Connecting structure suitable for missile launcher loading

Abstract

The invention provides a connecting structure suitable for missile launcher loading. The connecting structure comprises a missile united loading module, a missile launcher and a vehicle-bone launchingcontrol cable, wherein the missile united loading module is provided with a united loading frame cable, the united loading frame cable adopts a one-driving-four structure mode and comprises a rectangular connector plug, and the vehicle-bone launching control cable comprises a rectangular connector socket; the rectangular connector socket is arranged on the upper portion of a launcher body, and the rectangular connector plug is arranged on the lower portion of a missile united loading frame; and when the missile united loading module is arranged on the missile launcher, the rectangular connector plug can be connected into the rectangular connector socket in a matched and inserted mode, so that rapid inserting connection of a large-diameter missile launching cable is achieved. According tothe connecting structure suitable for missile launcher loading, the connection of the electrical plug is completed while a launcher structure is loaded with the united loading module, so that the loading time is saved, the loading efficiency is improved, and the reliability and the firmness of the connection are improved.

Description

technical field [0001] The invention relates to the launcher technology of a vehicle-mounted anti-aircraft missile weapon system, in particular to a structure and method for loading and connecting a missile assembly module to a missile launcher, and in particular to a connection structure suitable for loading a missile launcher. Background technique [0002] Anti-aircraft missiles refer to missiles launched by the ground, ships or submarines to intercept air targets, and are also called surface-to-air missiles in the West. Due to the high speed and high mobility of most air targets, the vast majority of anti-aircraft missiles have an axisymmetric layout. The power plant mostly uses solid rocket motors, and liquid rocket motors, ram air jet engines and rocket ramjet engines can also be used. [0003] The launcher of the vehicle-mounted air defense missile weapon system is limited by the total weight and the number of missiles loaded is limited. In order to achieve the ability...

AI Technical Summary

Problems solved by technology

No matter which method is used, after the missile is loaded into the launcher, the launch cable needs to be laid one by one from the launch device to each missile. Since the missile is relatively compact and the diameter of the launch cable is large, this process takes a lot of time. Affect loading efficiency and restrict combat effectiveness

[0004] Patent document CN205980935U discloses a missile loading device, which includes a bomb-carrying guide rail, a hand drive device, a bomb-pushing trolley, a leveling support device and a vehicle frame, and the described bomb-pushing trolley is slidably installed on the bomb-carrying guide rail, and pushes The missile trolley is driven by a hand drive device installed at the end of the bomb-carrying guide rail, the vehicle frame is installed on the leveling support device, and the bomb-carrying guide rail is installed on the vehicle frame, but this design still cannot solve the problem of missile loading. The problem of low efficiency when connecting large diameter cables

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