| 摘要 |
<p>The invention features a turbofan thrust reverser comprising pivoting doors (7) integrated in direct jet flow in the external pod wall and constituting thrust reversing flow deviation obstacles after pivoting by an actuator (8). Each door (7) bears at least one deflecting blade (22) aerodynamically profiled in wing shape, set in contact with the flow in the ring-shaped channel (21) such that the flow exerts an action on the said blade (22) which tends to maintain the door (7) in its closed direct jet position.</p> |
