The present application relates to an aircraft assembly. The aircraft assembly has a wing tip device connected to a wing tip of a wing by a first connector, a second connector and a third connector. The wing tip device includes a front device spar and a rear device spar. The first connector is associated with the rear device spar. The second connector is spaced apart in a chordwise direction forward of the first connector, and the third connector is spaced apart in a chordwise direction rearward of the first connector. The third connector comprises a spigot mounting formation.
An aircraft assembly including a wingtip device
2020-01-29
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |