| 摘要 |
<p>The invention concerns a turbojet thrust reverser comprising hollow pivoting doors (3), integrated in direct jet in the external pod cowling and constituting in reverse jet flux deviating obstacles forming scoops. A mobile part forming a visor (23) is arranged, in direct jet, between the door (3) upstream edge and the upstream fixed structure (6) covering the front frame (8) downstream structure. The upstream visor (23) is articulated on the fixed structure and associated with control means, uncovers, in thrust reversal, the front frame (8) downstream structure which has an aerodynamic surface guiding the reversed flux</p> |
