A droop panel linkage for aircraft includes a lever arm, a main lever, a main tube and at least one drive strut. The lever arm is pivotally attached at a first end to a flap and is pivotally connected at a second end to a first end of the main lever. A second end of the main lever is provided with a first engagement element for engaging with a second engagement element incorporated into or associated with the main tube. The main tube is pivotally connected to a proximal end of the drive strut. A distal end of the drive strut is pivotally attached to the droop panel.


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    Titel :

    DROOP PANEL LINKAGE


    Weitere Titelangaben:

    VERBINDUNG FÜR DACHSCHRÄGEPLATTEN
    DISPOSITIF DE LIAISON À PANNEAU BASCULANT


    Beteiligte:
    YUE HAIKUO (Autor:in)

    Erscheinungsdatum :

    2017-09-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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