| 摘要 |
<p>Thrust reverser for aircraft turbojet engine nacelle, comprising at least one pair of twin doors (7, 9), this pair comprising an upstream door (7) and a downstream door (9) which move in concert between a "direct jet" position in which these two doors are closed, and a "reverse jet" position in which these two doors are open and able to deflect at least some (I1, I2) of the stream of cold air capable of flowing inside the nacelle, this thrust reverser being notable in that it comprises means (23, 33) for making the amount of the stream of cold air circulating between the extrados of said upstream door and the intrados of said downstream door suitable.</p> |
