| 摘要 |
<p>The invention relates to a reverse thrust device including a stationary upstream structure including a front frame (30) and a cowl (40). Said cowl (40) is extended by a nozzle (41) with a variable cross-section and is translatable between a deployed position, causing a variation in the cross-section of the nozzle (41), and a retracted position, wherein the nozzle (41) is in a position wherein it ensures aerodynamic continuity of the cowl (40). Said device is remarkable in that at least part of the front frame (30) is translatable with the cowl (40) during the movement thereof to a position causing a variation in the nozzle cross-section.</p> |
