A leading edge assembly for an aircraft wing. The leading edge assembly includes a housing configured to be connectable to a fixed wing section of the wing, the housing formed with a first opening connecting an exterior of the housing with an interior of the housing, an actuating element movably connected to the housing, such that the actuating element is movable between a first position and at least one second position. The actuating element extends through the first opening and includes a first section arranged in the interior of the housing and a second section arranged at the exterior of the housing. The actuating element is configured to be connectable to a high lift device.
LEADING EDGE ASSEMBLY, WING, AND AIRCRAFT
EINTRITTSKANTENANORDNUNG, FLÜGEL UND FLUGZEUG
ENSEMBLE BORD D'ATTAQUE, AILE ET AÉRONEF
2024-05-08
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |