THRUST REVERSER DEVICE WITHOUT A CONTROL ROD IN THE STREAM

摘要

The present invention relates to a jet engine nacelle (1) provided with at least one thrust reverser device which includes a deflection means (41) and at least one cowl (30) translatable in a direction substantially parallel to a longitudinal axis of the nacelle between a closed position, in which said cowl ensures the aerodynamic continuity of the nacelle and covers the deflection means, and an open position, in which said cowl opens a passage into the nacelle and uncovers the deflection means, the thrust reverser device moreover including at least one blocking flap (60) pivotably mounted by at least one end attached to a rear portion of the deflection means, wherein said jet engine nacelle is characterized in that the pivoting end is also translatably connected to the rear portion of the deflection means.