Patent ID: 8070101
Filing Date: 2011-12-06
Classification: B64D,Y10T

Abstract:
1. An assembly comprising a nacelle of a turbojet engine connected to a pylon of an aircraft, said nacelle comprising at least one lateral movable cowl having at least one locking system, the movable cowl pivotable about an axis substantially perpendicular to a longitudinal axis of the nacelle, said locking system comprising, a clevis connected to the pylon, and a rod mounted on the movable cowl and able to engage with the clevis when the movable cowl is in the closed position, wherein the rod is mounted translationally mobile relative to said movable cowl along a substantially longitudinal axis of the movable cowl so as to form a slider that can move between a locked position in which the rod is engaged with the clevis and provides a structural connection between the pylon and the movable cowl, and an unlocked position in which the rod is disengaged from the clevis and allows the movable cowl to open.