A propulsion assembly includes an engine below a pylon by engine attachments, including a thrust force uptake device, the engine having a longitudinal axis and a vertical median plane parallel to the longitudinal axis, the thrust force uptake device having a main fitting fixed below the pylon and two links disposed on either side of the vertical median plane and which each have a rear end articulated to the main fitting by a spreader mounted to pivot on the main fitting about an axis of rotation which, on the one hand, is orthogonal to a mean plane for transmitting thrust forces parallel to the longitudinal axis of each of the links, and which is disposed in the vertical median plane, each link being articulated to the spreader by a connecting pin extending parallel to the mean plane for transmitting thrust forces and perpendicular to the longitudinal axis of the link.


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    Title :

    ENSEMBLE DE MOTORISATION D´AÉRONEF COMPRENANT UN DISPOSITIF DE REPRISE D'EFFORTS DE POUSSÉE CONFIGURÉ POUR ÊTRE ATTACHÉ À UN AÉRONEF


    Additional title:

    AIRCRAFT ENGINE ASSEMBLY COMPRISING A THRUST LOAD-RECEIVING DEVICE CONFIGURED TO BE MOUNTED TO AN AIRCRAFT
    FLUGTRIEBWERKSAUFBAU MIT EINER VORRICHTUNG ZUR AUFNAHME VON SCHUBKRÄFTEN GEEIGNET ZUR AUFHÄNGUNG AN EINEM FLUGZEUG



    Publication date :

    2024-08-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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