Missile bay section butt joint and disconnection device

Abstract

A missile bay section butt joint and disconnection device comprises a fixed clamp (1), a movable clamp (4), two guide rods (2) and two lead screws (3). The two guide rods (2) are arranged on the fixed clamp (1) and the movable clamp (4) in a vertically symmetrical mode, the two lead screws (3) are arranged on the fixed clamp (1) and the movable clamp (4) in a bilaterally symmetrical mode, the guide rods (2) and the lead screws (3) are fixed to the fixed clamp (1), and the movable clamp (4) can move along the guide rods (2) and the lead screws (3). The fixed clamp (1) is composed of an upper part and a lower part, and the movable clamp (4) is composed of an upper part and a lower part. Adjusting handles (5) connected to the guide rods (2) or the lead screws (3) in a sleeving mode are arranged on the movable clamp (1) and drive the movable clamp (4) to move along the guide rods (2) and the lead screws (3). Missile bay sections can be driven to move synchronously with the movable clamp by rotating the adjusting handles (5), and thus butt joint or disconnection of the missile bay sections can be achieved.

Description

technical field [0001] The invention belongs to the invention and relates to a docking disassembly device for a missile compartment. Background technique [0002] The connection forms of the missile compartment are becoming more and more diverse, and sockets have been widely used in various models. Compared with other connection methods, the socket has a great dependence on the machining accuracy, so the requirements for the docking device are correspondingly high. In the past, the docking of cabins mostly adopted the structure of a jig, which required an easy-to-move cabin docking vehicle body, multiple snap rings and operating mechanisms. This structure is relatively cumbersome, and there is a moment between the direction of the force and the axis of the projectile body. It is time-consuming and labor-intensive to dock and disassemble the cabin, and the versatility is poor. Contents of the invention [0003] The purpose of the present invention: to propose a docking di...

AI Technical Summary

Problems solved by technology

This structure is relatively cumbersome, and there is a moment between the direction of the force and the axis of the projectile body. It is time-consuming and labor-intensive to dock and disassemble the cabin, and the versatility is poor.

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