A nacelle having a longitudinal axis and comprising a chassis, two articulated fan cowl doors and a sliding fan cowl door. Each articulated fan cowl door is rotatably mounted in an upper portion of the chassis, each about their own opening axis. The opening axes are parallel to the longitudinal axis. The articulated doors pivot between a closed position and an open position. The sliding fan cowl door, in its closed position, is placed between free edges of the articulated fan cowl doors. A sliding arrangement for the sliding door is configured such that, in the open position of either articulated door, the sliding fan cowl door can rotate about the longitudinal axis. The nacelle has fan cowl doors which take up less space when in the open position and which are more compact, in comparison to articulated fan cowl doors without a sliding fan cowl door.


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    Title :

    NACELLE D'AERONEF COMPORTANT AU MOINS UN CAPOT MONTE ROTATIF AUTOUR DE L'AXE LONGITUDINAL DE LA NACELLE


    Additional title:

    AIRCRAFT NACELLE COMPRISING AT LEAST ONE COVER MOUNTED ROTATABLY ABOUT THE LONGITUDINAL AXIS OF THE NACELLE
    LUFTFAHRZEUGGONDEL, DIE MINDESTENS EINE UM DIE LÄNGSACHSE DER GONDEL DREHBAR MONTIERTE VERKLEIDUNG UMFASST


    Contributors:

    Publication date :

    2018-04-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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