FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to thrust reversers. Claimed thrust reverser comprises at least one fixed structural element with at least one flap fitted thereat. Said flap can turn between closed position and open position. As-closed, it covers the reverser to make the cowling outer section. As-open, it opens the structural element channel to shut off the turbojet airflow partially. Fixed structural element retains two sets of deflecting grates arranged sideways, on the flap both sides.
EFFECT: decreased overall dimensions and weight of thrust reverser.
8 cl, 4 dwg
