A multi-degree-of-freedom restraint auxiliary support device for reverse launching missiles

Abstract

The invention provides a multi-degree-of-freedom restraint auxiliary support device for reverse launch missiles, which includes a guide rail, which is fastened and installed in the launch equipment, grooves are arranged on the guide rail, and axial limit blocks are fastened on the guide rail; push plates Located between the axial limiting block and the groove, the axial limiting block is in close contact with the push plate, and the push plate is in close contact with the groove; the parallelogram mechanism includes a bottom plate, a first rotating shaft, and a second rotating shaft , the third rotating shaft, the fourth rotating shaft, the first connecting rod, the second connecting rod and the arc baffle device; The rotating shaft is connected to the bottom plate; the first connecting rod and the second connecting rod are connected to the arc baffle device through the third rotating shaft and the fourth rotating shaft; the first connecting rod and the second connecting rod are connected through the first rotating shaft, The second rotating shaft, the third rotating shaft and the fourth rotating shaft are linked. The invention realizes full constraints of missiles with multiple degrees of freedom and improves product transportation safety.

Description

technical field [0001] The invention relates to the technical field of missile auxiliary support, in particular to a multi-degree-of-freedom restraint auxiliary support device for reverse launch missiles. Background technique [0002] Missile transportation, also known as "missile handling" or "missile transfer". The process of using vehicles, trains, planes, ships and other means of transportation to transfer missiles from one point to another. [0003] At present, the missiles are mostly fixed by the ammunition-fixing mechanism during transportation, but the function of the ammunition-fixing mechanism is single, and most of them can only restrain a single degree of freedom of the missile, while the remaining five degrees of freedom still have a certain range of motion, and it is impossible to realize the full freedom of the missile. The degree of reliability is constrained, resulting in a decrease in the firmness and an increase in the danger of the missile during transpo...

AI Technical Summary

Problems solved by technology

This patent document discloses a support mechanism with a guide that can be adjusted steplessly. It does not solve the problems of insufficient freedom constraints and low firmness during missile transportation, and the reliability of missile transportation is poor.

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