Missile fixing mechanism

Abstract

The invention provides a missile fixing mechanism, comprising a base, a connecting rod structure, a reset structure and a starting device; a limiting block is arranged on the connecting rod structure, the missile is arranged on the base, and the axis of the missile is parallel to the base; the missile fixing mechanism includes a locking state and unlocked state, when the missile fixing mechanism is in the locked state, the limit block is connected to the end face of the missile; when the missile fixing mechanism is in the unlocked state, the limit block is separated from the end face of the missile, and in the radial direction of the missile, the limit block is connected to the end face of the missile. The block is located outside the outer surface of the missile; the missile fixing mechanism can be switched from the locked state to the unlocked state under the action of the starting device, and the link structure can be reset under the action of the reset structure. The invention realizes the fixing and unlocking of the missile through the mutual switching between the two states. The invention acts on the tail of the missile, solves the problem of insufficient installation space in the middle of the missile launching device, and can effectively adapt to the reverse launching form of the missile. .

Description

technical field [0001] The invention relates to the technical field of missile fixation, in particular to a missile fixation mechanism, in particular to an axial missile fixation mechanism suitable for launching missiles in reverse. Background technique [0002] In the process of missile storage and transportation, it is necessary to ensure that the missile can be reliably fixed in the axial direction. During the launch process, it needs to be able to quickly unlock and successfully complete the launch. At present, most of the missiles use the fixing mechanism to achieve the function of axial fixing and unlocking. [0003] A survey is conducted on the fixing methods of domestic multi-type missiles. The research shows that most of the fixing mechanisms are currently installed in the middle or tail of the missile. When the mechanism is installed in the middle, the missile slider is hooked by the hook to realize the axial limit function, but there is enough space for the instal...

AI Technical Summary

Problems solved by technology

However, this device adopts a fixed structure installed in the middle of the missile. When there is not enough space for the installation of the mechanism in the middle of the launching device, the device is not applicable, and the device cannot realize the reverse launch of the missile.

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