A propulsion assembly having a pylon, a turbomachine comprising an engine and a fan that is enclosed by a fan casing, a nacelle surrounding the engine and the fan casing and having a load support disposed in the top part of the nacelle, a front engine attachment between the pylon and a front part of the engine, a rear engine attachment between the pylon and a rear part of the engine, a front fan attachment between the fan casing and the load support, and a rear pylon attachment between the pylon and the load support. Such a propulsion assembly allows a reduction in bulk since the load of the turbojet engine is distributed between the load support and the pylon, and the pylon is attached to the engine.


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    Title :

    ENSEMBLE DE MOTORISATION POUR UN AÉRONEF COMPRENANT UN SUPPORT DE CHARGE


    Additional title:

    MOTOR ASSEMBLY FOR AN AIRCRAFT COMPRISING A LOAD SUPPORT
    MOTORISIERUNGSEINHEIT FÜR EIN LUFTFAHRZEUG, DIE EINEN LASTTRÄGER UMFASST


    Contributors:

    Publication date :

    2021-12-01


    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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