A turbojet engine including an engine, a fan casing and a nacelle including a fixed structure and a thrust-reversing system having a mobile assembly with a mobile cowl and a frame, in which the mobile assembly is translationally mobile on the fixed structure between an advanced position and a retracted position to define a window between the secondary jet and the outside of the nacelle, inner doors and outer doors, a runner translationally mobile between a first position and a second position, in which each door is mounted articulated by a rear edge on the runner between a stowed position and a deployed position, an actuator for ensuring the translational displacement of the runner from the first position to the second position and an actuator for ensuring the displacement of the frame from the advanced position to the retracted position.


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    Titel :

    TURBOJET ENGINE COMPRISING A NACELLE EQUIPPED WITH A THRUST-REVERSING SYSTEM COMPRISING OUTER AND INNER DOORS


    Beteiligte:
    RAMBAUD ERIC (Autor:in) / BROSSARD DENIS (Autor:in) / RIDRAY FRÉDÉRIC (Autor:in) / DESCAMPS PHILIPPE (Autor:in) / BARDEY XAVIER (Autor:in) / LE CLAINCHE STÉPHANE (Autor:in)

    Erscheinungsdatum :

    2019-08-22


    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 / F16H Getriebe , GEARING



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