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
05.06.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |