An aircraft 1 has a wing 3 and a wing tip device 4 at the tip of the wing 3. The wing tip device 4 has front and rear spars 14, 13. 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. Also disclosed is a method of making a wing tip device.
A spar arrangement in a wing tip device
19.12.2018
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |