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
HOLMANORDNUNG IN EINER FLÜGELSPITZE
AGENCEMENT DE LONGERONS DANS UNE EXTRÉMITÉ D'AILE
2021-06-02
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |