The device for aiming anti-aircraft missile self-propelled units

摘要

The invention relates to military equipment and can be used in the construction of launchers mounted on towers of self-propelled anti-aircraft short-range and employees for a single, sequential or salvo launch homing missiles. The apparatus comprises two actuating units, each of which consists of a universal trigger module platform guidance, the guidance control unit platform. guidance platform rigidly mounted on brackets that are mounted at the stern of the tower symmetrically about its longitudinal axis. guidance platform is designed as an electromechanical drive guided weapons and speed reducer. The output shaft gear rigidly connected to the turntable and connected by a kinematic pair with a sensor measuring the rotary angle position platform elevation and sector through kinematic pairs kinematically connected to the output shaft of the electromechanical actuator. The electromechanical actuator comprises a gear, an electric motor, two powder clutch, tachometer, manual transmission. The motor shaft is rigidly connected to the drive gear pinion that is connected kinematically with the driving gear reducer. Universal actuating modules fixedly mounted on the rotary platform via fastening elements, which are rotated in a horizontal plane at an angle α relative to the longitudinal axis and are inclined outwardly to the horizontal plane at an angle towers β. The control units are placed and secured in the brackets. The technical result - improvement drive for missile guidance vertically while ensuring a safe launch homing missiles. 5-yl.