Unmanned aerial vehicle with black flight capturing function

Abstract

The utility model is applicable to the technical field of unmanned aerial vehicles, and provides an unmanned aerial vehicle with a black fly capturing function, which comprises a fuselage, a camera is arranged in the middle of the front surface of the fuselage, a baffle is fixedly connected to the front surface of the fuselage and above the camera, and connecting arms are fixedly connected to four rectangular corners of two side surfaces of the fuselage. Driving boxes are fixedly connected to the outer ends of the multiple connecting arms, propellers are rotatably arranged at the top ends of the multiple driving boxes, and storage assemblies are arranged at the four rectangular corners of the bottom face of the fuselage. According to the unmanned aerial vehicle with the black flight capturing function, by arranging the storage assembly, the unmanned aerial vehicle is enabled to locally release the capturing net to capture a target, and a plurality of capturing nets can be stored at the same time, so that the capturing efficiency is improved, the capturing number is increased, and not only can most black flight unmanned aerial vehicles be captured, but also the capturing efficiency is improved. And the situation that the masses are accidentally injured can be prevented, the value is high, accidental injury is low, protection is high, and the working environment is not selected.

Description

Technical Field

[0001] The utility model belongs to the technical field of unmanned aerial vehicles, and in particular relates to a unmanned aerial vehicle with a function of catching black flies. Background Art

[0002] Drones are a general term for unmanned aerial vehicles, which are equipped with flight controllers, GPS and other equipment, and can be tracked and located by ground stations or pilots. Compared with manned aircraft, drones have the advantages of small size, low cost, and ease of use. They can be taken off and recovered under radio remote control and can be used repeatedly.

[0003] For example, a drone disclosed in Chinese patent CN214930615U can be used portable in daily life or various tasks. However, drones owned by individuals will inevitably affect the safety of urban public facilities and places and the safety and privacy of residential areas, and may even become a tool for terrorists to carry out terrorist attacks. In addition, the defense of "low, slow and small" aircraft in airports or urban environments has low value, high accidental injuries, weak protection, uncertain time and complex background images, which may even cause accidental injuries. Utility Model Content

[0004] The utility model provides a drone with a black-flying capture function, aiming to solve the problem that drones owned by individuals inevitably affect the safety of urban public facilities and places and the safety and privacy of residential areas, and even become tools used by terrorists to carry out terrorist attacks, and in the airport or urban environment, the defense of "low, slow and small" aircraft has low value, high accidental injury, weak protection, uncertain time and complex background images, and may even cause accidental injury.

[0005] The utility model is implemented as follows: a drone with a function of catching black flies comprises a fuselage, a camera is arranged in the middle of the front surface of the fuselage, a baffle is fixedly connected to the front surface of the fuselage and located above the camera, connecting arms are fixedly connected to the four corners of the two side surfaces of the fuselage in a rectangular shape, a plurality of the outer ends of the connecting arms are fixedly connected to drive boxes, a plurality of the top ends of the drive boxes are rotatably provided with propellers, a plurality of the bottom ends of the inner walls of the drive boxes are fixedly connected to motors, a plurality of the top ends of the motors are fixedly connected to connecting rods, a plurality of the top ends of the connecting rods are respectively fixedly connected to a plurality of propellers, and storage components are arranged at the four corners of the rectangular bottom surface of the fuselage.

[0006] Preferably, the storage assembly includes a mounting base, a storage box, a plurality of counterweights, a plurality of capture nets and two magnetic blocks. The mounting base is detachably mounted on a corner of the bottom surface of the fuselage, the storage box is fixedly connected to the bottom surface of the mounting base, a plurality of counterweights are arranged in the inner cavity of the storage box, a plurality of capture nets are respectively fixedly connected at one corner to the plurality of counterweights, and the two magnetic blocks are respectively arranged at the bottom ends of both sides of the inner wall of the storage box.

[0007] Preferably, a groove is provided on one side of the inner wall of the storage box, a plurality of spring rods are fixedly connected to one side of the inner wall of the groove, abutment plates are fixedly connected to the inner ends of the plurality of spring rods, a through hole is provided on one side of the inner wall of the storage box and is located opposite to the groove, a telescopic rod is fixedly connected to the bottom end of the inner wall of the through hole, and a top plate is fixedly connected to the inner end of the telescopic rod.

[0008] Preferably, a power supply box is fixedly connected to the surface of the storage box and located outside the through hole, and a battery is fixedly connected to the bottom end of the inner wall of the power supply box.

[0009] Preferably, a rotating block is rotatably connected to one side of the bottom end of the storage box, and a cover plate is fixedly connected to the top end of the rotating block.

[0010] Preferably, support legs are fixedly connected at the four corners of the lower surface of the fuselage and located on the outsides of the plurality of storage assemblies, and support seats are fixedly connected at the bottom ends of the plurality of support legs.

[0011] Beneficial Effects

[0012] Compared with the prior art, the beneficial effects of the utility model are as follows: the utility model is a drone with the function of catching illegal flying drones. By providing a storage component, the drone can locally drop a capture net to capture the target, and can store multiple capture nets at the same time, thereby improving the capture efficiency and increasing the number of captures. It can not only capture most illegal flying drones, but also prevent accidental injuries to the public. When the drone with the function of catching illegal flying drones is used for work, it has high value, low accidental injuries, strong protection, and is not picky about the working environment. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 This is a front view structural schematic diagram of the utility model;

[0014] Figure 2 For the utility model Figure 1 A schematic diagram of a local enlarged structure of A;

[0015] Figure 3 For the utility model Figure 1 A schematic diagram of a partially enlarged structure of B;

[0016] In the figure: 1-fuselage, 2-camera, 3-baffle, 4-connecting arm, 5-drive box, 6-propeller, 7-motor, 8-connecting rod, 9-mounting seat, 10-storage box, 11-counterweight, 12-capture net, 13-magnetic block, 14-resistance plate, 15-telescopic rod, 16-top plate, 17-power supply box, 18-battery, 19-rotating block, 20-cover plate, 21-support leg, 22-support seat. DETAILED DESCRIPTION

[0017] In order to make the purpose, technical solution and advantages of the utility model more clear, the utility model is further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the utility model and are not used to limit the utility model.

[0018] See also Figure 1-3 The utility model provides a technical solution: it includes a fuselage 1, a camera 2 is arranged in the middle of the front surface of the fuselage 1, a baffle 3 is fixedly connected to the front surface of the fuselage 1 and located above the camera 2, connecting arms 4 are fixedly connected at the four corners of the two side surfaces of the fuselage 1, and the outer ends of multiple connecting arms 4 are fixedly connected to drive boxes 5, and propellers 6 are rotatably arranged on the tops of multiple drive boxes 5. Motors 7 are fixedly connected to the bottom ends of the inner walls of the multiple drive boxes 5, and connecting rods 8 are fixedly connected to the tops of the multiple motors 7. The tops of the multiple connecting rods 8 are respectively fixedly connected to the multiple propellers 6, and storage components are arranged at the four corners of the bottom surface of the fuselage 1 in a rectangle.

[0019] In this embodiment, the detected illegal flying drone can be flown above it, and the four storage components are operated in the same way at the same time, the bottom cover 20 is rotated to open, and the two magnetic blocks 13 are powered off to lose their magnetic force, causing the sucked counterweight block to lose its suction and fall, thereby capturing the illegal flying drone below, and the cover 20 is closed, the telescopic rod 15 is retracted, and the multiple spring rods are rebounded, and the stored counterweight block 11 is unembedded through the abutment plate 13, so that it falls, and at this time the two magnetic blocks 13 are powered on again to restore the magnetic force, and the other counterweight block 11 falls, and the cycle is repeated.

[0020] By providing a storage component, the drone can locally release a capture net to capture the target, and can store multiple capture nets 12 at the same time, so that the capture efficiency is improved and the number of captures is increased. Not only can most illegal flying drones be captured, but also accidental injuries to the public can be prevented. When the drone with the illegal flying capture function is used, it is of high value, low accidental injury, strong protection, and is not picky about the working environment.

[0021] Furthermore, the storage assembly includes a mounting seat 9, a storage box 10, a plurality of counterweights 11, a plurality of capture nets 12 and two magnetic blocks 13. The mounting seat 9 is detachably mounted on a corner of the bottom surface of the fuselage 1, the storage box 10 is fixedly connected to the bottom surface of the mounting seat 9, a plurality of counterweights 11 are arranged in the inner cavity of the storage box 10, a corner of the plurality of capture nets 12 are respectively fixedly connected to the plurality of counterweights 11, and the two magnetic blocks 13 are respectively arranged at the bottom ends of both sides of the inner wall of the storage box 10.

[0022] In this embodiment, vertical grooves are vertically opened on the inner end surfaces of multiple storage boxes 10, and multiple counterweights 11 are respectively connected to a corner of the capture net 12 through multiple vertical grooves, and counterweights 11 are connected to the four corners of the capture net 12 to form a complete capture net 12, and are all stored in multiple storage components to wait for launch or storage. The counterweight 11 itself is not made of iron material, but an iron material is arranged at the outer end of the counterweight 11, and the two magnetic blocks 13 can control their magnetic force by powering on or off.

[0023] Furthermore, a groove is provided on one side of the inner wall of the storage box 10, and a plurality of spring rods are fixedly connected to one side of the inner wall of the groove. A support plate 14 is fixedly connected to the inner ends of the plurality of spring rods. A through hole is provided on one side of the inner wall of the storage box 10 and is located opposite to the groove. A telescopic rod 15 is fixedly connected to the bottom end of the inner wall of the through hole, and a top plate 16 is fixedly connected to the inner end of the telescopic rod 15.

[0024] In this embodiment, after the counterweight 11 at the lowest end of the storage box 10 is launched, the telescopic rod 15 extends, causing the top plate 16 to push one end of the counterweight 11 into the groove, causing it to push against the plate 14 to shrink, causing the spring rod to generate elastic force. When the cover 20 is closed and the capture net 12 needs to be supplemented to the bottom, the telescopic rod 15 will retract, causing the top plate 16 to stop pushing, and causing multiple spring rods to rebound, causing the counterweight 11 to retreat out of the groove and fall down. The counterweights 11 above will also fall down in turn, and the top plate 16 will again push the corresponding counterweight 11 into the groove to prevent it from falling down during launch.

[0025] Furthermore, a power supply box 17 is fixedly connected to the surface of the storage box 10 and outside the through hole, and a battery 18 is fixedly connected to the bottom end of the inner wall of the power supply box 17 .

[0026] Furthermore, a rotating block 19 is rotatably connected to one side of the bottom end of the storage box 10 , and a cover plate 20 is fixedly connected to the top end of the rotating block 19 .

[0027] In this embodiment, when the capture net 12 is to be launched, the rotating block 19 is first rotated to drive the cover 20 to open, so that the counterweight block 11 at the lowest end of the storage box 10 falls down, and the cover 20 acts as a safety lock. When the cover 20 is closed, it can serve as a support for the next capture net 12 to be launched.

[0028] Furthermore, support legs 21 are fixedly connected at the four corners of the lower surface of the fuselage 1 and located outside the multiple storage components, and the bottom ends of the multiple support legs 21 are fixedly connected to support bases 22.

[0029] The working principle and use process of the utility model: After the utility model is installed, the unmanned aerial vehicle (UAV) detected can be flown above it, and the four storage components are operated in the same way at the same time, the bottom cover 20 is rotated to open, and the two magnetic blocks 13 are powered off to lose their magnetic force, causing the sucked counterweight block to lose its suction and fall, thereby capturing the unmanned aerial vehicle below, and the cover 20 is closed, the telescopic rod 15 is retracted, and the multiple spring rods are rebounded, and the stored counterweight block 11 is unembedded through the abutment plate 13, so that it falls, and at this time the two magnetic blocks 13 are powered on again to restore the magnetic force, and the other counterweight block 11 falls, and the cycle is repeated.

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

Claims

1. A drone with a function of catching illegal flying objects, comprising a fuselage (1), characterized in that: A camera (2) is arranged in the middle of the front surface of the fuselage (1); a baffle (3) is fixedly connected to the front surface of the fuselage (1) and located above the camera (2); connecting arms (4) are fixedly connected at the four corners of the rectangular surfaces on both sides of the fuselage (1); the outer ends of the connecting arms (4) are fixedly connected to drive boxes (5); the tops of the drive boxes (5) are rotatably provided with propellers (6); the bottom ends of the inner walls of the drive boxes (5) are fixedly connected to motors (7); the tops of the motors (7) are fixedly connected to connecting rods (8); the tops of the connecting rods (8) are respectively fixedly connected to the propellers (6); and storage components are arranged at the four corners of the rectangular bottom surface of the fuselage (1); The storage assembly comprises a mounting seat (9), a storage box (10), a plurality of counterweights (11), a plurality of capture nets (12) and two magnetic blocks (13); the mounting seat (9) is detachably mounted on a corner of the bottom surface of the body (1); the storage box (10) is fixedly connected to the bottom surface of the mounting seat (9); the plurality of counterweights (11) are arranged in the inner cavity of the storage box (10); a corner of the plurality of capture nets (12) is respectively fixedly connected to the plurality of counterweights (11); and the two magnetic blocks (13) are respectively arranged at the bottom ends of both sides of the inner wall of the storage box (10).

2. The unmanned aerial vehicle with the function of catching illegal flying objects as claimed in claim 1, characterized in that: A groove is provided on one side of the inner wall of the storage box (10), a plurality of spring rods are fixedly connected to one side of the inner wall of the groove, abutment plates (14) are fixedly connected to the inner ends of the plurality of spring rods, a through hole is provided on one side of the inner wall of the storage box (10) and is located opposite to the groove, a telescopic rod (15) is fixedly connected to the bottom end of the inner wall of the through hole, and a top plate (16) is fixedly connected to the inner end of the telescopic rod (15).

3. The unmanned aerial vehicle with the function of catching illegal flying objects as claimed in claim 2, characterized in that: A power supply box (17) is fixedly connected to the surface of the storage box (10) and located outside the through hole, and a storage battery (18) is fixedly connected to the bottom end of the inner wall of the power supply box (17).

4. The unmanned aerial vehicle with the function of catching illegal flying objects as claimed in claim 1, characterized in that: A rotating block (19) is rotatably connected to one side of the bottom end of the storage box (10), and a cover plate (20) is fixedly connected to the top end of the rotating block (19).

5. The unmanned aerial vehicle with the function of catching illegal flying objects as claimed in claim 1, characterized in that: Support legs (21) are fixedly connected at the four corners of the lower surface of the body (1) and located outside the plurality of storage components, and support seats (22) are fixedly connected at the bottom ends of the plurality of support legs (21).

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