Warning device of unmanned aerial vehicle hovering support

By integrating the control system, sensors and shock-absorbing devices on the drone's hovering bracket, the potential safety risks posed by drones to ground personnel when hovering in the existing technology are solved, and timely detection of ground personnel when the drone is hovering and buffering protection when it falls are achieved.

CN223355923UActive Publication Date: 2025-09-19JIAXING MUNICIPAL PUBLIC SECURITY BUREAU XIUZHOU DISTRICT BRANCH +1
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Patent Information

Application Number
CN202422608397.4
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-10-28
Publication Date
2025-09-19
Estimated Expiration
2034-10-28

AI Technical Summary

Technical Problem

Existing drones pose a potential safety risk to people on the ground when hovering, and are easily damaged when falling. Existing alarm methods are not easy to detect.

Method used

A UAV hovering bracket was designed, which includes a control system, an alarm, a sensor, a reflector, a bidirectional screw and a shock-absorbing device. The sensor detects the ground conditions and controls the operation of the alarm and the motor. When the sensor detects that there is someone on the ground, the control system controls the reflector and the alarm, and the shock-absorbing device cushions the impact of falling.

Benefits of technology

It ensures that ground personnel can detect the drone in time when it is hovering, avoid injuries, reduce damage to the drone caused by ground personnel, and the shock-absorbing device cushions the impact of falling, improving safety and reliability.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model belongs to the technical field of unmanned aerial vehicles, and particularly relates to an unmanned aerial vehicle hovering support warning device which comprises an unmanned aerial vehicle, a control system is fixedly installed in the unmanned aerial vehicle, a connecting support is detachably fixed to the middle of the bottom of the unmanned aerial vehicle, and connecting pipes are fixedly installed on the two sides of the two bottoms of the connecting support. A supporting seat is fixedly installed at the end of each connecting pipe, an alarm is installed on one side of the connecting support at the bottom of the unmanned aerial vehicle, a sensor is installed on the other side of the connecting support at the bottom of the unmanned aerial vehicle, a light reflecting plate is fixedly arranged in the connecting pipe, and a first annular baffle and a second annular baffle which are movable are arranged on the lower portion of the light reflecting plate; and springs and damping rubber are arranged at the bottom of the supporting seat, and a baffle and sealing rubber are fixed to the side face of the supporting seat in a threaded mode, so that ground personnel can conveniently find the unmanned aerial vehicle and make a dodging reaction, the unmanned aerial vehicle has the damping effect, and the unmanned aerial vehicle is prevented from being damaged by the ground.
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Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles (UAVs), and in particular to a warning device for a UAV hovering bracket. Background Art

[0002] In contemporary society, drone technology is increasingly being used in police work, including aerial surveillance, traffic management, search and rescue, and on-site investigations. Police departments utilize drone hovering platforms to conduct long-term surveillance of specific areas, improving law enforcement efficiency and safety. However, when drones are performing missions, particularly in crowded or complex environments, their hovering state can pose a potential safety risk to personnel on the ground.

[0003] Existing drones usually use alarms to alert ground personnel. However, this method makes it difficult for ground personnel to detect drones flying in the air and avoid them in the first place, which can easily cause injuries to ground personnel. In addition, when the drone falls, the ground will generate a reaction force to damage the drone, so it is necessary to add a shock-absorbing device to the bottom bracket of the drone. Utility Model Content

[0004] Based on the existing UAV technical problems, the utility model proposes a warning device for a UAV hovering bracket.

[0005] The utility model proposes a warning device for a hovering bracket of an unmanned aerial vehicle, comprising a unmanned aerial vehicle, wherein a control system is fixedly installed inside the unmanned aerial vehicle, and a connecting bracket is detachably fixed to the middle part of the bottom of the unmanned aerial vehicle, connecting pipes are fixedly installed on both sides of the two bottoms of the connecting bracket, and a support seat is fixedly installed on the end of each connecting pipe, an alarm is installed on one side of the connecting bracket at the bottom of the unmanned aerial vehicle, and a sensor is installed on the other side of the connecting bracket at the bottom of the unmanned aerial vehicle.

[0006] Preferably, a reflective groove is provided at the bottom of each connecting tube, and a bidirectional screw is rotatably fixed in the middle of each connecting tube, and a first annular movable plate is threadedly fixed to one end of the bidirectional screw, and a second annular movable plate is threadedly fixed to the other end of the bidirectional screw, a first annular baffle adapted to the inner wall of the connecting tube is fixed to the bottom of the first annular movable plate, a second annular baffle adapted to the inner wall of the connecting tube is fixed to the bottom of the second annular movable plate, and a reflective plate is fixed to the upper part of the first annular baffle at the lower part of the bidirectional screw inside the connecting tube.

[0007] Through the above technical solution, the setting of the first annular baffle and the second annular baffle can block the reflector when it is not in use, thereby facilitating operation and not affecting operation due to reflection from the reflector. When encountering people during descent, the reflector opens, making it easier for people to observe the drone and preventing the drone from causing damage to people when it falls.

[0008] Preferably, a first mounting groove is provided at the bottom of the support seat, and a telescopic column is fixedly provided on the top wall of the first mounting groove, and a spring is sleeved on the outer wall of the telescopic column inside the first mounting groove, and a support plate adapted to the first mounting groove is fixedly installed at the bottom of the telescopic column, and shock-absorbing rubber is installed at the bottom of the support plate.

[0009] Through the above technical solution, the spring and the shock-absorbing rubber cooperate with each other to create a buffer when the drone lands, thereby preventing the reaction force of the ground from causing damage to the drone.

[0010] Preferably, a second mounting slot is provided inside the support seat above the first mounting slot, a micro motor is fixed on the top of the second mounting slot, and the drive shaft of the micro motor rotates through the support seat and is coaxially fixed with the bidirectional screw through a coupling; a battery box is installed at the bottom of the micro motor inside the second mounting slot, and a battery slot is provided on the side of the battery box away from the connecting tube.

[0011] Through the above technical solution, the motor and the battery box cooperate with each other, so that the battery can drive the motor to move, thereby enabling the motor to drive the first annular baffle and the second annular baffle to overlap or separate with each other.

[0012] Preferably, the support seat is provided with a first movable groove on the side away from the connecting pipe, and a second movable groove is provided on the outside of the first movable groove, a threaded groove is provided in the middle of the outside of the second movable groove, a baffle is fixed inside the second movable groove, and a box support plate adapted to the first movable groove is fixed to the bottom of the baffle, and an annular groove is provided in the middle of the baffle, and a fastening bolt adapted to the threaded groove is rotatably fixed in the middle of the annular groove.

[0013] Through the above technical solution, the function of tightening the bolts can conveniently fix the baffle inside the second movable groove, thereby achieving sealing of the support seat.

[0014] Preferably, a sealing rubber is fixedly provided on the bottom of the baffle around the box abutment plate.

[0015] Through the above technical solution, the role of the sealing rubber makes the sealing effect better and can play a waterproof role.

[0016] The beneficial effects of the present invention are:

[0017] 1. By setting up a control system, an alarm, a sensor, a reflector, a bidirectional screw, a first annular baffle, a second annular baffle, a micro motor and a battery box, the sensor can detect the state of the ground when the drone is falling. When a person is detected on the ground, the sensor transmits the information to the control system, so that the control system controls the micro motor to operate, thereby separating the first annular baffle and the second annular baffle, exposing the reflector, and the control system controls the alarm to sound an alarm in the first time, so that ground personnel can discover the drone in the first time and respond in the first time to prevent the drone from harming ground personnel.

[0018] 2. By setting up the coordination between the spring, telescopic column, support plate and shock-absorbing rubber, when the drone falls to the ground, the shock-absorbing rubber and spring act as a buffer to prevent the reaction force of the ground from causing damage to the drone.

[0019] 3. By setting the interaction between the fastening bolts, baffles, threaded grooves, and sealing rubber, the fastening bolts can drive the baffles to form a detachable seal on the support seat, and the sealing rubber can make the sealing effect better, thereby achieving a waterproof effect. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Figure 1 This is a schematic diagram of the overall appearance of a warning device for a drone hovering bracket proposed in the present invention;

[0021] Figure 2 This is a schematic diagram of the overall bottom view of a warning device for a drone hovering bracket proposed in the present invention;

[0022] Figure 3 This is a cross-sectional schematic diagram of a connecting pipe of a warning device for a UAV hovering bracket proposed in the present invention;

[0023] Figure 4 This is a cross-sectional schematic diagram of a support base of a warning device for a UAV hovering bracket proposed in the present invention;

[0024] Figure 5 for Figure 2 Enlarged view of point A in the middle;

[0025] Figure 6 for Figure 3 Enlarged view of point B in the middle;

[0026] Figure 7 for Figure 4 Enlarged view of point C in the middle;

[0027] Figure 8 for Figure 7 Enlarged view of point D in the middle.

[0028] In the figure: 1. UAV; 2. Control system; 3. Connecting bracket; 4. Connecting pipe; 401. Reflective groove; 402. Bidirectional screw; 403. First annular movable plate; 404. Second annular movable plate; 405. First annular baffle; 406. Second annular baffle; 5. Support seat; 501. First mounting groove; 502. Second mounting groove; 503. Spring; 504. Telescopic column; 505. Support plate; 506. Shock-absorbing rubber; 507. Micro motor; 508. Battery box; 509. Battery slot; 510. Baffle; 511. Box support plate; 512. Sealing rubber; 513. First movable groove; 514. Second movable groove; 515. Fastening bolt; 516. Annular groove; 517. Threaded groove; 6. Alarm; 7. Sensor; 8. Reflector. DETAILED DESCRIPTION

[0029] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all the embodiments.

[0030] Example 1:

[0031] Reference Figures 1-8 A warning device for a drone hovering bracket includes a drone 1, a control system 2 is fixedly installed inside the drone 1, and a connecting bracket 3 is detachably fixed to the middle part of the bottom of the drone 1, connecting pipes 4 are fixedly installed on both sides of the bottom of the connecting bracket 3, and a support base 5 is fixedly installed on the end of each connecting pipe 4, an alarm 6 is installed on one side of the connecting bracket 3 at the bottom of the drone 1, and a sensor 7 is installed on the other side of the connecting bracket 3 at the bottom of the drone 1. A reflective groove 401 is provided at the bottom of each connecting tube 4, and a bidirectional screw 402 is rotatably fixed in the middle of each connecting tube 4, and a first annular movable plate 403 is threadedly fixed to one end of the bidirectional screw 402, and a second annular movable plate 404 is threadedly fixed to the other end of the bidirectional screw 402, a first annular baffle 405 adapted to the inner wall of the connecting tube 4 is fixed to the bottom of the first annular movable plate 403, a second annular baffle 406 adapted to the inner wall of the connecting tube 4 is fixed to the bottom of the second annular movable plate 404, and a reflective plate 8 is fixed to the upper part of the first annular baffle 405 at the lower part of the bidirectional screw 402 inside the connecting tube 4.

[0032] Example 2:

[0033] In this embodiment, refer to Figures 1-8Based on the first embodiment, the support base 5 has a first mounting slot 501 defined at its bottom. A telescopic column 504 is fixedly mounted on the top wall of the first mounting slot 501. A spring 503 is sleeved on the outer wall of the telescopic column 504 within the first mounting slot 501. A support plate 505, which matches the first mounting slot 501, is fixedly mounted on the bottom of the telescopic column 504. A shock-absorbing rubber 506 is mounted on the bottom of the support plate 505. A second mounting slot 502 is defined within the support base 5 above the first mounting slot 501. A micromotor 507 is fixedly mounted on the top of the second mounting slot 502. The drive shaft of the micromotor 507 rotates through the support base 5 via a coupling and is coaxially fixed to the bidirectional screw 402. A battery box 508 is mounted below the micromotor 507 within the second mounting slot 502. A battery slot 509 is defined on the side of the battery box 508 away from the connecting tube 4. The support base 5 has a first movable groove 513 formed on the side away from the connecting tube 4. A second movable groove 514 is formed outside the first movable groove 513. A threaded groove 517 is formed in the middle of the outer side of the second movable groove 514. A baffle 510 is fixedly secured inside the second movable groove 514. A box retaining plate 511 that matches the first movable groove 513 is fixedly secured to the bottom of the baffle 510. An annular groove 516 is formed in the middle of the baffle 510. A fastening bolt 515 that matches the threaded groove 517 is rotatably secured to the middle of the annular groove 516. A sealing rubber 512 is fixedly secured to the bottom of the baffle 510 around the box retaining plate 511.

[0034] Working principle: when in use, when the drone is falling, the sensor 7 detects the situation on the ground. When someone is found on the ground, the sensor 7 transmits the detected information to the control system 2, so that the control system 2 controls the alarm 6 to alarm, and at the same time the control system 2 controls the micro motor 507 to operate, so that the first annular baffle 405 and the second annular baffle 406 are separated from each other, thereby exposing the reflector 8, making it easier for ground personnel to observe the drone and thus facilitate avoidance. When falling to the ground, due to the action of the spring 503 and the shock-absorbing rubber 506, the reaction force of the ground on the drone can be absorbed, thereby reducing the damage to the drone by the ground.

[0035] The above is only a preferred specific implementation method of the present invention, but the protection scope of the present invention is not limited to this. Any technician familiar with the technical field within the technical scope disclosed by the present invention can make equivalent replacements or changes based on the technical solution and utility model concept of the present invention, which should be covered by the protection scope of the present invention.

Claims

1. A warning device for a drone hovering bracket, comprising a drone (1), characterized in that: A control system (2) is fixedly installed inside the drone (1), and a connecting bracket (3) is detachably fixed to the middle of the bottom of the drone (1), connecting pipes (4) are fixedly installed on both sides of the bottom of the connecting bracket (3), and a support seat (5) is fixedly installed at the end of each connecting pipe (4), an alarm (6) is installed on one side of the connecting bracket (3) at the bottom of the drone (1), and a sensor (7) is installed on the other side of the connecting bracket (3) at the bottom of the drone (1).

2. The warning device for a drone hovering bracket according to claim 1, characterized in that: A reflective groove (401) is provided at the bottom of each connecting tube (4), and a bidirectional screw (402) is rotatably fixed in the middle of each connecting tube (4), and a first annular movable plate (403) is threadedly fixed to one end of the bidirectional screw (402), and a second annular movable plate (404) is threadedly fixed to the other end of the bidirectional screw (402), a first annular baffle (405) adapted to the inner wall of the connecting tube (4) is fixed to the bottom of the first annular movable plate (403), and a second annular baffle (406) adapted to the inner wall of the connecting tube (4) is fixed to the bottom of the second annular movable plate (404), and a reflective plate (8) is fixed to the upper part of the first annular baffle (405) below the bidirectional screw (402) inside the connecting tube (4).

3. The warning device for a drone hovering bracket according to claim 2, characterized in that: The support seat (5) is provided with a first mounting groove (501) at the bottom, and a telescopic column (504) is fixedly provided on the top wall of the first mounting groove (501), and a spring (503) is sleeved on the outer wall of the telescopic column (504) inside the first mounting groove (501), and a support plate (505) adapted to the first mounting groove (501) is fixedly provided at the bottom of the telescopic column (504), and a shock-absorbing rubber (506) is installed at the bottom of the support plate (505).

4. The warning device for a drone hovering bracket according to claim 3, characterized in that: A second mounting groove (502) is provided inside the support seat (5) above the first mounting groove (501); a micro motor (507) is fixedly provided at the top of the second mounting groove (502); and a transmission shaft of the micro motor (507) is rotated through the support seat (5) through a coupling and is coaxially fixed to the bidirectional screw (402); a battery box (508) is installed inside the second mounting groove (502) below the micro motor (507), and a battery slot (509) is provided on the side of the battery box (508) away from the connecting pipe (4).

5. The warning device for a drone hovering bracket according to claim 4, characterized in that: The support seat (5) is provided with a first movable groove (513) on the side away from the connecting pipe (4), and a second movable groove (514) is provided on the outside of the first movable groove (513), a threaded groove (517) is provided in the middle of the outside of the second movable groove (514), a baffle (510) is fixedly engaged with the inside of the second movable groove (514), and a box abutment (511) adapted to the first movable groove (513) is fixedly provided at the bottom of the baffle (510), and an annular groove (516) is provided in the middle of the baffle (510), and a fastening bolt (515) adapted to the threaded groove (517) is rotatably fixed in the middle of the annular groove (516).

6. The warning device for a drone hovering bracket according to claim 5, characterized in that: The bottom of the baffle (510) is fixedly provided with sealing rubber (512) around the box abutment plate (511).