Wireless data transmitting and receiving device, unmanned aerial vehicle, unmanned aerial vehicle control method, equipment and storage medium

Abstract

The invention discloses a wireless data transmitting and receiving device, an unmanned aerial vehicle, an unmanned aerial vehicle control method, equipment and a storage medium, and relates to the technical field of unmanned aerial vehicle inspection, and the device comprises a piston cylinder, a first annular inflation cushion, a second annular inflation cushion, a cylindrical piston connecting rod and a wireless communication module; the vertical lower end of the cylindrical piston connecting rod is fixedly connected with the wireless communication module, the vertical upper end of the cylindrical piston connecting rod is connected with the piston cylinder in an inserted connection mode, a protruding circular ring is arranged at the middle section position of the vertical upper end of the cylindrical piston connecting rod, and the first annular inflatable cushion is arranged above the protruding circular ring. The second annular inflatable cushion is arranged below the protruding circular ring; the wireless data receiving and transmitting device is connected with the unmanned aerial vehicle body through the piston cylinder. Through the design, the shock resistance and the stability of the wireless data receiving and transmitting device are enhanced, the influence of vibration on signal transmission in the flight process is effectively reduced, and it is ensured that the inspection task of the unmanned aerial vehicle is smoothly carried out in a complex environment.

Description

Technical Field

[0001] The present application relates to the field of drone inspection technology, and more specifically, to a wireless data transceiver, a drone, a drone control method, a device, and a storage medium. Background Art

[0002] With the continuous development of drone technology, drones are increasingly used in various industries, especially in the fields of inspection, monitoring, mapping, etc. As an aerial mobile platform, drones have the advantages of high flexibility and wide coverage of areas, and have gradually become an indispensable and important tool in the modern production process; however, since drones are often affected by environmental factors (such as air vibration, take-off and landing shock, etc.) and the movement of the fuselage itself during flight, the stability of the wireless communication module and the signal transmission quality face severe challenges; especially under high vibration or bad weather conditions, the vibration and shock generated during flight may have an adverse effect on the normal operation of the wireless communication module, resulting in signal transmission interruption, information loss or equipment damage, thereby affecting the execution effect of the drone's inspection mission.

[0003] At present, traditional wireless data transceivers mainly rely on fixed structures to connect to the drone body, lacking effective anti-vibration and buffering designs; these devices are difficult to resist the impact of flight vibrations, wind speed changes, or ground takeoffs and landings during flight, which can easily lead to communication interruptions or equipment damage. In other words, the current drone technology has technical problems such as poor stability and low reliability of wireless data transceivers in complex flight environments. Summary of the invention

[0004] A series of simplified concepts are introduced in the summary of the invention, which will be further described in detail in the detailed description. The summary of the invention of this application does not mean to attempt to define the key features and essential technical features of the technical solution claimed for protection, nor does it mean to attempt to determine the scope of protection of the technical solution claimed for protection.

[0005] The wireless data transceiver device provided in the present application can enhance the shock resistance and stability of the wireless data transceiver device through an inflatable cushion and a flexible connection design, effectively reduce the impact of vibration on signal transmission during flight, and ensure the smooth progress of the drone's inspection mission in complex environments.

[0006] In a first aspect, the present application provides a wireless data transceiver device, which includes: a piston cylinder, a first annular inflatable cushion, a second annular inflatable cushion, a cylindrical piston connecting rod and a wireless communication module; the vertical lower end of the cylindrical piston connecting rod is connected to the wireless communication module by a fixed connection, the vertical upper end of the cylindrical piston connecting rod is connected to the piston cylinder by an insertion connection, a protruding ring is provided at the middle section of the vertical upper end of the cylindrical piston connecting rod, the first annular inflatable cushion is provided above the protruding ring, and the second annular inflatable cushion is provided below the protruding ring; the wireless data transceiver device is connected to the drone fuselage through the piston cylinder.

[0007] In a feasible embodiment, a trapezoidal flange is provided at the upper end of the piston cylinder; the aforementioned wireless data transceiver device is connected to the drone body through the piston cylinder, including: the wireless data transceiver device is connected to the drone body in a snap-fit ​​manner through the trapezoidal flange.

[0008] In a feasible implementation manner, the wireless communication module is in the shape of an elongated strip, and two ends of the wireless communication module are respectively connected to one of the cylindrical piston connecting rods.

[0009] In a feasible implementation manner, the first cylindrical piston connecting rod and the second cylindrical piston connecting rod are connected by a tension bolt, wherein the first cylindrical piston connecting rod and the second cylindrical piston connecting rod are cylindrical piston connecting rods respectively arranged at two ends of the wireless communication module.

[0010] In a feasible embodiment, the first cylindrical piston connecting rod is provided with a first externally threaded screw, and the second cylindrical piston connecting rod is provided with a second externally threaded screw; the tensioning bolt is provided with a first internally threaded through hole and a second internally threaded through hole; the first externally threaded screw is threadedly fastened to the first internally threaded through hole, and the second externally threaded screw is threadedly fastened to the second internally threaded through hole.

[0011] In a feasible implementation manner, both the first externally threaded screw and the second externally threaded screw are configured as hollow tubular structures.

[0012] In a feasible implementation manner, connecting sockets are respectively provided at both ends of the wireless communication module, and the connecting sockets are connected to the cylindrical piston connecting rod by means of threads or snaps.

[0013] In a feasible implementation manner, an annular protrusion is provided inside the piston cylinder, and the annular protrusion is arranged above the first annular inflatable cushion.

[0014] In a feasible implementation manner, a guide groove is provided on the inner wall of the piston cylinder, and a guide protrusion is provided on the outer surface of the cylindrical piston connecting rod, and the guide groove and the guide protrusion cooperate to form a stable connection structure.

[0015] In a second aspect, the present application provides a drone, which is equipped with a wireless data transceiver provided in an embodiment of the present application.

[0016] In a third aspect, the present application provides a drone control method, which is applied to the drone provided in an embodiment of the present application, and the method includes: performing inspection task path planning according to the terrain of the production site and the layout of the production equipment, and obtaining inspection point information and inspection paths; collecting inspection data based on the inspection point positions and the inspection paths, wherein the inspection data includes images, videos and temperature data of the production equipment; transmitting the inspection data to a server through the wireless data transceiver, so that the server generates inspection results based on the inspection data, and pushes alarm information based on the inspection results.

[0017] In a fourth aspect, the present application also provides an electronic device, comprising: a memory and a processor, wherein the processor is used to implement the steps of the drone control method provided in the embodiment of the present application when executing the computer program stored in the memory.

[0018] In a fifth aspect, the present application also provides a computer-readable storage medium storing a computer program, which, when executed by a processor, implements the steps of the drone control method provided in an embodiment of the present application.

[0019] In a sixth aspect, the present application also provides a computer program product, including a computer program or computer executable instructions, which, when executed by a processor, implements the drone control method provided in an embodiment of the present application.

[0020] In summary, the present application uses the first annular inflatable cushion and the second annular inflatable cushion, and effectively fixes them at both ends of the cylindrical piston connecting rod through the protruding ring, which can provide better shock resistance and buffering effect. Especially during the take-off, flight and landing of the drone, the turbulence and vibration of the flight can easily affect the stability of the wireless data transceiver device, which may cause unstable or damaged signal transmission, and the two inflatable cushions can effectively reduce or eliminate the impact and vibration during the flight, and maintain the stable operation of the wireless communication module; the cylindrical piston connecting rod of the wireless data transceiver device is connected to the piston cylinder by an insertion connection method and a fixed connection method, which not only ensures the stable connection between the wireless data transceiver device and the drone body, but also makes the device have a certain flexibility, which can effectively cope with different mechanical impacts during the flight; the wireless communication module is connected to the drone body through the cylindrical piston connecting rod. Since the piston connecting rod itself has a certain elasticity and buffering function, it can effectively reduce the impact of vibration during flight on the wireless communication module, thereby enhancing the stability and transmission quality of the wireless signal, especially in a high vibration environment, signal stability is a key factor to ensure the smooth progress of the drone inspection task. To sum up, the wireless data transceiver device provided in this application enhances the shock resistance and stability of the wireless data transceiver device through an inflatable cushion and a flexible connection design, effectively reduces the impact of vibration on signal transmission during flight, and ensures the smooth progress of the drone's inspection mission in complex environments. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] Various other advantages and benefits will become apparent to those of ordinary skill in the art by reading the detailed description of the preferred embodiments below. The accompanying drawings are only for the purpose of illustrating the preferred embodiments and are not to be considered as limiting the present specification. Also, the same reference symbols are used throughout the accompanying drawings to represent the same components. In the accompanying drawings:

[0022] Figure 1 A schematic diagram of the structure of a wireless data transceiver provided in an embodiment of the present application;

[0023] Figure 2 A flowchart of a drone control method provided in an embodiment of the present application;

[0024] Figure 3 A schematic diagram of the structure of an electronic device provided in an embodiment of the present application.

[0025] In the figure, 1 is the first annular inflatable cushion; 2 is the second annular inflatable cushion; 3 is the cylindrical piston connecting rod; 4 is the wireless communication module; 6 is the piston cylinder; 6-1 and 6-2 are trapezoidal flanges; 8 is the tensioning bolt; 8-1 and 8-2 are the first internal threaded through hole and the second internal threaded through hole respectively; 8-3 and 8-4 are the first external threaded screw and the second external threaded screw respectively. DETAILED DESCRIPTION

[0026] Terms in the specification, claims and drawings of this application, such as "first", "second", "third", "fourth", etc. (if any), are used to distinguish similar objects rather than to describe a specific order or sequence. Therefore, it is understood that these terms can be used interchangeably where appropriate, so that the described embodiments can be implemented in a different order unless otherwise specified in the diagram or description. In addition, the terms "is" and "has" and any variations thereof in this application are intended to cover all possible constituent elements on a non-exclusive basis. For example, a process, method, system, product or device comprising a number of steps or units is not necessarily limited to the steps or units that are explicitly listed, but may also include other steps or units that are not explicitly listed, or steps or units that are inherent to the process, method, product or device.

[0027] In this application, a "module" or "unit" refers to a computer program or a part of a computer program that has a specific function and works in conjunction with other related parts to achieve a predetermined goal. These modules or units can be implemented by software, hardware (such as processing circuits or memories), or a combination of the two. One or more processors or memories can implement one or more modules or units. At the same time, each module or unit can also be a part of a larger module or unit.

[0028] The technical solutions in the present application will be described in detail below in conjunction with the drawings in the embodiments. It should be noted that the described embodiments are only a part of the present application, not all embodiments. In the following description, the "some embodiments" mentioned are only subsets of all possible embodiments, which may be the same or different subsets, and different embodiments may be combined with each other without conflict.

[0029] See also Figure 1 , Figure 1 It is a structural schematic diagram of a wireless data transceiver provided in an embodiment of the present application, the wireless data transceiver includes a piston cylinder 6, a first annular inflatable cushion 1, a second annular inflatable cushion 2, a cylindrical piston connecting rod 3 and a wireless communication module 4; the vertical lower end of the cylindrical piston connecting rod 3 is connected to the wireless communication module 4 by a fixed connection, the vertical upper end of the cylindrical piston connecting rod 3 is connected to the piston cylinder 6 by an insertion connection, a protruding ring is provided at the middle section of the vertical upper end of the cylindrical piston connecting rod 3, the first annular inflatable cushion 1 is provided above the protruding ring, and the second annular inflatable cushion 2 is provided below the protruding ring; the wireless data transceiver is connected to the drone fuselage through the piston cylinder 6.

[0030] Specifically, the piston cylinder 6 is a cylindrical / tubular component, which serves as a shell for accommodating the piston and other moving components, and has sufficient space inside to accommodate moving parts, such as a piston connecting rod; the piston cylinder 6 can be made of high-strength aluminum alloy, steel or engineering plastics to ensure its strength, durability and lightness, and the inside can have a certain surface treatment or coating to reduce wear and friction. The first annular inflatable cushion 1 is an annular inflatable cushion located above the protruding ring at the middle position (not at the two ends) of the cylindrical piston connecting rod 3. Its main function is to generate elastic support through inflation, reduce the impact of vibration and impact on the wireless communication module 4 during flight, and provide a buffering effect; the second annular inflatable cushion 2 is an annular inflatable cushion located below the protruding ring, and its function is the same as that of the first annular inflatable cushion 1, further strengthening the vibration absorption function to ensure that vibration and impact are effectively alleviated during flight; the material of the annular inflatable cushion can include rubber, silicone or synthetic polymer, etc., with good elasticity, wear resistance and anti-aging properties, and there is an air bag inside, which can be inflated or deflated to adjust the buffering effect. The cylindrical piston connecting rod 3 is a component connecting the wireless communication module 4 and the piston cylinder 6. It transmits motion through the piston cylinder 6 and ensures that the wireless communication module 4 is stably connected to the UAV fuselage. Its upper and lower ends are respectively connected to the piston cylinder 6 and the wireless communication module 4, which play a supporting and fixing role. The protruding ring is set at the middle position of the vertical upper end of the cylindrical piston connecting rod 3. It is mainly used to support the first annular inflatable cushion 1 and the second annular inflatable cushion 2 to ensure that these cushions will not be displaced due to external pressure and provide a stable supporting effect. The wireless communication module 4 is responsible for transmitting data between the UAV and the background control system (such as a cloud server) and is the core part of the wireless data transceiver device; a lightweight metal (such as aluminum alloy) or plastic shell can be used to facilitate heat dissipation and reduce weight. The wireless communication module 4 can integrate electronic components such as antennas, circuit boards, and wireless chips inside, and the outside is designed to be connected to the piston connecting rod.

[0031] The fixed connection method refers to that the vertical lower end of the cylindrical piston connecting rod 3 and the wireless communication module 4 are firmly connected and cannot be easily separated through some mechanical method. This mechanical method may include welding, threaded connection, nailing and bonding, etc. The purpose is to ensure that the wireless communication module 4 is firmly fixed to the lower end of the piston connecting rod, and to ensure that the two can be stably matched during operation without displacement or looseness.

[0032] The insertion connection method refers to inserting the vertical upper end of the cylindrical piston connecting rod 3 into the interior of the piston cylinder 6, forming a connection method achieved by insertion. The connection after insertion can be physically fixed by relying on the protruding ring of the cylindrical piston connecting rod 3 and the matching surface (lower annular packaging surface) of the piston cylinder 6. No additional fasteners are required, and it has a certain flexibility during assembly, which facilitates the installation and disassembly of the components.

[0033] In summary, the embodiment of the present application uses the first annular inflatable cushion 1 and the second annular inflatable cushion 2, and effectively fixes them at both ends of the cylindrical piston connecting rod 3 through the protruding ring, which can provide better shock resistance and buffering effect. Especially during the take-off, flight and landing of the drone, the turbulence and vibration of the flight are likely to affect the stability of the wireless data transceiver device, which may cause unstable or damaged signal transmission, and the two inflatable cushions can effectively reduce or eliminate the impact and vibration during the flight, and maintain the stable operation of the wireless communication module 4; the cylindrical piston connecting rod 3 of the wireless data transceiver device is connected to the piston cylinder 6 by an insertion connection method and a fixed connection method, which not only ensures the stable connection between the wireless data transceiver device and the drone fuselage, but also makes the device have a certain flexibility, which can effectively cope with different mechanical impacts during the flight; the wireless communication module 4 is connected to the drone fuselage through the cylindrical piston connecting rod 3. Since the piston connecting rod itself has a certain elasticity and buffering function, it can effectively reduce the impact of vibration during flight on the wireless communication module 4, thereby enhancing the stability and transmission quality of the wireless signal, especially in a high vibration environment, signal stability is a key factor to ensure the smooth progress of the drone inspection task. To sum up, the wireless data transceiver device provided in the embodiment of the present application enhances the shock resistance and stability of the wireless data transceiver device through an inflatable cushion and a flexible connection design, effectively reduces the impact of vibration on signal transmission during flight, and ensures the smooth progress of the drone's inspection mission in a complex environment.

[0034] In some embodiments, a trapezoidal flange (6-1 and 6-2) is provided at the upper end of the piston cylinder 6; the aforementioned wireless data transceiver is connected to the drone body through the piston cylinder 6, including: the wireless data transceiver is connected to the drone body through the trapezoidal flange (6-1 and 6-2) in a snap-fit ​​manner.

[0035] Specifically, the trapezoidal flanges (6-1 and 6-2) are usually used to provide a connection surface to ensure that the wireless data transceiver connected to the piston cylinder 6 can be firmly connected to the drone fuselage through a snap connection; the shape of the trapezoidal flanges (6-1 and 6-2) is similar to a trapezoid, that is, the upper end is wide and the lower end is narrow, and the shape is a trapezoidal structure, so that the snap or connector can be firmly buckled and not easy to fall off.

[0036] Through the implementation of the above-mentioned embodiment, by setting a trapezoidal flange (6-1 and 6-2) on the upper end of the piston cylinder 6 and connecting the wireless data transceiver device to the drone fuselage by snap-fitting, the installation process is simplified, which not only ensures the stability of the device during flight, but also makes the installation and disassembly of the device more convenient, thereby improving the flexibility and efficiency of maintenance.

[0037] In some embodiments, the wireless communication module 4 is in the shape of a long strip, and two ends of the wireless communication module 4 are respectively connected to a cylindrical piston connecting rod 3 .

[0038] Specifically, the wireless communication module 4 is designed to be long and narrow, and is connected to the cylindrical piston connecting rod 3 at both ends, thereby optimizing the structure of the device and making the connection between the wireless communication module 4 and the piston connecting rod more compact and stable, which can effectively improve the overall stability and shock resistance of the entire device, increase the reliability of the connection between the wireless communication module 4 and the fuselage, and reduce the impact of vibration on signal transmission.

[0039] In some embodiments, the first cylindrical piston connecting rod and the second cylindrical piston connecting rod are connected by a tension bolt 8 , wherein the first cylindrical piston connecting rod and the second cylindrical piston connecting rod are cylindrical piston connecting rods 3 respectively disposed at two ends of the wireless communication module 4 .

[0040] Specifically, the first cylindrical piston connecting rod and the second cylindrical piston connecting rod are connected by the tensioning bolt 8, so that the piston connecting rods at both ends are more tightly fixed to the two ends of the wireless communication module 4. At the same time, the trapezoidal flanges (6-1 and 6-2) are more firmly combined with the drone, which can further enhance the stability of the wireless communication module 4, avoid loosening or displacement caused by vibration or other factors, and improve the reliability of the device in complex flight environments.

[0041] In some embodiments, the first cylindrical piston connecting rod is provided with a first externally threaded screw, and the second cylindrical piston connecting rod is provided with a second externally threaded screw; the tensioning bolt 8 is provided with a first internally threaded through hole 8-1 and a second internally threaded through hole 8-2; the first externally threaded screw 8-3 is threadedly fastened to the first internally threaded through hole 8-1, and the second externally threaded screw 8-4 is threadedly fastened to the second internally threaded through hole 8-2.

[0042] Specifically, by providing an externally threaded screw and an internally threaded through hole, the first cylindrical piston connecting rod and the second cylindrical piston connecting rod are tightly connected, thereby improving the connection strength of the device, ensuring the stability of the wireless data transceiver device in high load and vibration environments, and avoiding communication interruption or signal instability caused by looseness of the device.

[0043] In some embodiments, the first externally threaded screw 8 - 3 and the second externally threaded screw 8 - 4 are both configured as hollow tubular structures.

[0044] Specifically, by designing the first externally threaded screw 8-3 and the second externally threaded screw 8-4 as a hollow tubular structure, not only the weight of the device is reduced, but also its seismic resistance can be further improved, which helps to reduce the weight of the device and improve the flight efficiency of the UAV. At the same time, it also reduces the physical impact that the device may be subjected to during flight, further ensuring the stability of the wireless communication module 4.

[0045] In some embodiments, two ends of the wireless communication module 4 are respectively provided with connection sockets, and the connection sockets are connected to the cylindrical piston connecting rod 3 by means of threads or snap-fits.

[0046] Specifically, by providing connecting sockets at both ends of the wireless communication module 4 and connecting them to the cylindrical piston connecting rod 3 by means of threads or snap-fits, a simpler and more secure connection method is provided, which can make the connection between the wireless communication module 4 and the piston connecting rod more stable, while improving the shock resistance of the device, helping to ensure the reliable transmission of wireless signals.

[0047] In some embodiments, an annular protrusion is provided inside the piston cylinder 6 , and the annular protrusion is arranged above the first annular inflatable cushion 1 .

[0048] Specifically, by providing an annular protrusion inside the piston cylinder 6 and positioning it above the first annular inflatable cushion 1, the fixation and stability of the inflatable cushion can be further enhanced to prevent displacement or damage during flight, thereby improving the overall shock resistance of the wireless data transceiver device, helping to better absorb vibrations during flight, and improving the stable working performance of the wireless communication module 4.

[0049] In some embodiments, a guide groove is disposed on the inner wall of the piston cylinder 6, and a guide protrusion is disposed on the outer surface of the cylindrical piston connecting rod 3, and the guide groove and the guide protrusion cooperate to form a stable connection structure.

[0050] Specifically, a guide groove is provided on the inner wall of the piston cylinder 6, and the outer surface of the cylindrical piston connecting rod 3 cooperates therewith to form a stable connection structure. Through this guide design, the displacement or instability of the device due to vibration during flight can be further reduced, ensuring that the wireless communication module 4 can still maintain stable operation in a high vibration environment, thereby improving the reliability and stability of data transmission.

[0051] The present application also provides a drone, which is equipped with the wireless data transceiver provided in the embodiments of the present application.

[0052] Specifically, applying the wireless data transceiver provided in the embodiment of the present application to a drone can enable the drone to transmit data more stably when performing inspection tasks; the anti-vibration and buffering characteristics of the wireless data transceiver effectively reduce the interference to the communication signal during the flight, ensuring that the drone can perform tasks in complex environments, and improving the performance of the drone in industrial and commercial applications.

[0053] The present application also provides a drone control method, which is applied to the drone provided in the embodiment of the present application, see Figure 2 , Figure 21 is a flow chart of a method for controlling a drone provided in an embodiment of the present application. The method may specifically include the following steps 101 to 103:

[0054] Step 101, perform inspection task path planning according to the terrain of the production site and the layout of the production equipment, and obtain inspection point information and inspection path;

[0055] In this step, you first need to have a detailed understanding of the terrain of the production site and the layout of the production equipment; by using the drone management platform software to perform 3D modeling of the site, you can generate a virtual model of the production site, and perform path planning on this basis; the purpose of path planning is to ensure that the drone can complete the inspection task safely and efficiently, and avoid possible obstacles in the site.

[0056] Specifically, drones can be used to take panoramic photos of the site at different angles and heights to obtain detailed image data including equipment, pipelines, buildings, etc. After these data are imported into the modeling software, a 3D model of the production environment is generated; during the modeling process, the distribution of production equipment and pipelines, obstacles on the site, and the distribution of inspection points can be analyzed to ensure the accuracy of the modeling. Then, according to the production process requirements and the operating status of the equipment, the equipment that needs to be inspected regularly is selected, and the number, location, frequency and time of the inspection points are determined according to the requirements of the task; for example, the inspection points may include motors, pipelines, temperature control equipment, etc. Once the inspection point information (the number and location of inspection points, and the inspection frequency and time for each inspection point) is determined, the next step is to optimize the inspection path. Path planning can generate the inspection flight path of the drone based on the spatial coordinates of each inspection point (inspection point location) and other inspection point information, using the Dijkstra algorithm (shortest path algorithm) and particle swarm optimization algorithm (PSO), combined with factors such as obstacle avoidance, flight distance and flight time. At the same time, considering efficient energy use, the path needs to be optimized to save battery energy and avoid unnecessary flights. Through algorithm calculation, the flight route of the drone is automatically generated and optimized to ensure that the path is safe and efficient during inspections, avoiding collisions with obstacles or unnecessary energy waste.

[0057] The goal of this step is to ensure that the drone can accurately perform tasks according to the set inspection points, thereby achieving the goals of efficient inspection and energy optimization.

[0058] Step 102, collecting inspection data based on the inspection point information and the inspection path, wherein the inspection data includes images, videos and temperature data of the production equipment;

[0059] In this step, the drone will automatically perform flight missions and collect relevant data according to the preset inspection routes and inspection tasks.

[0060] Specifically, the drone will first take off automatically according to the path planning and fly along the optimized inspection path. During the flight, the drone needs to ensure that it reaches each inspection point accurately. During the flight, the flight control system will adjust the flight attitude in real time to avoid affecting the completion of the inspection task due to environmental changes or obstacles. Then, the visible light camera and infrared thermal imaging equipment installed on the drone will collect image and video data in real time near the inspection point. The visible light camera is mainly used to shoot the appearance of the equipment and check whether there are cracks, stains or other abnormal conditions on the surface of the equipment. The infrared thermal imaging equipment is used to detect the temperature distribution of the equipment and find hidden dangers such as overheating and abnormal temperature. The drone uses infrared thermal imaging equipment during the inspection process to monitor the temperature of key equipment in real time; for example, the temperature data of equipment such as motors, pipelines, and storage tanks can help determine whether they are operating normally; by comparing the normal operating temperature of the equipment with the current temperature data, potential equipment failures can be discovered in time, such as motor overheating, pipeline leakage, etc. All collected data will be transmitted to the storage device in the drone in real time, and marked with the corresponding time, location and equipment information to ensure that each piece of data has a detailed record. The spatial coordinates of the inspection point and related images, videos, and temperature data are stored synchronously for subsequent analysis and processing.

[0061] The goal of this step is to ensure the comprehensiveness and accuracy of data collection, record the equipment status of each inspection point as detailed as possible, and provide a basis for subsequent analysis.

[0062] Step 103, the inspection data is transmitted to the server through the wireless data transceiver, so that the server generates inspection results according to the inspection data, and pushes alarm information according to the inspection results.

[0063] In this step, the inspection data needs to be uploaded to the server via wireless data transmission equipment for subsequent analysis, processing and alarm push.

[0064] Specifically, the real-time transmission of inspection data is the key; the drone transmits the collected images, videos and temperature data to the ground station (airport) through a wireless data transceiver. This process relies on a wireless network connection to ensure that the data is not interrupted during the flight; the data can be transmitted to the ground station through point-to-point wireless communication, and then the data is transmitted to the central server system through a wired network. After the server receives the data, it will use special data analysis and processing software for processing. The data analysis software may include an AI recognition module that can analyze images, videos and infrared thermal imaging data to identify the operating status of process equipment; by comparing with normal process parameters, analyze whether the equipment has abnormalities, such as whether the motor is overheated, whether the pipeline is leaking, and whether the equipment is operating normally. Based on the results of data analysis, the server will automatically generate an inspection report to show the health status of the equipment; if the analysis results show abnormalities, such as excessive equipment temperature, water leakage, equipment position offset, etc., the alarm mechanism will be triggered, and the alarm information will be pushed to the relevant management personnel in real time. The push method can be SMS, email or through a dedicated management platform. The push of alarm information is a key component of the entire inspection system. Through Internet technology, alarm information will be pushed to the mobile phones or tablets of relevant managers in real time, so that managers can immediately know the operating status of the equipment and quickly take necessary maintenance measures.

[0065] The goal of this step is to ensure that the collected inspection data can be transmitted to the server quickly and stably, generate accurate inspection results through data analysis, and push alarm information in a timely manner to ensure the safe operation of the equipment.

[0066] Through the implementation of the above three steps, the entire inspection process realizes functions such as drone automated flight, real-time data collection, data transmission and intelligent analysis, and abnormal alarm push. It not only improves the inspection efficiency, but also can monitor the operating status of the equipment in real time, discover potential equipment failures in advance, and ensure the safety and stability of the production process.

[0067] The present application also provides a computer-readable storage medium, which stores computer-executable instructions or computer programs. When the computer-executable instructions or computer programs are executed by a processor, the processor will be caused to execute any step of the drone control method provided in the present application.

[0068] In some embodiments, the computer-readable storage medium may be a memory such as RAM, read-only memory (ROM), flash memory, magnetic surface memory, optical disk, or compact disc read-only memory (CD-ROM); or it may be various devices including one or any combination of the above memories.

[0069] In some embodiments, computer executable instructions may be in the form of a program, software, software module, script or code, written in any form of programming language (including compiled or interpreted languages, or declarative or procedural languages), and may be deployed in any form, including as a stand-alone program or as a module, component, subroutine or other unit suitable for use in a computing environment.

[0070] In some embodiments, computer-executable instructions may, but need not, correspond to a file in a file system, may be stored as part of a file storing other programs or data, for example, in one or more scripts in a HyperText Markup Language (HTML) document, in a single file dedicated to the program in question, or in multiple coordinated files (e.g., files storing one or more modules, subroutines, or code portions).

[0071] In some embodiments, computer executable instructions may be deployed to be executed on one electronic device, or on multiple electronic devices located at one site, or on multiple electronic devices distributed at multiple sites and interconnected by a communication network.

[0072] like Figure 3 As shown, the present application also provides an electronic device 30, including a memory 310, a processor 320, and a computer program 311 stored in the memory 310 and executable on the processor, and when the processor 320 executes the computer program 311, any step of the above-mentioned drone control method is implemented.

[0073] The present application also provides a computer program product, which includes a computer program or a computer executable instruction, and the computer program or the computer executable instruction is stored in a computer readable storage medium. The processor of the electronic device reads the computer program or the computer executable instruction from the computer readable storage medium, and the processor executes the computer program or the computer executable instruction, so that the electronic device performs any step of the drone control method described above in the present application.

[0074] The above embodiments are only used to illustrate the technical solutions of the present application, rather than to limit them. Although the present application has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that they can still modify the technical solutions described in the aforementioned embodiments, or make equivalent replacements for some of the technical features therein. However, these modifications or replacements do not deviate the essence of the corresponding technical solutions from the spirit and scope of the technical solutions of the embodiments of the present application.

Claims

1. A wireless data transceiver, characterized in that: The wireless data transceiver device comprises: a piston cylinder, a first annular inflatable cushion, a second annular inflatable cushion, a cylindrical piston connecting rod and a wireless communication module; The vertical lower end of the cylindrical piston connecting rod is connected to the wireless communication module by a fixed connection, the vertical upper end of the cylindrical piston connecting rod is connected to the piston cylinder by an insertion connection, a protruding ring is provided at the middle section of the vertical upper end of the cylindrical piston connecting rod, the first annular inflatable cushion is provided above the protruding ring, and the second annular inflatable cushion is provided below the protruding ring; The wireless data transceiver is connected to the UAV fuselage through the piston cylinder.

2. The wireless data transceiver device according to claim 1, characterized in that: The upper end of the piston cylinder is provided with a trapezoidal flange; The wireless data transceiver is connected to the drone body through the piston cylinder, and includes: The wireless data transceiver is connected to the UAV fuselage in a snap-fit ​​manner via the trapezoidal flange.

3. The wireless data transceiver device according to claim 1, characterized in that: The wireless communication module is in the shape of an elongated strip, and two ends of the wireless communication module are respectively connected to one of the cylindrical piston connecting rods.

4. The wireless data transceiver device according to claim 3, characterized in that: The first cylindrical piston connecting rod and the second cylindrical piston connecting rod are connected by a tension bolt, wherein the first cylindrical piston connecting rod and the second cylindrical piston connecting rod are cylindrical piston connecting rods respectively arranged at two ends of the wireless communication module.

5. The wireless data transceiver device according to claim 4, characterized in that: The first cylindrical piston connecting rod is provided with a first externally threaded screw rod, and the second cylindrical piston connecting rod is provided with a second externally threaded screw rod; the tensioning bolt is provided with a first internally threaded through hole and a second internally threaded through hole; the first externally threaded screw rod is threadedly fastened to the first internally threaded through hole, and the second externally threaded screw rod is threadedly fastened to the second internally threaded through hole.

6. The wireless data transceiver device according to claim 5, characterized in that: The first externally threaded screw and the second externally threaded screw are both configured as hollow tubular structures.

7. A drone, characterized in that: A wireless data transceiver as described in any one of claims 1 to 6 is installed.

8. A method for controlling a drone, characterized in that: Applied to the drone according to claim 7, the drone control method comprises: According to the terrain of the production site and the layout of production equipment, the inspection task path is planned to obtain the inspection point information and inspection path; Collecting inspection data based on the inspection point location and the inspection path, wherein the inspection data includes images, videos and temperature data of the production equipment; The inspection data is transmitted to the server through the wireless data transceiver, so that the server generates inspection results according to the inspection data and pushes alarm information according to the inspection results.

9. An electronic device, comprising: A memory and a processor, wherein the processor is used to implement the steps of the drone control method as claimed in claim 8 when executing the computer program stored in the memory.

10. A computer-readable storage medium having a computer program stored thereon, characterized in that: When the computer program is executed by a processor, the steps of the drone control method according to claim 8 are implemented.

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