Double flux turbine thrust reverser with asymmetric doors

摘要

The thrust reverser consists of hinged flaps which fit into the outer wall of the flow duct behind the turbojet fan when in the closed position and deflect the flow when deployed. The flaps (27) on one side of the engine are narrower than the flaps (37) on the opposite side. The jet engine is mounted beneath the wing of an aircraft, with the narrower thrust reversal flaps situated at the top of the engine and the broader ones at the bottom, producing a thrust reversal flow which is greater on the underside.