Actuation assembly for a trailing edge flap of an aircraft wing, comprising: a track fixable to the aircraft wing; a carriage arranged on the track so as to be movable across a range of carriage positions along the track; a flap-to-carriage connector configured to hingeably connect the carriage to a leading edge of the flap so as to determine a flap-to-carriage hinging axis extending transverse to a main track direction of the track at the leading edge of the flap; and a first actuator configured to controllably rotate the flap with respect to the carriage about the flap-to-carriage hinging axis, wherein the actuation assembly is configured to enable the flap, when connected, to be adjusted with respect to the wing between a retracted flap position and an extended flap position by moving the carriage within the range of carriage positions along the track.


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    Titel :

    TRAILING EDGE FLAP ASSEMBLY


    Weitere Titelangaben:

    HINTERKANTENKLAPPENANORDNUNG
    ENSEMBLE DE VOLET DE BORD DE FUITE


    Beteiligte:

    Erscheinungsdatum :

    2023-12-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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