Unmanned aerial vehicle capturing device

Abstract

The utility model relates to an unmanned aerial vehicle capturing device which comprises a control assembly, the control assembly comprises a holding cylinder, a first partition plate and a release mechanism, the first partition plate is arranged in the holding cylinder, and the release mechanism is arranged on the first partition plate; the functional assembly comprises a high-pressure gas cylinder mounting cylinder, a locking cylinder, a high-pressure gas cylinder and a gas pipe mounting cylinder, the high-pressure gas cylinder is arranged on the inner side of the high-pressure gas cylinder mounting cylinder, one end of the high-pressure gas cylinder extends into the holding cylinder and is provided with the locking cylinder, the locking cylinder is connected with the clamping mechanism in an inserted mode, and the gas pipe mounting cylinder is connected with the high-pressure gas cylinder. A step base is arranged at the end, away from the holding cylinder, of the high-pressure gas cylinder mounting cylinder and connected with the gas pipe mounting cylinder in an inserted mode. Through cooperative use of the functional assembly and the control assembly, primary flight is achieved, then secondary throwing is achieved through the launching assembly, and the launching range of the net bag is greatly prolonged.

Description

Technical Field

[0001] This invention belongs to the field of capture devices, specifically a drone capture device. Background Technology

[0002] Drone capture devices primarily use high-voltage launchers to send out capture nets, which then wrap around the drone's propellers or fuselage, rendering it unable to fly and thus capturing the drone.

[0003] Existing capture devices simply throw out a capture net. The net opens instantly upon being thrown out, and the resulting resistance is extremely high, leading to a very limited range. Therefore, a drone capture device is proposed. Utility Model Content

[0004] The purpose of this section is to outline some aspects of embodiments of the present invention and to briefly describe some preferred embodiments. Simplifications or omissions may be made in this section, as well as in the abstract and title of this application, to avoid obscuring the purpose of these documents; however, such simplifications or omissions should not be construed as limiting the scope of the invention.

[0005] Given the following technical problems in the existing technology: the existing capture devices directly throw out the capture net, which opens instantly upon being thrown out, and the resistance after the net opens is extremely high, resulting in a very limited range.

[0006] To solve the above-mentioned technical problems, the present invention provides the following technical solution: a drone capture device, comprising,

[0007] A control component, comprising a gripping cylinder, a partition, and a release mechanism, wherein the gripping cylinder contains the partition and the partition is equipped with the release mechanism;

[0008] The functional component includes a high-pressure gas cylinder mounting cylinder, a locking cylinder, a high-pressure gas cylinder, and a gas pipe mounting cylinder. The high-pressure gas cylinder is provided inside the high-pressure gas cylinder mounting cylinder. One end of the high-pressure gas cylinder extends into the holding cylinder and is provided with a locking cylinder. The locking cylinder is inserted into the clamping mechanism. A stepped seat is provided at the end of the high-pressure gas cylinder mounting cylinder away from the holding cylinder. The stepped seat is inserted into the gas pipe mounting cylinder.

[0009] The launching assembly includes a second partition and a capturing assembly. The second partition is provided on the inner side of the air tube mounting cylinder, and the capturing assembly is provided on the second partition.

[0010] As a preferred technical solution for the drone capture device, the release mechanism includes a mounting base, a limiting frame, and a sealing arc plate. The upper side of the gripping cylinder has an installation port, and the sealing arc plate is inserted into the installation port. A limiting frame is provided on the sealing arc plate, and the limiting frame extends into the inner side of the gripping cylinder. The limiting frame is inserted into both the mounting base and the locking cylinder. The inner side of the mounting base has two vertical grooves, and the locking cylinder also has two vertical grooves. The vertical grooves correspond to and cooperate with each other. The limiting frame is U-shaped, and the two sides of the limiting frame extend into the two vertical grooves and the two vertical grooves respectively.

[0011] The limit bracket is locked in the two vertical grooves 1 and 2, so that the locking cylinder and the mounting base are locked together.

[0012] As a preferred technical solution for the drone capture device, the control component includes a valve core, which is movably inserted into a locking cylinder, and the middle part of the mounting base is fixedly connected to the valve core.

[0013] High-pressure gas can be pumped into the high-pressure gas cylinder through the valve core.

[0014] As a preferred technical solution for the drone capture device, one end of the air tube mounting cylinder is recessed with a receiving cavity one, and the other end of the air tube mounting cylinder is recessed with a receiving cavity two. The receiving cavity one and the receiving cavity two are separated by a partition two, and one end of the receiving cavity two is trumpet-shaped.

[0015] The trumpet shape can accommodate a net.

[0016] As a preferred technical solution for the drone capture device, the launching assembly also includes an air guide tube and a counterweight. Several air guide tubes are evenly arranged on the side of the partition plate facing the receiving cavity. Several through holes are recessed on the partition plate, and each through hole corresponds to one of the air guide tubes. The through holes are connected to the air guide tubes. The air guide tubes extend into the inside of the receiving cavity. A counterweight is movably inserted into the end of the air guide tube away from the partition plate. The counterweight is connected to the edge of the net.

[0017] The heavy hammer can carry the net as it flies.

[0018] As a preferred technical solution for the drone capture device, a gas generator is provided on the side of the partition facing the receiving cavity, and the gas generator is model DTN60F.

[0019] The beneficial effects of the drone capture device of the present invention are: by using the functional components and control components in combination, a single flight is achieved, followed by a secondary deployment via the launching component, which greatly extends the range of the net. Attached Figure Description

[0020] To more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings used in the description of the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present invention. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort. Wherein:

[0021] Figure 1 This is a schematic diagram of the overall structure of the present invention;

[0022] Figure 2 This is a top-view cross-sectional structural diagram of the present invention;

[0023] Figure 3 This is a schematic diagram of the rear structure of the present invention.

[0024] Reference numerals: 100, Control component; 101, Holding cylinder; 102, Partition 1; 103, Mounting base; 104, Limiting bracket; 105, Valve core; 106, Sealing arc plate; 200, Functional component; 201, High-pressure gas cylinder mounting cylinder; 202, Locking cylinder; 203, High-pressure gas cylinder; 204, Gas pipe mounting cylinder; 300, Launching component; 301, Partition 2; 302, Gas generator; 303, Gas guide pipe; 304, Receiving cavity 1; 305, Receiving cavity 2; 306, Counterweight. Detailed Implementation

[0025] To make the above-mentioned objects, features and advantages of the present invention more apparent and understandable, the specific embodiments of the present invention will be described in detail below with reference to the accompanying drawings.

[0026] Many specific details are set forth in the following description in order to provide a full understanding of the invention. However, the invention may also be practiced in other ways different from those described herein, and those skilled in the art can make similar extensions without departing from the spirit of the invention. Therefore, the invention is not limited to the specific embodiments disclosed below.

[0027] Secondly, the term "one embodiment" or "embodiment" as used herein refers to a specific feature, structure, or characteristic that may be included in at least one implementation of the present invention. The phrase "in one embodiment" appearing in different places in this specification does not necessarily refer to the same embodiment, nor is it a single or selective embodiment that is mutually exclusive with other embodiments.

[0028] Secondly, the present invention is described in detail with reference to the schematic diagrams. When detailing the embodiments of the present invention, for ease of explanation, the cross-sectional views illustrating the device structure may be partially enlarged, not according to the usual scale. Furthermore, the schematic diagrams are merely examples and should not limit the scope of protection of the present invention. In addition, actual fabrication should include three-dimensional spatial dimensions of length, width, and depth.

[0029] like Figures 1-3 As shown, the present invention proposes a drone capture device, comprising,

[0030] The control component 100 includes a gripping cylinder 101, a partition 102, and a release mechanism. The gripping cylinder 101 is provided with the partition 102, and the partition 102 is equipped with the release mechanism.

[0031] Functional component 200 includes a high-pressure gas cylinder mounting cylinder 201, a locking cylinder 202, a high-pressure gas cylinder 203, and a gas tube mounting cylinder 204. The high-pressure gas cylinder 203 is disposed inside the high-pressure gas cylinder mounting cylinder 201. One end of the high-pressure gas cylinder 203 extends into the holding cylinder 101 and is provided with the locking cylinder 202. The locking cylinder 202 is inserted into the clamping mechanism. A stepped seat is provided at the end of the high-pressure gas cylinder mounting cylinder 201 away from the holding cylinder 101. The stepped seat is inserted into the gas tube mounting cylinder 204.

[0032] The launching assembly 300 includes a second partition 301 and a capture assembly. The second partition 301 is provided on the inner side of the air tube mounting cylinder 204, and the capture assembly is provided on the second partition 301.

[0033] The release mechanism includes a mounting base 103, a limiting frame 104, and a sealing arc plate 106. The upper side of the gripping cylinder 101 has an installation port, and the sealing arc plate 106 is inserted into the installation port. The limiting frame 104 is provided on the sealing arc plate 106 and extends into the inner side of the gripping cylinder 101. The limiting frame 104 is inserted into both the mounting base 103 and the locking cylinder 202. The inner side of the mounting base 103 has two vertical grooves, and the locking cylinder 202 also has two vertical grooves. The vertical grooves 1 and 2 are correspondingly matched. The limiting frame 104 is U-shaped, and its two sides extend into the two vertical grooves 1 and 2 respectively.

[0034] The limit bracket 104 is locked in the two vertical grooves 1 and 2, so that the locking cylinder 202 and the mounting base 103 are locked together.

[0035] The control component 100 includes a valve core 105, which is movably inserted into the locking cylinder 202, and the middle part of the mounting base 103 is fixedly connected to the valve core 105.

[0036] High-pressure gas can be pumped into the high-pressure gas cylinder 203 through the valve core 105.

[0037] One end of the tracheal tube mounting cylinder 204 is recessed with a receiving cavity 304, and the other end of the tracheal tube mounting cylinder 204 is recessed with a receiving cavity 305. The receiving cavity 304 and the receiving cavity 305 are separated by a partition 301. One end of the receiving cavity 305 is funnel-shaped.

[0038] The trumpet shape can accommodate a net.

[0039] The launching assembly 300 also includes an air guide tube 303 and a counterweight 306. Several air guide tubes 303 are evenly arranged on the side of the partition 2 301 facing the receiving cavity 2 305. Several through holes are recessed on the partition 2 301. Each through hole corresponds to one of the air guide tubes 303 and is connected to the corresponding air guide tube 303. The air guide tube 303 extends into the inside of the receiving cavity 2 305. The end of the air guide tube 303 away from the partition 2 301 is movably connected to the counterweight 306. The counterweight 306 is connected to the edge of the net.

[0040] The Heavy Hammer 306 can fly while carrying a net.

[0041] A gas generator 302 is provided on the side of the partition 2 301 facing the receiving cavity 1 304. The gas generator 302 is model DTN60F.

[0042] The cavity 304 is equipped with a time relay module control switch and a microcontroller. The time relay module control switch and the gas generator 302 are electrically connected to the microcontroller.

[0043] The time relay module control switch can control the gas generator 302 to work via a microcontroller.

[0044] A one-way valve is provided inside the valve core 105. Gas can be added to the high-pressure gas cylinder 203 through the valve core 105.

[0045] The time relay module control switch model is GRT8-A.

[0046] The specific implementation method is as follows: When in use, hold the gripping cylinder 101, then hook the limiting frame 104, pull the limiting frame 104 to disengage from the locking cylinder 202 and the mounting base 103, thereby releasing the constraint on the locking cylinder 202, the high pressure gas pressure in the high pressure cylinder 203 is unrestrained, the gas is released from the locking cylinder 202, the gas pushes the high pressure cylinder 203 to separate from the gripping cylinder 101, so that the functional component 200 flies out as a whole, and the net flies out with the functional component 200 at the same time;

[0047] The gas generator 302 inside the functional component 200 then generates a large amount of gas. Part of the gas enters the air duct 303, pushing the hammer 306 to detach from the air duct 303 and fly out. The hammer 306, carrying the net, flies to the target space a second time.

[0048] It should be understood that numerous specific implementation decisions can be made during the development of any practical implementation, such as in any engineering or design project. Such development efforts may be complex and time-consuming, but for those skilled in the art who benefit from this disclosure, the development effort will be a routine work of design, manufacturing, and production without requiring much experimentation.

[0049] It should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention and are not intended to limit it. Although the present invention has been described in detail with reference to preferred embodiments, those skilled in the art should understand that modifications or equivalent substitutions can be made to the technical solutions of the present invention without departing from the spirit and scope of the technical solutions of the present invention, and all such modifications or substitutions should be covered within the scope of the claims of the present invention.

Claims

1. A drone capture device, characterized in that: include, The control assembly (100) includes a gripping cylinder (101), a partition (102) is provided inside the gripping cylinder (101), and a release mechanism is installed in the partition (102); Functional component (200) includes a high-pressure gas cylinder mounting cylinder (201), a high-pressure gas cylinder (203) is provided inside the high-pressure gas cylinder mounting cylinder (201), one end of the high-pressure gas cylinder (203) extends into the holding cylinder (101) and is provided with a locking cylinder (202), the locking cylinder (202) is inserted into the clamping mechanism, and the end of the high-pressure gas cylinder mounting cylinder (201) away from the holding cylinder (101) is inserted into the air pipe mounting cylinder (204); The launching assembly (300) includes a second partition (301) and a capture assembly. The second partition (301) is provided on the inner side of the tracheal mounting tube (204), and the capture assembly is provided on the second partition (301).

2. The drone capture device according to claim 1, characterized in that: The release mechanism includes a mounting base (103), a limiting frame (104), and a sealing arc plate (106). The upper side of the gripping cylinder (101) is provided with an installation port. The sealing arc plate (106) is inserted into the installation port. The limiting frame (104) is provided on the sealing arc plate (106). The limiting frame (104) extends into the inner side of the gripping cylinder (101). The limiting frame (104) is inserted into both the mounting base (103) and the locking cylinder (202).

3. The drone capture device according to claim 2, characterized in that: The control assembly (100) includes a valve core (105) which is movably inserted into a locking cylinder (202), and the middle part of the mounting base (103) is fixedly connected to the valve core (105).

4. The drone capture device according to claim 3, characterized in that: One end of the tracheal tube mounting cylinder (204) is recessed with a second receiving cavity (305), and the other end of the tracheal tube mounting cylinder (204) is recessed with a first receiving cavity (304). The first receiving cavity (304) and the second receiving cavity (305) are separated by a second partition (301). One end of the second receiving cavity (305) is trumpet-shaped.

5. The drone capture device according to claim 4, characterized in that: The launching assembly (300) also includes an air guide tube (303) and a counterweight (306). Several air guide tubes (303) are evenly arranged on the side of the partition plate (301) facing the receiving cavity (305). Several through holes are recessed on the partition plate (301). The through holes correspond one-to-one with the air guide tubes (303). The through holes are connected to the air guide tubes (303). The air guide tubes (303) extend into the inner side of the receiving cavity (305). The counterweight (306) is movably inserted into the end of the air guide tube (303) away from the partition plate (301).

6. The drone capture device according to claim 5, characterized in that: A gas generator (302) is provided on the side of the partition 2 (301) facing the receiving cavity 1 (304).

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