FIELD: engines and pumps.
SUBSTANCE: flap for folding thrust reverser is arranged to turn on thrust reverser fixed structure. Flap has inner surface integrated into channel for airflow generated by turbojet and outer surface providing aerodynamic continuity of nacelle equipped with said thrust reverser. Flap is equipped with airflow deflectors arranged nearby flap front edge to displace in plane, in fact, perpendicular, to flap plane from first retracted position into second extended position wherein deflectors extend beyond flap edges. Said deflectors are arranged to turn in plane, in fact, perpendicular, to flap plane, about appropriate axis.
EFFECT: integration in airflow channel, simple and reliable design.
8 cl, 10 dwg
