A turbofan engine nacelle has a downstream section which includes at least one front frame. The front frame is attached to a stationary portion of the nacelle, and the downstream section is provided with at least one rail or slide which extends in a longitudinal direction of the nacelle and is capable of engaging with at least one corresponding slide or rail of an attachment pylon of the turbofan engine. The front frame is connected to the rail or slide of the downstream section by means of at least one swiveled connecting rod.


    Access

    Download


    Export, share and cite



    Title :

    NACELLE DE TURBORÉACTEUR À SECTION AVAL


    Additional title:

    TURBOFAN ENGINE NACELLE WITH DOWNSTREAM SECTION
    TURBINEN-TRIEBWERKSGONDEL MIT EINEM AUSLAUFBEREICH


    Contributors:

    Publication date :

    2016-04-13


    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



    NACELLE DE TURBOREACTEUR

    BOUTEILLER XAVIER / BLIN LAURENT ALBERT | European Patent Office | 2016

    Free access

    NACELLE POUR TURBOREACTEUR

    JORET JEAN-PHILIPPE / VAUCHEL GUY BERNARD | European Patent Office | 2016

    Free access

    NACELLE DE TURBOREACTEUR

    HURLIN HERVÉ / DEZEUSTRE NICOLAS / KERBLER OLIVIER et al. | European Patent Office | 2019

    Free access

    NACELLE DE TURBORÉACTEUR D'AÉRONEF

    KERBLER OLIVIER / METEZEAU FABRICE HENRI EMILE / GONIDEC PATRICK et al. | European Patent Office | 2016

    Free access

    NACELLE DE TURBORÉACTEUR D'AÉRONEF

    KERBLER OLIVIER / METEZEAU FABRICE HENRI EMILE / GONIDEC PATRICK et al. | European Patent Office | 2019

    Free access