| 摘要 |
Thrust reverser device (1) for a turbojet engine nacelle comprising at least two cowls (11, 12) each one mounted with the ability to move translationally with respect to a fixed structure between an upstream closed position in which it provides the aerodynamic continuity of the nacelle, and a downstream open position in which it opens a passage in the nacelle, the device comprising at least one synchronization cable (2) stretched between the two mobile cowls so as to have a first end (111) attached to an upstream point of a first cowl, a second end (121) attached to a downstream point of the second cowl, and the upstream and downstream attachment points being determined relative to a fixed central zone (3) where the cable passes between the two cowls. |
