The invention relates to an extension of an intermediate casing for an aircraft jet engine, intended to project towards the downstream end from an external shell of the intermediate casing, this extension comprising an annular connecting downstream end forming an annular groove open radially towards the outside, intended to receive nacelle covers. According to the invention, the annular connecting downstream end is produced by means of a plurality of angular sectors.


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    Titel :

    INTERMEDIATE CASING EXTENSION FOR AN AIRCRAFT JET ENGINE, COMPRISING A SECTORISED ANNULAR GROOVE FOR RECEIVING THE NACELLE COVERS


    Weitere Titelangaben:

    PROLONGEMENT DE CARTER INTERMEDIAIRE POUR REACTEUR D'AVION, COMPRENANT UNE GORGE CIRCULAIRE SECTORISEE POUR RECEVOIR LES CARENAGES DE LA NACELLE



    Erscheinungsdatum :

    2016-01-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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