Remote non-fatal electric shock bullet
Through the design of streamlined warheads and hinged tail wings, the range and stability problems of traditional non-lethal electric shock weapons are solved, and the efficient uniform effect of long-range non-lethal electric shock bullets is achieved, reducing damage to the target and reducing equipment costs.
Patent Information
- Application Number
- CN202411565501.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-11-05
- Publication Date
- 2025-01-07
AI Technical Summary
Traditional non-lethal electric shock weapons have too short range, low hit rate, and the flight stability of bullets at low speed flight is difficult to guarantee, resulting in low additional damage and shooting accuracy.
Design a long-range non-lethal electric shock bullet with a streamlined warhead and hinged tail wing, connected to the bullet body by a spring, the warhead exposes hidden electrodes in flight, and the tail wing provides rolling torque to reduce wind resistance, ensures stable flight, and during impact Release high voltage pulse current.
The flight stability and range of bullets at lower speeds are achieved, reducing additional damage to targets, low cost, launching with existing equipment, with strong repeatability and efficient ability to subdue multiple targets.
Smart Images
Figure CN119268482A_ABST
Abstract
Description
Technical Field
[0001] The invention relates to the technical field of non-lethal weapons, in particular to a long-range non-lethal electric shock bullet. Background Art
[0002] Traditional non-lethal electric shock weapons have problems such as short range and low hit rate due to wired connection of the firing gun. New products with longer range usually use faster initial velocity of the projectile, which will cause additional damage to the target when the object is close, and the stability of the projectile flight is difficult to ensure when flying at low speed, so there is room for improvement in shooting accuracy. In order to use shotguns to fire, reduce the resistance of the bullet in flight, and maintain spin stability, a long-range non-lethal electric shock bullet is proposed. Summary of the invention
[0003] The object of the present invention is to provide a long-range non-lethal electric shock bullet to solve the problems raised in the above background technology.
[0004] To achieve the above object, the present invention provides the following technical solution: a long-range non-lethal electric shock bullet, comprising:
[0005] A projectile body, the front end of which is connected to the warhead via a spring;
[0006] A warhead, the warhead comprising a spring, the warhead adopting a streamlined design to reduce flight resistance;
[0007] The tail fin is mounted on the projectile body through a hinge to provide a rolling moment to ensure the flight stability of the bullet.
[0008] Compared with the prior art, the beneficial effects of the present invention are as follows: the bullet flies at a relatively low speed, during the flight, the hidden electrode is completely exposed from the warhead, the tail wing is deployed at an angle according to the best lift-to-drag ratio to provide a rolling moment, and the wind resistance can be effectively reduced to ensure flight stability, and when impacting a target, the warhead is compressed to expose the electrode to release a high-voltage pulse current to subdue the target. The present invention has a simple overall structure, can be launched using existing equipment, has a low cost, and has strong repeatability, and the relatively low flight speed can effectively reduce additional damage to the target during use. BRIEF DESCRIPTION OF THE DRAWINGS
[0009] Figure 1 It is an isometric view schematic diagram of the present invention.
[0010] Figure 2 It is a schematic diagram of the isometric view of the projectile.
[0011] Figure 3 Schematic diagram of an isometric view of a warhead.
[0012] Figure 4 This is the front view and AA section view of the tail wing.
[0013] Figure 5 It is the main view of the projectile and the BB and CC cross-sectional views.
[0014] Figure 6 It is the main view and DD cross-sectional view of the warhead.
[0015] In the figure: tail fin 1, projectile body 2, warhead 3, spring 3-1, shoulder 3-2, through hole 3-3, electrode 4, hinge 5. DETAILED DESCRIPTION
[0016] like Figure 1 As shown, the present invention provides a long-range non-lethal electric shock bullet, comprising:
[0017] A projectile body 2, the front end of which is connected to the bullet head 3 via a spring 3-1;
[0018] The warhead 3 includes a spring 3-1, and the warhead 3 adopts a streamlined design to reduce flight resistance;
[0019] The tail 1 is mounted on the missile body 2 via a hinge 5 to provide a rolling moment.
[0020] As a further solution of the present invention, the projectile body 2 can be split into two equal parts for easy installation of internal parts. The interior of the projectile body is hollow and designed to install a high-voltage pulse power supply. The front part of the projectile body is recessed to accommodate the warhead 3. Two electrodes 4 extend from the front part of the projectile body to release pulse current. The length of the electrode is greater than the distance from the bottom of the recess to the front end of the projectile body, and the bottom of the electrode can be connected to the high-voltage pulse power supply. There is a groove at the tail of the projectile body for folding the tail fin. The groove is at a certain angle to the central axis of the bullet to ensure that the tail fin is installed obliquely to provide aerodynamic torque, and the length of the groove is slightly greater than the length of the tail fin. The rounded corners of the tail of the projectile body facilitate the assembly of the propellant.
[0021] As a further solution of the present invention, the bullet adopts a streamlined design to reduce resistance. The bullet has two through holes 3-3 for the body electrode 4 to pass through. The bullet 3 is connected to the body 2 through a spring 3-1 to ensure that the bullet will not shrink during the aerodynamic process, ensuring accurate positioning. The tail end of the bullet is provided with a shoulder 3-2 for positioning. The spring 3-1 is welded on the plane at the front end of the body, in free contact with the bullet 3, and should be in a compressed state when the bullet is not contracted, providing a certain elastic force to fix the bullet in front of the body.
[0022] As a further solution of the present invention, one end of the spring wire of the spring 3-1 contacts the bullet under the action of elastic force, and the other end contacts the recessed bottom of the front part of the bullet body under the action of elastic force; after installation, the spring 3-1 is in a compressed state to fix the bullet.
[0023] The aerodynamic drag on the warhead in flight is calculated through numerical simulation and experiments.
[0024] As a further solution of the present invention, the tail wing is connected to the projectile body through a hinged cylindrical pair, and is positioned in contact with the rear wall of the projectile body groove after unfolding. The wing tip and wing root of the tail wing are rounded to ensure that they do not contact the groove during the unfolding process.
[0025] As a further solution of the present invention, the long-range non-lethal electric shock bullet body is formed by plastic blow molding or metal stamping, the body and the thin wall thickness are 2mm, and the bullet head is formed by plastic blow molding.
[0026] As a further solution of the present invention, the tail wing can be replaced with different airfoils.
[0027] In order to make the purpose, technical solution and advantages of the present invention more clearly understood, the present invention is further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the present invention and are not intended to limit the present invention.
[0028] The specific implementation of the present invention is described in detail below in conjunction with specific embodiments.
[0029] Example
[0030] like Figure 1-Figure 6 As shown, a long-range non-lethal electric shock bullet provided by an embodiment of the present invention includes: a tail 1, a body 2, and a bullet 3. The tail 1 is connected to the body 2 by a hinge, and the body 2 and the bullet 3 are positioned and connected by a spring and a shoulder. The wing tip and wing root of the tail 1 are rounded, and a through hole is opened at the wing root. The front end of the body 2 is sunken to accommodate the bullet 3, and a groove is opened at the tail to accommodate the tail folded into the body. There is a hollow part inside for installing a high-voltage pulse power supply. The body 2 also includes a groove 2-1, an electrode 4, and a hinge 5. The bullet 3 includes a spring 3-1, a shoulder 3-2, and a through hole 3-3. The shoulder 3-2 and the through hole 3-3 are directly processed on the bullet 3. The spring 3-1 is welded on the plane of the front end of the body 2. When the bullet is not contracted, it should be in a compressed state to provide a certain elastic force to fix the bullet in front of the body.
[0031] The chord length, span and thickness of the tail 1 match the size of the groove 2-1, ensuring that the tail 1 can be smoothly unfolded and folded and will not exceed the cylindrical surface of the missile body 2 after folding. The wing tip and wing root are rounded to avoid hitting the groove 2-1 during rotation and causing failure to eject smoothly. The tail airfoil is replaceable.
[0032] The projectile body 2 is formed by metal stamping or plastic blow molding, with a wall thickness of 1 mm. The four grooves 2-1 are all at an angle of 5° with the axis to ensure that the tail has an optimal attack angle of 5° to provide a rolling moment.
[0033] The warhead 3 is blow-molded from plastic material to minimize the damage to the human body caused by impact, and the streamlined design reduces flight resistance. Two through holes 3-3 are opened on the surface of the warhead.
[0034] The elastic force of the spring 3 - 1 when supporting the bullet 3 is greater than the air resistance, thus preventing the bullet from shrinking during flight.
[0035] The electrode 4 is made of steel, with a sharpened head, a length of 2 cm and a diameter of 2 mm, to ensure that it can penetrate clothing and contact human muscles while avoiding excessive penetration into the human body and causing additional damage. The electrode 4 is welded to the projectile 2, and when the head is retracted, the electrode 4 acts as a guide rail, and the projectile slides down along the guide rail.
[0036] The hinge 5 is installed at the junction of the tail wing and the projectile body, so that the tail wing can rotate around it.
[0037] The working principle of the present invention is as follows: the non-lethal long-range electric shock bullet is fired from an existing shotgun. The bullet 3 is not retracted in the barrel, and the electrode 4 is hidden in the bullet 3. The spring is in a compressed state, and the bullet 3 is subjected to an outward elastic force. At the same time, the shoulder 3-2 at the tail of the bullet cooperates with the card slot in front of the bullet body to support the bullet to prevent the bullet from retracting. After leaving the barrel, the tail wing pops out around the hinge 5 under the action of inertia, generating a rolling moment to ensure the stable flight of the projectile. When the bullet hits the target, the bullet shrinks under the action of the impact force, and the two electrodes 4 are exposed from the through hole 3-3, penetrate into the target and release a high-voltage pulse current, so that the target object's muscles lose the ability to move.
[0038] After adopting the above technical scheme, the beneficial effect of the present invention is that the design of streamlined warhead and hidden electrode reduces the resistance of electric shock bullet at low flight speed to the maximum extent, increases the range, and the lower flight speed and plastic warhead reduce the additional damage to the target caused by the impact. At the same time, it can be fired using existing equipment and can be quickly replaced and reused, which improves the subduing effect on multiple targets and reduces equipment costs.
[0039] The above are only preferred embodiments of the present invention. It should be pointed out that, for those skilled in the art, several modifications and improvements can be made without departing from the concept of the present invention. These should also be regarded as the protection scope of the present invention. These will not affect the effect of the implementation of the present invention and the practicality of the patent.
Claims
1. A long-range non-lethal electric shock bullet, characterized in that: include: A projectile body, the front end of which is connected to the warhead via a spring; A warhead, the warhead comprising a spring, the warhead adopting a streamlined design to reduce flight resistance; The tail fin is mounted on the projectile body through a hinge to provide a rolling moment to ensure the flight stability of the bullet.
2. The long-range non-lethal electric shock bullet according to claim 1, characterized in that: The projectile body is divided into two equal parts, and the interior of the projectile body is hollow and designed to be used for installing a high-voltage pulse power supply.
3. The long-range non-lethal electric shock bullet according to claim 2, characterized in that: The front part of the projectile body is recessed to accommodate the warhead, and two electrodes extend from the front part of the projectile body to release pulse current; the tail part of the projectile body is provided with a groove for folding the tail wing, and the rounded corners of the tail part of the projectile body are convenient for the assembly of the propellant.
4. The long-range non-lethal electric shock bullet according to claim 3, characterized in that: The length of the electrode is greater than the distance from the bottom of the recess to the front end of the projectile, and the bottom of the electrode is connected to a high-voltage pulse power supply.
5. The long-range non-lethal electric shock bullet according to claim 3, characterized in that: The groove forms a certain angle with the central axis of the bullet to ensure that the tail fin is installed tilted to provide aerodynamic torque, and the length of the groove is slightly greater than the length of the tail fin.
6. The long-range non-lethal electric shock bullet according to claim 5, characterized in that: The groove forms an angle of 5° with the axis of the projectile.
7. The long-range non-lethal electric shock bullet according to claim 3, characterized in that: The bullet adopts a streamlined design, has two through holes for the projectile body electrodes to pass through, is connected to the projectile body through a spring to ensure accurate positioning, and a shoulder is provided at the tail end of the bullet for positioning.
8. The long-range non-lethal electric shock bullet according to claim 7, characterized in that: The spring is welded on the plane at the front end of the projectile body and is in free contact with the warhead; the spring is in a compressed state when connected to the warhead, and the pressure at this time is greater than the aerodynamic resistance experienced by the warhead in flight, ensuring that the warhead will not shrink when subjected to aerodynamic force.
9. The long-range non-lethal electric shock bullet according to claim 7, characterized in that: The tail wing is connected to the projectile body through a hinged cylindrical pair, and is positioned in contact with the rear wall of the projectile body groove after being unfolded. The wing tip and wing root of the tail wing are rounded to ensure that they do not contact the groove wall during the unfolding process.
10. The long-range non-lethal electric shock bullet according to claim 1, characterized in that: The projectile body is formed by plastic blow molding or metal stamping, and the warhead is formed by plastic blow molding.