| 摘要 |
The invention relates to a thrust reverser of a turbofan pod, comprising movable cowlings (4) that retract relative to stationary front structure (2) to reveal stationary or movable thrust reverser cascades, as well as a secondary variable nozzle section (8) connected to the movable cowlings by guiding means enabling movement controlled by actuators (10) engaged with the front structure to apply an axial thrust. The invention is characterized in that the actuators (10) are directly connected to the secondary nozzle (8), and in that the thrust reverser comprises latches (14) connected to the movable cowlings (4), comprising two positions providing, alternately, latching onto the front structure (2) or latching onto the control (10) of the secondary nozzle (8). |
