Unmanned aerial vehicle capturing device capable of conveniently carrying equipment

Abstract

The utility model discloses an unmanned aerial vehicle capturing device facilitating equipment carrying. The unmanned aerial vehicle capturing device comprises a shell; the central cylinder is arranged in the middle of the inner cavity of the shell; and the number of the launching cylinders is four, the four launching cylinders are arranged along the side walls of an inner cavity of the shell respectively, the launching cylinders are arranged along the diagonal lines of the corresponding side walls of the shell, the arrangement positions of the four launching cylinders are mutually staggered, the front ends of the four launching cylinders are in a divergent shape, and the launching cylinders are tangent to the center cylinder. According to the utility model, the structural design is novel, the size is small, the occupied space is small, the central cylinder is arranged in the middle, during carrying and assembling, other equipment can be carried in the central cylinder, or other equipment parts can be assembled in the central cylinder, or the central cylinder is used for wiring, the occupied space is saved, and simultaneous loading with other equipment is facilitated.

Description

Technical Field

[0001] The utility model relates to a drone capturing device facilitating equipment mounting, belonging to the technical field of capturing devices. Background Art

[0002] With the rapid development of the drone market, in special places such as civil airports, confidential places, and public places, drones will undoubtedly pose potential safety and economic losses to society, and may bring safety problems such as affecting aviation order, breaking into sensitive areas, and dropping prohibited items. Therefore, it is necessary to manage civilian drones in an orderly manner and take effective measures to capture harmful and dangerous suspicious drones.

[0003] When capturing illegal drones, the method of launching a capture net is often used. However, in the prior art, the launch method of the capture net often uses gunpowder and other methods, which have high manufacturing costs, increase the launch cost, are not conducive to frequent and multiple uses, and do not have universality. Moreover, the capture net launch device in the prior art is large in size, not convenient to be mounted on other devices. Limited by the volume of the capture net launch device, it is not convenient to mount multiple devices at the same time and cannot meet the usage requirements.

[0004] Therefore, we propose a drone capturing device facilitating equipment mounting. Content of the Utility Model

[0005] The purpose of the utility model is to provide a drone capturing device facilitating equipment mounting, which has low manufacturing and launch costs, is small and compact in size, convenient to mount, and has a central cylinder opened at the center, which can mount other devices or be used for the installation of other equipment parts.

[0006] To solve the above technical problems, the utility model adopts the following technical scheme: A drone capturing device facilitating equipment mounting, comprising:

[0007] A housing;

[0008] A central cylinder, which is placed in the middle of the inner cavity of the housing;

[0009] Four launching cylinders, which are respectively arranged along the side walls of the inner cavity of the housing, the four launching cylinders are arranged along the diagonals of the corresponding side walls of the housing, the arrangement positions of the four launching cylinders are staggered with each other and the front ends are divergent, and the launching cylinders are tangent to the central cylinder;

[0010] A net part, which is loaded in the inner cavity of the launching cylinder and wound around the front end of the central cylinder;

[0011] An ejection part, which is installed in the launching cylinder, and the net part is connected to the ejection part;

[0012] A triggering part, which is installed in the inner cavity of the housing. The triggering part is connected to the tail end of the ejection part, and the triggering part can control the ejection of the ejection part.

[0013] For the aforementioned drone capture net launching device, front covers and rear covers are respectively provided at the front and rear ends of the housing.

[0014] For the aforementioned drone capture net launching device, a positioning plate and a limiting plate are arranged in the inner cavity of the housing. The positioning plate is arranged on the front side of the limiting plate. The tail end of the launching tube penetrates through the positioning plate and is placed on the surface of the limiting plate. The central tube sequentially penetrates through the front cover, the positioning plate, the limiting plate and the rear cover.

[0015] For the aforementioned drone capture net launching device, the ejection part includes an ejection rod. An elastic element is sleeved on the surface of the ejection rod. The ejection rod sleeved with the elastic element is inserted and installed in the corresponding launching tube. The tail end of the ejection rod penetrates through the limiting plate, and a fixing hole is opened at the tail end of the ejection rod. A fixing rope connected end to end is sequentially penetrated through the fixing holes of each ejection rod.

[0016] For the aforementioned drone capture net launching device, the triggering part includes a cutter holder. The cutter holder is inserted into the inner cavity at the tail end of the ejection rod. A cutter groove is opened at the tail of the cutter holder. A cutter is arranged in the cutter groove. A through hole vertically penetrating the cutter groove is opened on the side wall at the tail of the cutter holder. The fixing rope penetrates through the through hole. One end of the cutter is connected to a traction rope, and the other end of the traction rope is connected to a driving component. The driving component is arranged on the inner side wall of the rear cover.

[0017] For the aforementioned drone capture net launching device, the driving component includes a driving motor and a roller. The driving motor is fixed on the inner side wall of the rear cover. A roller is arranged at the output end of the driving motor. The traction rope is fixed and wound on the surface of the roller.

[0018] For the aforementioned drone capture net launching device, a reinforcing plate is arranged in the middle of the inner cavity of the housing. The central tube penetrates through the reinforcing plate. Reinforcing holes are opened around the reinforcing plate. The launching tube penetrates through the corresponding reinforcing holes.

[0019] For the aforementioned drone capture net launching device, the net part includes a net body and net ropes. The net body is rectangular and net ropes are arranged around it. One end of the net rope far away from the net body is connected to the ejection rod. The net body is loaded in the launching tube.

[0020] For the aforementioned drone capture net launching device, a connection hole is opened at the top of the ejection rod. The net rope penetrates through the connection hole and is tied and fixed.

[0021] For the aforementioned drone capture net launching device, the length of the elastic element is twice or more than twice the length of the ejection rod.

[0022] Compared with the prior art, the utility model has at least the following beneficial effects:

[0023] (1) The utility model has a novel structural design, is small and compact in size, occupies little space, and is provided with a central cylinder in the middle. When carrying and assembling, other devices can be carried in the central cylinder, or other device parts can be assembled, or used for wire routing, saving occupied space and facilitating simultaneous loading with other devices.

[0024] (2) The whole of the utility model is light in texture and convenient to carry. Its structure is stable, suitable for various environments, and is provided with a structure of a coupling cutter, further reducing the overall volume.

[0025] (3) The utility model has a clever structural design, can realize the launch of the capture net through a mechanical structure, has a low cost and a low use cost, greatly saves the economic cost of countering illegal unmanned aerial vehicles, and has universality. BRIEF DESCRIPTION OF THE DRAWINGS

[0026] Figure 1 is a three-dimensional schematic diagram of the utility model;

[0027] Figure 2 is an exploded structural schematic diagram of the utility model;

[0028] Figure 3 is a structural schematic diagram of the ejection part of the utility model;

[0029] Figure 4 is a connection structural schematic diagram of the ejection part and the trigger part of the utility model;

[0030] Figure 5 is a structural schematic diagram of the cutter installation of the utility model;

[0031] Figure 6 is a structural schematic diagram of the net part of the utility model.

[0032] Reference numerals: 1 - housing, 2 - central cylinder, 3 - launch cylinder, 4 - net part, 401 - net body, 402 - net rope, 5 - ejection part, 501 - ejection rod, 502 - elastic element, 503 - fixing hole, 504 - fixing rope, 505 - connection hole, 6 - reinforcement plate, 601 - reinforcement hole, 7 - trigger part, 701 - cutter holder, 702 - cutter groove, 703 - cutter, 704 - perforation, 705 - traction rope, 706 - driving component, 707 - driving motor, 708 - roller, 8 - front cover, 9 - rear cover, 10 - limiting plate, 11 - positioning plate.

[0033] The following further describes the utility model in conjunction with the drawings and specific embodiments. SPECIFIC EMBODIMENTS

[0034] Embodiment 1 of the present utility model: A drone capture device facilitating equipment loading, characterized by comprising:

[0035] A housing 1, the housing 1 being in the shape of a square tube and hollow inside;

[0036] A central tube 2, the central tube 2 being placed in the middle of the inner cavity of the housing 1. Other equipment can be loaded in the central tube 2, or other equipment parts can be assembled, or it can be used for wiring, saving occupied space and facilitating simultaneous loading with other equipment;

[0037] Four launching tubes 3, the four launching tubes 3 being respectively arranged along the side walls of the inner cavity of the housing 1. The launching tubes 3 are arranged along the diagonals of the corresponding side walls of the housing 1, that is, one launching tube 3 is arranged along the diagonal of each side wall of the housing 1. The installation positions of the four launching tubes 3 are staggered with each other and the front ends are divergent. The front ends of the four launching tubes 3 are respectively at the four corners of the housing 1, and the launching tubes 3 are tangent to the central tube 2.

[0038] A net part 4, the net part 4 being loaded in the inner cavity of the launching tube 3 and wound around the front end of the central tube 2;

[0039] An ejection part 5, the ejection part 5 being installed in the launching tube 3. The net part 4 is connected to the ejection part 5. When the ejection part 5 acts, it can carry the net part 4 out and make it unfold;

[0040] A trigger part 7, the trigger part 7 being installed in the inner cavity of the housing 1. The trigger part 7 is connected to the tail end of the ejection part 5, and the trigger part 7 can control the ejection of the ejection part 5.

[0041] Embodiment 2 of the present utility model: A drone capture device facilitating equipment loading, characterized by comprising: a housing 1, the housing 1 being in the shape of a square tube and hollow inside; a central tube 2, the central tube 2 being placed in the middle of the inner cavity of the housing 1. Other equipment can be loaded in the central tube 2, or other equipment parts can be assembled, or it can be used for wiring, saving occupied space and facilitating simultaneous loading with other equipment; four launching tubes 3, the four launching tubes 3 being respectively arranged along the side walls of the inner cavity of the housing 1. The launching tubes 3 are arranged along the diagonals of the corresponding side walls of the housing 1, that is, one launching tube 3 is arranged along the diagonal of each side wall of the housing 1. The installation positions of the four launching tubes 3 are staggered with each other and the front ends are divergent. The front ends of the four launching tubes 3 are respectively at the four corners of the housing 1, and the launching tubes 3 are tangent to the central tube 2; a net part 4, the net part 4 being loaded in the inner cavity of the launching tube 3 and wound around the front end of the central tube 2; an ejection part 5, the ejection part 5 being installed in the launching tube 3. The net part 4 is connected to the ejection part 5. When the ejection part 5 acts, it can carry the net part 4 out and make it unfold; a trigger part 7, the trigger part 7 being installed in the inner cavity of the housing 1. The trigger part 7 is connected to the tail end of the ejection part 5, and the trigger part 7 can control the ejection of the ejection part 5.

[0042] At the front and rear ends of the housing 1, a front cover 8 and a rear cover 9 are respectively provided. Inside the cavity of the housing 1, a positioning plate 11 and a limiting plate 10 are arranged. The positioning plate 11 is arranged on the front side of the limiting plate 10. The tail end of the launch tube 3 penetrates through the positioning plate 11 and is placed on the surface of the limiting plate 10. At the same time, the central tube 2 sequentially penetrates through the front cover 8, the positioning plate 11, the limiting plate 10, and the rear cover 9.

[0043] The ejection part 5 includes an ejection rod 501. An elastic element 502 is sleeved on the surface of the ejection rod 501. The ejection rod 501 sleeved with the elastic element 502 is inserted and installed in the corresponding launch tube 3. The tail end of the ejection rod 501 penetrates through the limiting plate 10, and a fixing hole 503 is opened at the tail end of the ejection rod 501. Fixing ropes 504 connected end to end are sequentially penetrated in the fixing holes 503 of each ejection rod 501. After the ejection rod 501 compresses the elastic element 502, it is fixed by the fixing rope 504.

[0044] The triggering part 7 includes a cutter holder 701. The cutter holder 701 is inserted into the inner cavity at the tail end of the ejection rod 501. A cutter groove 702 is opened at the tail of the cutter holder 701. A cutter 703 is arranged in the cutter groove 702. A through hole 704 vertically penetrating the cutter groove 702 is opened on the side wall at the tail of the cutter holder 701. The fixing rope 504 penetrates through the through hole 704. One end of a traction rope 705 is connected to the cutter 703, and the other end of the traction rope 705 is connected to a driving component 706. The driving component 706 is arranged on the inner side wall of the rear cover 9. The driving component 706 is connected to the controller. The driving component 706 pulls the cutter 703 to act, and can cut off the fixing rope 504, and the compressed elastic element 602 ejects the ejection rod 501.

[0045] Embodiment 3 of the present invention: An unmanned aerial vehicle capturing device convenient for carrying equipment, which is characterized in that it includes: a housing 1, the housing 1 is in the shape of a square tube and is hollow inside; a central tube 2, the central tube 2 is placed in the middle of the inner cavity of the housing 1, and other equipment can be carried in the central tube 2, or other equipment parts can be assembled, or it can be used for wire routing, saving occupied space and being convenient for simultaneous loading with other equipment; four launch tubes 3, the four launch tubes 3 are respectively arranged along the inner side walls of each side of the housing 1, the launch tubes 3 are arranged along the diagonals of the corresponding side walls of the housing 1, that is, one launch tube 3 is arranged along the diagonal of each side wall of the housing 1, the installation positions of the four launch tubes 3 are staggered with each other and the front ends are divergent, the front ends of the four launch tubes 3 are respectively at the four corners of the housing 1, and the launch tubes 3 are tangent to the central tube 2; a net part 4, the net part 4 is loaded in the inner cavity of the launch tube 3 and wound around the front end of the central tube 2; an ejection part 5, the ejection part 5 is installed in the launch tube 3, the net part 4 is connected to the ejection part 5, and when the ejection part 5 acts, it can carry the net part 4 and shoot it out and make it unfold; a triggering part 7, the triggering part 7 is installed in the inner cavity of the housing 1, the triggering part 7 is connected to the tail end of the ejection part 5, and the triggering part 7 can control the ejection of the ejection part 5.

[0046] At the front and rear ends of the housing 1, a front cover 8 and a rear cover 9 are respectively provided. Inside the housing 1, a positioning plate 11 and a limiting plate 10 are arranged. The positioning plate 11 is arranged on the front side of the limiting plate 10. The tail end of the launch tube 3 penetrates through the positioning plate 11 and is placed on the surface of the limiting plate 10. At the same time, the central tube 2 sequentially penetrates through the front cover 8, the positioning plate 11, the limiting plate 10, and the rear cover 9.

[0047] The ejection part 5 includes an ejection rod 501. An elastic element 502 is sleeved on the surface of the ejection rod 501. The ejection rod 501 sleeved with the elastic element 502 is inserted and installed in the corresponding launch tube 3. The tail end of the ejection rod 501 penetrates through the limiting plate 10, and a fixing hole 503 is opened at the tail end of the ejection rod 501. A fixing rope 504 connected end to end is sequentially passed through the fixing holes 503 of each ejection rod 501. After the ejection rod 501 compresses the elastic element 502, it is fixed by the fixing rope 504.

[0048] The trigger part 7 includes a cutter holder 701. The cutter holder 701 is inserted into the inner cavity at the tail end of the ejection rod 501. A cutter groove 702 is opened at the tail of the cutter holder 701. A cutter 703 is arranged in the cutter groove 702. A through hole 704 vertically penetrating the cutter groove 702 is opened on the side wall at the tail of the cutter holder 701. The fixing rope 504 passes through the through hole 704. One end of a traction rope 705 is connected to the cutter 703, and the other end of the traction rope 705 is connected to a driving component 706. The driving component 706 is arranged on the inner side wall of the rear cover 9. The driving component 706 is connected to a controller. The driving component 706 pulls the cutter 703 to act, and can cut off the fixing rope 504. The compressed elastic element 602 ejects the ejection rod 501. Among them, the driving component 706 includes a driving motor 707 and a roller 708. The driving motor 707 is fixed on the inner side wall of the rear cover 9. A roller 708 is arranged at the output end of the driving motor 707. The traction rope 705 is fixed and wound on the surface of the roller 708. The driving motor 707 is connected to a controller. By controlling the driving motor 707 to rotate, the roller 708 is driven to rotate, and the traction rope 705 can be pulled.

[0049] Among them, a reinforcing plate 6 is arranged in the middle of the inner cavity of the housing 1. The central tube 2 penetrates through the reinforcing plate 6. Reinforcing holes 601 are opened around the reinforcing plate 6. The launch tube 3 penetrates through the corresponding reinforcing holes 601. The reinforcing plate 6 is used to further reinforce the central tube 2 and the launch tube 3.

[0050] Embodiment 4 of the present utility model: An unmanned aerial vehicle capture device facilitating equipment mounting, characterized by comprising: a housing 1, the housing 1 being in the shape of a square tube and hollow inside; a central tube 2, the central tube 2 being placed in the middle of the inner cavity of the housing 1, where other equipment can be mounted in the central tube 2, or other equipment parts can be assembled, or it can be used for wire routing, saving occupied space and facilitating simultaneous loading with other equipment; four launch tubes 3, the four launch tubes 3 being respectively arranged along the inner sidewalls of the housing 1, the launch tubes 3 being arranged along the diagonals of the corresponding sidewalls of the housing 1, that is, one launch tube 3 is arranged along the diagonal of each sidewall of the housing 1, the four launch tubes 3 being arranged at staggered positions and having divergent fronts, the fronts of the four launch tubes 3 being respectively at the four corners of the housing 1, and the launch tubes 3 being tangent to the central tube 2; a net part 4, the net part 4 being loaded into the inner cavity of the launch tubes 3 and wound around the front end of the central tube 2; an ejection part 5, the ejection part 5 being installed in the launch tubes 3, the net part 4 being connected to the ejection part 5, and when the ejection part 5 operates, it can carry the net part 4 and shoot it out and make it unfold; a trigger part 7, the trigger part 7 being installed in the inner cavity of the housing 1, the trigger part 7 being connected to the tail end of the ejection part 5, and the trigger part 7 can control the ejection of the ejection part 5.

[0051] A front cover 8 and a rear cover 9 are respectively provided at the front and rear ends of the housing 1, a positioning plate 11 and a limiting plate 10 are arranged in the inner cavity of the housing 1, the positioning plate 11 is arranged on the front side of the limiting plate 10, the tail end of the launch tube 3 penetrates through the positioning plate 11 and is placed on the surface of the limiting plate 10, and at the same time, the central tube 2 sequentially penetrates through the front cover 8, the positioning plate 11, the limiting plate 10 and the rear cover 9.

[0052] The ejection part 5 includes an ejection rod 501, an elastic element 502 is sleeved on the surface of the ejection rod 501, the ejection rod 501 sleeved with the elastic element 502 is inserted and installed in the corresponding launch tube 3, the tail end of the ejection rod 501 penetrates through the limiting plate 10, and a fixing hole 503 is opened at the tail end of the ejection rod 501. A fixing rope 504 connected end to end is sequentially passed through the fixing holes 503 of the ejection rods 501. After the ejection rod 501 compresses the elastic element 502, it is fixed by the fixing rope 504, wherein the length of the elastic element 502 is twice or more than twice the length of the ejection rod 501.

[0053] The trigger part 7 includes a cutter holder 701. The cutter holder 701 is inserted into the inner cavity at the tail end of the ejection rod 501. A cutter groove 702 is formed at the tail of the cutter holder 701. A cutter 703 is arranged in the cutter groove 702. A through hole 704 vertically penetrating the cutter groove 702 is formed in the side wall at the tail of the cutter holder 701. The fixing rope 504 passes through the through hole 704. One end of a traction rope 705 is connected to the cutter 703, and the other end of the traction rope 705 is connected to a driving component 706. The driving component 706 is arranged on the inner side wall of the rear cover 9. The driving component 706 is connected to the controller. The driving component 706 pulls the cutter 703 to act, and can cut off the fixing rope 504. The compressed elastic element 602 ejects the ejection rod 501. Among them, the driving component 706 includes a driving motor 707 and a roller 708. The driving motor 707 is fixed on the inner side wall of the rear cover 9. A roller 708 is arranged at the output end of the driving motor 707. The traction rope 705 is fixedly wound on the surface of the roller 708. The driving motor 707 is connected to the controller. By controlling the driving motor 707 to rotate, the roller 708 is driven to rotate, and the traction rope 705 can be pulled.

[0054] Among them, a reinforcing plate 6 is arranged in the middle of the inner cavity of the housing 1. The central cylinder 2 penetrates through the reinforcing plate 6. Reinforcing holes 601 are formed around the reinforcing plate 6. The launching tube 3 penetrates through the corresponding reinforcing holes 601. The reinforcing plate 6 is used to further reinforce the central cylinder 2 and the launching tube 3.

[0055] The net part 4 includes a net body 401 and net ropes 402. The net body 401 is rectangular and net ropes 402 are arranged around it. One end of the net rope 402 away from the net body 401 is connected to the ejection rod 501. The net body 401 is loaded into the launching tube 3. A connecting hole 605 is formed at the top of the ejection rod 501. The net rope 402 passes through the connecting hole 605 and is fastened and fixed.

[0056] The working principle of an embodiment of the present utility model: The present utility model is provided with a central cylinder 2. During the loading and assembly, other devices can be loaded in the central cylinder 2, or other device parts can be assembled, or it can be used for wire routing, saving occupied space and facilitating simultaneous loading with other devices. When the present utility model is in use, it can be carried on devices such as unmanned aerial vehicles. During launch, the driving motor 707 is controlled to rotate, driving the roller 708 to rotate, which can pull the traction rope 705. The traction rope 705 pulls the cutter 703 to act, cutting off the fixing rope 504. The compressed elastic element 602 ejects the ejection rod 501. The ejection rod 501 carries the net body 401 through the net rope 402 and flies out of the launching tube 3, and unfolds in the air and pounces on the target to implement capture.

Claims

1. A drone capture device that is easy to carry equipment, characterized in that: include: Housing (1); A central tube (2), wherein the central tube (2) is disposed in the middle of the inner cavity of the shell (1); A launching tube (3), wherein four launching tubes (3) are provided, and the four launching tubes (3) are respectively provided along the side walls of the inner cavity of the shell (1), and the launching tubes (3) are arranged along the diagonal lines of the corresponding side walls of the shell (1), and the arrangement positions of the four launching tubes (3) are staggered with each other and the front ends are divergent, and the launching tubes (3) are tangent to the central tube (2); A net portion (4), the net portion (4) is loaded into the inner cavity of the launch tube (3) and is wound around the front end of the central tube (2); An ejection part (5), the ejection part (5) is installed in the launching tube (3), and the net part (4) is connected to the ejection part (5); a trigger part (7), the trigger part (7) is installed in the inner cavity of the shell (1), the trigger part (7) is connected to the tail end of the ejection part (5), and the trigger part (7) can control the ejection part (5) to be ejected.

2. The drone capture device that is easy to carry equipment according to claim 1 is characterized in that: The front and rear ends of the housing (1) are respectively provided with a front cover (8) and a rear cover (9).

3. The drone capture device that is easy to carry equipment according to claim 1 is characterized in that: The inner cavity of the shell (1) is provided with a positioning plate (11) and a limiting plate (10); the positioning plate (11) is arranged in front of the limiting plate (10); the tail end of the launching tube (3) passes through the positioning plate (11) and is placed on the surface of the limiting plate (10); the central tube (2) passes through the front cover (8), the positioning plate (11), the limiting plate (10) and the rear cover (9) in sequence.

4. The drone capture device that is easy to carry equipment according to claim 3 is characterized in that: The ejection part (5) comprises an ejection rod (501), the surface of which is sleeved with an elastic element (502), the ejection rod (501) sleeved with the elastic element (502) is inserted and installed in a corresponding launching tube (3), the tail end of the ejection rod (501) passes through a limiting plate (10), and a fixing hole (503) is provided at the tail end of the ejection rod (501), and a first-connected fixing rope (504) is sequentially passed through the fixing holes (503) of the ejection rods (501).

5. The drone capture device that is easy to carry equipment according to claim 4 is characterized in that: The trigger part (7) comprises a cutter frame (701), the cutter frame (701) is inserted into the inner cavity of the tail end of the ejection rod (501), the tail of the cutter frame (701) is provided with a cutter groove (702), a cutter (703) is arranged in the cutter groove (702), a through hole (704) vertically penetrating the cutter groove (702) is arranged on the side wall of the tail of the cutter frame (701), the fixing rope (504) passes through the through hole (704), the cutter (703) is connected to one end of a traction rope (705), the other end of the traction rope (705) is connected to a driving component (706), and the driving component (706) is arranged on the inner wall of the rear cover (9).

6. The drone capture device that is easy to carry equipment according to claim 5, characterized in that: The driving component (706) comprises a driving motor (707) and a roller (708); the driving motor (707) is fixed to the inner wall of the rear cover (9); the output end of the driving motor (707) is provided with a roller (708); a traction rope (705) is fixed to and wound around the surface of the roller (708).

7. The drone capture device that is easy to carry equipment according to claim 6, characterized in that: A reinforcement plate (6) is provided in the middle of the inner cavity of the shell (1), the central tube (2) passes through the reinforcement plate (6), reinforcement holes (601) are provided around the reinforcement plate (6), and the launching tube (3) passes through the corresponding reinforcement holes (601).

8. A drone capture device that is easy to carry equipment according to claim 1 or 7, characterized in that: The net part (4) comprises a net body (401) and a net rope (402); the net body (401) is rectangular and is surrounded by net ropes (402); one end of the net rope (402) away from the net body (401) is connected to a launching rod (501); and the net body (401) is loaded into a launching tube (3).

9. The drone capture device that is easy to carry equipment according to claim 8, characterized in that: A connection hole (505) is provided on the top of the ejection rod (501), and the net rope (402) passes through the connection hole (505) and is fastened and fixed.

10. The drone capture device that is easy to carry equipment according to claim 4, characterized in that: The length of the elastic element (502) is twice or more than the length of the ejection rod (501).

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