Missile fixing mechanism

A technology for fixing mechanisms and missiles, applied in the field of axial fixing mechanisms, can solve problems such as inapplicability and inability to achieve reverse launch of missiles, and achieve the effects of convenient operation, simple structure, and reduced damage probability

Active Publication Date: 2020-07-17
SHANGHAI INST OF ELECTROMECHANICAL ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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.

Method used

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Embodiment Construction

[0044] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several changes and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0045] In the description of this application, it should be understood that the terms "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", The orientation or positional relationship indicated by "bottom", "inner", "outer", etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the application and simplifying the description, rather than indicating or implying the referred device Or elements must hav...

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Abstract

The invention provides a missile fixing mechanism. The missile fixing mechanism comprises a base, a connecting rod structure, a resetting structure and a starting device; a limiting block is arrangedon the connecting rod structure, a missile is arranged on the base, and the axis of the missile is parallel to the base; the missile fixing mechanism comprises a locking state and an unlocking state;when the missile fixing mechanism is in the locking state, the limiting block is connected with the end face of the missile; when the missile fixing mechanism is in the unlocking state, the limiting block is separated from the end face of the missile; in the radial direction of the missile, the limiting block is located outside the outer surface of the missile; and the missile fixing mechanism canbe switched from the locking state to the unlocking state under the action of the starting device, and the connecting rod structure can be reset under the action of the resetting structure. Accordingto the missile fixing mechanism, the fixing and unlocking of the missile are realized through mutual switching between the two states, the missile fixing mechanism acts on the tail of the missile, the problem of insufficient installation space in the middle of a missile launching device is solved, and the missile fixing mechanism can effectively adapt to a reverse launching form of the missile.

Description

technical field [0001] The invention relates to the technical field of missile fixing, in particular to a missile fixing mechanism, especially an axial fixing mechanism suitable for launching missiles in reverse. Background technique [0002] During the storage and transportation of missiles, it is necessary to ensure that the axial direction of the missile is reliably fixed, and during the launch process, it must be able to be quickly unlocked and successfully completed. At present, most missiles use a fixed mechanism to achieve the axial fixing and unlocking functions. [0003] According to the research on the way of fixing the missiles of various types of missiles in China, the research shows that most of the fixing mechanisms are installed in the middle or tail of the missiles. When the mechanism is installed in the middle, it hooks the missile slider through the hook to realize the axial limit function, but it needs enough space for the mechanism to be installed in the ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B39/22F42B39/00F42B15/00
CPCF42B39/22F42B39/00F42B15/00
Inventor 张保刚李微微夏津俞刘建刘广许斌蒋君庭赵利娟王萌王波兰
Owner SHANGHAI INST OF ELECTROMECHANICAL ENG
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