| 摘要 |
The invention relates to a downstream assembly (6) of a nacelle of a turbojet engine (5) of an aircraft, comprising: - a fixed internal structure (7) intended to surround the turbojet (5), the said fixed internal structure (7) comprising an upstream part and a downstream part (11), - a fixed external structure (13) at least partially surrounding the upstream part of the fixed internal structure (7), and - a moving cowl (15) surrounding the fixed internal structure (7) and the fixed external structure (13), characterized in that the moving cowl (15) comprises a main part (20) able to move in a translational movement between a work position and a maintenance position corresponding to the reverse thrust position, and a secondary part (25) fixed securely to the fixed external structure (13) and extending at least partially over the circumference of the main part (20). The invention also relates to a nacelle intended to surround a turbojet engine (5) of an aircraft comprising a downstream assembly (6) according to the invention. |
