A ducted fan turbojet including a nacelle including a fixed structure, a thrust reverser system having a frame, a mobile structure fastened to the frame, inner doors and outer doors hinged at the frame. The frame is mobile in translation on the fixed structure between a forward position and a rear position so as to define a window between the fixed structure and the mobile structure, the window being open between a bypass duct and the exterior of the nacelle. Each door is mobile between a stowed position and a deployed position and the mobile structure is assembled hinged on the frame via at least one hinge whose axis of rotation is globally parallel to a longitudinal axis of the ducted fan turbojet.


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    Title :

    TURBORÉACTEUR COMPORTANT UNE NACELLE ÉQUIPÉE D'UN SYSTÈME INVERSEUR COMPORTANT UN CAPOT ARTICULÉ


    Additional title:

    TURBINE ENGINE COMPRISING A NACELLE PROVIDED WITH A REVERSER SYSTEM COMPRISING A HINGED COVER
    TURBOMASCHINE, DIE EINE MIT EINEM UMKEHRSYSTEM AUSGESTATTETE GONDEL MIT SCHARNIERDECKEL UMFASST


    Contributors:

    Publication date :

    2021-02-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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