A locking linkage system may comprise a lockable assembly comprising an upper brace, a lower brace coupled to the upper brace, and a linkage coupled to the upper brace and the lower brace. The locking linkage system may further comprise a downlock actuator comprising an electric motor coupled to the upper brace, a rotary output shaft coupled to the electric motor, a connecting output coupled to the rotary output shaft, wherein the connecting output shaft is configured to rotate between a fixed locked position and a fixed unlocked position, and a link rod having a distal end coupled to the linkage and a proximal end comprising a lost-motion joint, the lost-motion joint being coupled to a connection pin of connecting output shaft. The downlock actuator may be configured to toggle the linkage, the upper brace, and the lower brace between an unlocked position and a locked position.


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    Titel :

    Electrically powered downlock actuation system


    Beteiligte:
    DITZLER ADAM J (Autor:in)

    Erscheinungsdatum :

    2019-07-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16H Getriebe , GEARING



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