Aircraft lifting surface (2) having a span direction, the lifting surface (2) comprising:- a stationary part (3),- a movable part (1), movable with respect to the stationary part (3) and comprising an end (4) in the span direction,- an actuation system configured to actuate the movable part (1) with respect to the stationary part (3).The actuation system comprising a sliding system joined to:- the end (4) of the movable part (1), and- configured to be joined to a stationary structure (6) of the aircraft, said stationary structure (6) being:• located adjacent in the span direction to the end (4) of the movable part (1), and• connected with the stationary part (3) of the lifting surface,so that the sliding system allows the movable part (1) to slide with respect to the stationary structure (6).
AIRCRAFT LIFTING SURFACE
FLUGZEUGAUFTRIEBSFLÄCHE
SURFACE DE SUSTENTATION D'AÉRONEF
2024-11-06
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
AIRCRAFT LIFTING SURFACE AND AIRCRAFT COMPRISING SUCH LIFTING SURFACE
European Patent Office | 2024
|AIRCRAFT LIFTING SURFACE AND AIRCRAFT COMPRISING SUCH LIFTING SURFACE
European Patent Office | 2024
|NTIS | 1975
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