A aircraft wing assembly comprising a wing box comprising: an upper surface 12; a lower surface 14; and a leading edge structure 16, connecting the upper surface to the lower surface and secured to the upper surface at a connection point 30, and a drive mechanism secured to the wing box; and a high lift device mounted to the drive mechanism. The drive mechanism 24, 25, is configured to 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.
Aircraft wing assembly
2024-06-05
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |