A turbofan with a fan casing and a nacelle which comprises a fixed structure, a movable assembly with a movable cowl and a slide, which is translationally movable between an advanced position and a retreated position in which the movable cowl is moved away from the fan casing in order to define a window open between a duct and the outside of the nacelle, a plurality of blades, each being mounted rotatably on the slide, where each blade is movable between a retracted position in which the blade is outside of the duct and a deployed position in which the blade is across the duct, a set of actuators for moving the slide and an operating system configured to move each blade from the retracted position to the deployed position, and vice versa.


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    Title :

    TURBORÉACTEUR DOUBLE FLUX COMPORTANT UNE SÉRIE DE LAMES ROTATIVES POUR OBTURER LA VEINE DU FLUX SECONDAIRE


    Additional title:

    DUAL-FLOW TURBOJET ENGINE COMPRISING A SERIES OF ROTARY STRIPS FOR BLOCKING THE SECONDARY FLOW STREAM
    DOPPELSTROM-TURBOTRIEBWERK, DAS EINE REIHE VON VERSCHWENKBAREN LAMELLEN UMFASST, UM DEN KANAL DES SEKUNDÄRSTROMS ABZUDICHTEN


    Contributors:

    Publication date :

    2020-12-23


    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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