KR100545245B1 - Electricity ignition Tear Bomb - Google Patents

Abstract

The present invention relates to an electric ignition tear gas, and more particularly, to an electric ignition tear gas in which a ward can be automatically discharged from the launch tube after the launch of the tear gas using the launch tube.

The first feature of the present invention for achieving the above object is

Warheads filled with tear gas and embedded with a detonating tube and a detonating tube; In the electric ignition tear gas consisting of a ward coupled to the rear of the warhead, and a propellant and a built-in ignition device,

The ward is located in the electric ignition tear gas is provided with an elastic member in the rear, the air discharge hole is formed to penetrate from the front to the rear.

The second feature of the present invention for achieving the above object is

Warheads filled with tear gas and embedded with a detonating tube and a detonating tube; In the electric ignition tear gas consisting of a ward coupled to the rear of the warhead, and a propellant and a built-in ignition device,

The ward is located in the electric ignition tear gas is provided with an electrode terminal separator in the rear, the air discharge hole is formed to penetrate from the front to the rear.

The third feature of the present invention for achieving the above object is

Warheads filled with tear gas and embedded with a detonating tube and a detonating tube; In the electric ignition tear gas consisting of a ward coupled to the rear of the warhead and a built-in propellant and ignition device,

The ward has an annular outer ignition terminal provided at the rear, a circular inner ignition terminal provided inside the outer telephone terminal, and a plurality of elastic members provided at the inner and outer ignition terminals and penetrating from the front to the rear. It is in an electric ignition tear gas with an air discharge hole formed.

The fourth feature of the present invention for achieving the above object is

Warheads filled with tear gas and embedded with a detonating tube and a detonating tube; In the electric ignition tear gas consisting of a ward coupled to the rear of the warhead, and a propellant and a built-in ignition device,

The ward is in an electric ignition tear gas having an annular outer ignition terminal provided at the rear, a circular inner ignition terminal provided inside the outer telephone terminal, and a plurality of air exhaust holes penetrating from the front to the rear.

Electric ignition, tear gas, ward,

Description

Electric Ignition Tear Bomb {Electricity ignition Tear Bomb}

1 is a cross-sectional view of a conventional electric ignition tear gas.

2A is a cross-sectional view of the first embodiment

2B is a cross-sectional perspective view of the ward of the first embodiment

2C is a bottom view of the ward of the first embodiment

3a, b, c are operational states of the first embodiment

4A is a sectional view of a second embodiment

4B is a cross-sectional perspective view of the ward of the second embodiment

4C is a bottom view of the ward of the second embodiment

5a, b, c are operational states of the second embodiment

6A is a cross-sectional perspective view of the third embodiment

6B is a bottom view of the ward of the third embodiment

7A is a cross-sectional perspective view of the fourth embodiment

7B is a bottom view of the ward of the fourth embodiment

* Description of the main parts of the drawings *

200: electric ignition tear gas

10: warhead 11: tear gas 12: detonator 13: delay tube

20: Ward 22: Propellant 23: Ignition Device

23a: ignition jade 23b: ignition cable 23c: ignition terminal 24: support

25: elastic member 26: air discharge hole

30: launch tube 31: insulating support 32: electrode terminal 33: electrode cable

34: electrode terminal separator

400: electric ignition tear gas

40: Ward 42: Propellant 43: Ignition Device

43a: ignition jade 43b: ignition cable 43c: ignition terminal 45: air exhaust hole

46: electrode terminal separator

50: launch tube 51: insulating support 52: electrode terminal 53: electrode cable

54: elastic member

600: electric ignition tear gas

60: Ward 62: Propellant 63: Ignition Device

63a: ignition jade 63b: ignition cable 63c: outer ignition terminal 63d: inner ignition terminal

64: support 65: elastic member 66: air exhaust hole

70: launch tube 71: insulating support 72a: outer electrode terminal 72b: inner electrode terminal

73: electrode cable 74: electrode terminal isolator

800: electric ignition tear gas

80: Ward 82: Propellant 83: Ignition Device

83a: ignition jade 83b: ignition cable 83c: outer ignition terminal 83d: inner ignition terminal

86: air outlet

90: launch tube 91: insulating support 92a: outer electrode terminal

92b: inner electrode terminal 93: electrode cable 94: electrode terminal isolation portion

95: elastic member 96: support

TECHNICAL FIELD The present invention relates to tear gas, and more particularly, to a tear gas in which a ward can be automatically discharged from the launch tube after the tear gas is released using the launch tube.

In general, the conventional electric ignition tear gas is shown in Figure 1,

The tear gas 11 is filled with a warhead 10 is filled with a detonation tube 12 and a delay tube 13, and a ward 20 coupled to the rear of the warhead (10).

In particular, the ward 20 has a built-in propellant 22 to explode into the ignition device 23,

The ignition device 23 is an ignition jade 23a embedded in the propellant 22, an ignition terminal 23c installed behind the ward 20, and an ignition jade 23a connected to the ignition terminal 23c. It consists of a cable 23b.

In the conventional firing process of the electric ignition tear gas, the tear gas is inserted into the launch tube 30 in full length, and at this time, the ignition terminal 23c of the ward 20 is in contact with the electrode terminal 32 of the launch tube 30 to prepare for launch. Is done.

Thereafter, an electric ignition trigger device (not shown) is operated to supply current to the electrode terminal 32,

Thereafter, a current is supplied to the ignition terminal 23c of the electric ignition tear gas, and a current is supplied to the ignition jade 23a connected to the ignition terminal 23c and the ignition cable 23b to ignite.

Then, the explosive propellant 22 surrounding the ignition jade 23a is exploded and the warhead 10 is separated from the ward 20 and fired by the explosive force.

However, the conventional electric ignition tear gas has a problem in that it is inconvenient to use because it discharges and reloads the launch port of the launch tube 30 toward the ground to discharge the ward 20 in the launch tube 30 after the tear gas is released.

Accordingly, the present invention has been made to solve the above problems, by providing an elastic member on the rear of the ward to enable the ward to automatically discharge from the launch tube by using the explosion pressure and elastic force of the elastic member generated during tear gas firing. Its purpose is.

The first feature of the present invention for achieving the above object is

Warheads filled with tear gas and embedded with a detonating tube and a detonating tube; In the electric ignition tear gas consisting of a ward coupled to the rear of the warhead and a built-in propellant and ignition device, the ward is provided with an elastic member in the rear, the electric ignition tear gas is formed in the air discharge hole to penetrate from the front to the rear have.

The second feature of the present invention for achieving the above object is

Warheads filled with tear gas and embedded with a detonating tube and a detonating tube; An electric ignition tear gas, comprising: a ward coupled to the rear of a warhead and having a built-in propellant and an ignition device, wherein the ward is provided with an electrode terminal separator at the rear and an air discharge hole is formed to penetrate from the front to the rear. Is in.

The third feature of the present invention for achieving the above object is

Warheads filled with tear gas and embedded with a detonating tube and a detonating tube; In the electric ignition tear gas consisting of a ward coupled to the rear of the warhead, and a propellant and a built-in ignition device,

The ward has an annular outer ignition terminal provided at the rear, a circular inner ignition terminal provided inside the outer telephone terminal, and a plurality of elastic members provided at the inner and outer ignition terminals and penetrating from the front to the rear. It is in an electric ignition tear gas with an air discharge hole formed.

The fourth feature of the present invention for achieving the above object is

Warheads filled with tear gas and embedded with a detonating tube and a detonating tube; In the electric ignition tear gas consisting of a ward coupled to the rear of the warhead, and a propellant and a built-in ignition device,

The ward is in an electric ignition tear gas having an annular outer ignition terminal provided at the rear, a circular inner ignition terminal provided inside the outer telephone terminal, and a plurality of air exhaust holes penetrating from the front to the rear.

Hereinafter, the present invention will be described by dividing the first to fourth embodiments as follows.

Electro-ignition tear gas 200 as a first embodiment of the present invention is shown in the accompanying drawings, Figures 2a to 3c,

Ward 20 is coupled to the warhead (10)

The warhead 10 is filled with tear gas 11, the detonation tube 12 and the retardation tube 13 is made of,

The ward 20 includes a propellant powder 22 installed to correspond to the delay tube 13 of the warhead 10, a ignition jade 23a embedded in the propellant powder 22, and a rear of the ward 20. A pair of ignition terminals 23c installed in the ignition device, an ignition cable 23b connecting the ignition jade and the ignition terminal, an ignition device 23 for igniting the propellant 22, and a protrusion formed at the rear of the ward 20. It consists of a pair of elastic members 25 fixed to the support 24 and connected to the ignition terminal 23c, and a plurality of air exhaust holes 26 penetrating from the front of the ward 20 to the rear.

Hereinafter, the firing process of the electric ignition tear gas 100 according to the first embodiment of the present invention will be described with reference to FIGS. 3A, 3B and 3C.

3A is a cross-sectional view showing a state where an electric ignition tear gas is loaded into the launch tube 30.

In particular, the launch tube 30 is an insulating support 31 which is installed in close contact with the inner bottom,

A pair of electrode terminals 32 provided in front of the insulating support 31;

An electrode cable 33 connected to the electrode terminal 32 and connected to an electric ignition trigger device (not shown) through the insulating support 31;

 An inner bottom surface of the launch tube 30, that is, protruding from the insulation support 31, is formed of an electrode terminal separator 34 to isolate the pair of electrode terminals 32 from each other,

The electric ignition tear gas 100 is inserted into the launch tube 30 in the electric field is prepared by firing the elastic member 25 in contact with the electrode terminal 32.

In this case, the electrode terminal separator 34 induces the pair of elastic members 25 of the electric ignition tear gas in contact with the pair of electrode terminals 32 of the launch tube 30, respectively.

When the electric ignition trigger device (not shown) is operated, a current is supplied to the connected electrode cable 33, and then, the current is supplied to the ignition jade 23a via the elastic member 25.

Thereafter, the ignition jade 23a supplied with the current is ignited to explode the propellant powder 22.

Then, as shown in Figure 3b, the warhead 10 is launched from the launch tube by the explosive force of the propellant 22, and at the same time the elastic member 25 toward the insulating support 31 by the reaction ward 20 Moves elastically.

Thereafter, as shown in FIG. 3C, the ward 20 is discharged from the launch tube 30 again by the restoring force of the elastic member 25.

At this time, since the resistance of the air is reduced by the air discharge hole 26, the ward 20 is made much smoother discharge in the launch tube 30.

Hereinafter, a second embodiment of the present invention will be described with reference to FIGS. 4A to 5C.

The second embodiment of the present invention is that the part of the ward is different in the electroignition tear gas of the first embodiment,

In the second embodiment, the electric ignition tear gas 200 is composed of an ignition terminal separator 46 behind the ward 40.

The ward 40 includes a propellant powder 42 installed to correspond to the delay tube 13 of the warhead 10, a ignition jade 43a embedded in the propellant powder 42, and a rear of the ward 40. A pair of ignition terminals (43c) installed in the ignition device consisting of a ignition cable (43b) connecting the ignition jade and the ignition terminal (43) for igniting the propellant (42), and protruding to the rear of the ward 40 And an ignition terminal separator 46 for isolating the pair of ignition terminals 43c from each other, and a plurality of air exhaust holes 45 penetrating from the front to the rear of the ward 40.

Hereinafter, the firing process of the electric ignition tear gas 200 according to the second embodiment of the present invention will be described with reference to FIGS. 5A, 5B and 5C.

5A is a cross-sectional view showing a state in which the electric ignition tear gas 200 is loaded in the launch tube 50.

In particular, the launch tube 50 is connected to the insulating support 51 which is installed in close contact with the inner bottom, a pair of electrode terminals 52 provided in front of the insulating support 51, and the electrode terminal 52 It consists of an electrode cable 53 connected to the electrical ignition trigger device (not shown) through the insulating support 51 and the elastic member 54 is connected to the electrode terminal 52, the electrical The ignition tear gas 200 is fully inserted into the launch tube 50, and the elastic member 54 is in contact with the electrode terminal 32.

At this time, the ignition terminal separator 46 has a pair of elastic members 54 of the launch tube 50 and a pair of ignition terminals 43c of the electric ignition tear gas 200 individually contact each other in a loading process. Do not induce.

Then, when the electric ignition trigger device (not shown) is operated, a current is supplied to the connected electrode cable 53, and then the current is supplied to the ignition jade 43a via the elastic member 54.

Thereafter, the ignition jade 43a supplied with the current is ignited to explode the propellant powder 42.

Thereafter, as shown in FIG. 5B, the warhead 10 is fired from the launch tube by the explosive force of the propellant 42, and at the same time, the elastic member 54 is moved toward the insulating support 51 by the ward 40. Moves elastically.

Thereafter, as shown in FIG. 5C, the ward 40 is discharged from the launch tube 50 again by the restoring force of the elastic member 54 of the launch tube 50.

At this time, since the resistance of the air is reduced by the air discharge hole 45, the ward 40 is discharged in the launch tube 50 much smoother.

Hereinafter, a third embodiment of the present invention will be described with reference to FIGS. 6A to 6B.

The third embodiment of the present invention is that the part of the ward is different in the electroignition tear gas of the first embodiment,

In the third embodiment, the electric ignition tear gas 600 includes a circular ignition terminal of the ward 60 and an elastic member is installed.

The ward 60 has a propellant powder 62 installed to correspond to the delay tube 13 of the warhead 10, a ignition jade 63a embedded in the propellant 62, and a rear of the ward 60. Annular outer ignition terminal 63c installed at the inner side, circular inner ignition terminal 63d provided inside the outer telephone terminal 63c at the rear of the ward 60, ignition jade 63a, inner and outer ignition terminals. An ignition device 63 consisting of an ignition cable 63b connecting 63c and 63d to ignite the propellant 62, and fixed to a support 64 protruding from the rear of the ward 60, the inner and outer ignition terminals. A plurality of elastic members 65 connected to 63c and 63d, and a plurality of air discharge holes 66 penetrating from the front to the rear of the ward 60.

In particular, the launch tube 70 for loading and firing the electric ignition tear gas 600 has an insulating support 71 which is installed in close contact with the inner bottom, and an annular outer electrode terminal provided in front of the insulating support 71. 72a), a circular inner electrode terminal 72b provided inside the outer electrode terminal 72a, and connected to the inner and outer electrode terminals 72a and 72b to penetrate the insulating support 71 to form an electric ignition type. Electrode cable 73 connected to the trigger device (not shown), and formed in an annular shape in front of the insulating support 71, the electrode terminal is located between the inner and outer electrode terminals (72a, 72b) to insulate each other It has an isolation 74.

Since the firing process of the electric ignition tear gas of the third embodiment of the present invention is the same as that of the first embodiment, description thereof will be omitted.

Hereinafter, a fourth embodiment of the present invention will be described with reference to FIGS. 7A to 7B.

The fourth embodiment of the present invention is that the part of the ward is different in the electroignition tear gas of the second embodiment,

In the fourth embodiment, the electric ignition tear gas 800 is composed of a circular ignition terminal of the ward 80.

The ward 80 is provided with a propellant gun 82 installed to correspond to the delay tube 13 of the warhead 10, an ignition jade 83a embedded in the propellant gun 82, and an annular ring installed at the rear. Outer ignition terminal 83c, circular inner ignition terminal 83d provided inside the outer telephone terminal 83c at the rear of the ward 80, ignition jade 83a, inner and outer ignition terminals 83c, 83d ) And an ignition device (83) for igniting the propellant (82) and a plurality of air discharge holes (86) penetrating from the front to the rear of the ward (80).

In particular, the launch tube (90) for loading and firing the electric ignition tear gas (800) is an insulated support (91) installed in close contact with the inner bottom, and an annular outer electrode terminal (installed in front of the insulated support (91) ( 92a), a circular inner electrode terminal 92b provided inside the outer electrode terminal 92a, and connected to the inner and outer electrode terminals 92a and 92b to penetrate the insulating support 91 to be electrically ignited. An electrode cable 93 connected to a trigger device (not shown) and an electrode formed in an annular shape in front of the insulating support 91 and positioned between the inner and outer electrode terminals 92a and 92b to isolate each other. It consists of a terminal isolator 94 and a plurality of elastic members 95 fixed to the support 96 protruded from the inner and outer electrode terminals 92a and 92b.

Since the firing process of the electric ignition tear gas of the fourth embodiment of the present invention is the same as that of the second embodiment, description thereof will be omitted.

As described above, the present invention has an effect of quickly and easily reloading the tear gas by automatically discharging the ward of the tear gas from the launch tube.

Claims (4)

A warhead 10 filled with a tear gas 11 and having an aeration tube 12 and a retardation tube 13 embedded therein; In the electric ignition tear gas consisting of: a ward (20) coupled to the rear of the warhead (10) and the propellant (22) and the ignition device (23) built-in, The ward is equipped with an elastic member 25 in the rear, the electric ignition tear gas, characterized in that the air discharge hole 26 is formed so as to penetrate from the front to the rear. A warhead 10 filled with a tear gas 11 and having an aeration tube 12 and a retardation tube 13 embedded therein; In the electric ignition tear gas consisting of; ward (40) coupled to the rear of the warhead 10, the propellant 42 and the ignition device 43 is built-in, The ward 40 is provided with an electrode terminal separator 46 at the rear, the electric ignition tear gas, characterized in that the air discharge hole 45 is formed so as to penetrate from the front to the rear. A warhead 10 filled with a tear gas 11 and having an aeration tube 12 and a retardation tube 13 embedded therein; In the electric ignition tear gas consisting of; ward (60) coupled to the rear of the warhead (10), the propellant (62) and the ignition device (63) built-in, The ward 60 has an annular outer ignition terminal 63c installed at the rear, a circular inner ignition terminal 63d provided inside the outer telephone terminal 63c, and the inner and outer ignition terminals 63c, 63d) is provided with an elastic member 65, the electric ignition tear gas, characterized in that a plurality of air discharge holes 66 penetrating from the front to the rear is formed. A warhead 10 filled with a tear gas 11 and having an aeration tube 12 and a retardation tube 13 embedded therein; In the ignition tear gas consisting of; ward 80 is coupled to the rear of the warhead (10) and the propellant (82) and the ignition device (83) built-in, The ward 80 includes an annular outer ignition terminal 83c installed at the rear, a circular inner ignition terminal 83d provided inside the outer telephone terminal 83c, and a plurality of air penetrating from the front to the rear. Electric ignition tear gas, characterized in that the discharge hole 86 is formed.

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