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.
DISPOSITIF DE VERROUILLAGE/DÉVERROUILLAGE POUR CAPOT MONOBLOC D'INVERSEUR DE POUSSÉE DE NACELLE DE TURBORÉACTEUR
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
2016-03-23
Patent
Electronic Resource
French
SYSTEME DE COMMANDE DE CAPOT D'INVERSEUR DE POUSSEE POUR NACELLE DE TURBOREACTEUR
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