于缩回位置时与连接点重叠。
Aircraft wing assembly
飞行器机翼组件
2024-05-31
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |