A linking device connecting an aircraft engine and a primary structure of an aircraft pylon, comprising a support connected to the primary structure, a spreader, extending between first and second ends that has a central part connected to the support by a principal link comprising a principal rotation axis, at least one system for limiting the deflection of the spreader comprising an extension secured to the spreader and also upper and lower stops, secured to a fitting secured to the support, between which the extension is positioned.


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    Title :

    DISPOSITIF DE LIAISON RELIANT UN MOTEUR D'AÉRONEF ET UNE STRUCTURE PRIMAIRE D'UN MÂT D'AÉRONEF COMPRENANT UN PALONNIER ET UN SYSTÈME DE LIMITATION DU DÉBATTEMENT HORS PLAN DU PALONNIER, AÉRONEF COMPRENANT UN TEL DISPOSITIF DE LIAISON


    Additional title:

    LINKING DEVICE CONNECTING AN ENGINE OF AN AIRCRAFT AND A PRIMARY STRUCTURE OF AN AIRCRAFT MAST COMPRISING A RUDDER AND A SYSTEM FOR LIMITING THE OUT-OF-PLANE DISPLACEMENT OF THE RUDDER, AIRCRAFT COMPRISING SUCH A LINKING DEVICE
    VERBINDUNGSVORRICHTUNG ZWISCHEN EINEM LUFTFAHRZEUGMOTOR UND EINER PRIMÄRSTRUKTUR EINES LUFTFAHRZEUGMASTS, DIE EIN SEITENSTEUERPEDAL UND EIN SYSTEM FÜR DIE BEGRENZUNG DES RUDERAUSSCHLAGS AUSSERHALB DER EBENE UMFASST, UND EINE SOLCHE VERBINDUNGSVORRICHTUNG UMFASSENDES LUFTFAHRZEUG


    Contributors:

    Publication date :

    2021-12-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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