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Pressure disturbance wave opening launching box front cover capable of laterally moving and overturning

A technology of lateral movement and disturbance wave, which is applied in the direction of launching devices, rocket launching devices, offensive equipment, etc., can solve the problems of the impact of the projectile’s movement out of the box, long residence time, etc., and achieve a simple and convenient way of opening the cover, shortening the time, The effect of avoiding secondary collisions

Active Publication Date: 2020-11-24
BEIJING INSTITUTE OF TECHNOLOGYGY +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The opening of the front cover by the pressure disturbance wave has the advantages of simple structure and little impact on the projectile body. However, in the traditional structure, the front cover that falls off does a parabolic motion under the initial velocity and gravity generated by the pressure disturbance wave, and stays in the projectile movement channel for a long time. It has a great influence on the movement of the projectile out of the box

Method used

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  • Pressure disturbance wave opening launching box front cover capable of laterally moving and overturning
  • Pressure disturbance wave opening launching box front cover capable of laterally moving and overturning
  • Pressure disturbance wave opening launching box front cover capable of laterally moving and overturning

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Embodiment Construction

[0051] The present invention will be further described in detail through the drawings and examples below. Through these descriptions, the features and advantages of the present invention will become more apparent.

[0052] The word "exemplary" is used exclusively herein to mean "serving as an example, embodiment, or illustration." Any embodiment described herein as "exemplary" is not necessarily to be construed as superior or better than other embodiments. While various aspects of the embodiments are shown in drawings, the drawings are not necessarily drawn to scale unless specifically indicated.

[0053] In the prior art, in the structure where the pressure disturbance wave opens the front cover of the launch box, the gas jet flow ejected from the rocket and missile engine at the initial stage of launch acts on the back cover, and the pressure shock wave generated is reflected to the front cover through the back cover, and the front cover of the launch box 9 Under the actio...

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Abstract

The invention discloses a pressure disturbance wave opening launching box front cover capable of laterally moving and overturning. The launching box front cover is characterized in that a flange seatsleeve and a separation cover body are glued through AB glue, so that the rocket missile launching box front cover can be quickly opened under the action of the pressure disturbance wave to do lateralturnover movement, and the rocket missile launching box front cover can be quickly separated from a missile body movement channel; the structure is safe and reliable, the manufacturing process is simple, and the safety of a projectile body and a launcher can be effectively prevented from being influenced by contact of the cover body and the projectile body.

Description

technical field [0001] The invention relates to the field of the front cover of a rocket and missile launch box, in particular to a pressure disturbance wave which moves sideways and turns over to open the front cover of the launch box. Background technique [0002] The front cover of the rocket missile launch box is an important part of the rocket missile launch box. The front cover must ensure the effective sealing of the launch box during storage and transportation, and provide a suitable storage and transportation environment for rockets and missiles; the front cover must be reliably opened and safely dropped during the launch process to ensure the safe launch of the projectile. [0003] The design of the front cover of the launch box has always been an important part of the design of the rocket and missile launching device. The key points include: 1) When the missile is stored normally, there is an inert gas in the missile launch box, so it is required that the box cove...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F3/04F41F1/00
CPCF41F3/04F41F1/00
Inventor 傅德彬刘浩天陈刚左应朝
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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