FIELD: mechanical engineering; engines. SUBSTANCE: device is designed for reversing of thrust of turbojet engine with efflux of primary and secondary air. Device has doors turning under action of jack. Point of connection of jack to thrust reverser fixed structure, forward in direction of flow, and point of connection of jack to above-indicated movable door are located on one line with point of contact at level of mechanism of thrust reverser installation on turbojet engine between knife-edge support rigidly coupled with thrust reverser fixed structure, forward in direction of flow, and connecting flange rigidly coupled with boot of turbojet engine. EFFECT: reduced or eliminated torque developed in front fixed structure of device. 6 cl, 5 dwg
