KR20150077504A - Submunition have delayed self-destruct with independent pyrotechnic - Google Patents

Submunition have delayed self-destruct with independent pyrotechnic Download PDF

Info

Publication number
KR20150077504A
KR20150077504A KR1020130165019A KR20130165019A KR20150077504A KR 20150077504 A KR20150077504 A KR 20150077504A KR 1020130165019 A KR1020130165019 A KR 1020130165019A KR 20130165019 A KR20130165019 A KR 20130165019A KR 20150077504 A KR20150077504 A KR 20150077504A
Authority
KR
South Korea
Prior art keywords
slider
striker
fuse
housing
screw
Prior art date
Application number
KR1020130165019A
Other languages
Korean (ko)
Inventor
황성배
김민석
Original Assignee
주식회사 한화
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 주식회사 한화 filed Critical 주식회사 한화
Priority to KR1020130165019A priority Critical patent/KR20150077504A/en
Publication of KR20150077504A publication Critical patent/KR20150077504A/en

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/20Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C1/00Impact fuzes, i.e. fuzes actuated only by ammunition impact
    • F42C1/02Impact fuzes, i.e. fuzes actuated only by ammunition impact with firing-pin structurally combined with fuze
    • F42C1/08Impact fuzes, i.e. fuzes actuated only by ammunition impact with firing-pin structurally combined with fuze with delayed action after ignition of fuze or after impact
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C11/00Electric fuzes
    • F42C11/06Electric fuzes with time delay by electric circuitry

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Air Bags (AREA)

Abstract

The present invention relates to a submissile fuze having an independent pyrotechnic self-destruct unit, wherein an impulse fuze part and a delay part emitted from a submissile to be exploded after a certain amount of time are independently operated. Therefore, the submissile fuze having an independent pyrotechnic self-destruct unit minimizes the chance of non-detonation, thereby securing sufficient delay time.

Description

{SUBMUNITION HAVE DELAYED SELF-DESTRUCT WITH INDEPENDENT PYROTECHNIC}

More particularly, the present invention relates to a jacket fuse having self-explosion means, and more specifically, a detonator operative in an impact-like manner and a delay portion detonated after a certain time elapses from a charcoal operate independently of each other, To thereby ensure a sufficient delay time.

Generally, jatang is transported from the ground through a carrier such as a shot or rocket that is fired by a gun, then released from the air and dropped to the ground.

At this time, the conveying body may be rotated or not rotated. Such a conventional charcoal is filled with a high-explosive gas for exploding the inside of the ordinary charcoal, and a penetrator for penetrating gloves such as an armored vehicle or a tank is attached to the bottom of the ordinary charcoal. Such as the penetration of gloves by the use of the dual purpose.

These charcoals are dropped into the air as they are discharged into the atmosphere due to the explosion pressure caused by the explosion of the discharge charge in the conveyance body after the discharged conveyance body reaches the predetermined upper limit. At this time, each of the magazines is dropped by the inertia that they had when they were released, and they fall down on the ground and explode. For this purpose, the jacket is equipped with a new pipe for detonating the high explosive powder. The new pipe is a mechanical pipe which is explosioned by the impact force generated when the charcoal collides with the target or the ground.

However, if the above-mentioned conventional charcoal is not sufficiently impacted at the moment of collision with the ground structure after being released from the air, the conventional charcoal can not be exploded because it is not attacked. That is, when the spark plug is dropped on a buffer zone such as a forest, snow, desert, tree or the like, a sufficient impact force is not applied to the mechanical fuse, so that the mechanical fuse can not be operated and the high explosive can not be attacked.

Such inexplicable self-destructs cause weakening of the attack power and cause explosion in the course of operations in the area, causing material damage. Therefore, most of the jar is additionally equipped with a delay fuse blowing off the jar when the mechanical fuse is not working. This delay fuse is classified into an electromechanical delayed self-destructive fuse that ignites a gunpowder in a mechanical fuse and causes self-destruction when a certain time elapses, and an electronic delayed self-destruct fuse that permits self-propagation using a power circuit and a charging circuit and a timer .

On the other hand, as a means for solving the problem of the ignition of the self-discharge, there has been introduced a technique for preventing the discharge of the spark plug. This is related to the formal delayed self-destructive firing, in which the ignition gun, the delayed gunpowder, and the connecting gunpowder are sequentially ignited through the striker using the rotational inertia force generated during the discharge of the self-propelled gun, So as to neutralize the charm. In the case of the electronic delayed self-destructive fuse, it includes a reserve battery, a power source device, an electric detonator, a timer circuit, a charging circuit, a resistance device, an electronic switch and a wind sensing device. The reserve battery is activated through a striking device operated by the air resistance generated in the process, and the printed circuit board composed of the above-described components is operated and the electric explosion-proof pipe is detonated to neutralize the charcoal.

As a prior art related to this, there is the Korean Registered Patent Publication No. 0306357 (self-destruct device of the grenade, registered on Aug. 8, 2001).

It is an object of the present invention to minimize the failure rate of the self-priming fuse by allowing the delay portion to operate independently when the self-priming fuse is released from the charcoal regardless of whether the slider is loaded or not.

Another object of the present invention is to improve the operation stability and reliability of the self-deflating fuse by preventing the detachment of the detonator in the firing range of the firing pin by moving the slider due to an impact applied to the fuse housing after the slider is mounted have.

In order to solve the above problems,

The present invention relates to a self-destructing fire extinguisher for a fire extinguisher, comprising: a fuse housing having a receiving portion formed therein and a firing pin screw fastened thereto; a main ribbon coupled to an upper portion of the firing screw, A detonator which is accommodated in the receiving portion and which is driven independently of the driving of the declination screw and which is delayed for a predetermined time after the fist housing is discharged from the coin, And a plate coupled to a lower portion of the fuse housing and covering the receiving portion.

The retarder includes a striker rotatably mounted on one side of the slider and rotatably driven by the restraining means, an elastic member embedded in the slider to elastically support the striker, A detonating primer to which the striker rotates and strikes, and a detonator to detonate the detonator after a predetermined time that is ignited by the detonating primer.

Wherein the restricting means comprises a metal sphere which is opposed to the elastic member and supports the striker in an initial state in which the elastic member is compressively deformed, a safety pin inserted into the slider and opposed to the striker to support the metal sphere, And a secondary ribbon which is engaged with the top of the fuse housing and is deployed when the fuse housing is released from the spark plug.

And a position fixing means installed in the housing portion formed in the housing to maintain a loading state in which the slider is vertically positioned below the thinning screw.

Wherein the position fixing means includes: an installation groove recessed in a side wall surface of the accommodating portion; an elastic spring provided in the installation groove; and an elastic spring provided in the installation groove, And a fixing groove formed on a side surface of the slider and into which the fixing pin is inserted.

The fixing groove is formed at a position where the fixing pin can be retracted when the slider is loaded and the igniter is positioned below the vertical scanning screw.

According to the solution of the above problems,

The present invention has the effect of reducing the erroneous rate of the self-priming fuse by allowing the delay unit to operate independently when the self-priming fuse is discharged from the charcoal regardless of whether the slider is loaded or not.

Further, the slider is moved due to an impact applied to the fuse housing after the slider is loaded, thereby preventing detachment of the detonation portion in the sinking range of the dimple screw, thereby improving the operational stability and reliability of the self-deflating fuse.

BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a perspective view showing a configuration of a self-falling fuse according to the present invention; FIG.
2 is a view showing a slider provided with a delay unit according to the present invention;
Fig. 3 is a view showing a state in which the restraining means is released in Fig. 2; Fig.
FIG. 4 is a view showing a state in which the striker strikes the cockpit primer with the restraining means released in FIG. 3; FIG.
5 is a view showing a position fixing means according to the present invention.
6 is a view showing a state in which a slider is loaded;
7 is a view showing a position fixing means which operates according to loading of a slider;

The present invention will now be described in detail with reference to the accompanying drawings.

Hereinafter, a detailed description of known functions and configurations that may unnecessarily obscure the subject matter of the present invention will be omitted.

And embodiments of the present invention are provided to more fully describe the present invention to those skilled in the art.

Accordingly, the shapes and sizes of the elements in the drawings and the like can be exaggerated for clarity.

1 is a perspective view showing a configuration of a self-ignition fuse according to the present invention.

Referring to FIG. 1, a magnet tube 110 according to the present invention includes a fuse housing 100 in which a receiving portion 110 is formed and a firing pin 120 is fastened to an upper portion thereof. A main ribbon 200 coupled to an upper portion of the thumb screw 120 to be deployed when the fuse housing 100 is ejected from the magazine and a main ribbon 200 housed in the receiving portion 110, The detonator 310 is driven independently of the driving of the dimple screw 120 so that the detonator 310 is delayed for a predetermined period of time after the dimple housing 100 is discharged from the charcoal. And a plate 400 coupled to a lower portion of the fuse housing 100 and covering the receptacle 110. The slider 300 includes a slider 300 and a plate 400,

The receiving portion 110 is formed inside the fuse housing 100 and the slider 300 is seated on the fuse housing 100. The slider 300 is seated on the fuse housing 100, As shown in Fig.

Therefore, the receiving portion 110 is opened to extend from one side of the fuse housing 100 to the other side.

The main ribbons 200 are folded at an initial stage and are deployed by a drag force when the fuse housing 100 is discharged from the charcoal.

The slider 300 includes a detonating part 310 which is configured to be detonated by an impact applied to the charging tube, And a delay unit 320 that can be excited when a predetermined time elapses.

The slider 300 has a rectangular shape extending in a predetermined direction and is provided with the structure of the delay unit 320. The slider 300 has a detonator 310 for igniting the discharge tube 300 Respectively.

When the new tube housing 100 is discharged from the magazine, the slider 300 is loaded by being slid in the housing 110. In the loaded state, the detonator 310 is positioned at the center of the fuse housing 100 .

The slider 300 will be described in more detail as follows.

FIG. 2 is a view showing a slider 300 having a delay unit 320 according to the present invention, FIG. 3 is a view showing a state in which the restraining means is released in FIG. 2, 3, the striker 322 strikes the batched primer tube 324 when the restraining means is released.

As described above, the slider 300 is formed in a rectangular shape, and the slider 300 is provided therein with a delay unit 320 for allowing the fuselage housing 100 to be exploded when a predetermined time elapses after the fuselage housing 100 is discharged.

The retarder 320 includes a striker 322 rotatably mounted on one side of the slider 300 and constrained to be rotationally driven by restraining means and a striker 322 built in the slider 300, An igniter 324 for igniting the striker 322 when the striker 322 is rotationally driven upon release of the restraint by the restraining means and an igniter 324 for igniting the igniter And a sparger 325 to detonate the detonator 310.

The ground connection 325 is installed inside the slider 300 along the longitudinal direction of the slider 300 formed in a rectangular shape and has a sinker primer 324 ignited by the striker 322 at one side thereof Respectively.

The striker 322 is installed at one side of the striker 322 provided with the decelerated primer 324.

The striker 322 is installed so as to be pivotally driven in place, and one end of the striker 322 is formed with a striking portion capable of striking the blind primer pipe 324. And the other end is resiliently supported by an elastic member 323 provided inside the slider 300.

The other end of the striker 322 is provided with elastic members 323 and restraining means on both sides thereof.

The elastic member 323 is provided at one side of the other end of the striker 322, and the other side of the elastic member 323 is provided with restraining means.

2 to 4, the striker 322 is forcibly rotated in a clockwise direction so that the elastic member 323 is compressed and deformed, and the striker 322 is in a restrained state .

The slider (300) is provided at the other side with a detonator (310) for igniting the discharge tube.

The restraining means strikes the firing primer 324 by releasing the restraint of the striker 322 at a certain point of time so that the firing primer 324 is ignited to ignite the firing link 325.

The gecko 325 is gradually ignited from one side to the other to ignite and detonate the detonator 310.

That is, the delay time can be adjusted according to the length of the geo-linkage 325.

The restraining means includes a metal sphere 326 which opposes the elastic member 323 and supports the striker 322 in an initial state in which the elastic member 323 is compressively deformed, A safety pin 327 which is inserted into the safety pin 327 and supports the metal sphere 326 while being opposed to the striker 322 and an auxiliary ribbon 327 which is coupled to the upper portion of the safety pin 327, (328).

That is, the other end of the striker 322 has a resilient member 323 compressed and deformed at one side thereof, and a metal sphere 326 is disposed at the opposite side thereof. The metal sphere 326 slides on the slider 300 It is in a state of being held by the safety pin 327 inserted through.

The auxiliary ribbon 328 is expanded and the safety pin 327 is removed from the slider 300 by the drag force so that the restraint of the metal sphere 326 is released and compression deformed And the striker 322 is rotated in the counterclockwise direction to strike the priming primer tube 324.

As described above, in the discharge tube 320 according to the present invention, when the fuse housing 100 is discharged from the charcoal regardless of whether the slider 300 is loaded or not, Is released and the striker 322 can ignite the sinking primer pipe 324, thereby improving the operation stability and reliability of the discharge pipe.

The magazine tube according to the present invention is installed in a receiving portion 110 formed in the new tube housing 100 so that the detonating portion 310 of the slider 300 is positioned vertically below the thumb screw 120 And a position fixing means for maintaining the state of the loading state.

Fig. 5 is a view showing the position fixing means according to the present invention. Fig. 6 is a view showing a state in which the slider 300 is loaded. Fig. 7 is a view showing a position Fig.

5 to 7, the position fixing means includes an installation groove 130 formed in a sidewall of the accommodating portion 110 and an elastic spring 140 provided in the installation groove 130. [ And a fixing pin 150 provided in the mounting groove 130 and resiliently supported in an outer direction of the mounting groove 130 by the elastic spring 140. The fixing pin 150 is recessed on the side surface of the slider 300, And a fixing groove 321 into which the fixing pin 150 is inserted.

The mounting groove 130 is recessed in a side wall of the receiving portion 110 so that the fixing pin 150 can be elastically supported in a direction perpendicular to the moving direction of the slider 300, As shown in Fig.

The elastic spring 140 and the fixing pin 150 are installed in the mounting groove 130. The fixing pin 150 is perpendicular to the sliding direction of the slider 300 in the mounting groove 130, And is installed so as to be movable in one direction.

A flange is formed on the outer circumferential surface of the fixing pin 150 to prevent the fixing pin 150 from being detached from the mounting groove 130.

A part of the fixing pin 150 can be drawn out to the outside of the mounting groove 130, that is, the receiving portion 110. When the slider 300 is slidably driven, the fixing groove 321, The slider 300 is inserted into the fixing groove 321 by the elastic spring 140 so that the position of the slider 300 is fixed.

When the slider 300 is loaded and the detonating part 310 is positioned vertically below the decentering screw 120, the fixing pin 150 is inserted into the fixing groove 321 As shown in Fig.

As such, when the slider 300 is loaded, the position of the slider 300 is fixed by the position fixing means, so that the slider moves due to the impact applied to the fuse housing 100, It is possible to prevent the detonator 310 from deviating from the striking range of the battery 120, thereby minimizing the unintentional rate and improving the operational stability and reliability.

As described above, according to the present invention, when the discharge tube is discharged from the jar, the shock type detonator 310 and the delay type retarder 320 are independently operated do.

That is, when the main ribbon 200 is developed and the thumb screw 120 is prepared to strike the detonator 310 of the slider 300, and when the magenta fuse falls on the ground or collides with the target, When the declination screw 120 strikes the detonator 310, the detonator flare is ignited.

At this time, the slider 300 maintains the loading state in which the detonating part 310 is positioned vertically below the declamping screw 120 by the position fixing means of the present invention.

In addition, the auxiliary ribbon 328 is developed together with the main ribbon 200 to remove the safety fingers from the slider 300, whereby the restraint of the striker 322 by the metal sphere 326 is released, The striker 322 is rotated by the resilient restoring force of the trigger 323, and the triggering cock 324 is hit and ignited.

The ground connection 325 is ignited by the ignition of the sinking primer 324 and when the ground connection 325 is burnt, the ignition is ignited while igniting the ignition portion 310.

Therefore, in the magnetostrictive tube of the present invention, the delay unit 320 operates independently of whether the slider 300 is loaded or not, and when the fuse housing 100 is discharged, the slider 300 is loaded Thereby preventing detachment of the detonating part 310 from the striking range of the declamping screw 120, thereby improving the stability and reliability of operation while minimizing the unintentional shrinkage of the charging tube.

While the present invention has been particularly shown and described with reference to exemplary embodiments thereof, it is clearly understood that the same is by way of illustration and example only and is not to be taken as limitations. It will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the spirit and scope of the invention as defined by the appended claims.

100: Fuse housings
110:
120: Negative screw
130: Installation home
140: Elastic spring
150: Fixing pin
200: Main ribbon
300: Slider
310:
320:
321: Fixing groove
322: Striker
323: elastic member
324: Sash detonator
325: Linkage
326: metal spheres
327: Safety pin
328: Auxiliary ribbon
400: plate

Claims (6)

In the self-destructing fuse of Jatan,
A fuse housing having an accommodating portion formed therein and a thumb screw secured to an upper portion thereof;
A main ribbon coupled to an upper portion of the thumb screw and developed upon ejection of the fuse housing from the magazine;
A detonator which is accommodated in the receiving portion and which is driven independently of the driving of the declination screw and which is delayed for a predetermined time after the fist housing is discharged from the coin, A slider provided with a delay unit for a portion to warp; And
And a plate coupled to a lower portion of the fuse housing to cover the receiving portion.
The method according to claim 1,
Wherein the delay unit comprises:
A striker rotatably installed at one side of the slider and restrained by the restraining means;
An elastic member incorporated in the slider to elastically support the striker;
A decelerating primer which rotates and strikes the striker when the constraining means releases the constraint; And
Wherein the detonator is detonated after a predetermined time that has been ignited by the detonating primer.
The method of claim 2,
The restraining means
A metal sphere opposed to the elastic member and supporting the striker in an initial state in which the elastic member is compressively deformed;
A safety pin inserted into the slider and opposed to the striker to support the metal ball; And
And a secondary ribbon coupled to an upper portion of the safety pin to be deployed upon discharge of the fuse housing from the jar.
The method according to claim 1,
Further comprising a position fixing means installed in a housing portion formed in the housing to maintain a loading state in which the slider is vertically positioned below the thinning screw, Jatan fuse.
The method of claim 4,
The position fixing means,
An installation groove formed on the sidewall of the accommodating portion;
An elastic spring provided in the installation groove;
A fixing pin provided in the mounting groove and elastically supported by the elastic spring in an outward direction of the mounting groove; And
And a fixing groove formed on a side surface of the slider and into which the fixing pin is inserted.
The method of claim 5,
The fixing groove
Wherein the slider is formed at a position where the fixing pin can be inserted when the slider is installed and the igniter is positioned vertically below the sinker screw.
KR1020130165019A 2013-12-27 2013-12-27 Submunition have delayed self-destruct with independent pyrotechnic KR20150077504A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
KR1020130165019A KR20150077504A (en) 2013-12-27 2013-12-27 Submunition have delayed self-destruct with independent pyrotechnic

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR1020130165019A KR20150077504A (en) 2013-12-27 2013-12-27 Submunition have delayed self-destruct with independent pyrotechnic

Publications (1)

Publication Number Publication Date
KR20150077504A true KR20150077504A (en) 2015-07-08

Family

ID=53790239

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020130165019A KR20150077504A (en) 2013-12-27 2013-12-27 Submunition have delayed self-destruct with independent pyrotechnic

Country Status (1)

Country Link
KR (1) KR20150077504A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20170079685A (en) * 2015-12-30 2017-07-10 주식회사 한화 Pyrotechnic self-destruct fuze of submunition with one-piece stab delay tube

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20170079685A (en) * 2015-12-30 2017-07-10 주식회사 한화 Pyrotechnic self-destruct fuze of submunition with one-piece stab delay tube

Similar Documents

Publication Publication Date Title
KR101078153B1 (en) Self-destruct fuze of submunition
KR101543615B1 (en) Grenade mechanism
KR100915706B1 (en) 40mm training shot of a grenade launcher
US9562755B2 (en) Safe and arm mechanisms and methods for explosive devices
KR20010086205A (en) Method and apparatus for removing obstructions in mines
EP2933598A2 (en) Multi-action separator fitted to a munition for separating the fuze and the warhead of the munition
CN113587749B (en) Safety ignition fuze adopting space explosion-proof principle
KR101595699B1 (en) Submunition for Cluster Bomb having a Fuse Protecting Body
KR101331360B1 (en) fuse and method for self-destruct for sub-munition
KR20070101676A (en) Grenade for medium distance fire extinguish
KR101358935B1 (en) Shock resistance self-destruct fuze
KR101519387B1 (en) Independent self-destruct fuse of submunition, unit for fixing slider in loading position and submunition including the same or the sames
KR101768823B1 (en) Submunition for Cluster Bomb having the Forced Arming Device for the Slider Assembly
KR101016834B1 (en) Electronic Delayed Self-Destruct Fuse of Submunition
KR101354783B1 (en) Method of check for electronic delayed self-destruct fuse of submunition
KR20150077504A (en) Submunition have delayed self-destruct with independent pyrotechnic
KR101879944B1 (en) Concussion fuse that ensures alignment between armoring part and firing part
KR101519782B1 (en) Bomblet unit for test that possess withdrawal and blind shell confirmation function
CN102466435A (en) Grenade fuse
RU2456537C2 (en) Firing mechanism for shells of multiple artillery rocket systems
KR101368642B1 (en) pyrotechnic self-destruct device of sub-munition
KR101887257B1 (en) Pyrotechnic self-destruct fuze of submunition with one-piece stab delay tube
KR101541592B1 (en) Independent Self-Destruct Fuse of Submunition
KR101210583B1 (en) 155mm training shot
CN220670341U (en) Self-jump air-explosion ammunition

Legal Events

Date Code Title Description
A201 Request for examination
E902 Notification of reason for refusal
E601 Decision to refuse application