An assembly for a turbojet engine includes a pylon, a nacelle supported by the pylon, and a locking device interposed between the pylon and a cowl of the nacelle. The cowl slides between operating and maintenance positions. The locking device is movable between active and inhibited positions, and the device allows an operation mode in the active position and a maintenance mode in the inhibited position. In particular, the locking device comprises a rocker to maintain the cowl to the pylon, and the rocker includes an inhibiting lever and an activation lever. The inhibiting and activation levers are mounted on a switching shaft of the locking device. The inhibiting lever is set in rotation through an actuator, providing direct access from a bypass flow duct in the active position while the activation lever is set in rotation from the bypass duct in the inhibited position.


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    Title :

    DISPOSITIF DE VERROUILLAGE/DÉVERROUILLAGE POUR CAPOT MONOBLOC D'INVERSEUR DE POUSSÉE DE NACELLE DE TURBORÉACTEUR


    Additional title:

    LOCKING/UNLOCKING DEVICE FOR A ONE-PIECE COVER OF A THRUST REVERSER OF A TURBOJET ENGINE NACELLE
    VERRIEGELUNGS-/ENTRIEGELUNGSVORRICHTUNG FÜR EINE EINTEILIGE ABDECKUNG EINER SCHUBUMKEHRVORRICHTUNG EINER TURBODÜSENTRIEBWERKSGONDEL


    Contributors:

    Publication date :

    2016-03-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64C AEROPLANES , Flugzeuge



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