A turbojet engine comprising an engine, a nacelle comprising a fan case, an intermediate case having a part forming a hub and an outer shroud radially spaced away from the hub by a secondary, or bypass, flow path and fixed to the hub via arms, in which the outer shroud is situated to the rear and in the continuity of the fan case, a fixed structure fixed to the outer shroud, a mobile assembly mounted with the ability to effect translational movement on the fixed structure, and a ramp fixed to the outer shroud and configured to direct the secondary or bypass flow to exit the outer shroud. Such a turbojet engine makes it possible to simplify assembly and among other things, makes it possible to fix the ramp directly to the outer shroud.


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    Title :

    TURBOREACTEUR COMPORTANT UNE NACELLE EQUIPEE D'UN CARTER DE SOUFFLANTE ET D'UNE STRUCTURE FIXE


    Additional title:

    TURBINE ENGINE COMPRISING A NACELLE PROVIDED WITH A FAN COWL AND A STATIONARY STRUCTURE
    TURBOTRIEBWERK, DAS EINE GONDEL UMFASST, DIE MIT EINEM GEBLÄSEGEHÄUSE UND EINER FESTEN STRUKTUR AUSGESTATTET IST


    Contributors:

    Publication date :

    2020-07-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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



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