| 摘要 |
<p>The invention concerns a turbofan thrust reverser comprising an annular assembly of pivoting flaps (12) closing a channel (17) circulating the flow and a turning vane assembly (20) deviating the reversed flow, covered in direct jet by a cowling (7) mobile in translation. On each peripheral sector, a first vane part (21) is fixed and at least a second vane part (22) is mobile, radially superposed on the first vane part (21) in direct thrust and after axial translation in the turbojet longitudinal direction, the second part (22) is juxtaposed with the first part (21).</p> |
