METHOD FOR REVERSING THE THRUST PRODUCED BY A POWER PLANT OF AN AIRCRAFT, DEVICE FOR IMPLEMENTING IT AND NACELLE EQUIPPED WITH SAID DEVICE

摘要

The object of the invention is a method aimed at reducing, canceling or reversing the force generated by at least one air flow exiting from a propulative assembly (14) of an aircraft by deflecting at least part of the flow (Fi) likely to participate in the thrust. It consists in injecting at the level (30) of the propulsion unit a fluid (F1, F2, F3) called thrust reversal fluid for deviating by a entrainment effect, from the interior. of the nacelle (12) in the direction of the exterior of the nacelle, at least part (Fi ′) of the flow likely to participate in the thrust.