A device for attaching an aircraft engine including a thrust force take-up device that includes a main fitting to be fixed to an engine mounting beam fixed to a box structure, an additional fitting fixed to the main fitting, and two load reacting link rods connected to the main fitting by a balance beam, each of the link rods being connected to the balance beam by a first longitudinal end by a first mechanical connection that has at least one axis of rotation, each of the link rods being connected to the additional fitting by a second longitudinal end by a second mechanical connection that has at least one axis of rotation, the second mechanical connection having play, the first and second mechanical connections having at least one axis of rotation in common.


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    Title :

    DISPOSITIF D'ACCROCHAGE DE MOTEUR D'AERONEF ET AERONEF COMPORTANT AU MOINS UN TEL DISPOSITIF


    Additional title:

    DEVICE FOR ATTACHING AN AIRCRAFT ENGINE AND AIRCRAFT COMPRISING AT LEAST ONE SUCH DEVICE
    VORRICHTUNG ZUR BEFESTIGUNG EINES FLUGZEUGTRIEBWERKS UND FLUGZEUG MIT MINDESTENS EINER DERARTIGEN VORRICHTUNG


    Contributors:

    Publication date :

    2017-05-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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