KR100437008B1 - Warhead - Google Patents

Abstract

The present invention relates to a warhead, and in the related art, a warhead fired from a barrel or a barrel is moved forward while rotating to the right, so that the effective range of the warhead decreases according to the right inclination. According to the present invention, a warhead that is rotated by a steel wire which forms a derivative that induces air flow in a direction opposite to the direction of rotation of the steel wire and forms inside the barrel or barrel is rotated in the opposite direction, and thus the warhead rotates. In order to extend the effective range straight forward instead.

Description

Warhead {Warhead}

The present invention relates to warheads fired from guns, and more particularly, to improving the effective range by improving the structure of the warheads.

For warheads, effective range is the distance within which a warhead may be in effect, which is also the maximum distance a flying warhead may fly immediately without bending from side to side by the rotational centrifugal force.

In general, gun guns manufactured for horse killing have increased the function of killing by forming a plurality of steel wires on the inner circumference of the barrel in order to increase the killing function and giving rotational force to warheads passing through the barrel.

Steel wires are classified into four tanks and six tanks according to the installation form, four tanks are configured to rotate the four steel wires to the right, six tanks are configured to rotate the six steel wires to the right.

If the steel wire turns to the left, it can be called a 4 or 6 trillion left line.

As such, when the warhead passing through the barrel is rotated by the steel wire, the warhead continues to rotate while passing through the target, causing severe damage to the target.

However, as described above, the rotation of the warhead by the steel wire may increase the ability to kill horses, but inversely, there is a problem of shortening the effective range of the warhead.

In other words, when the warhead that passed through the barrel rotates, the warhead gradually bends to the right due to the rotational centrifugal force, so the effective range of the gun is shortened. The effective range of the 2 rifle was limited to 400m.

The present invention has been made to solve the above-described problems, the present invention partially improves only the structure of the warhead without improving the structure of the gun, thereby straightening the ballistics of the warhead to increase the effective range while killing the original warhead Its purpose is to provide warheads that do not degrade.

The present invention is configured as follows to achieve the above object. That is, the present invention is to form a derivative that induces the flow of air in the warhead flying while rotating by the wire of the barrel, thereby preventing the warhead to be bent in one direction by the rotational centrifugal force to increase the effective range.

1 is a perspective view of one embodiment of the present invention

2 is a cross-sectional view of another embodiment of the present invention.

3 is a cross-sectional view showing an operating state of another embodiment of the present invention.

Figure 4 is another embodiment of the present invention

<Explanation of symbols for the main parts of the drawings>

1 ..................... casings

2 ..........................

3 ...... Inclined groove

4 ............... wing

41 .......... Shaft

42 .......... Spring

M-16, K-1, and K-2 rifles are currently used in the military, and the killing effect is further improved by the group 6 priority method, but the effective range of the rifle is M-16: 460M, K. -1 and K-2: 400M, M-60 machine gun: 1100M, and there are sniper rifles that are used for special purposes in the military. This will improve military mobility and contribute to the modernization and scientificization of military equipment.

In particular, in view of this fact, the maneuverability of the military is the same as that of military combat. Therefore, the technique of increasing the effective range of the rifles and machine guns according to the present invention is also necessary for the performance improvement and the functional improvement of personal portable equipment. Other technical developments are currently under study at the Department of Defense System Development and the Defense Science Research Institute. However, there is no doubt that modern war is a speed war and a technical war. In response to this fact, the developer of the technology has established the technology to increase the effective range of the rifles and machine guns, and to improve the killing effect.

Hereinafter, exemplary embodiments of the present invention will be described in detail with reference to the accompanying drawings.

1 is a perspective view illustrating a state in which a warhead and a casing are separated according to the present invention.

As shown in Figure 1, the present invention is configured by forming a derivative (3) in the warhead to induce the flow of air so that the warhead fired from the gun can rotate the warhead in the direction opposite to the direction in which it is rotated by the steel wire In this case, the derivative 3 may be configured with an inclined groove 30 formed in the body of the warhead 2, the inclined groove 30 is preferably formed on the rear side of the warhead.

The present invention configured as described above proceeds while the warhead (2) fired from the gun is rotated to the right along the line of the barrel, and from the time the warhead (2) passes through the barrel, the warp groove (30) formed at the rear of the warhead As a result, the flyhead is applied to the warhead while the rotational force is applied to the left, thereby correcting the warhead 2 to be deflected to the right by the rotational centrifugal force caused by the steel wire, thereby increasing the effective range of the warhead.

2 is a cross-sectional view showing another embodiment of the present invention, Figure 3 is a cross-sectional view showing an operating state of another embodiment of the present invention, the wing 4 is installed in the inside of the inclined groove 30 and the wing thereon The spreading means is installed, but the spreading means is constituted by a spring 42 so that the wings installed on the shaft 41 are unfolded by the spreading means while leaving the barrel or barrel, so that the warhead 2 is in the left direction opposite to the direction of rotation of the steel wire. The force to rotate was made larger.

Unfolding means of the wing 4 installed in the inclined groove 30 may be implemented by the configuration as shown in FIG. That is, the hollow inside the warhead to form a push rod 51, but the push rod 51 is elastically installed by the spring 52 , if the head of the push rod 51 is pushed outward push the wing 4 to the outside to configure and head unit by installing gunpowder unit 53 connected to the fuse (fuse) 54, a fuse 54 by a charge, the explosion in the gunpowder explosion or barrel in the cartridge case of the plunger 51 is When the ignition is exploded 53 explodes, and when the explosive 53 is formed a space portion, the push rod 51 is pushed outward by the spring 52 to spread the wings (4).

According to another embodiment of the present invention as the propulsion force by the explosion of the ammunition inside the casing (1), the warhead (2) proceeds along the barrel and while rotating through the barrel is rotated to the right by the direction of the barrel's steel wire.

At this time, the gunpowder 53 installed at the rear side of the warhead is ignited through a fuse (firing line) ignited by the heat of the explosives in the casing. Is generated.

Then, when the warhead 2 passes through the barrel, the spring 52 pushes the pusher 51 , so the pusher 53 pushes the wing 4, and the wing 4 moves the shaft 41. It is pivoted to the center and the rear end of the wing 4 protrudes outward of the inclined groove 30 to apply a rotational force to the warhead 2 in the left direction.

The present invention is not limited to the above embodiments, and various modifications can be made within the scope of the technical idea of the present invention.

The present invention solves the disadvantages of the conventional M-16, K-1, K-2 rifle as described above means to improve the existing shortcomings by increasing the effective range, while exhibiting the technical means for the purpose of improving the performance, function Due to the structure function of the first six guns of the existing rifle, the ammunition explodes in the chamber of the gun and is guided through the six tanks of the barrel, that is, the right six-bar steel line, passing through the muzzle and exiting the barrel. As a result of the rotational centrifugal force caused by the group 6 priority in the barrel, the barrel is expelled from the chamber and guided to the steel line inside the barrel of the existing group 6 in order to give a relative functional effect on the warp. As soon as the bullet leaves the muzzle, it is designed to receive the left turn force. It is possible to increase the effective range of the rifle without improving the existing rifle.

Claims (4)

In the structure of the warhead (2) is formed by forming a derivative (3) for inducing the flow of air, the derivative (3) is inclined groove 30, the wing which is rotatably installed in the shaft (41) therein (4), and warhead, characterized in that consisting of the spreading means for rotating the wings 4 after the launch by rotating around the axis (41). The spreading means according to claim 1, wherein the spreading means of the blades (4) includes a spring (52), a push rod (51) provided by the spring (52), and a gunpowder that restricts contact between the push rod (51) and the blade (4). Warhead, characterized in that consisting of a fuse (53) for igniting part 53 and gunpowder (53). delete delete