An artificial intelligence unmanned aerial vehicle city management target identification and alarm pushing device

Abstract

The application discloses an artificial intelligence unmanned aerial vehicle city management target identification and alarm pushing device, which comprises a body, a control panel is fixedly arranged in the body, a horizontal rod is fixedly connected to the outer surface of the body, a rotor is rotatably arranged at the end of the horizontal rod, a hinged seat is arranged at the bottom of the horizontal rod, a supporting leg is hingedly arranged at one end of the hinged seat, a return spring is fixedly connected to one side of the supporting leg, an installation cylinder is fixedly connected to the upper surface of the body, a steering motor is fixedly arranged in the installation cylinder, a steering plate is rotatably arranged at one end of the steering motor, a connecting seat is arranged at one side of the steering plate, a steering cylinder is hingedly arranged at one side of the connecting seat, and an antenna is connected to the rod head of the first telescopic rod, so that multi-angle shooting and identification are realized, the unmanned aerial vehicle can be suspended and controlled after being loosened, low-altitude shooting can be realized while the flight height is ensured, safety and stability are ensured, combined control is facilitated, and adjustment and use are facilitated.

Description

Technical Field

[0001] This invention relates to the field of drones, and more specifically, to an artificial intelligence drone-based target recognition and alarm push device for urban management. Background Technology

[0002] Unmanned aerial vehicles (UAVs) are unmanned aircraft controlled by radio remote control equipment and onboard program control devices, or operated autonomously by an onboard computer, either completely or intermittently. Compared with manned aircraft, UAVs are often more suitable for tasks that are too "dull, dirty, or dangerous".

[0003] Drones can be categorized into military and civilian applications. In the military field, drones are divided into reconnaissance drones and target drones. In the civilian field, drones combined with industry applications represent the true necessity of drones. Currently, their applications in aerial photography, agriculture, plant protection, miniature selfies, express delivery, disaster relief, wildlife observation, infectious disease monitoring, surveying, news reporting, power line inspection, disaster relief, film and television production, and creating romantic moments have greatly expanded the uses of drones. Developed countries are also actively expanding industry applications and developing drone technology.

[0004] Unmanned aerial vehicles (UAVs) first appeared in the 1920s. In 1914, during the height of World War I, British Generals Cadell and Pitcher proposed to the British Military Aeronautical Society the development of a small, radio-controlled aircraft capable of flying over enemy target areas and dropping pre-loaded bombs. This bold idea immediately caught the eye of Sir David Henderson, then president of the British Military Aeronautical Society. He appointed Professor A.M. Lowe to lead a team to develop it. UAVs were initially used as target drones for training. The term "unmanned aerial vehicle" is used by many countries to describe the latest generation of unmanned aircraft. Literally, the term can describe everything from kites and radio-controlled aircraft to cruise missiles developed from the V-1 missile, but in military terminology, it is limited to reusable, heavier-than-air aircraft.

[0005] With the development of drone technology, its application in urban management is becoming increasingly widespread. It can take pictures of the city interior to identify targets and send early warnings, thereby improving the efficiency and quality of urban management. However, the structure and function of drones used in urban management rely on built-in antennas for signal transmission and lack corresponding combination and adjustment structures. This makes it impossible to switch between comprehensive and precise transmission modes, resulting in poor accuracy and timeliness of information transmission and push notifications. Furthermore, it is not conducive to adjusting the height and position of the camera, affecting the stability of the drone's flight. Fixed-point shooting and identification are required, which poses a high risk. Therefore, a new drone device needs to be proposed. Summary of the Invention

[0006] To address the problems existing in the prior art, the present invention aims to provide an artificial intelligence-based unmanned aerial vehicle (UAV) urban management target recognition and alarm push device. The device features hinged legs connected to crossbars on the side of the fuselage for cushioning and protection. A steering plate is mounted on the top mounting cylinder, allowing for the hinged mounting of the steering cylinder and antenna, facilitating angle adjustment for precise transmission. It can also be vertically positioned for comprehensive transmission, offering high adaptability. Simultaneously, a combination cylinder at the bottom connects to a hemispherical head, which, along with connecting cables, mounts a recognition camera, enabling multi-angle shooting and recognition. The camera can also be released for suspension control, ensuring both flight altitude and low-altitude shooting, guaranteeing safety and stability. The device is designed for combined control and easy adjustment.

[0007] To solve the above problems, the present invention adopts the following technical solution.

[0008] An AI-powered drone-based target recognition and alarm push device for urban management includes a body. A control board is fixedly installed inside the body. A crossbar is fixedly connected to the outer surface of the body. A rotor is rotatably mounted at the end of the crossbar. A hinge seat is provided at the bottom of the crossbar. A support leg is hinged to one end of the hinge seat. A return spring is fixedly connected to one side of the support leg and is fixedly connected to one side surface of the crossbar. A mounting cylinder is fixedly connected to the upper surface of the body. A steering motor is fixedly installed inside the mounting cylinder. A steering plate is rotatably mounted at one end of the steering motor. A connecting seat is provided on one side of the steering plate. A steering cylinder is hinged to one side of the connecting seat. A concave mirror is fixedly connected to the end of the steering cylinder. A first telescopic rod is fixedly connected inside the steering cylinder. An antenna is connected to the head of the first telescopic rod, located inside the concave mirror. A second telescopic rod is hinged to one side surface of the steering cylinder and is hinged to the surface of the steering plate.

[0009] A combined cylinder is fixedly connected to the lower surface of the body. A threaded tube is threadedly installed at one end of the combined cylinder. A combined block is connected to one end of the threaded tube. A spherical groove is provided at the bottom of the combined block. A hemispherical head is slidably installed inside the spherical groove. A connecting plate is provided at the bottom of the hemispherical head. A recognition camera is hinged to one end of the connecting plate. A third telescopic rod is hinged to one end of the recognition camera. The third telescopic rod is hinged to one side surface of the hemispherical head.

[0010] The control board includes a control module, a shooting module, a storage module, and an action module. The control module is connected in parallel to the shooting module, the storage module, and the action module via a circuit. The control module is connected in series with the recognition module, the transmission module, and the antenna module via a current. The antenna module is connected in series with the antenna via a circuit. The shooting module is connected in series with the recognition camera via a current.

[0011] Furthermore, the upper part of the spherical groove is provided with a threading hole, which is located at the upper end of the assembly block.

[0012] Furthermore, a winding rod is rotatably installed inside the combined cylinder, and a connecting wire is wound around the surface of the winding rod. By winding the connecting wire around the winding rod, it can be wound and positioned, and it is convenient to loosen and adjust the length, which is beneficial for control and use.

[0013] Furthermore, one end of the connecting wire is slidably connected to the inside of the wire hole, and the other end of the connecting wire is fixedly connected to the upper surface of the hemispherical head.

[0014] Furthermore, an adjusting motor is installed at one end of the winding rod. The adjusting motor is fixedly installed on the outer surface of the combined cylinder. By adjusting the motor to install the winding rod, forward and reverse rotation can be controlled, which facilitates winding and unwinding, and is highly efficient, stable, and adaptable.

[0015] Furthermore, one end of the support leg is provided with a buffer hole, and a buffer rod is slidably installed inside the buffer hole.

[0016] Furthermore, a support head is fixedly connected to one end of the buffer rod, and the support head is located at the bottom of the buffer rod.

[0017] Furthermore, a buffer spring is fixedly connected to one end of the buffer rod. The buffer spring is slidably installed inside the buffer hole. The buffer rod and the buffer spring can be combined and positioned through the buffer hole, which is beneficial for auxiliary support during take-off and landing, as well as for sliding buffering, ensuring safety, stability, and ease of use.

[0018] Furthermore, both sides of the support head are fixedly connected with arc-shaped anti-collision bars, which are combined to form a circular ring structure. By forming a circular ring with the arc-shaped anti-collision bars, the structure can be adjusted to a lateral position after takeoff, which is beneficial for protecting the rotor, improving safety and stability, and facilitating control and operation.

[0019] Furthermore, right-angle plates are fixedly installed on both sides of the bottom of the machine body, and an adjusting telescopic rod is fixedly installed on one side of the right-angle plate. A conical ring is installed at one end of the adjusting telescopic rod, and the conical ring is fitted onto the outer surface of the machine body. By adjusting the telescopic rod and installing the conical ring, the outriggers can be limited and adjusted, making it convenient to switch the protective position, ensuring safety and stability, and facilitating use.

[0020] Compared with the prior art, the advantages of this invention are:

[0021] (1) This solution uses the crossbar on the side of the fuselage to hinge the outriggers, which can provide buffer protection. At the same time, the steering plate is installed through the mounting cylinder on the top, thereby hinged to install the steering cylinder and antenna, which is conducive to adjusting the angle for precise transmission. It can also be vertically positioned and then transmitted in all directions, which is highly adaptable. Meanwhile, the combination cylinder at the bottom is connected to the hemispherical head, and the identification camera is installed with the connecting line, which can shoot and identify from multiple angles. At the same time, it can be released and suspended for control, which is conducive to ensuring the flight altitude while shooting at low altitude, ensuring safety and stability, and is conducive to combination control and convenient adjustment and use.

[0022] (2) The connecting line can be wound and positioned by the winding rod, making it easy to loosen and adjust the length, which is beneficial for control.

[0023] (3) By adjusting the motor mounting winding rod, forward and reverse rotation can be controlled, which is convenient for winding and unwinding, highly efficient and stable, and highly adaptable.

[0024] (4) The buffer rod and buffer spring can be installed through the buffer hole, which can be combined and positioned to facilitate auxiliary support for take-off and landing, and at the same time facilitate sliding buffering, making it safe, stable and easy to use.

[0025] (5) The circular ring formed by the combination of arc-shaped anti-collision bars can be adjusted to the lateral position after takeoff, which is beneficial for protecting the rotor, improving safety and stability, and facilitating control operation.

[0026] (6) By adjusting the tapered ring installed on the telescopic rod, the outrigger can be limited and adjusted, making it convenient to switch the protective position, safe and stable, and easy to use. Attached Figure Description

[0027] Figure 1 This is a schematic diagram of the overall structure of the present invention;

[0028] Figure 2 This is a partial schematic diagram of the antenna connection of the present invention;

[0029] Figure 3 For the present invention Figure 2 Enlarged view of point A where the steering cylinder is connected;

[0030] Figure 4 This is a partial structural diagram of the identification camera connection of the present invention;

[0031] Figure 5 A structural diagram showing the connection between the buffer rod and the arc-shaped anti-collision rod of the present invention;

[0032] Figure 6 For the present invention Figure 1 Enlarged view of point B where the conical ring connects;

[0033] Figure 7 This is a system principle block diagram of the control board of the present invention.

[0034] Explanation of the labels in the diagram:

[0035] 1. Airframe, 11. Crossbar, 12. Rotor, 13. Hinge mount, 14. Outriggers, 15. Mounting cylinder, 16. Steering motor, 17. Steering plate, 18. Connecting seat, 19. Return spring, 2. Steering cylinder, 21. Concave mirror, 22. First telescopic rod, 23. Antenna, 24. Second telescopic rod, 25. Combined cylinder, 26. Threaded pipe, 27. Combined block, 3. Spherical groove, 31. Hemispherical head, 32. Connecting plate, 33. Identification camera, 34. Third telescopic rod, 35. Threading hole, 36. Winding rod, 37. Connecting wire, 38. Adjusting motor, 4. Buffer hole, 41. Buffer rod, 42. Support head, 43. Buffer spring, 44. Arc-shaped anti-collision bar, 45. Right angle plate, 46. Adjusting telescopic rod, 47. Conical ring. Detailed Implementation

[0036] The technical solutions of the present invention will be clearly and completely described below with reference to the accompanying drawings of the embodiments of the present invention. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. All other embodiments obtained by those skilled in the art based on the embodiments of the present invention without creative effort are within the scope of protection of the present invention.

[0037] Example 1

[0038] Please see Figure 1 , Figure 2 , Figure 4 and Figure 7An AI-powered unmanned aerial vehicle (UAV) target recognition and alarm push device for urban management includes a body 1. A control board 5 is fixedly installed inside the body 1. A crossbar 11 is fixedly connected to the outer surface of the body 1. A rotor 12 is rotatably mounted at the end of the crossbar 11. A hinge seat 13 is provided at the bottom of the crossbar 11. A support leg 14 is hinged to one end of the hinge seat 13. The hinged support leg 14 provides auxiliary support from four positions, ensuring stability during takeoff and landing. It can also be rotated and adjusted around the hinge seat 13, thereby compressing the return spring 19 for reset, facilitating auxiliary buffering and improving stability. High safety protection effect, convenient for combined use. A return spring 19 is fixedly connected to one side of the outrigger 14. The return spring 19 is fixedly connected to one side surface of the crossbar 11. A mounting cylinder 15 is fixedly connected to the upper surface of the body 1. A steering motor 16 is fixedly installed inside the mounting cylinder 15. A steering plate 17 is rotatably mounted at one end of the steering motor 16. By rotating the steering plate 17 with the steering motor 16, the tilted antenna 23 can be adjusted to different directions. In this way, the transmission direction can be changed without adjusting the position of the body 1, which is conducive to precise pushing and convenient for multiple bodies. 1. Interconnected control, high efficiency and stability: A connecting seat 18 is provided on one side of the steering plate 17. A steering cylinder 2 is hinged to one side of the connecting seat 18. A concave mirror 21 is fixedly connected to the end of the steering cylinder 2. A first telescopic rod 22 is fixedly connected inside the steering cylinder 2. An antenna 23 is connected to the head of the first telescopic rod 22. The antenna 23 is located inside the concave mirror 21. A second telescopic rod 24 is hinged to one side surface of the steering cylinder 2. The second telescopic rod 24 is hinged to the surface of the steering plate 17. By pushing the steering cylinder 2 around the connecting seat 18 through the second telescopic rod 24, the steering cylinder 2 can be rotated. Adjusting the state of antenna 23 allows for vertical positioning, enabling comprehensive pushing in multiple directions and improving the breadth of identification and alarm capabilities. Adjusting the steering cylinder 2 to a tilted position allows antenna 23 to be precisely oriented in one direction. At this point, controlling the retraction of the first telescopic rod 22 pulls antenna 23 to retract, bringing it into the focal position of concave mirror 21. This concentrates the reflected signal, enhancing transmission strength, and allows for precise pushing along the reflection direction of concave mirror 21. This facilitates control, allows for easy switching, provides precision and stability, and ensures good safety.

[0039] A combination cylinder 25 is fixedly connected to the lower surface of the body 1. A threaded tube 26 is threadedly installed at one end of the combination cylinder 25. A combination block 27 is connected to one end of the threaded tube 26. A spherical groove 3 is provided at the bottom of the combination block 27. A hemispherical head 31 is slidably installed inside the spherical groove 3. A connecting plate 32 is provided at the bottom of the hemispherical head 31. A recognition camera 33 is hinged to one end of the connecting plate 32. A third telescopic rod 34 is hinged to one end of the recognition camera 33. The third telescopic rod 34 is hinged to one side surface of the hemispherical head 31. In use, the recognition camera 33 can be pushed around the connecting plate 32 by the third telescopic rod 34 to adjust the shooting and recognition direction, which is convenient for control operation. At this time, the hemispherical head 31 can be positioned inside the spherical groove 3 for easy assembly and alignment, avoiding misalignment and interference, ensuring shooting and recognition when flying at moving altitude, improving accuracy and wide applicability, and high adaptability.

[0040] The control board 5 includes a control module, a shooting module, a storage module, and an action module. The control module is connected in parallel to the shooting module, storage module, and action module via a circuit. The control module is connected in series with the identification module, transmission module, and antenna module via a current. The antenna module is connected in series with the antenna 23 via a circuit. The shooting module is connected in series with the identification camera 33 via a current. The outriggers are hinged to the crossbars on the side of the fuselage for cushioning and protection. The steering plate is mounted on the top mounting cylinder, which hinges the steering cylinder and antenna, facilitating angle adjustment for precise transmission. It can also be vertically positioned for full-range transmission, offering high adaptability. The bottom combination cylinder connects to the dome head, and the identification camera is mounted with the connecting wire, enabling multi-angle shooting and identification. It can also be released for suspension control, facilitating low-altitude shooting while maintaining flight altitude, ensuring safety and stability, and facilitating combined control and easy adjustment.

[0041] Example 2

[0042] Please see Figure 1 , Figure 3 , Figure 4 and Figure 7An AI-powered unmanned aerial vehicle (UAV) target recognition and alarm push device for urban management includes a body 1. A control board 5 is fixedly installed inside the body 1. A crossbar 11 is fixedly connected to the outer surface of the body 1. A rotor 12 is rotatably mounted at the end of the crossbar 11. A hinge seat 13 is provided at the bottom of the crossbar 11. A support leg 14 is hinged to one end of the hinge seat 13. The hinged support leg 14 provides auxiliary support from four positions, ensuring stability during takeoff and landing. It can also be rotated and adjusted around the hinge seat 13, thereby compressing the return spring 19 for reset, facilitating auxiliary buffering and improving stability. High safety protection effect, convenient for combined use. A return spring 19 is fixedly connected to one side of the outrigger 14. The return spring 19 is fixedly connected to one side surface of the crossbar 11. A mounting cylinder 15 is fixedly connected to the upper surface of the body 1. A steering motor 16 is fixedly installed inside the mounting cylinder 15. A steering plate 17 is rotatably mounted at one end of the steering motor 16. By rotating the steering plate 17 with the steering motor 16, the tilted antenna 23 can be adjusted to different directions. In this way, the transmission direction can be changed without adjusting the position of the body 1, which is conducive to precise pushing and convenient for multiple bodies. 1. Interconnected control, high efficiency and stability: A connecting seat 18 is provided on one side of the steering plate 17. A steering cylinder 2 is hinged to one side of the connecting seat 18. A concave mirror 21 is fixedly connected to the end of the steering cylinder 2. A first telescopic rod 22 is fixedly connected inside the steering cylinder 2. An antenna 23 is connected to the head of the first telescopic rod 22. The antenna 23 is located inside the concave mirror 21. A second telescopic rod 24 is hinged to one side surface of the steering cylinder 2. The second telescopic rod 24 is hinged to the surface of the steering plate 17. By pushing the steering cylinder 2 around the connecting seat 18 through the second telescopic rod 24, the steering cylinder 2 can be rotated. Adjusting the state of antenna 23 allows for vertical positioning, enabling comprehensive pushing in multiple directions and improving the breadth of identification and alarm capabilities. Adjusting the steering cylinder 2 to a tilted position allows antenna 23 to be precisely oriented in one direction. At this point, controlling the retraction of the first telescopic rod 22 pulls antenna 23 to retract, bringing it into the focal position of concave mirror 21. This concentrates the reflected signal, enhancing transmission strength, and allows for precise pushing along the reflection direction of concave mirror 21. This facilitates control, allows for easy switching, provides precision and stability, and ensures good safety.

[0043] A combination cylinder 25 is fixedly connected to the lower surface of the body 1. A threaded tube 26 is threadedly installed at one end of the combination cylinder 25. A combination block 27 is connected to one end of the threaded tube 26. A spherical groove 3 is provided at the bottom of the combination block 27. A hemispherical head 31 is slidably installed inside the spherical groove 3. A connecting plate 32 is provided at the bottom of the hemispherical head 31. A recognition camera 33 is hinged to one end of the connecting plate 32. A third telescopic rod 34 is hinged to one end of the recognition camera 33. The third telescopic rod 34 is hinged to one side surface of the hemispherical head 31. In use, the recognition camera 33 can be pushed around the connecting plate 32 by the third telescopic rod 34 to adjust the shooting and recognition direction, which is convenient for control operation. At this time, the hemispherical head 31 can be positioned inside the spherical groove 3 for easy assembly and alignment, avoiding misalignment and interference, ensuring shooting and recognition when flying at moving altitude, improving accuracy and wide applicability, and high adaptability.

[0044] The control board 5 includes a control module, a shooting module, a storage module, and an action module. The control module is connected in parallel to the shooting module, storage module, and action module via a circuit. The control module is connected in series with the identification module, transmission module, and antenna module via a current. The antenna module is connected in series with the antenna 23 via a circuit. The shooting module is connected in series with the identification camera 33 via a current. The outriggers are hinged to the crossbars on the side of the fuselage for cushioning and protection. The steering plate is mounted on the top mounting cylinder, which hinges the steering cylinder and antenna, facilitating angle adjustment for precise transmission. It can also be vertically positioned for full-range transmission, offering high adaptability. The bottom combination cylinder connects to the dome head, and the identification camera is mounted with the connecting wire, enabling multi-angle shooting and identification. It can also be released for suspension control, facilitating low-altitude shooting while maintaining flight altitude, ensuring safety and stability, and facilitating combined control and easy adjustment.

[0045] The upper end of the spherical groove 3 is provided with a wire hole 35, which is located at the upper end of the assembly block 27. A winding rod 36 is rotatably installed inside the assembly cylinder 25. A connecting wire 37 is wound on the surface of the winding rod 36. By winding the connecting wire with the winding rod, it can be wound and positioned, and it is convenient to loosen and adjust the length, which is conducive to control and use.

[0046] One end of the connecting wire 37 is slidably connected to the inside of the wire hole 35, and the other end is fixedly connected to the upper surface of the hemispherical head 31. One end of the winding rod 36 is equipped with an adjusting motor 38, which is fixedly installed on the outer surface of the combined cylinder 25. By adjusting the motor and the winding rod, forward and reverse control can be achieved, facilitating winding and unwinding. This method is highly efficient, stable, and adaptable. By winding the connecting wire 37 with the winding rod 36, the hemispherical head 31 can be pulled closer, thus stably positioning it inside the spherical groove 3, ensuring stability and facilitating integrated assembly and positioning. This is also convenient for high-altitude shooting. When adjustment is needed, the adjusting motor 38 can be controlled to rotate the winding rod 36 in the opposite direction, thereby releasing the connecting wire 37. This allows the hemispherical head 31 and the connecting plate 32 to fall downwards. The height of the fall can be adjusted by loosening the length of the connecting wire 37, thereby adjusting the height of the identification camera 33. This ensures the flight altitude of the aircraft 1, improves stability, reduces interference from low-altitude positions, and ensures the stability of signal transmission. At the same time, it allows for low-altitude shooting for identification and confirmation, ensuring the timeliness of alarms and facilitating urban management.

[0047] Example 3

[0048] Please see Figure 1 , Figure 2 , Figure 5 and Figure 6An AI-powered unmanned aerial vehicle (UAV) target recognition and alarm push device for urban management includes a body 1. A control board 5 is fixedly installed inside the body 1. A crossbar 11 is fixedly connected to the outer surface of the body 1. A rotor 12 is rotatably mounted at the end of the crossbar 11. A hinge seat 13 is provided at the bottom of the crossbar 11. A support leg 14 is hinged to one end of the hinge seat 13. The hinged support leg 14 provides auxiliary support from four positions, ensuring stability during takeoff and landing. It can also be rotated and adjusted around the hinge seat 13, thereby compressing the return spring 19 for reset, facilitating auxiliary buffering and improving stability. High safety protection effect, convenient for combined use. A return spring 19 is fixedly connected to one side of the outrigger 14. The return spring 19 is fixedly connected to one side surface of the crossbar 11. A mounting cylinder 15 is fixedly connected to the upper surface of the body 1. A steering motor 16 is fixedly installed inside the mounting cylinder 15. A steering plate 17 is rotatably mounted at one end of the steering motor 16. By rotating the steering plate 17 with the steering motor 16, the tilted antenna 23 can be adjusted to different directions. In this way, the transmission direction can be changed without adjusting the position of the body 1, which is conducive to precise pushing and convenient for multiple bodies. 1. Interconnected control, high efficiency and stability: A connecting seat 18 is provided on one side of the steering plate 17. A steering cylinder 2 is hinged to one side of the connecting seat 18. A concave mirror 21 is fixedly connected to the end of the steering cylinder 2. A first telescopic rod 22 is fixedly connected inside the steering cylinder 2. An antenna 23 is connected to the head of the first telescopic rod 22. The antenna 23 is located inside the concave mirror 21. A second telescopic rod 24 is hinged to one side surface of the steering cylinder 2. The second telescopic rod 24 is hinged to the surface of the steering plate 17. By pushing the steering cylinder 2 around the connecting seat 18 through the second telescopic rod 24, the steering cylinder 2 can be rotated. Adjusting the state of antenna 23 allows for vertical positioning, enabling comprehensive pushing in multiple directions and improving the breadth of identification and alarm capabilities. Adjusting the steering cylinder 2 to a tilted position allows antenna 23 to be precisely oriented in one direction. At this point, controlling the retraction of the first telescopic rod 22 pulls antenna 23 to retract, bringing it into the focal position of concave mirror 21. This concentrates the reflected signal, enhancing transmission strength, and allows for precise pushing along the reflection direction of concave mirror 21. This facilitates control, allows for easy switching, provides precision and stability, and ensures good safety.

[0049] A combination cylinder 25 is fixedly connected to the lower surface of the body 1. A threaded tube 26 is threadedly installed at one end of the combination cylinder 25. A combination block 27 is connected to one end of the threaded tube 26. A spherical groove 3 is provided at the bottom of the combination block 27. A hemispherical head 31 is slidably installed inside the spherical groove 3. A connecting plate 32 is provided at the bottom of the hemispherical head 31. A recognition camera 33 is hinged to one end of the connecting plate 32. A third telescopic rod 34 is hinged to one end of the recognition camera 33. The third telescopic rod 34 is hinged to one side surface of the hemispherical head 31. In use, the recognition camera 33 can be pushed around the connecting plate 32 by the third telescopic rod 34 to adjust the shooting and recognition direction, which is convenient for control operation. At this time, the hemispherical head 31 can be positioned inside the spherical groove 3 for easy assembly and alignment, avoiding misalignment and interference, ensuring shooting and recognition when flying at moving altitude, improving accuracy and wide applicability, and high adaptability.

[0050] The control board 5 includes a control module, a shooting module, a storage module, and an action module. The control module is connected in parallel to the shooting module, storage module, and action module via a circuit. The control module is connected in series with the identification module, transmission module, and antenna module via a current. The antenna module is connected in series with the antenna 23 via a circuit. The shooting module is connected in series with the identification camera 33 via a current. The outriggers are hinged to the crossbars on the side of the fuselage for cushioning and protection. The steering plate is mounted on the top mounting cylinder, which hinges the steering cylinder and antenna, facilitating angle adjustment for precise transmission. It can also be vertically positioned for full-range transmission, offering high adaptability. The bottom combination cylinder connects to the dome head, and the identification camera is mounted with the connecting wire, enabling multi-angle shooting and identification. It can also be released for suspension control, facilitating low-altitude shooting while maintaining flight altitude, ensuring safety and stability, and facilitating combined control and easy adjustment.

[0051] One end of the outrigger 14 is provided with a buffer hole 4. A buffer rod 41 is slidably installed inside the buffer hole 4. A support head 42 is fixedly connected to one end of the buffer rod 41. The support head 42 is located at the bottom of the buffer rod 41. A buffer spring 43 is fixedly connected to one end of the buffer rod 41. The buffer spring 43 is slidably installed inside the buffer hole 4. The buffer rod and buffer spring can be combined and positioned through the buffer hole, which is conducive to auxiliary support for take-off and landing. At the same time, it is conducive to sliding buffering, which is safe, stable and easy to use. During take-off and landing, by tilting and adjusting the outrigger 14 to both sides of the body 1, the support head 42 and the arc-shaped anti-collision bar 44 provide auxiliary support to improve stability. During landing, the support head 42 contacts the ground first. As the body 1 continues to descend, the buffer rod 41 slides inside the buffer hole 4, which can compress the buffer spring 43 to provide auxiliary buffering and ensure the safety of landing. Moreover, it is evenly installed at multiple angle positions, which can provide multi-directional support and protection to prevent tipping and facilitate combined use.

[0052] Both sides of the support head 42 are fixedly connected with arc-shaped anti-collision bars 44. The arc-shaped anti-collision bars 44 are combined to form a circular ring structure. The circular ring formed by the combination of arc-shaped anti-collision bars can be adjusted to a lateral position after takeoff, which is beneficial for protecting the rotor, improving safety and stability, and facilitating control and operation.

[0053] Right-angle plates 45 are fixedly installed on both sides of the bottom of the fuselage 1. An adjusting telescopic rod 46 is fixedly installed on one side of the right-angle plate 45. A conical ring 47 is installed at one end of the adjusting telescopic rod 46. The conical ring 47 is fitted onto the outer surface of the fuselage 1. By adjusting the telescopic rod and installing the conical ring, the outriggers can be limited and adjusted, facilitating the switching of protective positions. This ensures safety, stability, and ease of use. After takeoff, the adjusting telescopic rod 46 can be extended to push the conical ring 47 upward along the outer surface of the fuselage 1, thereby increasing the altitude. The outer surface of the conical ring 47 can press against the outrigger 14, thereby pushing the outrigger 14 to rotate upward around the hinge seat 13. Adjusting to a horizontal position and evenly distributing them on the side of the body 1 can avoid interference with the recognition camera 33, ensuring the shooting effect. On the other hand, after horizontal adjustment, multiple arc-shaped anti-collision bars 44 can be arranged horizontally to form a ring structure. The lateral diameter is larger than the width of the rotor 12, which can play a protective role. When the body 1 comes into contact with a building, the arc-shaped anti-collision bars 44 arranged on the side will contact the building surface first, thereby pushing the buffer bar 41 to add buffer spring 43, which can buffer and avoid collision. This can also prevent the rotating rotor 12 from directly contacting the building, improve the safety of anti-collision, facilitate combination adjustment, and make it convenient to control and use.

[0054] The above description is merely a preferred embodiment of the present invention; however, the scope of protection of the present invention is not limited thereto. Any equivalent substitutions or modifications made by those skilled in the art within the scope of the technology disclosed in the present invention, based on the technical solution and its improved concepts, should be covered within the scope of protection of the present invention.

Claims

1. An artificial intelligence-based unmanned aerial vehicle (UAV) target recognition and alarm push device for urban management, comprising a body (1), characterized in that: A control board (5) is fixedly installed inside the body (1). A crossbar (11) is fixedly connected to the outer surface of the body (1). A rotor (12) is rotatably installed at the end of the crossbar (11). A hinge seat (13) is provided at the bottom of the crossbar (11). A support leg (14) is hinged to one end of the hinge seat (13). A return spring (19) is fixedly connected to one side of the support leg (14). The return spring (19) is fixedly connected to one side surface of the crossbar (11). A mounting cylinder (15) is fixedly connected to the upper surface of the body (1). A steering motor (16) is fixedly installed inside the mounting cylinder (15). A steering plate (17) is rotatably mounted on one end of a steering motor (16). A connecting seat (18) is provided on one side of the steering plate (17). A steering cylinder (2) is hinged to one side of the connecting seat (18). A concave mirror (21) is fixedly connected to the end of the steering cylinder (2). A first telescopic rod (22) is fixedly connected inside the steering cylinder (2). An antenna (23) is connected to the head of the first telescopic rod (22). The antenna (23) is located inside the concave mirror (21). A second telescopic rod (24) is hinged to one side of the surface of the steering cylinder (2). The second telescopic rod (24) is hinged to the surface of the steering plate (17). A combination cylinder (25) is fixedly connected to the lower surface of the body (1). A threaded tube (26) is threaded onto one end of the combination cylinder (25). A combination block (27) is connected to one end of the threaded tube (26). A spherical groove (3) is provided at the bottom of the combination block (27). A hemispherical head (31) is slidably installed inside the spherical groove (3). A connecting plate (32) is provided at the bottom of the hemispherical head (31). A recognition camera (33) is hinged to one end of the connecting plate (32). A third telescopic rod (34) is hinged to one end of the recognition camera (33). The third telescopic rod (34) is hinged to one side surface of the hemispherical head (31). The control board (5) includes a control module, a shooting module, a storage module and an action module. The control module is connected in parallel to the shooting module, the storage module and the action module through a circuit. The control module is connected in series with the identification module, the transmission module and the antenna module through a current. The antenna module is connected in series with the antenna (23) through a circuit. The shooting module is connected in series with the identification camera (33) through a current.

2. The artificial intelligence drone urban management target recognition and alarm push device according to claim 1, characterized in that: The upper part of the spherical groove (3) is provided with a threading hole (35), which is located at the upper end of the assembly block (27).

3. The artificial intelligence drone urban management target recognition and alarm push device according to claim 1, characterized in that: The combined cylinder (25) is rotatably mounted with a winding rod (36), and the surface of the winding rod (36) is wound with a connecting wire (37).

4. The artificial intelligence drone urban management target recognition and alarm push device according to claim 3, characterized in that: One end of the connecting line (37) is slidably connected to the inside of the thread hole (35), and the other end of the connecting line (37) is fixedly connected to the upper surface of the hemispherical head (31).

5. The artificial intelligence drone urban management target recognition and alarm push device according to claim 3, characterized in that: An adjusting motor (38) is installed at one end of the winding rod (36), and the adjusting motor (38) is fixedly installed on the outer surface of the combined cylinder (25).

6. The artificial intelligence drone urban management target recognition and alarm push device according to claim 1, characterized in that: One end of the support leg (14) is provided with a buffer hole (4), and a buffer rod (41) is slidably installed inside the buffer hole (4).

7. The artificial intelligence drone urban management target recognition and alarm push device according to claim 6, characterized in that: One end of the buffer rod (41) is fixedly connected to a support head (42), which is located at the bottom of the buffer rod (41).

8. The artificial intelligence drone urban management target recognition and alarm push device according to claim 6, characterized in that: One end of the buffer rod (41) is fixedly connected to a buffer spring (43), which is slidably installed inside the buffer hole (4).

9. The artificial intelligence drone urban management target recognition and alarm push device according to claim 7, characterized in that: Both sides of the support head (42) are fixedly connected with arc-shaped anti-collision bars (44), and the arc-shaped anti-collision bars (44) are combined to form a circular ring structure.

10. The artificial intelligence drone urban management target recognition and alarm push device according to claim 9, characterized in that: Right-angle plates (45) are fixedly installed on both sides of the bottom of the body (1). An adjusting telescopic rod (46) is fixedly installed on one side of the right-angle plate (45). A conical ring (47) is installed at one end of the adjusting telescopic rod (46). The conical ring (47) is sleeved on the outer surface of the body (1).

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