Power transmission line unmanned aerial vehicle carrying operation platform

Abstract

The invention relates to the field of unmanned aerial vehicle operation platforms, in particular to a power transmission line unmanned aerial vehicle carrying operation platform which comprises a vehicle body, a mounting structure is arranged at the top of the vehicle body, and the mounting structure is used for hanging an unmanned aerial vehicle body on a power transmission line so as to operate the power transmission line; the hot melting mechanism is arranged at the top of the machine body and is used for performing hot melting treatment on foreign matters on the power transmission line; the bearing structure is arranged at the bottom of the machine body, and the bearing structure is used for bearing and fixing the electricity testing device; the device comprises a mounting hook, a suspension rope is connected to the mounting hook, a damping disc is installed on the suspension rope and movably arranged on the suspension rope in a penetrating mode, the bottom of the suspension rope is connected with a hollowed-out release box, and the hollowed-out release box is used for carrying and releasing a solid bird repellent. The integration of hanging, hot melting, electricity testing and bird repelling functions can meet various requirements of power transmission line maintenance, and has high practicability.

Description

Technical Field

[0001] The present invention relates to the field of unmanned aerial vehicle (UAV) operation platforms, and in particular to a transmission line UAV-mounted operation platform. Background Art

[0002] With the rapid economic development and the growing demand for electricity in society, the power industry plays a vital role in modern society. As a key infrastructure for power transmission, the safe and stable operation of transmission lines is directly related to the reliability and quality of power supply. In recent years, the scale of the power grid has continued to expand, and the length and distribution range of transmission lines have continued to increase. At the same time, the operating environment faced by transmission lines has become increasingly complex, including the diversity of topography, changeable climatic conditions, and the influence of various natural and human factors. These factors have brought huge challenges to the maintenance of transmission lines. Traditional manual inspection methods can no longer meet the growing maintenance needs. There is an urgent need to introduce more efficient and intelligent inspection technologies and means.

[0003] In the existing technology, a large number of maintenance work processes for transmission lines require personnel to work at high altitudes, such as testing electricity, installing odor-repellent bird repellent devices on the top of poles and towers, and removing foreign objects from optical cables. There are problems such as high safety risks and low efficiency. When drones are lifting tools and materials, ropes may cross or be bundled, which may easily cause drones to lose control.

[0004] Therefore, it is necessary to propose a transmission line UAV-mounted operation platform to solve the above problems. Summary of the invention

[0005] The purpose of the present invention is to provide a transmission line drone-mounted operating platform to solve the problem that a large number of maintenance operations on the transmission lines need to be completed by personnel at high altitudes, such as electrical testing, installation of odor bird repellent devices on the top of poles and towers, and removal of foreign objects on optical cables. There are problems such as high operational safety risks and low efficiency. When drones are lifting tools and materials, ropes may cross and bundle, which may easily lead to the problem of drone out of control.

[0006] To achieve the above object, the present invention provides the following technical solutions: A transmission line UAV carrying operation platform comprises a body, a mounting structure, wherein the mounting structure is arranged on the top of the body, and the mounting structure is used to mount the UAV body on the transmission line so as to operate the transmission line; a hot melt mechanism, wherein the hot melt mechanism is arranged on the top of the body, the hot melt mechanism and the mounting structure are located on the same horizontal line, and the hot melt mechanism is symmetrically arranged on the body with the mounting structure as a reference plane, and the hot melt mechanism is used to perform hot melt treatment on foreign objects on the transmission line; a bearing structure, wherein the bearing structure is arranged at the bottom of the body, and the bearing structure is used to carry and fix an electrical test device to prevent the electrical test device from shaking during the flight of the UAV; four mounting hooks are fixedly installed at the bottom of the body, and the four mounting hooks are evenly distributed at the bottom of the body, and the mounting hooks are all connected with a suspension rope, and a damping disk is installed on the suspension rope, and the damping disk is movably inserted on the suspension rope, and a hollow release box is connected to the bottom of the suspension rope, and the hollow release box is used to carry and release solid bird repellent, and a camera is installed at one end of the bottom of the body.

[0007] Preferably, the mounting structure includes a support member 1 and a support member 2, a roller 1 is rotatably mounted on the support member 1, two mounting plates 1 are arranged on the top of the support member 2, the two mounting plates 1 are connected by a rotating shaft, and a roller 2 is rotatably mounted between the two mounting plates 1, a positioning plate is fixedly mounted on one side of one of the mounting plates 1, the positioning plate is arranged at a position close to the roller 1, and a side of the positioning plate close to the roller 1 is arranged as a curved smooth arc surface, a slide groove is arranged on the top of the support member 2, the mounting plate 1 is slidably connected to the slide groove, a linear motor is fixedly mounted on the top of the support member 2, and the linear motor is drivingly connected to the mounting plate 1.

[0008] Preferably, the hot melt mechanism includes a sliding sleeve and a sliding rod, the number of the sliding sleeve and the sliding rod are both four, the sliding rod is slidably mounted on the sliding sleeve, a mounting plate 2 is fixedly mounted on one side of the sliding rod near the top, a rotating shaft is rotatably mounted between every two mounting plates 2, threads are provided on the rotating shaft near both ends, and the screwing directions of the two threads are opposite, a connecting block is threadedly mounted on the thread of the rotating shaft, a metal hot melt sheet is fixedly connected to the top of the connecting block, a side of the metal hot melt sheets close to each other is set as a semicircular curved surface, a side of the metal hot melt sheets away from each other is fixedly mounted with a heat conducting rod, a resistance wire is wound on the outer side of the heat conducting rod, a relay is fixedly mounted on the inner side of the mounting plate 2, a power supply is connected to the relay, the relay is electrically connected to the resistance wire, a motor is fixedly mounted on the mounting plate 2, and the motor is drivingly connected to the rotating shaft.

[0009] Preferably, a ducted air duct is fixedly installed on the second mounting plate, a fan is installed inside the ducted air duct, the fan is electrically connected to the power supply of the drone, the ducted air duct is tilted on the second mounting plate, and the air outlet of the ducted air duct is arranged at a certain angle to the axis of the two metal heat-melting plates.

[0010] Preferably, the bearing structure includes an upper bearing frame, two lower bearing frames, and four connecting frames, wherein two of the connecting frames are fixedly mounted on the bottom of the machine body, and the remaining connecting frames are rotatably mounted on the bottom of the machine body, both ends of the two lower bearing frames are fixedly connected to the bottom of the connecting frames, through grooves are provided on the connecting frames, and lock buckles are rotatably mounted on the sides of the upper bearing frame, the lock buckles are slidably arranged with the through grooves, and the width of the lock buckles is adapted to the width of the through grooves, and sockets are provided on the connecting frames and the lock buckles.

[0011] Preferably, the damping plate includes an upper damping plate and a lower damping plate, the upper damping plate and the lower damping plate are fixedly connected by bolts, the upper damping plate and the lower damping plate are both provided with through holes, the suspension rope is passed through the through holes, and driving motors are fixedly installed inside the upper damping plate and the lower damping plate, and locking plates 1 and 2 are respectively connected to the output shafts of the two driving motors, and the locking plates 1 and 2 are arranged between the upper damping plate and the lower damping plate, and locking teeth 1 and 2 are respectively fixedly installed on the sides of the locking plates 1 and 2, the locking teeth 1 and 2 are staggered, and the locking teeth 1 and 2 are arranged on both sides of one end of the through hole.

[0012] Preferably, an electromagnet is fixedly installed on the internal top of the release box, and the electrical wire of the electromagnet is electrically connected to the power supply of the drone. A mounting tube is slidably installed inside the release box. There are multiple mounting tubes, and the mounting tubes pass through the bottom of the release box. A magnetic sheet 1 is fixedly connected to the top of the mounting tube, and a magnetic sheet 2 is fixedly connected to the bottom of the mounting tube.

[0013] Preferably, a connecting rod is rotatably mounted on the side of the body, a fan blade is mounted on the connecting rod, and a driving motor of the fan blade is electrically connected to a power supply of the drone.

[0014] Technical effects and advantages of the present invention: 1. The present invention can replace manual work in some aerial operations, such as testing electricity, removing foreign objects, releasing bird repellents, etc., which greatly saves time and manpower and improves work efficiency; 2. Through the precise design of the mounting structure, hot-melt mechanism, bearing structure, etc., it is possible to achieve precise operation of the transmission line and improve the work quality; 3. The setting of the damping disc reduces the spinning and entanglement of the suspension rope, and improves the stability of the UAV during operation; the design of the mounting structure also enables the UAV to be stably mounted on the transmission line; 4. The operating platform integrates multiple functions, such as mounting, hot melting, electrical testing, bird repelling, etc., which can meet the various needs of transmission line maintenance and has high practicality. Through the automatic control of electromagnets, motors, etc., it realizes the automation of some operations, reduces manual intervention, and improves the accuracy and reliability of work. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 The present invention is a schematic diagram of the structure of a transmission line UAV-mounted operating platform.

[0016] Figure 2 It is a schematic diagram of the mounting structure of the present invention.

[0017] Figure 3 For the present invention Figure 2 Schematic diagram of the proposed enlarged structure at point A.

[0018] Figure 4 It is a schematic diagram of the hot melt mechanism structure of the present invention.

[0019] Figure 5 For the present invention Figure 4 Schematic diagram of the proposed enlarged structure at location B.

[0020] Figure 6 It is a schematic diagram of the bearing structure of the present invention.

[0021] Figure 7 For the present invention Figure 6 Schematic diagram of the proposed enlarged structure at location C.

[0022] Figure 8 It is a schematic diagram of the internal structure of the damping disk of the present invention.

[0023] Fig. 9 It is a schematic diagram of the internal structure of the hollow release box of the present invention.

[0024] In the figure: 1. body; 2. mounting structure; 201. support member 1; 202. support member 2; 203. roller 1; 204. roller 2; 205. mounting plate 1; 206. linear motor; 207. slide; 3. hot melt mechanism; 301. sliding sleeve; 302. slide rod; 303. mounting plate 2; 304. rotating shaft; 305. thread; 306. connecting block; 307. metal hot melt sheet; 308. heat conducting rod; 309. resistance wire; 310. motor; 311. relay; 312. ducted air duct; 4. mounting Carrying hook; 5. Carrying structure; 501. Upper bearing frame; 502. Lower bearing frame; 503. Connecting frame; 504. Through slot; 505. Plug hole; 506. Lock buckle; 6. Suspension rope; 7. Damping disc; 701. Upper damping disc; 702. Lower damping disc; 703. Locking disc one; 704. Locking disc two; 705. Locking tooth one; 706. Locking tooth two; 707. Perforation; 8. Hollow release box; 9. Camera; 10. Electromagnet; 11. Magnetic sheet one; 12. Mounting tube; 13. Magnetic sheet two; 14. Connecting rod; 15. Fan blade. DETAILED DESCRIPTION

[0025] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0026] The present invention provides Figure 1-Figure 9 The transmission line UAV carrying operation platform shown in the figure includes a body 1, a mounting structure 2, the mounting structure 2 is arranged on the top of the body 1, and the mounting structure 2 is used to mount the UAV body 1 on the transmission line to facilitate the operation of the transmission line; a hot melt mechanism 3, the hot melt mechanism 3 is arranged on the top of the body 1, the hot melt mechanism 3 and the mounting structure 2 are located on the same horizontal line, and the hot melt mechanism 3 is symmetrically arranged on the body 1 with the mounting structure 2 as a reference plane, and the hot melt mechanism 3 is used to perform hot melt treatment on foreign objects on the transmission line; a bearing structure 5, a bearing The structure 5 is arranged at the bottom of the body 1, and the bearing structure 5 is used to bear and fix the electric test device to prevent the electric test device from shaking during the flight of the UAV; four mounting hooks 4 are fixedly installed at the bottom of the body 1, and the four mounting hooks 4 are evenly distributed at the bottom of the body 1, and the mounting hooks 4 are connected with suspension ropes 6, and the suspension ropes 6 are equipped with damping discs 7, and the damping discs 7 are movably arranged on the suspension ropes 6, and the bottom of the suspension ropes 6 is connected with a hollow release box 8, and the hollow release box 8 is used to carry and release solid bird repellent, and a camera 9 is installed at one end of the bottom of the body 1; See also Figure 1-Figure 9When the UAV is processing the power line, the UAV body is mounted on the power line through the mounting structure 2, so that the UAV can operate stably on the power line. When foreign matter is found on the power line, the hot melt mechanism 3 is activated to perform hot melt treatment on the foreign matter so that it falls off the power line. The bearing structure 5 can fix the electrical testing device to ensure that the electrical testing device remains stable during the flight of the UAV and accurately performs electrical testing. The suspension rope 6 on the mounting hook 4 is connected to the damping plate 7, the hollow release box 8 and other components. During the flight, the damping plate 7 can reduce the spinning and entanglement of the suspension rope 8 and improve the stability of the UAV. The hollow release box 8 is equipped with solid bird repellent. When it is necessary to During the bird-repelling operation, the UAV places the hollow release box 8 at the designated position to release the solid bird repellent. The camera 9 records the working process in real time to provide visual feedback to the operator so as to better control the operation of the UAV. It can replace manual work in some high-altitude operations, such as testing electricity, removing foreign objects, releasing bird repellent, etc., which greatly improves work efficiency, reduces the need for personnel to perform high-altitude operations, and reduces safety risks such as electric shock, falling from heights, and being hit by objects. The setting of the damping disk 7 reduces the instability of the suspension rope 6 and improves the stability of the UAV during operation. The operating platform integrates multiple functions, can meet the various needs of power transmission line maintenance, and has high practicality.

[0027] The mounting structure 2 includes a support member 201 and a support member 202. A roller 203 is rotatably mounted on the support member 201. Two mounting plates 205 are arranged on the top of the support member 202. The two mounting plates 205 are connected by a rotating shaft. A roller 204 is rotatably mounted between the two mounting plates 205. A positioning plate 208 is fixedly mounted on one side of one of the mounting plates 205. The positioning plate 208 is arranged at a position close to the roller 203. One side of the positioning plate 208 close to the roller 203 is arranged as a curved smooth arc surface. A slide groove 207 is arranged on the top of the support member 202. The mounting plate 205 is slidably connected to the slide groove 207. A linear motor 206 is fixedly mounted on the top of the support member 202. The linear motor 206 is drivingly connected to the mounting plate 205. See also Figure 2-3When the UAV needs to be hung on the transmission line, the linear motor 206 works to push the mounting plate 205 to slide on the slide groove 207, so that the roller 204 approaches the roller 1 203. During the approaching process, the transmission line first contacts the curved smooth arc surface of the positioning plate 208. Due to the guiding effect of the arc surface, when the UAV rises in height, the transmission line will smoothly move along the arc surface to the roller 1 203. Then the linear motor 206 continues to push the mounting plate 205 so that the roller 204 and the roller 1 203 are kept on the same horizontal line. The roller 1 20 3 and roller two 204 clamp the transmission line, so as to realize the hanging of the UAV on the transmission line. The automatic movement of roller two 204 is realized through the control of linear motor 206, without manual intervention, which improves the efficiency and convenience of mounting. The curved and smooth arc surface of positioning plate 208 can effectively guide the transmission line into between roller one 203 and roller two 204, ensuring the accuracy of mounting. Roller one 203 and roller two 204 can clamp the transmission line, so that the UAV can be hung on the transmission line stably, not easy to shake or fall off, and ensure the safety of work.

[0028] The hot melt mechanism 3 includes a sliding sleeve 301 and a sliding rod 302. The number of the sliding sleeve 301 and the sliding rod 302 are both four. The sliding rod 302 is slidably mounted on the sliding sleeve 301. A mounting plate 2 303 is fixedly mounted on the sliding rod 302 near the top. A rotating shaft 304 is rotatably mounted between each two mounting plates 2 303. Threads 305 are arranged near both ends of the rotating shaft 304, and the screwing directions of the two threads 305 are opposite. A connecting block 306 is threadedly mounted on the thread 305 of the rotating shaft 304. A metal hot melt sheet 307 is fixedly connected to the top of the connecting block 306. The side of the metal hot melt sheets 307 close to each other is set as a semicircular curved surface, and the side of the metal hot melt sheets 307 away from each other is fixed. A heat conducting rod 308 is fixedly installed, and a resistance wire 309 is wound and installed on the outer side of the heat conducting rod 308. A relay 311 is fixedly installed on the inner side of the second mounting plate 303, and the relay 311 is connected to a power supply. The relay 311 is electrically connected to the resistance wire 309. A motor 310 is fixedly installed on the second mounting plate 303, and the motor 310 is drivingly connected to the rotating shaft 304. A ducted air duct 312 is fixedly installed on the second mounting plate 303, and a fan is installed inside the ducted air duct 312. The fan is electrically connected to the power supply of the drone. The ducted air duct 312 is tilted on the second mounting plate 303, and the air outlet of the ducted air duct 312 is set at a certain angle to the axis of the two metal heat-melting sheets 307; See also Figure 4-5When the drone finds that foreign matter on the transmission line needs to be hot-melted, while the transmission line smoothly moves along the arc surface to the roller 203, because the hot-melt mechanism 3 and the roller 203 of the mounting structure 2 are kept at the same level in the initial state, the motor 310 starts, driving the rotating shaft 304 to rotate. Since the threads 305 near the two ends of the rotating shaft 304 are screwed in opposite directions, the two connecting blocks 306 are moved closer to or away from each other, and the connecting block 306 drives the metal hot-melt sheet 307 to move, so that the two metal hot-melt sheets 307 are close to each other, clamping the transmission line and the foreign matter on the transmission line. At the same time, the relay 311 connects the power supply of the resistor 309, the resistor 309 heats up, and transfers the heat to the metal hot-melt sheet 307 through the heat-conducting rod 308, and the metal hot-melt sheet 307 heats the foreign matter. During the hot melting process, the fan in the ducted air duct 312 is started, and the generated wind is blown toward the foreign matter through the air outlet to blow away the residue after hot melting. The rotating shaft 304 is controlled by the motor 310 to realize the movement of the metal hot melt sheet 307, which can accurately clamp the power transmission line to ensure the hot melting effect. The resistance wire 309 is heated and the heat is quickly transferred to the metal hot melt sheet 307 through the heat conducting rod 308 to perform hot melting treatment on the foreign matter with high efficiency. The setting of the ducted air duct 312 can blow away the residue after hot melting in time to keep the power transmission line clean. The side of the metal hot melt sheet 307 close to each other is set as a semicircular curved surface to improve the versatility of the treatment. The working process of the entire hot melting mechanism 3 is automatically controlled by the motor 310, the relay 311, etc., which reduces manual intervention and improves work efficiency and safety.

[0029] The bearing structure 5 includes an upper bearing frame 501, two lower bearing frames 502, and four connecting frames 503, wherein two connecting frames 503 are fixedly mounted on the bottom of the machine body 1, and the remaining connecting frames 503 are rotatably mounted on the bottom of the machine body 1, both ends of the two lower bearing frames 502 are fixedly connected to the bottom of the connecting frames 503, and a through slot 504 is provided on the connecting frames 503, and a lock buckle 506 is rotatably mounted on the side of the upper bearing frame 501, and the lock buckle 506 is slidably arranged with the through slot 504, and the width of the lock buckle 506 is adapted to the width of the through slot 504, and a plug hole 505 is provided on both the connecting frame 503 and the lock buckle 506; See also Figure 6-7When the electrical testing device needs to be installed, the electrical testing device is placed between the upper carrier frame 501 and the two lower carrier frames 502. Then, the lock buckle 506 on the side of the upper carrier frame 501 is rotated to insert it into the through slot 504 of the connecting frame 503. Next, the lock buckle 506 is rotated 180 degrees to keep it perpendicular to the through slot on the connecting frame 503. Finally, a pin or other fixing part is inserted into the socket 505 to fix the lock buckle 506 on the connecting frame 503, thereby realizing the bearing and fixing of the electrical testing device. Through the combination of the upper carrier frame 501, the lower carrier frame 502 and the connecting frame 503, the electrical testing device can be stably carried to prevent it from vibrating or displacing during the flight of the drone, thereby ensuring the normal operation of the electrical testing device. The matching design of the lock buckle 506 and the through slot 504 makes the installation process of the electrical testing device simple and quick, and improves the work efficiency. The positions of the upper carrier frame 501 and the lower carrier frame 502 can also be adjusted according to the size and shape of the electrical testing device to adapt to different types of electrical testing devices.

[0030] The damping plate 7 includes an upper damping plate 701 and a lower damping plate 702, the upper damping plate 701 and the lower damping plate 702 are fixedly connected by bolts, the upper damping plate 701 and the lower damping plate 702 are both provided with a through hole 707, the suspension rope 6 is passed through the through hole 707, the upper damping plate 701 and the lower damping plate 702 are both fixedly installed with a driving motor, the output shafts of the two driving motors are respectively connected with a lock plate 1 703 and a lock plate 2 704, the lock plate 1 703 and the lock plate 2 704 are arranged between the upper damping plate 701 and the lower damping plate 702, the sides of the lock plate 1 703 and the lock plate 2 704 are respectively fixedly installed with a lock tooth 1 705 and a lock tooth 2 706, the lock tooth 1 705 and the lock tooth 2 706 are staggered, and the lock tooth 1 705 and the lock tooth 2 706 are arranged on both sides of one end of the through hole 707; See also Figure 8 During the flight of the UAV, when the suspension rope 6 appears to be unstable such as spinning or entangled, the drive motor is started, and the drive motor in the upper damping disk 701 drives the lock disk 1 703 to rotate, so that the lock tooth 1 705 moves the suspension rope 6 to one side of the through hole 707; the drive motor in the lower damping disk 702 drives the lock disk 2 704 to rotate, so that the lock tooth 2 706 moves the same suspension rope 6 to the other side of the through hole 707. Since the lock tooth 1 705 and the lock tooth 2 706 are staggered, they will tighten the suspension rope 6 on the damping disk, increase the friction of the suspension rope 6 at the through hole 707, thereby preventing the suspension rope from spinning and entangled, and keeping the UAV stable.

[0031] An electromagnet 10 is fixedly installed on the top of the release box 8, and the electric wire of the electromagnet 10 is electrically connected to the power supply of the drone. A mounting tube 12 is slidably installed inside the release box 8. There are multiple mounting tubes 12, and the mounting tubes 12 are arranged to penetrate the bottom of the release box 8. A magnetic sheet 11 is fixedly connected to the top of the mounting tube 12, and a magnetic sheet 2 13 is fixedly connected to the bottom of the mounting tube 12. A connecting rod 14 is rotatably installed on the side of the body 1, and a fan blade 15 is installed on the connecting rod 14. The driving motor of the fan blade 15 is electrically connected to the power supply of the drone. See also Fig. 9 Through the interaction between the electromagnet 10 and the magnetic sheet 11, the mounting tube 12 can be fixed in the release box. When the electromagnet 10 is energized, the magnetic sheet 11 is attracted to fix the mounting tube 12, which is convenient for loading and fixing the solid bird repellent. When the bird repellent needs to be released, the electromagnet 10 is de-energized, and the mounting tube 12 descends under the action of gravity. The bird repellent and the mounting tube 12 fall from the bottom of the release box 8 and are fixedly adsorbed on the top of the transmission line tower by the magnetic sheet 2 (13), thereby achieving precise control of the release and improving the efficiency of the use of the bird repellent.

[0032] The above shows and describes the basic principles, main features and advantages of the present invention. Those skilled in the art should understand that the present invention is not limited to the above embodiments. The above embodiments and descriptions only describe the principles of the present invention. The present invention may be subject to various changes and improvements without departing from the spirit and scope of the present invention. These changes and improvements fall within the scope of the present invention. The scope of protection claimed by the present invention is defined by the attached claims and their equivalents.

Claims

1. A transmission line UAV-mounted operating platform, comprising a body (1), characterized in that: Also includes: A mounting structure (2), the mounting structure (2) being arranged on the top of the body (1), and the mounting structure (2) being used to mount the drone body (1) on a power transmission line so as to facilitate operation of the power transmission line; A hot melt mechanism (3), the hot melt mechanism (3) being arranged on the top of the body (1), the hot melt mechanism (3) and the mounting structure (2) being located on the same horizontal line, and the hot melt mechanism (3) being symmetrically arranged on the body (1) with the mounting structure (2) as a reference plane, and the hot melt mechanism (3) being used to perform hot melt treatment on foreign matter on the transmission line; A bearing structure (5), the bearing structure (5) being arranged at the bottom of the body (1), and the bearing structure (5) being used to bear and fix the electrical testing device, so as to prevent the electrical testing device from shaking during the flight of the unmanned aerial vehicle; Four mounting hooks (4) are fixedly mounted on the bottom of the machine body (1), and the four mounting hooks (4) are evenly distributed on the bottom of the machine body (1). The mounting hooks (4) are all connected to a suspension rope (6), and a damping plate (7) is mounted on the suspension rope (6). The damping plate (7) is movably arranged on the suspension rope (6). The bottom of the suspension rope (6) is connected to a hollow release box (8), and the hollow release box (8) is used to carry and release solid bird repellent. A camera (9) is mounted on one end of the bottom of the machine body (1).

2. The transmission line UAV-mounted operating platform according to claim 1, characterized in that: The mounting structure (2) comprises a support member 1 (201) and a support member 2 (202); a roller 1 (203) is rotatably mounted on the support member 1 (201); two mounting plates 1 (205) are arranged on the top of the support member 2 (202); the two mounting plates 1 (205) are connected via a rotating shaft; a roller 2 (204) is rotatably mounted between the two mounting plates 1 (205); a positioning plate (208) is fixedly mounted on one side of one of the mounting plates 1 (205). The positioning plate (208) is arranged at a position close to roller one (203), and a side of the positioning plate (208) close to roller one (203) is arranged as a curved smooth arc surface. A slide groove (207) is arranged on the top of the support member two (202), and the mounting plate one (205) is slidably connected to the slide groove (207). A linear motor (206) is fixedly installed on the top of the support member two (202), and the linear motor (206) is drivingly connected to the mounting plate one (205).

3. The transmission line UAV-mounted operating platform according to claim 1, characterized in that: The hot melt mechanism (3) comprises a sliding sleeve (301) and a sliding rod (302). The number of the sliding sleeve (301) and the number of the sliding rod (302) are both four. The sliding rod (302) is slidably mounted on the sliding sleeve (301). A second mounting plate (303) is fixedly mounted on one side of the sliding rod (302) near the top. A rotating shaft (304) is rotatably mounted between each two second mounting plates (303). Threads (305) are arranged near both ends of the rotating shaft (304), and the screwing directions of the two threads (305) are opposite. A connecting block (306) is threadedly mounted on the thread (305) of the rotating shaft (304). The connecting block (306) is 6) is fixedly connected to the top of the second mounting plate (303), the side of the metal hot melt sheets (307) close to each other is set as a semicircular curved surface, the side of the metal hot melt sheets (307) away from each other is fixedly installed with a heat conducting rod (308), the outer side of the heat conducting rod (308) is wound with a resistance wire (309), the inner side surface of the second mounting plate (303) is fixedly installed with a relay (311), the relay (311) is connected to a power supply, the relay (311) is electrically connected to the resistance wire (309), and the second mounting plate (303) is fixedly installed with a motor (310), and the motor (310) is drivingly connected to the rotating shaft (304).

4. The transmission line UAV-mounted operating platform according to claim 3, characterized in that: A ducted air duct (312) is fixedly mounted on the second mounting plate (303), a fan is mounted inside the ducted air duct (312), and the fan is electrically connected to the power supply of the drone. The ducted air duct (312) is tiltedly arranged on the second mounting plate (303), and an air outlet of the ducted air duct (312) is arranged at a certain angle to the axes of the two metal heat-melting sheets (307).

5. The transmission line UAV-mounted operating platform according to claim 1, characterized in that: The bearing structure (5) comprises an upper bearing frame (501), two lower bearing frames (502), and four connecting frames (503), wherein two of the connecting frames (503) are fixedly mounted on the bottom of the machine body (1), and the remaining connecting frames (503) are rotatably mounted on the bottom of the machine body (1), both ends of the two lower bearing frames (502) are fixedly connected to the bottom of the connecting frames (503), a through slot (504) is provided on the connecting frames (503), a locking buckle (506) is rotatably mounted on the side of the upper bearing frame (501), the locking buckle (506) is slidably arranged with the through slot (504), and the width of the locking buckle (506) is adapted to the width of the through slot (504), and both the connecting frames (503) and the locking buckle (506) are provided with a plug hole (505).

6. The transmission line UAV-mounted operating platform according to claim 1, characterized in that: The damping plate (7) comprises an upper damping plate (701) and a lower damping plate (702); the upper damping plate (701) and the lower damping plate (702) are fixedly connected by bolts; the upper damping plate (701) and the lower damping plate (702) are both provided with through holes (707); the suspension rope (6) is passed through the through holes (707); the upper damping plate (701) and the lower damping plate (702) are both fixedly installed with drive motors; the output shafts of the two drive motors are respectively connected with locks. Plate 1 (703) and lock plate 2 (704), the lock plate 1 (703) and lock plate 2 (704) are arranged between the upper damping plate (701) and the lower damping plate (702), and the sides of the lock plate 1 (703) and lock plate 2 (704) are respectively fixedly mounted with lock teeth 1 (705) and lock teeth 2 (706), the lock teeth 1 (705) and lock teeth 2 (706) are staggered, and the lock teeth 1 (705) and lock teeth 2 (706) are arranged on both sides of one end of the through hole (707).

7. The transmission line UAV-mounted operating platform according to claim 1, characterized in that: An electromagnet (10) is fixedly installed on the top of the release box (8), and the electric wire of the electromagnet (10) is electrically connected to the power supply of the drone. A mounting tube (12) is slidably installed inside the release box (8), and there are multiple mounting tubes (12). The mounting tubes (12) are arranged to pass through the bottom of the release box (8). The top of the mounting tube (12) is fixedly connected to a magnetic sheet 1 (11), and the bottom of the mounting tube (12) is fixedly connected to a magnetic sheet 2 (13).

8. The transmission line UAV-mounted operating platform according to claim 1, characterized in that: A connecting rod (14) is rotatably mounted on the side of the body (1), a fan blade (15) is mounted on the connecting rod (14), and a drive motor of the fan blade (15) is electrically connected to a power source of the drone.

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