TURBOBLOWER THRUST REVERSER

摘要

The invention concerns a turboblower thrust reverser comprising obstacles (3) retracted, in direct thrust, in the turboblower primary cowling wall (4) and unfolded to form a ring-shaped flux-deviating assembly providing thrust reversal by the action of actuators (6) arranged inside the primary cowling (4). Each obstacle (3) is driven in rotation by a linking element (9) about a mobile pivot (12) which is driven in translation by at least an assembly consisting of said actuator (6) and a guide element (10), the actuator (6) drives the obstacle (3) by its downstream part towards an upstream direction parallel to the turboblower axis and is located in the guide element (10) alignment.