| 摘要 |
The present invention relates to a thrust reverser for a jet engine nacelle comprising at least one movable cowl (2) mounted on a fixed reverser structure between a closed position, in which they provide the nacelle with aerodynamic continuity and deactivate means for deflecting at least part of the air flow, and an open position in which they open a passage in the nacelle and activate said deflection means, each movable cowl being able to be moved between these two positions by at least one actuating means (6a, 6b), characterized in that the actuating means are combined with at least one means (10) for mechanically braking said actuating means. |
