| 摘要 |
<p>A turbojet thrust reverser comprises pivoting doors (7) capable of pivoting by the action of a thrustor (4) whose linking point (8) with the fixed structure upstream of the reverser and whose linking point (9) with the door (7) are in a straight line with the contact point (2), at the level of the device for installing the reverser on the turbojet, between a blade (3) integral with the fixed structure upstream of the reverser and an interface flange (5) integral with the housing of the turbojet.</p> |
