Flight capture device

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a flying arresting device which comprises an unmanned aerial vehicle body, a connecting base and a camera shooting frame are fixedly connected to the bottom of the unmanned aerial vehicle body, a camera is installed on the inner side of the camera shooting frame, and an arresting frame is fixedly connected to the bottom of the connecting base. An adjusting motor is installed on one side of the capturing frame, a capturing gun body is fixedly connected to the driving end of the adjusting motor, a capturing gun head is fixedly connected to one end of the capturing gun body, a launching tube is fixedly connected to the interior of the capturing gun head, a launching head is installed in the launching tube, and an electromagnetic valve is fixedly connected to one end of the launching tube; a gas tank is installed in the capturing gun body, one end of the gas tank is fixedly connected with a gas pipe, and through the arrangement of the adjusting motor, the launching pipe and the gas tank, the flying capturing device can conduct capturing tasks within a certain distance range, the situation that a target is disturbed in the capturing process is avoided, and therefore the capturing accuracy is improved.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, specifically a flight capture device. Background Technology

[0002] In recent years, drone technology has developed rapidly, with flight control, navigation, and battery technologies becoming increasingly mature and sophisticated. Drones can achieve stable flight, precise positioning, and flexible control, providing a reliable flight platform for aerial capture devices.

[0003] Existing patent document CN115180153A discloses a flying capture device, capture method, and rescue method. The flying capture device includes an aircraft, a capture device, and a camera device. A controller controls a first drive component to rotate a propeller, enabling the aircraft to fly and thus driving the capture device and camera device. Simultaneously, the camera device searches for the capture target and feeds relevant information back to the controller. The controller adjusts the flight path based on the feedback information. When the camera device locates the capture target and feeds back to the controller, the aircraft flies towards the target's location and captures or rescues the target using a capture net. This device can fly in the air, no longer limited by traditional land transportation environments. Capture targets include suspects, vehicles, or animals such as cattle and sheep on land, birds or unidentified flying objects in the air, or rescued individuals, meeting capture or rescue needs in multiple fields.

[0004] However, existing flight capture devices, while capable of capturing targets, require the drone to be very close to the target to complete the capture mission. Due to the difficulty in launching the capture net and the ease with which the target can be disturbed during the capture process, the accuracy of the capture is affected. To address this issue, we propose a flight capture device. Utility Model Content

[0005] (a) Technical problems to be solved

[0006] In view of the shortcomings of the prior art, the present invention provides a flight capture device to solve the problems mentioned in the background art.

[0007] (II) Technical Solution

[0008] To achieve the above objectives, this utility model provides the following technical solution: a flying capture device, comprising a drone body, a connecting base and a camera frame fixedly connected to the bottom of the drone body, a camera mounted on the inner side of the camera frame, a capture frame fixedly connected to the bottom of the connecting base, an adjustment motor mounted on one side of the capture frame, a capture gun body fixedly connected to the drive end of the adjustment motor, a capture gun head fixedly connected to one end of the capture gun body, a launch tube fixedly connected inside the capture gun head, a launch head mounted inside the launch tube, a solenoid valve fixedly connected to one end of the launch tube, an air tank mounted inside the capture gun body, and an air pipe fixedly connected to one end of the air tank.

[0009] Preferably, connecting brackets are fixedly connected to both sides of the main body of the drone, a movable shaft is movably connected through the top of the connecting bracket, and an adjusting arm is movably connected through the movable shaft to the inner side of the connecting bracket.

[0010] Preferably, a rotary motor is fixedly connected to one end of the adjusting arm, the drive end of the rotary motor is fixedly connected to an wing frame, and an wing blade is fixedly connected to the outer side of the wing frame.

[0011] Preferably, one end of the capture gun head has a net opening, and a capture net is installed inside the net opening, and the capture net is fixedly connected to the launch head.

[0012] Preferably, the other end of the capture gun body is threaded with a fixing cover, which is made of metal.

[0013] Preferably, the bottom of both the connecting seat and the adjusting arm are fixedly connected to support legs, and four support legs are provided, which are arranged symmetrically in pairs.

[0014] (III) Beneficial Effects

[0015] This utility model provides a flying capture device, which has the following beneficial effects:

[0016] (1) This type of flying capture device, through the setting of an adjustment motor, a launch tube and an air tank, uses a camera to capture images when using the flying capture device to search for the capture target. After the target is found, the adjustment motor drives the capture gun body to adjust the angle so that the capture gun head is aligned with the capture target. Then the solenoid valve opens, and the gas in the air tank enters the launch tube. At the same time, the gas pushes the launch head, and the launch head drives the capture net to be launched, so that the capture net can capture the target. This allows the flying capture device to carry out the capture task within a certain distance range, avoiding disturbing the target during the capture process, thus improving the capture accuracy. Attached Figure Description

[0017] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0018] Figure 2 This is a partial structural schematic diagram of the adjusting arm of this utility model;

[0019] Figure 3 This is a partial structural schematic diagram of the main body of the UAV of this utility model;

[0020] Figure 4 This is a cross-sectional view of the capture gun head of this utility model.

[0021] In the diagram: 1. Drone body; 2. Connecting bracket; 3. Movable shaft; 4. Adjustable arm; 5. Rotary motor; 6. Wing frame; 7. Wing blades; 8. Connecting seat; 9. Support leg; 10. Camera mount; 11. Camera; 12. Capture frame; 13. Adjustable motor; 14. Capture gun body; 15. Capture gun head; 16. Launch tube; 17. Net opening; 18. Launch head; 19. Capture net; 20. Fixing cover; 21. Air tank; 22. Air pipe; 23. Solenoid valve. Detailed Implementation

[0022] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments of the present utility model. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. All other embodiments obtained by those skilled in the art based on the embodiments of the present utility model without creative effort are within the protection scope of the present utility model.

[0023] Please see Figure 1-4 This utility model provides a technical solution: a flying capture device, including a drone body 1, a connecting seat 8 and a camera frame 10 fixedly connected to the bottom of the drone body 1, a camera 11 installed on the inner side of the camera frame 10, a capture frame 12 fixedly connected to the bottom of the connecting seat 8, an adjustment motor 13 installed on one side of the capture frame 12, a capture gun body 14 fixedly connected to the drive end of the adjustment motor 13, a capture gun head 15 fixedly connected to one end of the capture gun body 14, a launch tube 16 fixedly connected inside the capture gun head 15, a launch head 18 installed inside the launch tube 16, a solenoid valve 23 fixedly connected to one end of the launch tube 16, an air tank 21 installed inside the capture gun body 14, and an air pipe 22 fixedly connected to one end of the air tank 21.

[0024] Furthermore, connecting brackets 2 are fixedly connected to both sides of the drone body 1, and a movable shaft 3 is movably connected through the top of the connecting brackets 2. An adjusting arm 4 is movably connected to the inner side of the connecting brackets 2 through the movable shaft 3. The adjusting arm 4 can be folded and adjusted through the connecting brackets 2 and the movable shaft 3, making it convenient for personnel to store the drone.

[0025] Furthermore, a rotary motor 5 is fixedly connected to one end of the adjusting arm 4, and a wing frame 6 is fixedly connected to the drive end of the rotary motor 5. A wing blade 7 is fixedly connected to the outer side of the wing frame 6. By starting the rotary motor 5, the rotary motor 5 drives the wing blade 7 to rotate at high speed through the wing frame 6, at which point the main body of the UAV 1 can take off.

[0026] Furthermore, a net opening 17 is provided at one end of the capture gun head 15, and a capture net 19 is installed inside the net opening 17. The capture net 19 is fixedly connected to the launch head 18, and the net opening 17 facilitates the installation of the capture net 19 for capture missions.

[0027] Furthermore, the other end of the capture gun body 14 is threaded with a fixing cover 20, which is made of metal. The fixing cover 20 can compress the gas canister 21, thereby firmly fixing the position of the gas canister 21.

[0028] Furthermore, the bottom of both the connecting seat 8 and the adjusting arm 4 are fixedly connected to support legs 9. There are four support legs 9, which are arranged symmetrically in pairs. The support legs 9 enable the drone to be placed stably on the ground.

[0029] Working Principle: After installation, first check the installation, fixation, and safety protection of this utility model. When using the flight capture device, the operator starts the rotary motor 5. The rotary motor 5 drives the wing blades 7 to rotate at high speed through the wing frame 6. At this time, the main body 1 of the drone can take off. Then, the camera 11 captures the scene to search for the capture target. After the target is found, the adjustment motor 13 drives the capture gun body 14 to adjust the angle so that the capture gun head 15 is aligned with the capture target. Then, the solenoid valve 23 opens, and the gas in the gas tank 21 enters the launch tube 16. At the same time, the gas pushes the launch head 18, which drives the capture net 19 to be launched, so that the capture net 19 can capture the target. This completes the use of this utility model. This utility model has a simple structure and is safe and convenient to use.

[0030] The above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present utility model should be included within the protection scope of the present utility model.

Claims

1. A flight capture device, comprising a drone body (1), characterized in that: The bottom of the main body (1) of the drone is fixedly connected to a connecting seat (8) and a camera frame (10). A camera (11) is installed on the inner side of the camera frame (10). A capture frame (12) is fixedly connected to the bottom of the connecting seat (8). An adjustment motor (13) is installed on one side of the capture frame (12). A capture gun body (14) is fixedly connected to the drive end of the adjustment motor (13). A capture gun head (15) is fixedly connected to one end of the capture gun body (14). A launch tube (16) is fixedly connected inside the capture gun head (15). A launch head (18) is installed inside the launch tube (16). A solenoid valve (23) is fixedly connected to one end of the launch tube (16). An air tank (21) is installed inside the capture gun body (14). An air pipe (22) is fixedly connected to one end of the air tank (21).

2. The flying capture device according to claim 1, characterized in that: The two sides of the main body (1) of the drone are fixedly connected to the connecting brackets (2), the top of the connecting brackets (2) is movably connected to the movable shaft (3), and the inner side of the connecting brackets (2) is movably connected to the movable shaft (3) with the adjusting arm (4).

3. The flying capture device according to claim 2, characterized in that: One end of the adjusting arm (4) is fixedly connected to a rotary motor (5), the drive end of the rotary motor (5) is fixedly connected to an wing frame (6), and the outer side of the wing frame (6) is fixedly connected to an wing blade (7).

4. The flying capture device according to claim 1, characterized in that: The capture gun head (15) has a net opening (17) at one end, and a capture net (19) is installed inside the net opening (17). The capture net (19) is fixedly connected to the launch head (18).

5. The flying capture device according to claim 1, characterized in that: The other end of the capture gun body (14) is threaded with a fixing cover (20), which is made of metal.

6. The flying capture device according to claim 1, characterized in that: The bottom of the connecting seat (8) and the adjusting arm (4) are both fixedly connected to support legs (9). There are four support legs (9), and the four support legs (9) are arranged symmetrically in pairs.

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