An aircraft (1) having a wing (3) and a wing tip device (4) at the tip of the wing (3), the wing tip device (4) having front and rear spars (14, 13), wherein the wing tip device (4) has a cross-brace spar (18) that links the front and rear spars and is oriented such that it is oblique to the front and rear spars (14, 13). A wing assembly (2) of the aircraft (1). A wing tip device (4) of the aircraft (1). A method of manufacture of the aircraft (1), wing assembly (2) and wing tip device (4).
A spar arrangement in a wing tip device
02.08.2017
Patent
Elektronische Ressource
Englisch