A leading edge high-lift device (22), that may be deployable from a wing (12) of an aircraft, may include a leading edge (26) and a trailing edge (28). A lower surface (32) and an upper surface (30) may both extend between the leading edge (26) and the trailing edge (28). A trailing edge region (34) may be defined by the trailing edge (28) and an adjacent region thereto. A shaping device (36) may be disposed at the trailing edge region (34) and may be movable between a non-activated position and an activated position.
LEADING EDGE HIGH-LIFT DEVICE
VORDERKANTENAUFTRIEBSERHÖHENDE VORRICHTUNG
DISPOSITIF HYPERSUSTENTATEUR DE BORD D'ATTAQUE
2019-11-06
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |