Guided missile hanging system

Abstract

The invention discloses a guided missile hanging system. The guided missile hanging system comprises a car body and a wheel driving mechanism; and the wheel driving mechanism is arranged below the car body. The guided missile hanging system further comprises a missile support mechanism and a six-degree-of-freedom adjusting mechanism; the six-degree-of-freedom adjusting mechanism is arranged above the car body; the missile support mechanism comprises missile support bases, missile support clamps and clamping blocks; the six-degree-of-freedom adjusting mechanism comprises a pitching frame; two missile support bases are respectively fixed at the front and back ends of the upper surface of the pitching frame; the clamping blocks are mounted on the missile support bases; arc grooves A are formed in the clamping blocks in the left-right direction; the missile support clamps are semicircular, and are provided with coaxial arc grooves B in the side surface edges; the arc grooves B are through grooves, and are provided with teeth on the inner sides; the missile support clamps are mounted in the arc grooves A in the clamping blocks; the missile support clamps and the clamping blocks are connected through rotating shafts; the rotating shafts penetrate through clamping plates and the arc grooves B; the rotating shafts and the clamping blocks are matched and mounted through bearings; teeth are arranged on the surfaces of the rotating shafts; the teeth on the rotating shafts are engaged with the teeth in the arc grooves B in the missile support clamps; and the rotating shafts are connected with corresponding servo motors. The guided missile hanging system has the beneficial effects of: firm fixation of guided missiles, stable lifting, high adjusting precision and capability of steering in situ.

Description

technical field [0001] The invention relates to the technical field of missile transportation and installation, in particular to a missile hanging system. Background technique [0002] When the vehicle is lifted, especially for a vehicle with a long length, such as a bomb vehicle, the lifting force distribution of the general lifting mechanism is uneven, resulting in the inability to lift smoothly. In order to make the lifting force distribution more uniform, the general In the practice, the number of lifting arm mechanisms is simply increased, but the overall weight of the vehicle is increased, which is not conducive to the driving of the vehicle. And general missile transport equipment is the same as common automobile, realizes turning by steering wheel, but for missile transport equipment, because the length of missile is long, traditional steering equipment is beneficial to the steering of missile transport equipment. When transported to the designated location for inst...

AI Technical Summary

Problems solved by technology

[0002] When the vehicle is lifted, especially for a vehicle with a long length, such as a bomb vehicle, the lifting force distribution of the general lifting mechanism is uneven, resulting in the inability to lift smoothly. In order to make the lifting force distribution more uniform, the general The practice is simply to increase the number of lifting arm mechanisms, but it increases the overall weight of the vehicle, which is not conducive to the driving of the vehicle.

And the general missile transportation equipment is the same as the ordinary car, realizes steering through the steering wheel, but for the missile transportation equipment, due to the long length of the missile, the traditional steering equipment is not conducive to the steering of the missile transportation equipment.

When transported to the designated location for installation, other auxiliary machinery is usually required to clamp the missile and rotate it in multiple directions to finally realize the installation of the missile. Since the angles of the missiles on each missile transport vehicle are inconsistent, the auxiliary machinery clamps the The process of multi-directional rotation takes a lot of time, resulting in low efficiency of missile placement

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