Line-imitating inspection radar mounting structure and unmanned aerial vehicle
Through the design of positioning boxes, skateboards, plug blocks and adjustment components, combined with single-line lidar, visual identification module and microcontroller with specific communication protocols, the stability and data transmission problems of drone radar during flight are solved, and efficient and reliable patrol operations are achieved.
Patent Information
- Application Number
- CN202521462235.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-07-14
- Publication Date
- 2025-08-22
- Estimated Expiration
- 2035-07-14
AI Technical Summary
The existing radar installation methods have poor stability during the flight of the drone, are prone to shake or fall off, and are cumbersome to install and disassemble, which affects the accuracy and reliability of patrol data. At the same time, data transmission and processing efficiency are low, making it difficult to meet the high efficiency and high reliability operation needs.
The design of positioning boxes, sliders, plugs and adjustment components is adopted, and the radar system of single-line lidar and visual recognition module is combined with the radar system, and data transmission is used for microcontrollers with specific communication protocols, and the fusion technology of laser point cloud and visual recognition is achieved to achieve stable connection and efficient data processing.
It realizes stable connection of radar during flight, simplifies the installation and disassembly process, improves patrol efficiency, and ensures timely and accurate data transmission and processing, meeting a variety of patrol needs.
Smart Images

Figure CN223253311U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of radar installation, and in particular to an installation structure of a line inspection radar and an unmanned aerial vehicle (UAV). Background Art
[0002] Currently, in the field of drone-based line inspections, the existing radar installation methods are relatively simple, mostly using simple bolt fixation or snap-on connections. This installation method has poor stability during drone flight, especially when facing complex flight environments and airflow interference. The radar is prone to shaking or even falling off, which not only affects the accuracy and reliability of inspection data, but may also cause equipment damage and increase maintenance costs. At the same time, the existing installation structure is cumbersome and time-consuming during installation and disassembly, which is not conducive to improving the efficiency of inspection operations. In addition, the existing radar system also has certain deficiencies in data transmission and processing, and cannot efficiently realize data interaction and processing, making it difficult to meet the operational requirements of "improving efficiency, saving electricity, accurate positioning, and strong expansion." Utility Model Content
[0003] In order to make up for the above shortcomings, the utility model provides a line inspection radar installation structure and a UAV, aiming to improve the existing radar installation method which is relatively simple, mostly using simple bolt fixation or snap connection. This installation method has poor stability during the flight of the UAV, especially when facing complex flight environments and airflow interference.
[0004] In the first aspect, the utility model provides a linear inspection radar installation structure, including a body and an analysis box, a positioning box is fixedly installed on the top of the body, a positioning groove matching the positioning box is provided at the bottom of the body, a slide is symmetrically slidably installed on the inner wall of the positioning box, two slides are fixedly installed on one side away from each other, one end of the slide slides through one side of the positioning box and inserted into the inner wall of the positioning groove, an adjustment component is installed on the slide, and positioning plates are fixedly installed at the four corners of the analysis box, and the positioning plates are fixedly connected to the body by bolts.
[0005] In the preferred technical solution of the present invention, a radar system designed for drone line inspection is installed in the analysis box. The system integrates a single-line laser radar and a visual recognition module to adapt to the inspection of transmission lines with voltage levels of 110kV and above. In the entire system architecture, in order to achieve efficient data interaction and processing, key components responsible for data transmission and control are specially set up. It uses a single-chip microcomputer with specific communication protocols and data processing capabilities. The single-chip microcomputer is electrically connected to the inspection radar through a specific circuit connection method to ensure that data can be transmitted stably and at high speed between the two. At the same time, the single-chip microcomputer uses adaptive signal transmission technology to establish a signal connection with the control host, thereby ensuring that important information such as tree obstacle analysis data and spacer defect identification results can be transmitted to the control host in a timely and accurate manner for further analysis and processing by staff. The entire radar system has been optimized and weighs less than 200g. The system uses advanced laser point cloud and visual recognition fusion technology to achieve stable tracking of ground wire targets, and efficiently complete functions such as transmission line ground wire inspection, spacer defect identification, tree-line conflict analysis, conductor sag measurement, and conductor foreign object inspection.
[0006] In a preferred technical solution of the present utility model, the top of the body is provided with a first thread groove matched with the bolt, and the first thread groove is provided at the four corners of the positioning box.
[0007] In the preferred technical solution of the present invention, guide rods are symmetrically fixedly installed between the two sides of the inner wall of the positioning box, the slide is slidably installed on the guide rods, and the positioning box is opened on the side relatively close to the body.
[0008] In the preferred technical solution of the present invention, the adjustment assembly includes a support frame and a threaded rod, the support frame is fixedly installed between the top end of the inner wall of the positioning box and the machine body, the threaded rod is symmetrically rotatably installed on both sides of the support frame, the slide plate and the insert block are threadedly installed on the threaded rod, a driving assembly is installed at one end of the threaded rod, the slide plate and the insert block are provided with a first threaded hole and a second threaded hole matching the threaded rod and are connected to each other, a gap is provided between the threaded rod and the inner side wall of the positioning box, and the inner wall of the positioning groove is provided with a slot matching the insert block.
[0009] In the preferred technical solution of the present invention, the driving assembly includes a first rotating shaft, a second rotating shaft and an elastic telescopic rod. The first rotating shaft is rotatably installed between the two sides of the inner wall of the support frame, both ends of the first rotating shaft pass through the support frame and are fixedly connected to one end of the adjacent threaded rod, the second rotating shaft is rotatably installed between the inner wall of the positioning box and the machine body, a worm is fixedly installed on the second rotating shaft, a worm wheel is fixedly installed on the first rotating shaft, the worm and the worm wheel are transmission-connected, the elastic telescopic rod is fixedly installed on one end of the first rotating shaft, and one end of the elastic telescopic rod passes through the machine body and is fixedly installed on the turntable.
[0010] In the preferred technical solution of the present invention, the elastic telescopic rod includes a sleeve rod, a pull rod and a spring, one end of the second rotating shaft is fixedly installed with the sleeve rod, one end of the sleeve rod slides through the body and slides onto the pull rod, the spring is fixedly installed between the pull rod and the inner wall of the sleeve rod, one end of the pull rod is fixedly installed with the turntable, a slider is symmetrically fixedly installed on the outside of the pull rod, the inner wall of the sleeve rod is provided with a sliding groove matching the slider, a limiting ring is fixedly installed on the outside of the sleeve rod, and an annular groove matching the limiting ring is provided in the body.
[0011] In the preferred technical solution of the present invention, a circular groove matching the turntable is provided at the bottom of the body, a pull groove is provided on one side of the turntable, a pull block is fixedly installed on the inner wall of the pull groove, the cross-section of the pull block is T-shaped, and the turntable is slidably connected to the inner wall of the circular groove.
[0012] In the preferred technical solution of the present invention, a plurality of limit bars are fixedly installed on the outer side of the turntable, the inner wall of the circular groove is provided with a strip groove matching the limit bars, and the plurality of limit bars are equidistantly installed on the outer side of the turntable.
[0013] In a second aspect, the present invention further provides a drone, comprising the above-mentioned line inspection radar installation structure and a drone body, wherein the drone body is the fuselage.
[0014] The beneficial effects of the utility model are: the installation structure is stable and reliable: through the design of the positioning box, slide plate, plug block and adjustment component, a stable connection between the analysis box and the body is achieved, which effectively avoids the shaking and falling off of the radar during flight, and improves the stability and reliability of the equipment.
[0015] Installation and disassembly are convenient and efficient: the setting of the drive component and the elastic telescopic rod in the adjustment component makes the installation and disassembly process simple and convenient, greatly shortening the operation time and improving the efficiency of the inspection operation.
[0016] Powerful radar system: The radar system in the analysis box integrates a single-line laser radar and a visual recognition module. It can obtain uninterrupted visible light images and infrared images of the conductor, identify spacer defects, and calculate key data such as the maximum sag of the conductor and the distance to the tree line, meeting various inspection needs.
[0017] Efficient data transmission and processing: The use of a single-chip microcomputer with specific communication protocols and data processing capabilities ensures stable and high-speed data transmission between the inspection radar and the control host, ensuring that important information is transmitted to the control host in a timely and accurate manner for staff to analyze and process.
[0018] Strong adaptability: The entire radar system weighs less than 200g. With the help of advanced laser point cloud and visual recognition fusion technology, it can achieve stable tracking of ground wire targets and fully meet operational needs. BRIEF DESCRIPTION OF THE DRAWINGS
[0019] In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the following is a brief introduction to the drawings required for use in the embodiments. It should be understood that the following drawings only show certain embodiments of the present invention and therefore should not be regarded as limiting the scope. For ordinary technicians in this field, other relevant drawings can be obtained based on these drawings without creative work.
[0020] Figure 1 This is a schematic diagram of a structure of a line inspection radar installation structure provided by an embodiment of the present utility model;
[0021] Figure 2 A schematic diagram of the disassembled structure of a line inspection radar installation structure is provided for an embodiment of the present utility model;
[0022] Figure 3 A schematic diagram of the structure of the adjustment assembly is provided for the embodiment of the utility model;
[0023] Figure 4 for Figure 3 A in the middle is an enlarged schematic diagram;
[0024] Figure 5 A bottom view of a linear inspection radar installation structure is provided for an embodiment of the present utility model;
[0025] Figure 6 A cross-sectional view of the body is provided for an embodiment of the present utility model;
[0026] Figure 7 The present invention provides a structural diagram of an elastic telescopic rod.
[0027] In the figure: 110-body; 120-analysis box; 121-positioning plate; 122-bolt; 130-positioning box; 131-slide plate; 132-insert block; 133-guide rod; 140-support frame; 141-threaded rod; 142-first rotating shaft; 143-second rotating shaft; 144-elastic telescopic rod; 145-worm; 146-worm gear; 147-turntable; 148-pull block; 149-limiting strip; 150-sleeve rod; 151-pull rod; 152-spring; 153-slider. DETAILED DESCRIPTION
[0028] To make the purpose, technical solutions, and advantages of the embodiments of the present invention more clear, the technical solutions in the embodiments of the present invention will be clearly and completely described 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, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.
[0029] See also Figure 1-Figure 5 The present invention provides a technical solution: a line inspection radar installation structure, including a body 110 and an analysis box 120, a positioning box 130 is fixedly installed on the top of the body 110, and a positioning groove matching the positioning box 130 is provided at the bottom of the body 110, and a slide plate 131 is symmetrically slidably installed on the inner wall of the positioning box 130, and two slide plates 131 are fixedly installed on one side away from each other, and one end of the slide block 132 slides through one side of the positioning box 130 and is inserted into the inner wall of the positioning groove, and an adjustment component is installed on the slide plate 131, and positioning plates 121 are fixedly installed on the four corners of the analysis box 120, and the positioning plates 121 are fixedly connected to the body 110 by bolts 122.
[0030] In some specific implementation schemes, the analysis box 120 is equipped with a radar system designed specifically for drone line inspections. This system integrates a single-line laser radar and a visual recognition module, and is suitable for inspections of transmission lines at voltage levels of 110kV and above. It has a wide range of functions: it can obtain uninterrupted visible light images of the conductors, helping to visually view the appearance of the conductors; uninterrupted infrared images of the conductors can detect abnormal conductor temperatures; multi-angle visible light images and infrared images of the spacers are used to accurately identify various defects in the spacers; the system can also calculate key data such as the maximum sag of the conductors and the distance between dangerous points and trees. In the entire system architecture, key components responsible for data transmission and control are specially set up to achieve efficient data interaction and processing. It uses a single-chip microcomputer with specific communication protocols and data processing capabilities. The single-chip microcomputer is electrically connected to the inspection radar through a specific circuit connection method to ensure stable and high-speed data transmission between the two. At the same time, the microcontroller uses adaptive signal transmission technology to establish a signal connection with the control host, ensuring that important information such as tree obstacle analysis data and spacer defect identification results are transmitted to the control host in a timely and accurate manner for further analysis and processing by staff. The entire radar system has been optimized and weighs less than 200g, making it easily adaptable to a variety of drone platforms. Leveraging advanced laser point cloud and visual recognition fusion technology, the system achieves stable tracking of ground wire targets, efficiently completing functions such as transmission line ground wire inspections, spacer defect identification, tree-line conflict analysis, conductor sag measurement, and conductor foreign object inspections, fully meeting the operational requirements of "increasing efficiency, saving electricity, accurate positioning, and strong expansion."
[0031] In some specific embodiments, a first thread groove matching the bolt 122 is provided at the top of the body 110. The first thread groove is provided at the four corners of the positioning box 130, which can enhance the connection stability between the analysis box 120 and the body 110 and avoid the displacement of the installation structure due to single-point force.
[0032] In some specific embodiments, guide rods 133 are symmetrically fixed between the inner walls of the positioning box 130, and the slide 131 is slidably mounted on the guide rods 133. The positioning box 130 is opened on the side closer to the housing 110. This provides guidance for the movement of the slide 131 and ensures the precise positioning of the insert 132 when it is inserted into the positioning slot. The opening on the side of the positioning box 130 closer to the housing 110 facilitates the rapid docking of the insert 132 with the positioning slot.
[0033] See also Figure 5-Figure 7The adjustment assembly includes a support frame 140 and a threaded rod 141. The support frame 140 is fixedly mounted between the top end of the inner wall of the positioning box 130 and the body 110. The threaded rod 141 is symmetrically mounted on both sides of the support frame 140 for rotation. The slide 131 and the insert 132 are threadedly mounted on the threaded rod 141. A driving assembly is mounted on one end of the threaded rod 141. The slide 131 and the insert 132 are provided with a first threaded hole and a second threaded hole that match the threaded rod 141 and are interconnected. A gap is provided between the threaded rod 141 and the inner wall of the positioning box 130, and a slot is provided on the inner wall of the positioning groove that matches the insert 132. When the threaded rod 141 rotates, it drives the slide 131 to slide through the threaded hole, thereby achieving telescopic control of the insert 132. A gap is provided between the threaded rod 141 and the inner wall of the positioning box 130 to prevent friction and jamming. The slot on the inner wall of the positioning groove matches the insert 132, which can enhance the locking strength of the installation structure. The drive assembly includes a first rotating shaft 142, a second rotating shaft 143, and an elastic telescopic rod 144. The first rotating shaft 142 is rotatably mounted between the inner walls of the support frame 140. Both ends of the first rotating shaft 142 pass through the support frame 140 and are fixedly connected to one end of the adjacent threaded rod 141. The second rotating shaft 143 is rotatably mounted between the inner wall of the positioning box 130 and the body 110. A worm 145 is fixedly mounted on the second rotating shaft 143, and a worm gear 146 is fixedly mounted on the first rotating shaft 142. The worm 145 and the worm gear 146 are in transmission connection. The elastic telescopic rod 144 is fixedly mounted on one end of the first rotating shaft 142. One end of the elastic telescopic rod 144 passes through the body 110 and is fixedly mounted on a turntable 147. Rotating the turntable 147 synchronously drives the threaded rods 141 on both sides to rotate, ensuring the synchronous movement of the slide 131. The elastic telescopic rod 144 connects the first rotating shaft 142 and the turntable 147, facilitating external control of the drive assembly.
[0034] In some specific embodiments, the elastic telescopic rod 144 includes a sleeve rod 150, a pull rod 151, and a spring 152. The sleeve rod 150 is fixedly mounted on one end of the second rotating shaft 143. One end of the sleeve rod 150 slides through the body 110 and slides onto the pull rod 151. The spring 152 is fixedly mounted between the pull rod 151 and the inner wall of the sleeve rod 150. The turntable 147 is fixedly mounted on one end of the pull rod 151. A slider 153 is symmetrically fixedly mounted on the outer side of the pull rod 151. The inner wall of the sleeve rod 150 is provided with a groove that matches the slider 153. A limiting ring is fixedly mounted on the outer side of the sleeve rod 150. An annular groove that matches the limiting ring is provided in the body 110. The pull rod 151 cooperates with the slide groove of the sleeve rod 150 through the slider 153. When the spring 152 is stretched, the turntable 147 can be driven out of the circular groove to unlock the drive assembly. The structural design takes into account both elastic reset and sliding guide functions.
[0035] In some specific embodiments, the bottom end of the housing 110 is provided with a circular groove that matches the turntable 147. A pull groove is provided on one side of the turntable 147. A pull block 148 is fixedly mounted on the inner wall of the pull groove. The pull block 148 has a T-shaped cross section, and the turntable 147 is slidably connected to the inner wall of the circular groove. Pulling the pull block 148 can easily move the turntable 147, making it easier to operate.
[0036] In some specific embodiments, a plurality of limiting bars 149 are fixedly mounted on the outside of the turntable 147. The inner wall of the circular groove is provided with strip grooves that match the limiting bars 149. The plurality of limiting bars 149 are equidistantly mounted on the outside of the turntable 147. After installation, the limiting bars 149 fit into the strip grooves, preventing the turntable 147 from rotating accidentally, ensuring that the insert 132 remains locked, and enhancing the anti-loosening performance of the mounting structure.
[0037] An embodiment of the present invention further provides a drone, comprising the above-mentioned line inspection radar installation structure and a drone body, wherein the drone body is the body.
[0038] Working Principle: To install or remove the analysis cartridge 120, first pull the pull block 148 on the turntable 147, causing the turntable 147 to drive the pull rod 151 to slide within the sleeve 150, compressing the spring 152. Simultaneously, the slider 153 slides within the slot, ensuring smooth movement of the pull rod 151. At this point, the elastic telescopic rod 144 extends, disengaging the turntable 147 from the circular slot and releasing the position limit. Rotating the turntable 147 drives the pull rod 151 and sleeve 150, which in turn rotates the worm gear 146 via the first rotating shaft 142. The worm 145, meshing with the worm gear 146, drives the second rotating shaft 143, thereby rotating the threaded rod 141. Because the slide 131 and the insert 132 are provided with first and second threaded holes that match the threaded rod 141, the rotation of the threaded rod 141 drives the slide 131 to slide on the guide rod 133, driving the insert 132 to move, allowing it to be withdrawn from or inserted into the positioning slot, thereby completing the installation or removal of the analysis box 120 from the body 110. After installation, the turntable 147 is released. Under the elastic force of the spring 152, the pull rod 151 drives the turntable 147 back to its original position. The limit bar 149 on the turntable 147 engages the strip groove on the inner wall of the circular slot, completing the fixed position. The inspection radar inside the analysis box 120 performs a simulated line inspection operation, transmitting data to the single-chip microcomputer, which then transmits the signal to the control host for analysis and processing of the inspection data.
[0039] The above description is merely a preferred embodiment of the present invention and is not intended to limit the present invention. Those skilled in the art will readily appreciate that the present invention is susceptible to various modifications and variations. Any modifications, equivalent substitutions, or improvements made within the spirit and principles of the present invention shall be included within the scope of protection of the present invention.
Claims
1. A linear inspection radar installation structure, characterized in that: It includes a body and an analysis box, a positioning box is fixedly installed on the top of the body, a positioning groove matching the positioning box is provided at the bottom of the body, a slide is symmetrically slidably installed on the inner wall of the positioning box, two slides are relatively far away from one side and fixed with an insert block, one end of the insert block slides through one side of the positioning box and is inserted into the inner wall of the positioning groove, an adjustment component is installed on the slide, and positioning plates are fixedly installed at the four corners of the analysis box, and the positioning plates are fixedly connected to the body by bolts.
2. The installation structure of a line inspection radar according to claim 1, characterized in that: The analysis box is equipped with a radar system designed specifically for drone line inspection, which integrates a single-line laser radar and a visual recognition module.
3. The installation structure of a line inspection radar according to claim 1, characterized in that: The top of the body is provided with a first thread groove matched with the bolt.
4. The installation structure of a line inspection radar according to claim 1, characterized in that: Guide rods are symmetrically fixedly installed between two sides of the inner wall of the positioning box, and the slide plate is slidably installed on the guide rods.
5. The installation structure of the line inspection radar according to claim 1, characterized in that: The adjustment assembly includes a support frame and a threaded rod. The support frame is fixedly installed between the top of the inner wall of the positioning box and the machine body. The threaded rod is symmetrically and rotatably installed on both sides of the support frame. The slide plate and the insert are threadedly installed on the threaded rod. A driving assembly is installed at one end of the threaded rod.
6. The installation structure of the line inspection radar according to claim 5, characterized in that: The driving assembly includes a first rotating shaft, a second rotating shaft and an elastic telescopic rod. The first rotating shaft is rotatably installed between the two sides of the inner wall of the support frame. Both ends of the first rotating shaft pass through the support frame and are fixedly connected to one end of the adjacent threaded rod. The second rotating shaft is rotatably installed between the inner wall of the positioning box and the machine body. A worm is fixedly installed on the second rotating shaft. A worm wheel is fixedly installed on the first rotating shaft. The worm and the worm wheel are transmission-connected. The elastic telescopic rod is fixedly installed on one end of the first rotating shaft. One end of the elastic telescopic rod passes through the machine body and is fixedly installed on the turntable.
7. The installation structure of the line inspection radar according to claim 6, characterized in that: The elastic telescopic rod includes a sleeve rod, a pull rod and a spring. The sleeve rod is fixedly installed on one end of the second rotating shaft. One end of the sleeve rod slides through the body and slides onto the pull rod. The spring is fixedly installed between the pull rod and the inner wall of the sleeve rod. The turntable is fixedly installed on one end of the pull rod. A slider is symmetrically fixedly installed on the outside of the pull rod. The inner wall of the sleeve rod is provided with a sliding groove matching the slider.
8. The installation structure of the line inspection radar according to claim 7, characterized in that: The bottom end of the machine body is provided with a circular groove matching the turntable, and one side of the turntable is provided with a pull groove, and a pull block is fixedly installed on the inner wall of the pull groove.
9. The installation structure of the line inspection radar according to claim 8, characterized in that: A plurality of limiting bars are fixedly installed on the outer side of the turntable, and the inner wall of the circular groove is provided with strip grooves matching the limiting bars.
10. A drone, characterized in that: It comprises the installation structure of the line inspection radar according to any one of claims 1 to 9 and a drone body.