AIRCRAFT LIFTING SURFACE

AIRCRAFT LIFTING SURFACE

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...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: RUPEREZ, Javier, MARTINO GONZALEZ, Esteban, NOGUEROLES VIÑES, Pedro
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung: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).