A support assembly for deployment and retraction of an aero surface from an aircraft is disclosed. The assembly comprises a guide track (37), a primary support arm (52) having one end coupled to a carriage (36) mounted on the track such that the primary support arm is rotatable relative to the carriage about multiple axes, and a control arm (56) having one end coupled to the primary support arm and a second end pivotably attachable to a fixed support forming part of the structure of the aircraft. The assembly being configured such that, when the carriage is driven along the guide track, the control arm causes the primary support arm to pivot about said multiple axes to deploy and/or retract an aero surface pivotally attached to an opposite end of the primary support member along an arcuate path.


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    Titel :

    Slat support assembly


    Weitere Titelangaben:

    Vorflügelaufhängung
    Ensemble de support de volets


    Beteiligte:
    WILDMAN ERIC (Autor:in) / PARKER SIMON (Autor:in) / BRYANT ANTHONY (Autor:in) / FOLKARD CHRISTIAN (Autor:in)

    Erscheinungsdatum :

    2019-10-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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