CONTROL DEVICE FOR TURBOJET PUSH INVERTER, REALIZING LOCKING OF THE INVERTER

摘要

A thrust reverser control device for a turbojet engine nacelle comprising movable parts (10) powered by actuators (12), which deploy to reverse the thrust, which device comprises a first lock control (24) acting on the motorized system and a second blocking control acting mechanically on the movable elements, which prevent when they are deployed deployment of these movable parts (10), characterized in that it comprises a means (44) which in the case of the implementation of the mechanical control, prevents the disengagement of the first command.