CN217520353U - Remote electronic pulse bomb and weapon - Google Patents

Abstract

A remote electronic pulse bomb and weapon comprises a striking module, a circuit module, a connecting module and the like; the connecting module at least comprises a section of line body which is electrically connected with the striking module and the circuit module, and pulse current generated by the circuit module is transmitted to a remote target through the connecting module and the striking module so as to play a role; the module is arranged in a cartridge case, the striking module comprises at least two electrodes, and the electrodes are arranged adjacent to an ejection device; the electronic pulse bullet can be provided for a launching device, such as a shotgun to launch a tube cavity, the electrodes are launched and separated to the periphery under the action of the launching device, and the distance between the electrodes reaches at least 100 mm instantly; in dynamic operation, the circuit module lags behind the flight of the electrodes, so that the line body of the connecting module is stretched and tensed, the electrodes are pulled, the head of the electrodes always keep flying in a forward posture, excessive separation of the electrode spacing is limited, the electrodes can hit a target, and a needle body positioned at the head of the electrodes can effectively puncture the target.

Description

Remote electronic pulse bomb and weapon

Technical Field

The utility model relates to an electronic pulse weapon technical field, in particular to remote electronic pulse bullet and weapon.

Background

The electronic pulse weapon is an effective anti-terrorism and anti-riot electronic device, which is widely applied to military, police, security and other law enforcement departments at home and abroad. The prior common traditional electronic pulse weapon product has the appearance and the size similar to a pistol, mainly comprises a main body and a magazine in structure, wherein the main body is internally provided with a circuit module for generating pulse current; the magazine is generally a disposable consumable, and is detachably mounted on the front portion of the body, and includes a launching assembly and a power assembly, wherein the launching assembly includes at least one pair of electrodes with opposite polarities, the electrodes are connected to the circuit module through wires, and the power assembly is used for launching the electrodes to a remote target.

When the electric pulse weapon is used, an operator pulls a trigger on the main body of the electric pulse weapon, a power component in the magazine is excited, high-pressure gas is released instantly, the two electrodes are emitted to the outside of the magazine, and when the electrodes hit a remote target, a circuit module in the main body conducts current to the target through a lead, so that the muscle of the whole body of the target contracts in a tonic manner, and the autonomous movement capability is lost, so that the control purpose is achieved.

The authoritative research institute and a large amount of practical statistical data show that when two electrodes of the electronic pulse weapon hit a target, the distance between the electrodes needs to reach at least 100 mm, so that pulse current passes through enough organism tissues and organs to form a current loop, and satisfactory control effect can be obtained. To this end, the two electrodes in an electronic pulse weapon magazine are usually set at a firing angle of 5 to 8 degrees, in order to achieve the desired separation distance after firing before hitting the target and thus ensure uniform results. Theoretically, the effect is more pronounced the greater the spacing between the electrodes, the wider the tissue involved, but on the other hand, an excessively large spacing of the electrodes can cause at least one of the electrodes to be dislodged from the target, thereby causing the loss of the effect.

In order to meet the actual combat requirement, the traditional electronic pulse weapon has light, convenient and compact main body and magazine structure design requirements, and is convenient to carry and hide. Besides a launching component and a power component, a magazine of the electronic pulse weapon also contains a lead for conducting current, and the range of the traditional electronic pulse weapon is generally 5-10 meters, so that the magazine is required to store the lead with corresponding length; in addition, since the power structure of the electric pulse weapon requires insulation and is usually made of plastic, the capability of withstanding the kinetic energy shock is very limited, and the propulsion power provided by the power system for the transmitting electrode is also limited, which limits the range and application range of such products.

In recent years, a new type of Electronic pulse bomb, such as the remote Electronic Projectile (XREP) developed by Taser International, inc. The electronic pulse bomb is self-integrated when being launched, and the bomb body comprises a circuit module for generating pulse current, an electrode and other electronic components; the electronic weapon magazine is also called a wireless electronic pulse bullet or a wireless bullet because the electronic weapon magazine carries a circuit module system by itself and does not need a long lead between a connecting electrode and a main body circuit module; such electric pulse projectiles, which lack the power components found in the conventional electric pulse weapon magazines described above, require the use of an additional separate firing device, such as a riot shotgun, to fire them; the emitting device can use stronger emitting power, so that the range of the electronic pulse is greatly increased and can reach about 30 meters.

The Tathery XREP mainly comprises a torsional spring empennage, an electronic pulse generator, a front main electrode, a Jolia fairy palm thorn auxiliary electrode and the like. The torsion spring empennage assembly is unfolded after XREP leaves the tube cavity of the launching device, so that the projectile body is forced to start rotating, and the XREP can fly forwards stably; the electronic pulse generator comprises an integrated circuit module board and a power supply system, and is used for generating electronic pulse current for controlling a target; the front main electrode is 4 electrodes with barb needle bodies at the front parts of the main bodies, and the function of the front main electrode is mainly to puncture a target and fix the electrodes on the target; the front main electrode is structurally combined with the rest parts of the electronic pulse bomb in the flying process and separated from the main body when the bomb body impacts a target, the main body carrying the circuit module is hung on the surface of a human body through a connecting line between the front main electrode and the main body, and meanwhile, 6 Jolia cactus electrodes on the main body automatically expand so as to obtain a larger electrode distance between the main electrode and the auxiliary electrode to enhance the action effect.

The electric pulse bullet device mainly has the following technical defects: 1. the fixed spacing between the 4 main electrodes at the front of the projectile is only 8-15 mm, far less than at least 100 mm required to achieve full control objectives; in addition, because the naturally falling Jolia cactus auxiliary electrode needle body lacks power and hardly punctures the target body effectively, the structural design for increasing the distance between the auxiliary electrode and the main electrode by trying to increase the distance between the auxiliary electrode and the main electrode so as to improve the action effect is not ideal, especially when the target is worn thickly; 2. the torsion spring tail wing at the rear part of the XRAP has the function of promoting the projectile body to rotate after being launched so as to maintain the stable flight of the projectile body, however, the rotating projectile body can also cause the main electrode at the front part of the projectile body to rotate along with the projectile body, when the rotating projectile body contacts a target, the torsion force generated by the rotation of the rotating projectile body influences the target to effectively puncture the target, and the electronic pulse projectile is easy to fall off from the target body; 3. the diameter of the main electrode and the cross-sectional area of the solid structure at the front part of the XREP electronic pulse bomb are obviously increased compared with the electrode of the traditional wired electronic pulse weapon, and the weight of the pulse bomb as a whole is greatly increased when flying, so that the influence of flight resistance and gravity on the pulse bomb is increased; the technical defects influence the action effect, the range and the accuracy of the electronic pulse bomb.

SUMMERY OF THE UTILITY MODEL

The utility model provides an electronic pulse bullet and weapon aims at solving the technical defect of prior art electronic pulse bullet.

In order to achieve the above object, the utility model provides an electronic pulse bullet, include:

a striking module including at least one pair of electrodes for emitting to a remote target; the circuit module is used for generating pulse current; the connecting module is used for electrically connecting the electrode and the circuit module and conducting the pulse current to the remote target through the electrode;

the ejection device is arranged adjacent to the electrodes and ejects and separates the electrodes to the periphery when the electronic pulse bullet is emitted, so that the distance between the electrodes reaches at least 100 mm immediately.

The utility model discloses still provide an electronic pulse bullet, its dynamic structure includes:

the striking module comprises at least one pair of electrodes, the distance between the electrodes is at least 100 mm, and a circuit module is arranged to lag behind the electrode flying and connecting module, and the circuit module is respectively flexibly connected with the electrodes and the circuit module, and the connecting module stretches and tensions under the lagging flying action of the circuit module and acts on the electrodes, so that the electrodes always fly in a forward head posture, and the electrodes are limited from being excessively separated.

Optionally, the pitch of the electrodes is greater after the electrodes are catapulted apart than before the electrodes are catapulted apart.

Optionally, the distance between the electrodes after the electrodes are ejected and separated is 100-600 mm.

Optionally, the connection module includes at least one segment of a flexible wire body.

Optionally, the wire body is a conductor.

Optionally, the circuit module includes a switch, and the switch is turned on after the electronic pulse bomb is launched, so that the circuit module operates and generates a pulse current.

Optionally, the striking module includes an elastic frame, and the elastic frame is disposed on the electrode.

Optionally, the elastic frame maintains the distance between the electrodes after the electrodes are ejected and separated to be fixed at a preset length between 100 mm and 600 mm.

The utility model discloses still put forward a weapon, the weapon includes as above-mentioned any one the electron pulse bullet.

Rigidity for prior art electronic pulse bullet, integral type structure, the utility model provides a different technical solution has adopted different structure configuration and distribution, and is specific: split type emission; flexible connection; and a linearly elongated structural distribution. Compared with the technical scheme of the utility model, the taise XREP electronic pulse bomb in the prior art is taken as an example, the structural form and the interval of the front and the rear electrodes of the former before and after being launched are kept unchanged, and form an integral flight with the circuit and other components, etc., and after the electronic pulse bomb 100 with the technical characteristics of the utility model is launched, the electrodes 21 of the striking module 20 are ejected to the periphery under the action of an ejection device 30 and separated from each other, the interval of the electrodes reaches at least 100 mm instantly, in addition, the striking module 20 and the circuit module 40 are also separated from each other, and a flying unit with a relatively independent structure is formed respectively; all parts of the former structure are rigidly combined, and the striking module 20 and the circuit module 40 of the latter are connected by a connecting module 50 with flexible characteristics, even the striking module 20 or the circuit module 40 can be arranged in a flexible structure, so that the whole structure of the electronic pulse bomb 100 has flexible characteristics; the overall geometric length of the former structure is only 60-75 cm, while the latter is extended and distributed by 200-700 mm linear chains, so as to form dynamic ordered arrangement among the structures of the striking module, the connecting module and the circuit module.

The split type launching mechanism with the technical characteristics of the utility model can obviously reduce the volume and the weight of each independent structure part, and effectively reduce the power consumption and the wind resistance; the flexible structure adopted in the utility model is a new field (such as flexible wings, etc.) actively explored and researched by many countries at present, compared with the rigid structure, the flexible structure has self-adaptability, can realize the active adjustment of the structure form according to the aerodynamic stress condition, reduces the power consumption, and obtains the best aerodynamic characteristic; the linear extension structure distribution is adopted, so that the stress action point is obviously moved backwards, the lever power arm is extended, and the dynamic balance stability can be more easily obtained under the condition of the same mass.

The structure characteristics can reduce the weight of the projectile body of the electronic pulse projectile, reduce the aerodynamic resistance of the projectile body during flying, enhance the balance and flying stability of the structure, achieve the dynamic ordered arrangement of all functional parts, maintain the electrodes in the correct head forward attitude for flying all the time, limit the excessive separation between the electrodes, maintain the distance between the electrodes in the range of 100 plus one millimeter and 600 millimeters, and are beneficial to improving the range and accuracy of the electronic pulse projectile and improving the target hitting capability and action effect.

Drawings

In order to more clearly illustrate the technical solutions and features of the present invention, the following embodiments are briefly described and presented in the accompanying drawings, and it is obvious that the following embodiments are only specific embodiments of the present invention and are not intended to limit the technical field and scope thereof.

Fig. 1 is a schematic view of a dynamic structure of an embodiment of the electronic pulse bomb according to the present invention in a flight process;

fig. 2 is a schematic diagram of a dynamic structure of another embodiment of the electronic pulse bomb according to the present invention during flight;

fig. 3 is a schematic view of a dynamic structure of another embodiment of the electronic pulse bomb according to the present invention during flight;

fig. 4 is a schematic view of the overall basic structure of an embodiment of the electronic pulse bomb according to the present invention;

FIG. 5 is a front view of the structure of the electric pulse bullet of FIG. 3;

fig. 6-9 are schematic structural views of the receiving device in several embodiments of the electronic pulse bomb according to the present invention;

fig. 10 is a schematic structural view of an electronic pulse bomb inside a cartridge case according to an embodiment of the present invention;

fig. 11 is a schematic structural view of an electronic pulse bomb inside a cartridge case according to another embodiment of the present invention;

fig. 12 is a schematic view of a dynamic structure of another embodiment of the electronic pulse bomb according to the present invention during flight.

The reference numbers indicate:

the realization, the functional characteristics and the advantages of the utility model are further explained by combining the embodiment and referring to the attached drawings.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings, and it is obvious that the described embodiments are only some embodiments of the present invention, and not all of them. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.

It should be noted that, if directional indications (such as upper, lower, left, right, front and rear … …) are involved in the embodiments of the present invention, the directional indications are only used for explaining the relative position relationship between the components, the motion situation, etc. under a certain posture (as shown in the drawings), and if the certain posture is changed, the directional indications are changed accordingly.

In addition, if there is a description relating to "first", "second", etc. in the embodiments of the present invention, the description of "first", "second", etc. is for descriptive purposes only and is not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one of the feature. In addition, the technical solutions in the embodiments may be combined with each other, but it must be based on the realization of those skilled in the art, and when the technical solutions are contradictory or cannot be realized, the combination of the technical solutions should not be considered to exist, and is not within the protection scope of the present invention.

Referring to fig. 1, fig. 2 and fig. 3, which are schematic views of a dynamic structure of an electronic pulse projectile 100 according to three embodiments of the present invention in a flying process, in a dynamic operation, a separation distance between electrodes 21 in a striking module 20 is at least 100 mm, which is a minimum distance required for an acknowledged effective control target; the circuit module 40 is arranged to lag the flight of the striking module 20; the connecting module 50 at least comprises a section of wire 51, the wire 51 is respectively connected with each electrode 21 and the circuit module 40, and is stretched under the action of delayed flight of the circuit module 40 to be in a relatively tense state, the wire 21 and the circuit module 40 are both subjected to a restraining action, so that the flight attitude of the electrodes 21 is controlled, the excessive separation of the spacing of the electrodes 21 is limited, the electrodes 21 are always kept in the attitude with the heads facing forwards, and the spacing between the electrodes 21 is maintained in the range of 100 and 600 millimeters, so that the ordered arrangement and the dynamic balance stability of the structures of the striking module, the connecting module and the circuit module are formed.

The striking module 20 and the circuit module 40 are arranged in the shell 11 of the cartridge case 10 before being launched, wherein the distance between the electrodes 21 of the striking module 20 is only 5-15 mm, the circuit module 40 can be accommodated in a holding device 60, and the structural arrangement and the distance between the electrodes are similar to those of the prior art; however, different from the prior art, the structural shape and the distance of the electrode are kept unchanged after the electrode is transmitted, and the electrode and other components such as the circuit and the like form a whole flying, and after the electronic pulse bomb 100 with the technical characteristics of the present invention is transmitted, the electrode 21 is ejected and separated to the periphery under the action of an ejection device 30, the distance reaches at least 100 mm instantly, and in addition, the striking module 20 and the circuit module 40 are also separated from each other after the electronic pulse bomb is transmitted, and each flight module forms a relatively independent structure.

In dynamic flight, if the limitation on the electrodes 21 is lacked, each electrode 21 will continue to fly along the initial ejection angle to spread to the periphery, and the distance between the electrodes 21 will be larger and larger; in addition, due to the lack of a stabilizing mechanism such as self-rotation or balancing of a tail wing, the electrode 21 rolls over during flight, which may cause the electrode 21 to fly away from a distant target due to an excessively large distance therebetween and make it impossible to keep the head of the electrode 21 in a forward posture to strike the target; similarly, the unconstrained circuit module 40 may be in a disordered flight state, and may roll over and deviate from the flight trajectory due to its instability.

The technical solution provided by the present invention includes a connection module 50 for connecting the striking module 20 and the circuit module 40; the connecting module 50 at least comprises a section of wire body 51, and optionally, the diameter of the wire body 51 is 0.3-30 mm, and the length is 50-500 mm; the wire body 51 is preferably of a flexible structure and can be bent at will under stress, the material of the wire body can be a pure metal conductor, such as an insulated copper wire, or a combination of a conductor and a nonconductor, such as a metal wire and Kevlar fiber, wound and wrapped, or a nonconductor, and a conductive substance such as conductive adhesive and the like is coated on the surface of the wire body to enable the wire body to have conductive performance, and the wire body 51 and the conductor can obviously increase the toughness and the strength of the structure of the wire body 51, so that the wire body has stronger impact resistance and tensile capability. One end of the wire body 51 is connected to the output end of the circuit module 40, and the other end is connected to the rear portion 23 of the electrode 21.

The connection module 50 plays the following roles in the dynamic structure of the electronic pulse projectile 100: a. the wire body 51 of the connection module 50 has a conductive component, and a pulse current generated by the circuit module 40 of the electronic pulse bullet 100 is transmitted to the electrode 21 through the wire body 51, and then acts through a target; b. the wire body 51 is stretched under the lagging flying action of the circuit module 40 and is in a relatively tense state; the flying posture of the electrode 21 is controlled by pulling the rear part 23 of the electrode 21, so that the front part 22 of the electrode 21 always keeps the head flying forwards, the swinging and rolling of the electrode in the flying process are avoided, and the needle body 24 positioned at the head of the electrode 21 can effectively puncture a target organism when contacting the target; c. the wire body 51 can prevent the electrodes 21 from being separated from each other excessively, and the spacing between the electrodes 21 is maintained within a reasonable range relative to the size of the target body, optionally, the range is 100 mm to 600 mm, so as to effectively hit the target; d. the pulling action of the wire body 51 on the circuit module 40 also helps to keep the front end thereof flying in a forward attitude, suppressing or mitigating the roll thereof.

The electrode 21 in the illustrated embodiment is in the form of an elongated cylinder comprising a front portion 22 and a rear portion 23, wherein the front portion 22 comprises a needle body 24 and the head of the needle body 24 is provided with barbs to facilitate piercing of superficial body tissue and securing the electrode 21 to a target. Preferably, the front part 22 of the electrode 21 is made of a material with high specific gravity, such as lead metal, while the rear part 23 is made of a material with lower specific gravity, such as copper metal, stainless steel, aluminum alloy, or even plastic, so that the front part 22 of the electrode on the side with higher specific gravity can more easily keep the head in a forward posture under the pulling action of the wire body 51. In the embodiment of the present invention, the electronic pulse bomb 100 includes two pairs (4) of electrodes 21, and any pair of electrodes 21 with opposite polarities hits the target in practice, so that the current can form a loop through the target to achieve the control purpose, thereby increasing the probability of hitting the target. The positive and negative polarities of the electrodes 21 may be arranged adjacently or oppositely, in this embodiment, the electrodes are arranged oppositely, and the distance between the positive and negative electrodes 21 may be increased to the maximum extent by making full use of the characteristic that the diagonal distance of the rectangle is greater than the distance between two adjacent sides.

The circuit module 40 of the electronic pulse bullet comprises at least an electric circuit to generate a pulse current. Such circuits 40 are well described in the literature and will not be described in detail herein, and mainly include a power supply, an electronic chip, and an activation switch. In this embodiment, when the circuit module 40 is in a dormant or non-activated state when located in the cartridge case 10, the circuit module 40 does not work; when the electronic pulse bullet 100 is launched from the bullet case 10 and the lumen of the launching device, the trigger switch of the circuit module 40 is turned on, and the circuit module 40 starts to work and generate a pulse current.

In the dynamic operation, the circuit module 40 lags behind the striking module 20 to fly, so that the wire 51 of the connection module 50 is stretched to be in a relatively tense state, thereby generating a restraining effect on the electrode 21 and the circuit module 40, which is one of the necessary conditions for the dynamic structure of the electronic pulse bomb 100 to achieve linear ordered arrangement and balanced stability. Causing the circuit module 40 to lag flight can be accomplished in a variety of ways, one of which is to increase the dynamic wind resistance of the structure behind the electronic pulse projectile 100. As in the embodiment of fig. 1 and 2, the circuit module 40 is disposed inside a receiving device 60, and the diameter and cross-sectional area of the receiving device 60 are both larger than those of the electrode 21, and the wind resistance encountered after transmission is also larger than that of the electrode 21, so that the flying speed is slower than that of the electrode 21 and lags behind, and is separated from the electrode 21; the housing 61 of the receiver 60 may be provided with apertures to reduce and adjust the wind resistance as required, for example, the air holes 65 at the head of the receiver 60 and the diversion grooves 66 at the side walls in the figure may adjust the wind resistance by changing the size of the apertures, so as to obtain the best dynamic balance effect of the whole structure.

In the embodiment of fig. 1 and 2, the receiving device 60 forms a part of the electronic pulse bomb 100 in the flying state, and the embodiment of fig. 1 includes a balancing device 70, which is a balancing tail wing, unlike the prior art, the balancing tail wing in the embodiment of the present invention does not cause the main body of the electronic pulse bomb 100 to rotate, thereby preventing the prior art electrode from making circular motion around the central axis of the bomb during flying, and when hitting the target, the electrode generates deflection torque to affect the penetrating power of the target, even causing the target to fall off; the balancing device 70 in the embodiment of fig. 2 is a group of ribbons, which may be made of a soft thin-walled material such as a plastic film, one end of each ribbon is connected and fixed to the rear end of the receiving device 60, and the rest of each ribbon may be divided into a plurality of strips, which may be disposed inside the receiving device 60 when the electronic pulse bomb is in a static state and is not launched, and which are deployed to play a role after being launched. Compared with the balance tail wing in fig. 1, the ribbon in fig. 2 is lighter in weight and simpler in structure, and the effect is more obvious because the balance action point of the balance tail wing is moved backwards compared with the balance tail wing in the former and the lever power arm is prolonged. Of course, the structure may also function in other ways, such as a flexible sheet-like device attached to the rear of the receiver 60, which fans out after launch, without any intention of limiting its scope.

In the embodiment of fig. 3, the receiver 60 is separated from the other structures of the electronic pulse bomb 100 after being launched, and loses its function, and the structure behind the electronic pulse bomb 100 is only the circuit module 40 itself, which can reduce the mass of the structure and eliminate the dynamic wind resistance caused by the receiver 60 itself. Fig. 3 is a schematic diagram of the circuit module 40 in a dashed line frame, which shows that the components of the circuit module 40 are preferably arranged in a linear extending manner, and optionally, the components or assemblies are connected by a wire or a non-conductive wire body with a flexible feature, so that the circuit module 40 has a flexible feature as a whole; the linear length of the structure of the circuit module 40 is significantly longer than that of the circuit module arranged inside the receiving device 60, and at this time, the circuit module 40 itself is also the balancing device 70, although the mass of the structure of the section is lighter than that in fig. 1 and 2, the lever power arm is significantly lengthened by means of the backward movement of the power action point of the structure, and the balance and stabilization function can be effectively exerted by the wind resistance generated by the self-weight containment and the dynamic swing. Of course, if desired, other structures, such as the ribbons described above, may be added to the chain of linearly arranged structures of the circuit modules 40 to increase the balancing and stabilizing effect.

The balancing device 70 is used for further enhancing the balance stability of the accommodating device 60 and/or the circuit module 40, so that the linear flying posture with the head end facing forwards is maintained; secondly, the balancing device 70 itself can also increase the dynamic wind resistance of the rear structure of the electric pulse bullet 100, causing the circuit module 40 to fly behind the striking module 20. The balancing device 70 may be a single structure functioning, such as a balancing tail or the circuit module 40 itself; it may also be a combination of any suitable structure such as the containment device 60 and the balancing tail or flag, or the circuit module 40 and the above-described flag, even in combination with other structures such as the infill 14, etc. The advantage of using the solid structure of the electronic pulse bomb 100 itself as the counterbalance device 70 is that after it is fired, the solid structure flies with the main structure of the electronic pulse bomb, so that it will not fall off and splash after it is discharged, which may cause injury to bystanders.

Fig. 4 is a schematic view of an overall structure of an embodiment of the present invention. As shown in the figure, the electronic pulse bomb 100 comprises a hollow bomb shell 10, wherein the bomb shell 10 comprises a shell body 11, a primer 12, a propellant powder 13, a filler 14 and the like; the shell case comprises a striking module 20, a circuit module 40, a connecting module 50 and other main structural and functional components, an ejection device 30, a receiving device 60 and other auxiliary structures which are all arranged in a shell body 11 of the shell case 10; in a static state, the ejection device 30 is disposed adjacent to each electrode 21 of the striking module 20 to eject and separate the electrodes 21 after the electronic pulse bomb 100 is launched, so that the distance between the electrodes 21 instantaneously reaches at least 100 mm. Optionally, the front end of the cartridge case 10 may be provided with a front protective cover 15 to provide sealing protection for the contents of the cartridge case 10. The filling body 14 here includes at least one piston, which has one of the functions of sealing the propellant charge 13 and other components from each other, and of protecting and moisture-proofing the propellant charge 13; another important function of the piston is to promote high pressure inside the cartridge case 10 in a closed state when the propellant charge 13 is ignited, thereby increasing the bore pressure of the projectile firing device so as to effectively increase the initial velocity and the range of the dynamic projectile 100. The piston can be made of various materials, such as hard rubber, plastic and the like, and has the structural characteristics that the piston can be an elastic body and is forced to be pressed into the shell 11 by means of elastic deformation of the piston or a rigid body, and a gas-closing ring, a sealing snap ring and the like are additionally arranged on the structure to achieve the sealing effect; preferably, the piston is made of a material with a low specific gravity, such as cork or a foaming material, so that the piston cannot cause serious injury to other people when being separated from the projectile body after being launched; of course, the piston can also be coupled or connected with other components to dynamically fly, such as flexibly connected with the receiver 60 or the circuit module 40 and functioning as the balancing device 70. The electronic pulse bullet 100 can be shot by using a conventional military-police bullet riot gun, such as a 12-caliber bullet gun, and can be shot singly or continuously according to the structure of the shooting device, when in use, an operator pulls a trigger, the primer 12 of the pulse bullet 100 is triggered to ignite, the propellant 13 is ignited, high-pressure gas is generated instantaneously, and the filler 14 and other structures in the bullet shell 10 are pushed to open the front protective cover 15, so that the bullet can be shot from the tube cavity of the bullet gun.

Fig. 5 is a front view of the structure of the electric pulse bullet 100 in the bullet case 10 in fig. 4. As shown in the figure, the front protecting cover 15 is removed here, and it can be seen that the four electrodes 21 of the striking module 20 are uniformly distributed in the casing 11 of the cartridge case 10 in the upright pre-firing position with the puncture needle 24 facing forward, and the firing device 30 in this embodiment is a leaf spring device, located inside the electrodes 21 and in an elastically compressed state, so as to eject and separate the electrodes 21 to the outer periphery by virtue of the elastic resetting function after the electronic pulse bomb 100 is fired. It is also shown that a part of the housing 61 of the receiving device 60 and a wire hole 63 provided in the housing are provided for the wire body 51 of the connecting circuit module 40 to pass through.

Fig. 6-9 are schematic views of several structures of the receiving device 60 according to an embodiment of the present invention; the receiving device 60 is a hollow structure, and mainly plays a role of supporting and receiving various structures and functional modules of the electronic pulse bomb 100, and the interior of the housing 61 is mainly used for receiving the circuit module 40 and other parts of the electronic pulse bomb 100. It can be seen that the front part of the receiving device 60 is provided with an electrode base 62 for receiving and fixing the rear part 23 of the electrode 21, the ejection device 30 is located at the front end of the receiving device 60, the ejection device 30 in the embodiment of fig. 6 is an elastic solid made of materials such as rubber, elastic plastic, etc., while the ejection device 30 in the embodiment of fig. 7 and 8 is an elastic sheet-like structure in the spring-open reset state; the elastic means 30 may be a separate structure from the receiving means 60 as shown in fig. 6, or may be attached to the receiving means 60 by means of an extended fixing rod 67 at the front of the structure of the receiving means 60 as shown in fig. 7 and 8. The ejection device 30 is provided with a U-shaped structure 31, which functions together with the electrode base 62 to maintain the orientation of each electrode 21 at the vertical position to be ejected, so as to prevent the electrodes 21 from deflecting during storage or ejection, and thus the ejection mechanism 30 from exerting its ejection separation effect. Of course, the ejector 30 may take other suitable forms, such as a spring mechanism disposed on the body of the electrode 21 or the structure of the securing bar 67, and the like, without limiting the scope thereof.

The front part of the housing 61 of the receiving device 60 may be provided with wire holes 63 for the wire bodies 51 of the connecting circuit module 40 to pass through, in fig. 6, 7, and 8, there are 4 wire holes 63 for each wire body 51 of the connecting module 50 to pass through and then to be connected to one electrode 21, while in the embodiment of fig. 9, there is only one wire hole 63 for all the connecting wire bodies 51 to pass through and then to be connected to each electrode 21; another difference of the receiving device 60 shown in fig. 9 is that it is constructed as two half-shells, which are joined together in a single body inside the cartridge case 10, in which the circuit module 40 is housed; after firing, the receiver 60 is split along the split line 68 and separated and detached from the rest of the electronic pulse projectile 100 as shown in fig. 3, and the circuit module 40 is ejected therefrom and continues to fly forward. Of course, the structure of the receiving device 60 in the figure can also be divided into a plurality of shells, for example, four shells are combined into a whole in the cartridge case 10, the more the number of the shells is, the lighter the weight is, the smaller the volume and the surface cross-sectional area are, and the smaller the dynamic wind resistance is; the receiving means 60, separated from each other, can also be connected to other structures, such as the circuit module 40 and trailing behind it, to take on or enhance the function of the balancing means 70.

Referring to fig. 10 and fig. 11, which are static diagrams illustrating the structure of the electronic pulse bomb 100 in the cartridge case 10 according to two embodiments of the present invention. Here, the structures of the parts of the electronic pulse bomb 100 are set in place and in a static state to be launched. The wire body 51 is seen in a folded state and stored between a wire storage groove 64 formed in the side wall of the receiving device 60 and the inner wall of the casing 11 of the cartridge case 10, and has one end connected to the output end of the circuit module 40 located inside the receiving device 60 and extending out through the aperture 63 and the other end connected to the electrode rear portion 23 of the striking module 20; fig. 9 and 10 each include a balancing fin 70, the former being in a folded configuration and the latter illustrating its deployed configuration. The balancing tail 70 may be made of different materials and processes, such as an elastic engineering plastic sheet, or a metal frame structure as shown in the figure, and is filled and adhered with a light film to form a solid plane, so as to reduce the weight of the balancing tail as much as possible.

Unlike the structure of fig. 10, the embodiment of fig. 11 further includes a flexible frame 24, which is used to substantially fix and maintain the distance between the electrodes 21 at a predetermined length after the electronic pulse bomb 100 is fired, instead of the distance between the electrodes 21 varying with the distance in a certain range as in the previous embodiment. The spacing between the electrodes 21 can be preset according to different body shape characteristics of the target, for example, when the electrode 21 is used for a human target, the spacing between the electrodes 21 is at least 100 mm, but preferably not more than 600 mm. The flexible frame 24 may be made of various materials, such as thin metal wire or other non-conductive fiber, which has good flexibility and flexibility so that it can be folded and stored in the casing 10 as shown in the gap formed between two adjacent electrodes 21 and the inner wall of the casing 11. The basic structure of the elastic frame 24 is a closed approximately rectangular structure, four corner end parts of the rectangle are respectively fixed on the electrode 21, and optionally, the four corner end parts are clamped and fixed between the front part 22 and the rear part 23 of the electrode and are positioned at or close to the gravity center part of the whole structure of the electrode 21 as much as possible; if the elastic frame is made of conductive material, the contact portion with the electrode 21 needs to be insulated to prevent short circuit between the electrodes 21 during use.

Referring to fig. 12, which is a schematic diagram illustrating a dynamic structural feature of the electronic pulse bomb 100 in the embodiment of fig. 11 in flight, it can be seen that the elastic frame 25 is already in an expanded state. The principle of the firing and the main dynamic features of the electric pulse projectile 100 shown in this embodiment are the same as those shown in fig. 1-3, except that when the electrodes 21 in the striking module 20 reach the preset separation distance under the action of the ejection device 30, the elastic frame 25 maintains the separation distance of the electrodes 21 at the preset separation distance for dynamic flight by virtue of the restraining and elastic supporting functions of the elastic frame 25. The electronic pulse bullet 100 having the present structural feature has the advantages of: the situation that the electrode 21 is not restrained or restrained excessively by the connecting module 50 due to structural errors or other factors such as dynamic unbalance between modules and structures can be avoided, so that the accuracy and the effect are influenced due to the fact that the distance between the electrodes 21 is too large or too small.

The above only be the several preferred embodiments of the present invention, not therefore the restriction of the patent scope of the present invention, all are in the utility model discloses a conceive under, utilize the equivalent structure transform that the content of the description and the attached drawing was done, or direct/indirect application all is included in other relevant technical field the patent protection of the present invention is within the scope.

Claims (10)

1. A remote electronic pulse bomb comprising: a striking module including at least one pair of electrodes for emitting to a remote target; the circuit module is used for generating pulse current; the connecting module is used for electrically connecting the electrode and the circuit module and conducting the pulse current to the target through the electrode; the method is characterized in that: the ejection device is arranged adjacent to the electrodes and ejects and separates the electrodes to the periphery when the electronic pulse bullet is emitted, so that the distance between the electrodes reaches at least 100 mm immediately.

2. The electron pulse projectile of claim 1 wherein the spacing of said electrodes is greater after said electrodes are catapulted apart than before said electrodes are catapulted apart.

3. A remote electronic pulse bomb is characterized in that the dynamic structure is as follows: the method comprises the following steps: the striking module comprises at least one pair of electrodes, the distance between the electrodes is at least 100 mm, the circuit module lags behind the electrode flying and connecting module, the electrodes and the circuit module are respectively connected, and the connecting module stretches and tensions under the lagging flying action of the circuit module and acts on the electrodes, so that the electrodes always fly in a head-forward posture, and the electrodes are limited from being excessively separated.

4. The electron pulse bullet of any one of claims 1 to 3, wherein the distance between said electrodes after separation by ejection is 100-600 mm.

5. The electronic pulse bomb according to claim 4, wherein the connection module comprises at least one length of flexible wire.

6. The electronic pulse bomb according to claim 5, wherein the wire body is a conductor.

7. The electronic pulse bomb according to claim 6, wherein the circuit module includes a switch which is turned on after the electronic pulse bomb is fired to operate the circuit module and generate a pulse current.

8. The electric pulse bomb according to claim 7, wherein said striking module comprises an elastic frame, and said elastic frame is disposed on said electrode.

9. The electronic pulse bullet as claimed in claim 8, wherein said elastic frame maintains a predetermined length between 100 mm and 600 mm after said electrodes are separated by ejection.

10. A weapon comprising an electronic pulse projectile as claimed in any one of claims 1 to 9.

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