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A step-by-step shearing type directional button automatic release device

A technology of automatic release and directional buttons, which is applied in the direction of self-propelled bombs, projectiles, offensive equipment, etc., can solve the problems of potential safety hazards, the need for manual operation of the detachment function, and prolonging the launch time, achieving simple structure, convenient assembly, and improved fitness effect

Active Publication Date: 2017-02-08
JINXI IND GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to solve the problem that the shedding function of the traditional directional button structure requires manual operation, prolongs the launch time, and has potential safety hazards, and provides a directional button automatic release device with reliable structure and excellent performance

Method used

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  • A step-by-step shearing type directional button automatic release device
  • A step-by-step shearing type directional button automatic release device
  • A step-by-step shearing type directional button automatic release device

Examples

Experimental program
Comparison scheme
Effect test

Embodiment

[0025] A step-by-step shearing type directional button automatic release device of the present invention, such as figure 1 As shown, it includes a locking screw 1, an orientation button 2, a positioning cylinder 3, a pull rod 4, a support block 5, a screw cover 6 and a screw 7;

[0026] Such as figure 2 As shown, the center of the directional button 2 has a stepped through hole, and the inner wall of the larger hole at the upper end of the directional button 2 stepped through hole is processed with an internal thread;

[0027] Such as image 3 As shown, the locking screw 1 includes a threaded section at the lower end and a cylindrical positioning section at the upper end, and an annular shear groove is opened between the threaded section and the positioning section at the locking screw 1; the outer diameter of the positioning section of the locking screw 1 is smaller than the lower end of the directional button 2 The inner diameter of the hole matches;

[0028] Such as F...

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PUM

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Abstract

The invention relates to a step-by-step shearing type automatic release device for a directional button, which belongs to the field of civilian rockets. A step-by-step shearing type directional button automatic release device of the present invention includes a locking screw, a directional button, a positioning cylinder, a pull rod, a support block and a screw cover; The rectangular hole on the table, the outer plate surface of the locking screw connection hole at the front end of the pull rod is welded to fix the directional button, and the locking screw passes through the stepped through hole in the center of the directional button, so that the front end is threadedly connected with the threaded hole on the side wall of the projectile body; the pull rod The inner board surface at the connecting hole of the rear end support block fixes the support block by screws, and the front end of the support block is against the side wall of the projectile body, so that the pull bar is parallel to the axis of the projectile body. The automatic release device of the directional button of the present invention has simple structure and convenient assembly. On the basis of ensuring the original positioning, locking and other basic functions, it realizes the automatic release function when launching, greatly improves the adaptability of civilian guided rockets, and has important advantages. Promote application value.

Description

technical field [0001] The invention relates to a step-by-step shearing type automatic release device for a directional button, which belongs to the field of civilian rockets. Background technique [0002] During the transportation of civilian rockets, the directional button located at the tail of the rocket is mainly used for positioning, guiding and locking; during the launch process, it cooperates with the spiral guide groove of the rocket barrel to ensure that the rocket will rotate at a low speed after ejecting from the muzzle Movement to reduce the adverse effects of engine thrust eccentricity and projectile shape asymmetry. [0003] At present, civil rockets are developing towards precision guidance, and their inertial navigation system cannot work normally when the projectile body is rotating. can fall off automatically. [0004] Although the existing structure can realize the shedding function of the directional button, it needs to be manually operated before the ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F42B15/00
Inventor 刘永兵李照勇王金东杜红英尹新明唐宏周伟强周波毕军民耿天翼
Owner JINXI IND GRP