A bypass turbofan engine comprising a nacelle surrounding a flow path for a secondary flow and comprising a fixed structure, a mobile assembly with a slide capable of translational movement on the fixed structure and bearing a mobile cowl and a frame capable of translational movement on the fixed structure and bearing deflectors. The mobile assembly is able to move between a forward position and a retreated position making it possible to open a passage between the flow path and the outside through the deflectors. A differentiation mechanism ensures a length of travel of the slide that is different from the length of travel of the frame, and actuators providing a translational travel of the slide. Fitting a differentiation mechanism means that the length of travel of the deflectors with respect to the length of travel of the mobile cowl can be regulated.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Bypass turbofan engine comprising mobile deflectors


    Beteiligte:
    MENOU FABIEN (Autor:in) / FESQUET STÉPHANIE (Autor:in)

    Erscheinungsdatum :

    2022-11-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Variable bypass turbofan engine

    ROLLING AUGUST J | Europäisches Patentamt | 2017

    Freier Zugriff

    Turbofan engine and aircraft comprising turbofan engine

    GARDES PASCAL / MENOU FABIEN / GOUGEON PASCAL et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Nacelle for a bypass turbofan engine

    GONIDEC PATRICK / BELLANGER ALEXANDRE | Europäisches Patentamt | 2016

    Freier Zugriff

    TURBOFAN GAS TURBINE ENGINE WITH BYPASS DUCT

    STRETTON RICHARD / WILLMOT MICHAEL | Europäisches Patentamt | 2020

    Freier Zugriff