Patent ID: 8840060
Filing Date: 2014-09-23
Classification: B64D,Y10T

Abstract:
1. A nacelle for a turbojet engine to equip an aircraft, the nacelle comprising: a first and a second half-shell; at least one locking system to lock one of the first and second half-shells relative to the other of the first and second half-shells; and an actuating device for actuating the at least one locking system between a locked state and an unlocked state, wherein the actuating device comprises a fixed body in which an actuating rod is translationally and rotationally mounted with respect to a longitudinal axis of the rod, the rod having a first end equipped with a handle and a second end connected to the locking system, the fixed body comprising a track collaborating with a follower element that projects from the rod, the track having a middle part running parallel to the longitudinal axis of the rod, and a first and a second end part respectively formed on each side of the middle part and running substantially perpendicular to the longitudinal axis of the rod, wherein the actuating device comprises means of immobilizing the rod, the immobilizing means being actuated alternately between a locked position in which the rod is prevented from moving and an unlocked position in which the rod rotates, wherein the immobilizing means comprise a first sleeve slidably mounted on the rod between a locked position and an unlocked position, the first sleeve equipped with an indicator ring being visible to an operator when the first sleeve is in the unlocked position and invisible when the first sleeve is in the locked position.