Individual-soldier anti-unmanned aerial vehicle capturing device

Abstract

The utility model belongs to the field of anti-unmanned aerial vehicles, and provides an individual-soldier anti-unmanned aerial vehicle catching device which comprises a hollow pipe, a first partition plate is installed in the hollow pipe, a second partition plate is installed on one side of the first partition plate, and a carbon fiber scattering net bullet is movably installed in the portion, on the other side of the first partition plate, of the hollow pipe. A sliding groove is formed in the hollow pipe between the first partition plate and the second partition plate, and a pressing mechanism is installed in the hollow pipe on one side of the second partition plate. The ejection mechanism is mounted in the hollow pipe; the position of the ejection mechanism in the hollow pipe can be adjusted through the hand bracket during use, the position of the ejection mechanism is limited through the pressing mechanism, the pressing mechanism is pressed after the unmanned aerial vehicle is aimed at, the extrusion spring in the extrusion state is instantly opened, and the ejection mechanism is fixed. And the ejection mechanism rapidly impacts the carbon fiber scattering net bomb, so that the carbon fiber scattering net bomb is ejected from the interior of the hollow pipe to capture the unmanned aerial vehicle, and the unmanned aerial vehicle is convenient to carry.

Description

Technical Field

[0001] This utility model belongs to the field of anti-drone technology, specifically a single-soldier anti-drone capture device. Background Technology

[0002] With the rapid development of drone technology, drones are increasingly widely used in military and civilian fields. However, the improper use of drones, such as "unauthorized flights" and "attacks on people," is frequent, posing a serious threat to public safety. To address this challenge, countries have strengthened their low-altitude protection policies and developed various anti-drone technologies and equipment. Anti-drone devices typically consist of two parts: a detection system and an interception system. The detection system uses radar detection, radio signal monitoring, photoelectric identification and tracking, and sound monitoring technologies to detect and identify drones. Once a drone is detected, the detection system transmits relevant information to the interception system, which uses jamming technology to cut off the communication link between the drone and its remote controller by emitting electromagnetic waves of a specific frequency.

[0003] However, existing anti-drone devices are mostly suitable for intercepting drones within a specific range, which is not very flexible, costly, and cannot be distributed to individual soldiers for use. Utility Model Content

[0004] To address the aforementioned technical problems, this utility model provides a capture device for individual soldiers against unmanned aerial vehicles (UAVs), thus solving the problem that existing technologies cannot be distributed to individual soldiers for carrying and use.

[0005] A man-portable anti-drone capture device, comprising:

[0006] A hollow tube, wherein a first partition is installed inside the hollow tube, a second partition is installed on one side of the first partition, and a carbon fiber distributing mesh is movably installed inside the hollow tube on the other side of the first partition.

[0007] A groove is provided on the hollow tube between the first partition and the second partition. A hand support is slidably installed on the periphery of the hollow tube. A compression ring connected to the hand support is slidably installed inside the groove. A pressing mechanism is installed inside the hollow tube on one side of the second partition.

[0008] A catapult mechanism, which is installed inside the hollow tube;

[0009] The ejection mechanism includes an impact rod movably installed inside the hollow tube, a plurality of sliders are installed around the impact rod, a slide rail is installed inside the hollow tube around the sliders, a hook is installed at the rear end of the impact rod, and the end of the impact rod passes through the compression ring.

[0010] A compression spring is sleeved around the impact rod on one side of the slider, and one side of the compression spring is connected to the second partition plate.

[0011] Preferably, the first and second partitions have through holes inside that are compatible with the impact rod and the hook, and a plurality of buffer springs are arranged around one side of the first partition.

[0012] Preferably, the outer contour of the hollow tube hand support is provided with several anti-slip grooves, and the top of the compression ring is provided with a protrusion extending into the slide rail.

[0013] Preferably, the pressing mechanism includes a movable frame movably installed inside the hollow tube, a locking block installed on the other side of the movable frame, and a pressing block extending out of the hollow tube installed on the top of the movable frame.

[0014] Preferably, the pressing mechanism further includes a return spring installed inside the movable frame, the bottom of which passes through the movable frame and connects to the inner wall of the hollow tube.

[0015] Preferably, the pressing mechanism further includes a limiting block installed at the rear end of the movable frame, and the inner wall of the hollow tube is provided with a groove to allow the limiting block to move.

[0016] Preferably, the hollow tube has an arc-shaped groove on its outer periphery, and a protective cover is slidably installed inside the arc-shaped groove, the protective cover being sleeved around the pressing block.

[0017] Compared with the prior art, the present invention has the following beneficial effects:

[0018] 1. This utility model allows for adjustment of the position of the catapult mechanism inside the hollow tube during use via a hand support. The position of the catapult mechanism is limited by a pressing mechanism. After aiming at the drone, pressing the pressing mechanism causes the compression spring, which is in a compressed state, to open instantly, allowing the catapult mechanism to quickly impact the carbon fiber dispersion net projectile, thereby launching the carbon fiber dispersion net projectile from inside the hollow tube to capture the drone. It has the advantages of simple operation, low production cost, and ease of carrying and use by individual soldiers.

[0019] 2. This utility model has a protective cover installed to shield and protect the pressing block, preventing the carbon fiber net bullet from being launched due to squeezing of the pressing block caused by operational errors during use. Attached Figure Description

[0020] Figure 1 This is a perspective view of the present utility model;

[0021] Figure 2 This is a schematic diagram of the internal structure of the present invention;

[0022] Figure 3 This is a partial sectional view of the hollow tube and hand support of this utility model;

[0023] Figure 4 This is a partial cross-sectional view of the pressing mechanism of this utility model;

[0024] Figure 5 This is a schematic diagram of the ejection mechanism of this utility model;

[0025] Figure 6 This is a rear view of the present invention.

[0026] In the picture:

[0027] 1. Hollow tube; 2. Arc groove; 3. Protective cover; 4. Hand support; 5. First partition; 6. Second partition; 7. Pressing mechanism; 701. Movable frame; 702. Locking block; 703. Pressing block; 704. Return spring; 705. Limiting block; 8. Compression ring; 9. Ejection mechanism; 901. Impact rod; 902. Hook; 903. Slider; 10. Compression spring; 11. Carbon fiber distributed mesh spring; 12. Slide rail; 13. Slide groove. Detailed Implementation

[0028] The embodiments of this utility model will be described in further detail below with reference to the accompanying drawings and examples. The following examples are for illustrative purposes only and should not be construed as limiting the scope of this utility model.

[0029] As attached Figure 1 Appendix Figure 2 Appendix Figure 3 Appendix Figure 4 Appendix Figure 5 and attached Figure 6 As shown:

[0030] Example 1: This utility model provides a capture device for a single-soldier anti-drone, comprising:

[0031] Hollow tube 1, with a first partition 5 installed inside the hollow tube 1, a second partition 6 installed on one side of the first partition 5, and a carbon fiber distributing mesh bullet 11 movably installed inside the hollow tube 1 on the other side of the first partition 5.

[0032] A groove 13 is provided on the hollow tube 1 between the first partition 5 and the second partition 6. A hand support 4 is slidably installed on the outer periphery of the hollow tube 1. A compression ring 8 connected to the hand support 4 is slidably installed inside the groove 13. A pressing mechanism 7 is installed inside the hollow tube 1 on one side of the second partition 6.

[0033] Ejection mechanism 9 is installed inside hollow tube 1;

[0034] The ejection mechanism 9 includes an impact rod 901 movably installed inside the hollow tube 1. Several sliders 903 are installed around the impact rod 901. A slide rail 12 is installed inside the hollow tube 1 around the sliders 903. A hook 902 is installed at the rear end of the impact rod 901. The end of the impact rod 901 passes through the compression ring 8.

[0035] A compression spring 10 is sleeved around the impact rod 901 on one side of the slider 903, and one side of the compression spring 10 is connected to the second partition 6.

[0036] The length and range of the hollow tube 1 can be customized to meet specific requirements. Ideally, the hollow tube 1 should be around 40cm, with a launch distance of around 10m and a capture area of ​​around ten square meters when the carbon fiber net projectile 11 is deployed.

[0037] As can be seen from the above, when using the hand support 4, pull it horizontally. As the hand support 4 moves around the hollow tube 1, it pulls the compression ring 8 and moves inside the hollow tube 1. After the compression ring 8 contacts the slider 903, the slider 903 compresses and contracts the compression spring 10. While the compression spring 10 is deformed, the pressing mechanism 7 hooks the hook 902 to limit the position of the ejection mechanism 9 inside the hollow tube 1. Release the force on the hand support 4 and add the carbon fiber dispersion net bullet 11 to be launched into the hollow tube 1, so that the carbon fiber dispersion net bullet 11 contacts the first partition 5, thereby completing the launch preparation.

[0038] After preparation, align the launch port of the hollow tube 1 with the drone. After aiming, press the pressing mechanism 7. After the pressing mechanism 7 releases the limit on the ejection mechanism 9, the compression spring 10, which is in a compressed state, opens instantly, pushing the ejection mechanism 9 to move quickly inside the hollow tube 1. The slide rail 12 guides the trajectory of the slider 903, making the movement of the impact rod 901 more stable. Under the push of the compression spring 10, the impact rod 901 moves instantaneously towards the carbon fiber net bullet 11. After the end contacts the side of the carbon fiber net bullet 11, the instantaneous impact force pushes the carbon fiber net bullet 11 out from inside the hollow tube 1. After the carbon fiber net bullet 11 is launched from inside the hollow tube 1 towards the drone, it automatically opens a carbon fiber net bullet 11 of about ten square meters to capture the drone.

[0039] The hand support 4 allows for adjustment of the position of the ejection mechanism 9 inside the hollow tube 1 during use. The pressing mechanism 7 limits the position of the ejection mechanism 9. After aiming at the drone, pressing the pressing mechanism 7 causes the compression spring 10, which is in a compressed state, to open instantly, allowing the ejection mechanism 9 to quickly impact the carbon fiber dispersion net bullet 11, thereby launching the carbon fiber dispersion net bullet 11 from inside the hollow tube 1 to capture the drone.

[0040] As attached Figure 2 Appendix Figure 3 and attached Figure 5 As shown:

[0041] Specifically, regarding the first partition 5 and the second partition 6 mentioned above, the interior of the first partition 5 and the second partition 6 is provided with through holes that are compatible with the impact rod 901 and the hook 902, and a number of buffer springs are surrounded on one side of the first partition 5.

[0042] As can be seen from the above, the through holes inside the first partition 5 and the second partition 6 can satisfy the movement of the ejection mechanism 9 during use. The buffer spring can effectively buffer the extrusion ring 8, reduce the impact force between the extrusion ring 8 and the hollow tube 1, and extend the service life of the device structure.

[0043] As shown in the attached document Figure 1 Appendix Figure 2 Appendix Figure 3 and attached Figure 6 :

[0044] Specifically, regarding the hollow tube 1 mentioned above, the outer contour of the hand support 4 of the hollow tube 1 is provided with several anti-slip grooves, and the top of the compression ring 8 is equipped with a protrusion extending into the slide rail 12.

[0045] As can be seen from the above, the anti-slip groove on the outer periphery of the hand support 4 can increase the contact area between the hand support 4 and the user's palm during use, making the hand support 4 easier for the user to adjust. The protrusion on the compression ring 8 can assist in limiting the trajectory of the compression ring 8 in cooperation with the slide groove 13, making the movement of the compression ring 8 smoother.

[0046] As attached Figure 4 As shown:

[0047] Specifically, regarding the aforementioned pressing mechanism 7, the pressing mechanism 7 includes a movable frame 701 movably installed inside the hollow tube 1, a locking block 702 installed on the other side of the movable frame 701, and a pressing block 703 extending out of the hollow tube 1 installed on the top of the movable frame 701.

[0048] The pressing mechanism 7 also includes a return spring 704 installed inside the movable frame 701. The bottom of the return spring 704 passes through the movable frame 701 and is connected to the inner wall of the hollow tube 1.

[0049] The pressing mechanism 7 also includes a limiting block 705 installed at the rear end of the movable frame 701, and a groove is provided on the inner wall of the hollow tube 1 to allow the limiting block 705 to move.

[0050] As can be seen from the above, during use, when the hook 902 passes through the second partition 6 and squeezes the locking block 702, the locking block 702 moves downward automatically after being squeezed. The return spring 704 begins to deform after being compressed. After the locking block 702 hooks out the hook 902, the return spring 704 pushes the movable frame 701 to reset, thereby limiting the position of the ejection mechanism 9.

[0051] When firing is required, the pressing block 703 is pressed manually. After the pressing block 703 is under force, it pushes the movable frame 701 to move downward. During the downward movement of the limiting block 705, the locking block 702 moves downward and squeezes the return spring 704, causing the locking block 702 to disengage from the hook 902, thereby realizing the firing of the carbon fiber dispersion net bullet 11 from the hollow tube 1. After releasing the pressure on the pressing block 703, the movable frame 701 automatically resets under the push of the return spring 704.

[0052] During the movement of the movable frame 701, the limiting block 705 will move in the groove on the inner wall of the hollow tube 1, making the movement trajectory of the movable frame 701 more stable.

[0053] As attached Figure 1 Appendix Figure 2 Appendix Figure 3 Appendix Figure 4 and attached Figure 6 As shown:

[0054] Example 2: This example is basically the same as the previous example, except that:

[0055] An arc-shaped groove 2 is provided on the outer periphery of the hollow tube 1, and a protective cover 3 is slidably installed inside the arc-shaped groove 2. The protective cover 3 is sleeved on the outer periphery of the pressing block 703.

[0056] As can be seen from the above, the protective cover 3 can slide inside the arc groove 2. When the protective cover 3 is slid to the periphery of the pressing block 703, the protective cover 3 is used to shield and protect the pressing block 703, preventing the carbon fiber dispersion net bullet 11 from being launched due to squeezing the pressing block 703 due to operational errors during use. After confirming the launch angle, the pressing block 703 can be exposed by moving the protective cover 3 out from the top of the pressing block 703 along the arc groove 2, thereby enabling the pressing block 703 to be pressed.

[0057] The embodiments of this utility model are given for the purpose of illustration and description. Although embodiments of this utility model have been shown and described above, it is understood that the above embodiments are exemplary and should not be construed as limiting the utility model. Those skilled in the art can make changes, modifications, substitutions and variations to the above embodiments within the scope of this utility model.

Claims

1. A capture device for a single-soldier anti-drone, characterized in that, include: Hollow tube (1), a first partition (5) is installed inside the hollow tube (1), a second partition (6) is installed on one side of the first partition (5), and a carbon fiber dispersing net bullet (11) is movably installed inside the hollow tube (1) on the other side of the first partition (5). A groove (13) is provided on the hollow tube (1) between the first partition (5) and the second partition (6). A hand support (4) is slidably installed on the periphery of the hollow tube (1). A compression ring (8) connected to the hand support (4) is slidably installed inside the groove (13). A pressing mechanism (7) is installed inside the hollow tube (1) on one side of the second partition (6). Ejection mechanism (9), which is installed inside the hollow tube (1); The ejection mechanism (9) includes an impact rod (901) movably installed inside the hollow tube (1), a plurality of sliders (903) are installed around the impact rod (901), a slide rail (12) is installed inside the hollow tube (1) around the sliders (903), a hook (902) is installed at the rear end of the impact rod (901), and the end of the impact rod (901) passes through the compression ring (8); A compression spring (10) is sleeved around the impact rod (901) on one side of the slider (903), and one side of the compression spring (10) is connected to the second partition (6).

2. The capture device for a single-soldier anti-drone as described in claim 1, characterized in that: The first partition (5) and the second partition (6) have through holes that are compatible with the impact rod (901) and the hook (902) inside. A number of buffer springs are surrounded on one side of the first partition (5).

3. The capture device for a single-soldier anti-drone as described in claim 1, characterized in that: The hollow tube (1) has several anti-slip grooves on the outer contour of the hand support (4), and the top of the compression ring (8) is fitted with a protrusion extending into the slide rail (12).

4. The capture device for a single-soldier anti-drone as described in claim 1, characterized in that: The pressing mechanism (7) includes a movable frame (701) movably installed inside the hollow tube (1), a locking block (702) is installed on the other side of the movable frame (701), and a pressing block (703) extending out of the hollow tube (1) is installed on the top of the movable frame (701).

5. The capture device for a single-soldier anti-drone as described in claim 4, characterized in that: The pressing mechanism (7) also includes a return spring (704) installed inside the movable frame (701), the bottom of which passes through the movable frame (701) and is connected to the inner wall of the hollow tube (1).

6. The capture device for a single-soldier anti-drone as described in claim 5, characterized in that: The pressing mechanism (7) also includes a limiting block (705) installed at the rear end of the movable frame (701), and the inner wall of the hollow tube (1) is provided with a groove to allow the limiting block (705) to move.

7. The capture device for a single-soldier anti-drone according to any one of claims 4-6, characterized in that: The hollow tube (1) has an arc-shaped groove (2) on its periphery, and a protective cover (3) is slidably installed inside the arc-shaped groove (2). The protective cover (3) is sleeved on the periphery of the pressing block (703).

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