Reactor of the thrust reversal, reducing the distance to the landing of aircraft

摘要

Reactor (1) to the thrust reversal, characterized in that it comprises an air inlet (2), a nozzle (3) and a motor of base (5) as well as a secondary channel (4) made of annular shape between a casing (6) which is permeable to air and adjustable for the operation of the thrust reversing positions, and a wall of housing (7) of the motor of base (5), and upstream of the nozzle (3) it is provided with a cone of the turbine outlet (40) shells adjustable (10, 11), making it possible to obtain the degree of blocking flow through the nozzle (3) and the inner walls of the casing (6) are coated with refractory material.