Anti-unmanned aerial vehicle interception shotgun

Abstract

The utility model discloses an anti-unmanned aerial vehicle interception shotgun which comprises a metal base (1), a shell case (2), propellant powder (3), a shell support (4) and a bullet head (5) carrying a net body. The metal base (1) is arranged at the bottom end of the cartridge case (2), and the opening end of the cartridge case (2) is provided with a sealing piece (6) playing a sealing role. The bullet support (4) is arranged in the bullet case (2), the bullet head (5) is arranged on the upper portion of the bullet support (4), and the propellant powder (3) is arranged on the lower portion of the bullet support (4). A primer (7) abutting against the propellant powder (3) is arranged in the center of the bottom end of the metal base (1). The unmanned aerial vehicle has the advantages of being simple in structure and convenient to assemble, and a better countering effect can be achieved on the unmanned aerial vehicle by arranging the warheads carrying the net body.

Description

Technical Field

[0001] This utility model relates to the field of projectile technology, and in particular to an anti-drone intercepting shotgun. Background Technology

[0002] With the gradual opening of the national low-altitude flight sector, the application of drones is becoming increasingly widespread, but the problems caused by "black flights" of drones are also becoming increasingly prominent. To address this situation, there is an existing anti-drone munition, such as the Chinese invention patent with publication number CN118111284A, which discloses an anti-drone munition with a wide-ranging destructive effect, including a cartridge case, a projectile body, multiple tail fin assemblies, a launch assembly, a magazine, and a range-extending and detonation assembly; the projectile body is surrounded by multiple projectile lobes, which are evenly distributed circumferentially and are all locked above the cartridge case, with the lower ends of the multiple projectile lobes inserted into and fixed to a support plate; multiple tail fin assemblies are evenly distributed circumferentially; the launch assembly is fixed inside the cartridge case to push the projectile body to separate from the cartridge case; the magazine is fixed inside the projectile body and is used to store the projectile; the range-extending and detonation assembly is fixed inside the projectile body to propel the projectile body to continue flying, while forcing the projectile lobes to open the magazine and release the projectile. This type of projectile is an improvement on traditional shotgun shells. The projectile is launched by spinning, thereby improving the accuracy of the shot. However, it is more complex in structure and has more parts, making it more cumbersome to assemble. Utility Model Content

[0003] The purpose of this invention is to provide an anti-drone interceptor shotgun. This invention features a simple structure and easy assembly, and by incorporating a warhead with a mesh mount, it achieves a better counter-attack effect against drones.

[0004] The technical solution of this utility model is an anti-drone interceptor shotgun, comprising a metal base, a cartridge case, propellant, a sabot, and a warhead equipped with a net; the metal base is located at the bottom end of the cartridge case, and the open end of the cartridge case is provided with a sealing plate for sealing purposes; the sabot is located inside the cartridge case, the warhead is located at the upper part of the sabot, and the propellant is located at the lower part of the sabot; the bottom center of the metal base is provided with a primer that abuts against the propellant.

[0005] In the aforementioned anti-drone interceptor shotgun, the sealing piece includes a piece body, the circumferential surface of which has an annular edge that contacts the inner side of the cartridge case.

[0006] In the aforementioned anti-drone interceptor shotgun, the warhead includes a Kevlar fiber mesh, with lead blocks connected to the ends of the Kevlar fiber mesh. Multiple lead blocks are assembled into a disc block, which is positioned on the upper part of the sabot.

[0007] In the aforementioned anti-drone interceptor shotgun, the sabot includes a main body disposed within the cartridge case, a spacer section at the lower end of the main body, and a positioning plate at the lower part of the spacer section; the main body contains a main chamber for projectile positioning, the spacer section has an intermediate channel communicating with the main chamber, the lower end of the intermediate channel communicating with the groove of the positioning plate, and the propellant is in contact with the positioning plate.

[0008] In the aforementioned anti-drone interceptor shotgun, the cartridge case includes a shell, a base at the bottom of the shell, a sabot disposed inside the shell, and a through groove on the base.

[0009] In the aforementioned anti-drone interceptor shotgun, the metal base includes a ring that fits into the chassis, and the middle part of the ring has a central groove for placing the primer.

[0010] In the aforementioned anti-drone interceptor shotgun, the edge of the ring body has a conical edge.

[0011] Compared with the prior art, the advantages of this utility model are:

[0012] 1. In this utility model, the propellant is first precisely placed inside the cartridge case, and then the sabot is inserted. The lower part of the sabot cleverly fixes the propellant, forming a stable structure. Next, the projectile is installed on the upper part of the sabot, where the sabot plays a key role in separating the propellant and the projectile. Then, the metal base is tightly assembled to the bottom of the cartridge case, ensuring that the primer inside the metal base is in close contact with the propellant, achieving a reliable connection. Finally, a sealing piece is installed at the opening end of the projectile, completing the entire assembly process. The entire series of operation steps is simple and smooth, and the assembly is convenient, making the overall structural design streamlined. At the same time, this utility model uses a projectile with a mesh body, which greatly enhances the countermeasure effectiveness against UAVs and significantly improves the practicality of the product.

[0013] 2. The sabot structure of this utility model is simple, which can not only stably and effectively separate the propellant from the projectile, but also tightly seal the internal gas, ensuring stability and reliability during the firing process.

[0014] 3. The ring body of this utility model has a conical edge. This structural design allows the entire projectile to be placed stably on a plane, which greatly improves the convenience and safety of operation, whether in storage, transportation or preparation before use. Attached Figure Description

[0015] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0016] Figure 2 This is a longitudinal sectional view of the present invention;

[0017] Figure 3 This is a schematic diagram of a cartridge case;

[0018] Figure 4 A schematic diagram of a sabot;

[0019] Figure 5 This is a schematic diagram of a warhead;

[0020] Figure 6 This is a schematic diagram of a lead block;

[0021] Figure 7 This is a schematic diagram of a sealing sheet;

[0022] Figure 8 This is a schematic diagram of the metal base.

[0023] The markings in the attached diagram are as follows: 1-Metal base, 2-Cartridge case, 3-Propellant, 4-Sabot, 5-Cartridge, 6-Sealing plate, 7-Primer, 8-Plate body, 9-Annular edge, 10-Kevlar fiber mesh, 11-Lead block, 21-Disc block, 22-Main body, 23-Interval section, 24-Positioning plate, 25-Main chamber, 26-Intermediate channel, 27-Casing, 28-Chassis, 29-Gateway, 30-Ring body, 31-Conical edge, 32-Central groove. Detailed Implementation

[0024] The present invention will be further described below with reference to the accompanying drawings and embodiments, but this should not be construed as limiting the present invention.

[0025] Example: Anti-drone interceptor shotgun, comprising a metal base 1, a cartridge case 2, propellant 3, a sabot 4, and a warhead 5 equipped with a net, as shown in the attached diagram. Figure 1 and 2 As shown; the metal base 1 is disposed at the bottom end of the cartridge case 2, and a sealing piece 6 for sealing is installed at the open end of the cartridge case 2. The sealing piece 6 includes a piece body 8, as shown in the attached figure. Figure 7As shown, the circumferential surface of the piece 8 has an annular edge 9 that contacts the inner side of the cartridge case 2. The piece is inserted into the cartridge case, and the annular edge fits tightly against the inner wall of the cartridge case opening, achieving a certain degree of interference fit, which can improve the sealing performance and prevent the projectile from falling out. The sabot 4 is set inside the cartridge case 2, the projectile 5 is set on the upper part of the sabot 4, and the propellant 3 is set on the lower part of the sabot 4. The sabot can not only stably and effectively separate the propellant from the projectile, but also tightly seal the internal gas, ensuring the stability and reliability during the firing process. The metal base At the bottom center of the base 1 is a primer 7 that abuts against the propellant 3. The primer plays a key role in the entire anti-drone intercept shotgun system. It is located inside the metal base and is in close contact with the propellant. When the external environment provides a suitable trigger, the primer will quickly generate high-temperature and high-pressure gas. This gas can instantly ignite the propellant inside the cartridge case. The combustion of the propellant produces a large amount of gas. The rapidly expanding gas forms a powerful thrust. This thrust acts on the sabot, thereby propelling the warhead out of the cartridge case at high speed and flying towards the target drone, completing the interception operation.

[0026] The warhead 5 includes a Kevlar fiber mesh 10, as shown in the attached image. Figure 5 As shown, lead blocks 11 are connected to the ends of the Kevlar fiber mesh 10. Multiple lead blocks 11 are assembled into a disc block 21. The disc block 21 is set on the upper part of the sabot 4. After the Kevlar fiber mesh is unfolded, it is a rectangular mesh. The specific structure is shown in the attached figure. Figure 6 As shown; after the warhead is launched, the lead blocks, with their weight, maintain a stable trajectory during flight, guiding the warhead's flight direction. A Kevlar fiber mesh is attached to the lead blocks. As it approaches the drone, the mesh rapidly unfolds, like a large net, thanks to the kinetic energy of the projectile. Due to the high strength and wear resistance of Kevlar fibers, once the mesh contacts the drone, it can entangle and damage critical components such as the drone's propellers, interfering with its flight control and causing it to lose balance and flight capability, thus achieving the purpose of intercepting and countering the drone. In this embodiment, four lead blocks are used, corresponding to the four corners of the Kevlar fiber mesh.

[0027] The sabot 4 includes a main body 22 disposed inside the cartridge case 2, as shown in the attached figure. Figure 4 As shown, the lower end of the main body 22 has a spacer section 23, and the lower part of the spacer section 23 has a positioning disk 24; the main body 22 has a main chamber 25 for positioning the projectile 5, and the spacer section 23 has an intermediate channel 26 that communicates with the main chamber 25. The lower end of the intermediate channel 26 communicates with the groove of the positioning disk 24. The propellant 3 is in contact with the positioning disk 24, and the end of the positioning disk is in contact with the propellant. After the propellant is detonated by the primer, part of the gas generated will act on the sabot, and the sabot will push the projectile out of the cartridge case. Part of the gas will also act on the projectile through the intermediate channel, causing the projectile to separate from the sabot.

[0028] The cartridge case 2 includes a shell 27, and the bottom of the shell 27 has a base 28, as shown in the attached figure. Figure 3 As shown, the sabot 4 is disposed inside the housing 27, and the base 28 has a through groove 29 through which the primer comes into contact with the propellant; the metal base 1 includes a ring 30 that fits into the base 28, as shown in the attached figure. Figure 8 As shown, the ring 30 has a central groove 32 for placing the primer 7 in the middle. The ring of the metal base holds the chassis in place, and the primer is placed in the central groove. The entire metal base is a one-piece molded structure. The edge of the ring 30 has a conical edge 31, which provides stable support for the cartridge case, making the entire shotgun structure stable. The primer placed in the base is the starting device for initiating the firing process. By contacting the propellant, the energy generated after being excited ignites the propellant, providing a power source for the shotgun firing. Moreover, the conical edge design makes the projectile more stable when placed on a flat surface, effectively improving the convenience and safety in the stages of storage, transportation, and preparation for use, and reducing the risk of accidents caused by unstable placement.

[0029] The working principle of this utility model is as follows: When anti-drone interception of shotgun shells is required, the trigger of the launching device is pulled first. The firing pin of the launching device violently strikes the primer 7 at the center of the bottom of the metal base 1. The chemical agent inside the primer 7 undergoes a rapid chemical reaction under the impact, instantly generating a large amount of high-temperature and high-pressure gas. This gas quickly passes through the gap between the metal base 1 and the slot 29 of the cartridge case 2 chassis 28 and enters the interior of the cartridge case 2. The high-temperature and high-pressure gas comes into contact with the propellant 3 located in the groove of the positioning plate 24 at the lower part of the sabot 4, and immediately ignites the propellant 3. The propellant 3 begins to burn violently, generating an even larger amount of gas. This gas expands rapidly in the limited space of the cartridge case 2, forming a strong pressure. The high-pressure gas generated by the burning propellant 3, with the projectile 5 placed on top, causes the sabot 4 to be pushed upwards first under this strong pressure. The main body 22 of the sabot 4 tightly wraps around the projectile 5. Under the action of the upward push, the sabot 4 drives the projectile 5 to move upwards together. The lead blocks 11 are assembled into a disc block 21. Due to its large mass, it can maintain a relatively stable flight attitude at the moment of separation from the sabot 4 and the start of flight, relying on its own inertia and initial thrust, providing stable flight direction guidance for the entire warhead 5. As the warhead 5 flies at high speed toward the target drone, when it approaches the drone, due to the huge kinetic energy accumulated during the flight, the Kevlar fiber net 10 connected to the end of the lead block 11 quickly unfolds. The Kevlar fiber net 10 covers the drone like a large net. Kevlar fiber has high strength and wear resistance. Once the fiber net comes into contact with the drone, it will quickly wrap around and damage the drone's propeller and other key components, interfere with the drone's flight control system, and cause the drone to lose balance and flight ability, ultimately achieving the purpose of intercepting and countering the drone. After the sabot 4 pushes the warhead 5 out, it will complete the subsequent actions in a predetermined manner inside or outside the launching device, such as falling to the ground. The whole process efficiently and quickly achieves the interception of the "black flight" drone.

[0030] The above embodiments merely illustrate the implementation of this utility model, and while the descriptions are relatively specific and detailed, they should not be construed as limiting the scope of the utility model patent. Furthermore, in these embodiments, "up," "down," "left," "right," "front," and "back" represent relative positions only, not absolute positions. It should be noted that those skilled in the art can make various modifications and improvements without departing from the concept of this utility model, and these all fall within the protection scope of this utility model. Therefore, the protection scope of this utility model patent should be determined by the appended claims.

Claims

1. Anti-drone interceptor shotgun, characterized by: It includes a metal base (1), a cartridge case (2), a propellant (3), a sabot (4), and a projectile (5) with a mesh mounted on it; the metal base (1) is located at the bottom end of the cartridge case (2), and the open end of the cartridge case (2) is provided with a sealing piece (6) for sealing; the sabot (4) is located inside the cartridge case (2), the projectile (5) is located at the upper part of the sabot (4), and the propellant (3) is located at the lower part of the sabot (4); the bottom center of the metal base (1) is provided with a primer (7) that abuts against the propellant (3).

2. The anti-drone interceptor shotgun according to claim 1, characterized in that: The sealing piece (6) includes a piece body (8), the circumferential surface of which has an annular edge (9) that contacts the inner side of the cartridge case (2).

3. The anti-drone interceptor shotgun according to claim 1, characterized in that: The projectile (5) includes a Kevlar fiber mesh (10), with lead blocks (11) connected to the ends of the Kevlar fiber mesh (10). Multiple lead blocks (11) are assembled into a disc block (21), which is located on the upper part of the sabot (4).

4. The anti-drone interceptor shotgun according to claim 1, characterized in that: The sabot (4) includes a main body (22) disposed inside the cartridge case (2), the lower end of the main body (22) is provided with a spacer section (23), and the lower part of the spacer section (23) is provided with a positioning plate (24); the main body (22) is provided with a main chamber (25) for positioning the projectile (5), the spacer section (23) has an intermediate channel (26) communicating with the main chamber (25), the lower end of the intermediate channel (26) communicating with the groove of the positioning plate (24), and the propellant (3) is in contact with the positioning plate (24).

5. The anti-drone interceptor shotgun according to claim 1, characterized in that: The cartridge case (2) includes a housing (27), the bottom of the housing (27) has a chassis (28), the cartridge sabot (4) is disposed inside the housing (27), and the chassis (28) has a through groove (29).

6. The anti-drone interceptor shotgun according to claim 5, characterized in that: The metal base (1) includes a ring (30) that fits into the chassis (28), and the middle part of the ring (30) is provided with a central groove (32) for placing the primer (7).

7. The anti-drone interceptor shotgun according to claim 6, characterized in that: The ring (30) has a conical edge (31) at its edge.

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