An aircraft turbojet engine nacelle includes a rear section without a lower bifurcation, the rear section including a thrust reverser system, and the thrust reverser system including a movable cowl. The nacelle includes a guide system including a movable portion and a fixed portion, the movable portion being secured in translation to the movable cowl and cooperating with the fixed portion and the fixed portion being fixed relative to the nacelle. The guide system is disposed proximate to a position called the “6 O'clock” position. In one form, the length of the fixed portion of the guide system is larger than or equal to 50% of the length of the movable portion.


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    Title :

    NACELLE DE TURBORÉACTEUR D'AÉRONEF, ENSEMBLE PROPULSIF ET AÉRONEF COMPORTANT UNE TELLE NACELLE


    Additional title:

    AIRCRAFT TURBOPROP NACELLE, PROPELLER ASSEMBLY AND AIRCRAFT COMPRISING SUCH A NACELLE
    FLUGZEUGSTRIEBWERKSGONDEL, ANTRIEBSANORDNUNG UND FLUGZEUG BEINHALTEND SOLCHE GONDEL


    Contributors:

    Publication date :

    2020-07-15


    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



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