Low-altitude capturing unmanned device

Abstract

The invention relates to the technical field of low-altitude capture, in particular to a low-altitude capture unmanned aerial vehicle. Comprising a first pipe body, a bottom plate is arranged in the first pipe body, the bottom plate is arranged at the position, close to the center, of the first pipe body, a through hole is formed in the center of a bottom plate body, a rail is arranged in the center of the inner side of the first pipe body, a net pushing plate is placed above the bottom plate body, a catching net structure is placed on the net pushing plate, and the catching net structure comprises a net body; the net body is placed on the net pushing plate, an iron ball is arranged on the side of the net body and movably placed in the rail, and a sighting telescope is inserted into one side of the pipe body. The low-altitude catching unmanned aerial vehicle has the beneficial effects that the low-altitude catching unmanned aerial vehicle can effectively catch a low-altitude unmanned aerial vehicle, meanwhile, birds and ground animals can be effectively caught, and the low-altitude catching unmanned aerial vehicle is simple in structure, convenient to maintain, convenient to use, high in operability, rapid and convenient to install and high in practicability. The gunpowder filling and catching net structure is simple and quick to install and operate.

Description

Technical Field

[0001] The invention relates to the technical field of low-altitude capture, and in particular to a low-altitude capture unmanned vehicle. Background Art

[0002] The drone industry has developed rapidly in recent years, and drones have been widely used around the world.

[0003] However, compared with the rapid development of drones, laws, regulations and management technologies are relatively lagging behind, resulting in frequent occurrences of drones flying recklessly.

[0004] In view of the above problems, a low-altitude capture unmanned vehicle is proposed. Summary of the invention

[0005] The purpose of the present invention is to solve the shortcomings of the above-mentioned technology. The technical solution adopted by the present invention is:

[0006] A low-altitude unmanned capture device comprises a tube body, a bottom plate is arranged inside the tube body, and the bottom plate is arranged near the center of the tube body, a through hole is arranged at the center of the bottom plate body, a track is arranged at the center of the inner side of the tube body, a net pushing plate is placed above the bottom plate body, a capture net structure is placed above the net pushing plate, the capture net structure comprises a net body, and the net body is placed above the net pushing plate, an iron ball is arranged on the side of the net body, and the iron ball is movably placed inside the track, a sight is inserted on one side of the tube body, and a back A belt, a tube body 2 is provided on the inner side of the bottom end of the tube body 1, a thread is provided on the inner side of the bottom end of the tube body 1, a thread is provided on the outer side of the top end of the tube body 2, and the top end of the tube body 2 is threadedly connected to the bottom end of the tube body 1, gunpowder is placed inside the tube body 2, a fuse is provided near the center position inside the tube body 2, a firing pin is provided under the fuse, a spring is provided under the firing pin, pull bolts are provided on the sides of the tube bodies, triggers are provided on the sides of the tube bodies, a support bracket is inserted at the end of the tube body 2 away from the tube body 1, and the end of the shoulder strap away from the tube body 1 is clamped on one side of the tube body 2.

[0007] Preferably, a top end of the tube body is designed to expand outward.

[0008] Preferably, the number of the tracks is 6, and the 6 tracks are equidistantly distributed.

[0009] Preferably, the number of the iron balls is 6, and the 6 iron balls are distributed in a circular array on the side of the mesh body.

[0010] Preferably, the iron ball is adapted to the track, and the iron ball can move freely inside the track.

[0011] The beneficial effects of the present invention are:

[0012] The present invention discloses a low-altitude unmanned aerial vehicle capture device, which can effectively capture low-altitude unmanned aerial vehicles, and can also effectively capture birds and ground animals. The present invention has a simple structure, is easy to maintain, is convenient to use, has strong operability, is quick and easy to install, and the gunpowder filling and capture net structure installation and operation are simple and fast. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 It is a schematic diagram of the main structure of the present invention;

[0014] Figure 2 It is a schematic diagram of the main cross-sectional structure of the present invention;

[0015] Figure 3 For the present invention Figure 2 A schematic diagram of the enlarged structure of the middle part A;

[0016] Figure 4 It is a schematic diagram of the top view of the capture net structure of the present invention.

[0017] Reference table of reference numerals:

[0018] 1. Tube body one; 2. Tube body two; 3. Support bracket; 4. Sight; 5. Shoulder strap; 6. Track; 7. Bottom plate; 8. Through hole; 9. Push net plate; 10. Capture net structure; 11. Net body; 12. Iron ball; 13. Gunpowder; 14. Fuse; 15. Firing pin; 16. Bolt; 17. Trigger; 18. Spring. DETAILED DESCRIPTION

[0019] The specific implementation of the present invention is further described below in conjunction with the accompanying drawings, wherein the same components are represented by the same reference numerals.

[0020] It should be noted that the words "front", "rear", "left", "right", "up" and "down" used in the following description refer to directions in the drawings, and the words "inside" and "outside" refer to directions toward or away from the geometric center of a specific component, respectively.

[0021] In order to make the contents of the present invention more clearly understood, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention.

[0022] In order to solve the technical problems in the background technology, a method for capturing unmanned vehicles at low altitude is provided as follows:

[0023] Combination Figure 1-Figure 4As shown, a low-altitude unmanned capture device provided by the present invention includes a tube body 1, the top of the tube body 1 is designed to expand outward, a bottom plate 7 is provided inside the tube body 1, and the bottom plate 7 is arranged near the center of the tube body 1, a through hole 8 is provided at the center of the bottom plate 7, a track 6 is provided at the center of the inner side of the tube body 1, the number of the tracks 6 is 6, and the 6 tracks 6 are equidistantly distributed, a pushing net plate 9 is placed above the bottom plate 7, a capturing net structure 10 is placed above the pushing net plate 9, the capturing net structure 10 includes a net body 11, and the net body 11 is placed above the pushing net plate 9, iron balls 12 are provided on the side of the net body 11, the number of the iron balls 12 is 6, and the 6 iron balls 12 are distributed in a ring array on the side of the net body 11, and the iron balls 12 are movably placed inside the track 6 The iron ball 12 is adapted to the track 6, and the iron ball 12 can move freely inside the track 6. A sighting mirror 4 is inserted on the side of the tube body 1, and a shoulder strap 5 is clamped on the side of the tube body 1. A tube body 2 is provided on the inner side of the bottom end of the tube body 1, and a thread is provided on the inner side of the bottom end of the tube body 1. A thread is provided on the outer side of the top of the tube body 22, and the top of the tube body 22 is threadedly connected to the bottom end of the tube body 1, and gunpowder 13 is placed inside the tube body 22. A fuse 14 is provided near the center of the tube body 22, a firing pin 15 is provided below the fuse 14, and a spring 18 is provided below the firing pin 15. A pull bolt 16 is provided on the side of the tube body 22, and a trigger 17 is provided on the side of the tube body 22. A support bracket 3 is inserted on the end of the tube body 22 away from the tube body 1, and the shoulder strap 5 is clamped on one side of the tube body 22 at an end away from the tube body 1.

[0024] The working principle and use process of the present invention:

[0025] In use: hold the tube body 1 and the tube body 2 2, pull the pull bolt 16, put the end of the support bracket 3 against the shoulder, aim at the target through the sight 4, and then pull the trigger 17. The impact force of the gunpowder 13 hits the push-up mesh plate 9 through the through hole 8, and the push-up mesh plate 9 drives the mesh body 11 and the iron balls 12 to be pushed forward. In this process, the iron balls 12 run inside the track 6 and expand outward. When the six iron balls 12 expand outward, the mesh body will be pulled open to trap the target.

[0026] The above description is only a preferred specific implementation manner of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can make equivalent replacements or changes according to the technical scheme and inventive concept of the present invention within the technical scope disclosed by the present invention, which should be covered by the protection scope of the present invention.

[0027] It should be noted that, in this article, relational terms such as first and second, etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device.

[0028] The above description is only a preferred embodiment of the present invention, and does not limit the patent scope of the present invention. All equivalent structural changes made by using the contents of the present invention specification and drawings under the inventive concept of the present invention, or directly / indirectly applied in other related technical fields are included in the patent protection scope of the present invention.

[0029] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A low-altitude capture of unmanned vehicles, characterized in that: The invention comprises a tube body (1), wherein a bottom plate (7) is provided inside the tube body (1), and the bottom plate (7) is arranged near the center of the tube body (1), a through hole (8) is provided at the center of the bottom plate (7), a track (6) is provided at the center of the inner side of the tube body (1), a net pushing plate (9) is placed above the bottom plate (7), a capture net structure (10) is placed above the net pushing plate (9), the capture net structure (10) comprises a net body (11), and the net body (11) is placed above the net pushing plate (9), an iron ball (12) is provided on the side of the net body (11), and the iron ball (12) is movably placed inside the track (6), a sighting mirror (4) is inserted on the side of the tube body (1), a shoulder strap (5) is clamped on the side of the tube body (1), and the capture net structure (10) comprises a net body (11), and the net body (11) is placed above the net pushing plate (9), an iron ball (12) is provided on the side of the net body (11), and the iron ball (12) is movably placed inside the track (6), a sighting mirror (4) is inserted on the side of the tube body (1), a shoulder strap (5) is clamped on the side of the tube body (1), and The inner side of the bottom end of the tube body 1 (1) is provided with a tube body 2 (2), the inner side of the bottom end of the tube body 1 (1) is provided with a thread, the outer side of the top end of the tube body 2 (2) is provided with a thread, and the top end of the tube body 2 (2) is connected to the bottom end of the tube body 1 (1) by a thread, gunpowder (13) is placed inside the tube body 2 (2), a fuse (14) is provided near the center of the tube body 2 (2), a firing pin (15) is provided below the fuse (14), a spring (18) is provided below the firing pin (15), a pull bolt (16) is provided on the side of the tube body 2 (2), a trigger (17) is provided on the side of the tube body 2 (2), a support bracket (3) is inserted at one end of the tube body 2 (2) away from the tube body 1 (1), and the shoulder strap (5) is clamped on one side of the tube body 2 (2) at one end away from the tube body 1 (1).

2. The low-altitude capture unmanned vehicle according to claim 1, characterized in that: The top end of the tube body (1) is designed to expand outwards.

3. The low-altitude unmanned vehicle capture device according to claim 1, characterized in that: The number of the tracks (6) is 6, and the 6 tracks (6) are equidistantly distributed.

4. The low-altitude capture unmanned vehicle according to claim 1, characterized in that: The number of the iron balls (12) is 6, and the 6 iron balls (12) are distributed in a circular array on the side of the mesh body (11).

5. The low-altitude capture unmanned vehicle according to claim 4, characterized in that: The iron ball (12) is adapted to the track (6), and the iron ball (12) can move freely inside the track (6).

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