A wing assembly includes a main wing (500) and a slat (510) movable between stowed and deployed positions. The main wing (500) includes a panel (512) movable to a retracted position when the slat (510) is in the stowed position, such that the slat outer surface (514) and a wing upper surface (503) define a first continuous outer mold line shape. The panel (512) may further be movable to an extended position when the slat (510) is in the deployed position, such that an outer surface (525) of the panel (512) and the wing upper surface (503) define a second continuous outer mold line shape.
LEADING EDGE ASSEMBLY FOR AN AIRCRAFT
VORDERKANTENANORDNUNG FÜR EIN FLUGZEUG
ENSEMBLE DE BORD D'ATTAQUE POUR UN AVION
2017-02-15
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |