Collecting tube vacuum degree detection system, detection control method thereof, electronic device and storage medium

Abstract

This application discloses a vacuum degree detection system for solar collector tubes, its detection and control method, electronic equipment, and storage medium. The system is used to detect the vacuum degree of high-temperature solar collector tubes in a linear concentrated solar power (CSP) system in real time. Specifically, it includes a flight vehicle and a temperature detection device mounted on the flight vehicle, as well as a data processing device wirelessly connected to the temperature detection device. The flight vehicle moves within the collector tube array of the CSP system according to a preset pattern, sequentially orienting the temperature detection device toward the target collector tube. The temperature detection device collects a first temperature value of the glass tube of the target collector tube and a second temperature value of the inner metal tube. The data processing device calculates the vacuum degree of the target collector tube based on a predetermined algorithm using the first and second temperature values. By sequentially obtaining the vacuum degree of each collector tube, users can identify collector tubes with substandard vacuum degrees and take appropriate measures, such as repair or replacement, thereby preventing significant heat loss to the system due to vacuum reduction.

Description

Technical Field

[0001] This application relates to the field of new energy technology, and more specifically, to a vacuum detection system for a solar collector tube, a detection and control method thereof, electronic equipment and storage medium. Background Technology

[0002] High-temperature solar collector tubes are the core components of linear concentrated solar thermal power (CSP) systems, converting solar energy into heat. Their vacuum performance significantly impacts the thermal efficiency and economic viability of the system. A high-temperature solar collector tube consists of a metal inner tube with a selective absorption film and a glass tube coaxially surrounding it. The annular space between the glass tube and the metal inner tube is evacuated to create a vacuum zone. This vacuum process reduces heat loss by weakening convective heat transfer within the space and also protects the selective absorption film from oxidation.

[0003] Vacuum failure in high-temperature solar collector tubes has always been a major problem in linear concentrated solar thermal power generation systems. According to the heat loss mechanism of the collector tube, heat loss mainly originates from radiative heat loss through the selective absorption film of the inner metal tube and convective heat loss in the annular space. Once the vacuum in the annular space of the high-temperature solar collector tube fails, heat loss increases significantly, and the selective absorption film of the inner metal tube also degrades due to high-temperature oxidation, resulting in a significant reduction in the thermal efficiency of the collector tube. In particular, in recent years, it has been discovered that during operation, hydrogen gas generated from the decomposition of the heat transfer oil within the collector tube can permeate into the annular space, leading to a decrease in vacuum and a sharp increase in heat loss, resulting in "collector tube overheating." This overheating phenomenon exceeds four times that of collector tubes with intact vacuum performance, ultimately causing the system to lose more than 20% of its revenue annually, resulting in significant economic losses. Therefore, it is necessary to effectively monitor the vacuum status of the annular space within the tube so that timely measures can be taken when a decrease in vacuum occurs to avoid significant heat loss to the system. Summary of the Invention

[0004] In view of this, this application provides a vacuum degree detection system for solar collector tubes and its detection and control method, device, electronic equipment and storage medium, for real-time detection of the vacuum degree of high-temperature solar collector tubes in linear concentrating solar thermal power generation systems, so as to avoid the large heat loss of the system caused by the decrease in vacuum degree.

[0005] To achieve the above objectives, the following solution is proposed:

[0006] A vacuum detection system for solar collector tubes is provided for real-time detection of the vacuum level of high-temperature solar collector tubes in a linear concentrating solar thermal power generation system. The system includes a flight vehicle and a temperature detection device mounted on the flight vehicle, and further includes a data processing device wirelessly connected to the temperature detection device.

[0007] The flight vehicle is used to move in the collector tube array of the linear concentrated solar power generation system according to a preset pattern, and to make the temperature detection device sequentially face the target collector tubes selected sequentially from the collector tube array;

[0008] The temperature detection device is used to collect the temperature of the glass tube of the target heat collector tube to obtain a first temperature value, and is also used to collect the temperature of the metal inner tube of the target heat collector tube to obtain a second temperature value.

[0009] The data processing device is used to calculate the first temperature value and the second temperature value based on a predetermined algorithm to obtain the vacuum degree of the target heat collection tube.

[0010] Optionally, the flight vehicle is equipped with a satellite positioning module, which is used to provide positioning signals for the flight control of the flight vehicle.

[0011] Optionally, the temperature detection device includes a first temperature sensor for detecting the temperature of the glass tube and a second temperature sensor for detecting the temperature of the inner metal tube.

[0012] Optionally, the first temperature sensor is an infrared thermal imager.

[0013] Optionally, the second temperature sensor is a low-emissivity infrared thermometer.

[0014] A detection and control method, applied to the vacuum detection system for solar collector tubes as described above, the detection and control method comprising the following steps:

[0015] The target solar collector tubes are selected in sequence, and the flight vehicle is hovered above the target solar collector tubes.

[0016] The first and second temperature values ​​of the target solar collector tube are collected using a temperature detection device.

[0017] The vacuum degree of the target heat collector tube is obtained by calculating the first temperature value and the second temperature value using a preset algorithm.

[0018] Optionally, the step of using a temperature detection device to collect the first and second temperature values ​​of the target heat collector tube includes the following steps:

[0019] The flight vehicle is controlled to hover directly above the target heat collection tube, and the temperature of the glass tube is detected based on an infrared thermal imager to obtain the first temperature value;

[0020] The flight vehicle is controlled to hover directly above the target heat collection tube, and the lens of the low emissivity infrared thermometer is controlled to maintain a distance of 0.1 to 1 m from the glass tube. The low emissivity infrared thermometer is then controlled to collect temperature data from the inner metal tube to obtain the second temperature value.

[0021] Optionally, the vacuum degree of the target heat collector tube is obtained by calculating the first temperature value and the second temperature value using a preset algorithm, including the following steps:

[0022] The vacuum level is obtained by looking up the temperature-vacuum level MAP based on the first temperature value and the second temperature value.

[0023] Alternatively, the vacuum level can be obtained by calculating the first temperature value and the second temperature value based on a pre-trained neural network model.

[0024] An electronic device includes at least one processor and a memory connected to the processor, wherein:

[0025] The memory is used to store computer programs or instructions;

[0026] The processor is used to execute the computer program or instructions to enable the electronic device to implement the detection and control method described above.

[0027] A computer-readable storage medium is applied to an electronic device, the storage medium carrying one or more computer programs that can be executed by the electronic device, thereby enabling the electronic device to implement the detection and control method described above.

[0028] As can be seen from the above technical solution, this application discloses a vacuum degree detection system for solar collector tubes, its detection and control method, electronic equipment, and storage medium. This system is used to detect the vacuum degree of high-temperature solar collector tubes in a linear concentrated solar power (CSP) system in real time. Specifically, it includes a flight vehicle and a temperature detection device mounted on the flight vehicle, as well as a data processing device wirelessly connected to the temperature detection device. The flight vehicle moves within the collector tube array of the CSP system according to a preset pattern, and sequentially orients the temperature detection device toward the target collector tube. The temperature detection device collects a first temperature value of the glass tube of the target collector tube and a second temperature value of the inner metal tube of the target collector tube. The data processing device calculates the vacuum degree of the target collector tube based on a predetermined algorithm using the first and second temperature values. By sequentially obtaining the vacuum degree of each collector tube, users can identify collector tubes with substandard vacuum degrees and take appropriate measures, such as repair or replacement, thereby preventing significant heat loss to the system due to a decrease in vacuum degree. Attached Figure Description

[0029] To more clearly illustrate the technical solutions in the embodiments of this application or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this application. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0030] Figure 1 This is a schematic diagram of a vacuum detection system for a solar collector tube according to an embodiment of this application;

[0031] Figure 2 This is a flowchart of a detection control method according to an embodiment of this application;

[0032] Figure 3 This is a block diagram of an electronic device according to an embodiment of this application. Detailed Implementation

[0033] The technical solutions of the embodiments of this application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this application, and not all embodiments. Based on the embodiments of this application, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the scope of protection of this application.

[0034] Figure 1 This is a schematic diagram of a vacuum detection system for a solar collector tube according to an embodiment of this application.

[0035] like Figure 1 As shown, the vacuum detection system for solar collector tubes in this embodiment is used to detect the vacuum level of high-temperature solar collector tubes in a linear concentrating solar power generation system. The system includes a flight vehicle 1 and a temperature detection device mounted on the flight vehicle, as well as a data processing device 5 wirelessly connected to the temperature detection device. The flight vehicle can be a general-purpose quadcopter drone or a specially designed hovering or stretching vehicle that operates in other ways.

[0036] The linear concentrating solar power system includes at least one array of solar collectors, consisting of multiple high-temperature solar collectors 6 arranged in an array. During testing, the flight vehicle flies over each high-temperature solar collector according to a predetermined procedure or pattern and hovers above a selected target collector, with the temperature detection device facing the target collector. During hovering, the temperature detection device detects the temperature of the glass tube 7 and the temperature of the inner metal tube 8 of the selected target collector, obtaining a first temperature value reflecting the glass tube temperature and a second temperature value reflecting the inner metal tube temperature. After obtaining the first and second temperature values, the temperature detection device transmits them to a data processing device.

[0037] The temperature detection device includes a first temperature sensor 2 for acquiring a first temperature value and a second temperature sensor 3 for acquiring a second temperature value. The first temperature sensor is an infrared thermal imager with a wavelength range of 8–14 μm, used to acquire the overall temperature of the glass tube. The second temperature sensor is a low-emissivity infrared thermometer with a wavelength range of 1–5 μm. When acquiring the second temperature value, the distance between the lens of the infrared thermometer and the high-temperature solar collector tube is controlled to be 0.1–1 m, and the temperature at the center of the inner metal tube is acquired during the acquisition process.

[0038] The data processing device is used to calculate and process the first and second temperature values ​​based on a preset algorithm to obtain the vacuum degree of the high-temperature solar collector tube. The preset algorithm can either look up the vacuum degree from a temperature-vacuum MAP based on the first and second temperature values, or it can calculate the vacuum degree based on a pre-trained neural network model. The temperature-vacuum MAP is obtained by calibrating a standard collector tube; the neural network model is obtained by measuring the standard collector tube under different temperature and vacuum conditions to obtain training samples, and then training the constructed neural network based on the training samples.

[0039] In addition, the flight vehicle in this application is also equipped with a satellite positioning module 4, which is used to provide positioning signals to the flight vehicle so that the flight vehicle can obtain position information based on the positioning signals, and collect the temperature of each collector in the collector array in sequence based on the position information and the patrol plan.

[0040] As can be seen from the above technical solution, this embodiment provides a vacuum degree detection system for solar collector tubes. This system is used to detect the vacuum degree of high-temperature solar collector tubes in a linear concentrating solar thermal power generation system in real time. Specifically, it includes a flight vehicle and a temperature detection device mounted on the flight vehicle, as well as a data processing device wirelessly connected to the temperature detection device. The flight vehicle moves within the solar collector tube array of the linear concentrating solar power generation system according to a preset pattern, and sequentially orients the temperature detection device toward the target solar collector tube. The temperature detection device collects a first temperature value of the glass tube of the target solar collector tube and a second temperature value of the inner metal tube of the target solar collector tube. The data processing device calculates the vacuum degree of the target solar collector tube based on a predetermined algorithm using the first and second temperature values. By sequentially obtaining the vacuum degree of each solar collector tube, users can identify solar collector tubes with substandard vacuum degrees and take appropriate measures, such as repair or replacement, thereby avoiding significant heat loss to the system due to a decrease in vacuum degree.

[0041] Figure 2This is a flowchart of a detection control method according to an embodiment of this application.

[0042] like Figure 2 As shown, the detection and control method of this embodiment is applied to the vacuum degree detection system of the high-temperature solar collector tube of the linear concentrating solar power generation system in the previous embodiment to detect the vacuum degree, and is used to control the vacuum degree detection system to detect the collector tube in order to obtain the vacuum degree. The detection and control method specifically includes the following steps:

[0043] S1. Select the target heat collection tubes in sequence and hover the flight vehicle above the target heat collection tubes.

[0044] This involves sequentially selecting one high-temperature solar collector from among multiple high-temperature solar collectors in the collector array, designating it as the target collector. After selecting the target collector, the flight vehicle is controlled to hover directly above it, and the lens or detection element of the temperature detection device is directed towards the target collector. Given that the temperature detection device includes an infrared thermal imager and a low-reflectivity infrared thermometer, the infrared thermal imager is directed towards the glass tube of the target collector, and the lens of the low-reflectivity infrared thermometer is directed towards the inner metal tube.

[0045] S2. Use a temperature detection device to collect the first and second temperature values ​​of the target heat collector tube.

[0046] During the specific data acquisition process, the flight vehicle is controlled to hover directly above the target heat collection tube, and the temperature of the glass tube is detected based on the infrared thermal imager to obtain a first temperature value; simultaneously or subsequently, the flight vehicle is controlled to hover directly above the target heat collection tube, and the lens of the low emissivity infrared thermometer is controlled to maintain a distance of 0.1 to 1 m from the glass tube, and the low emissivity infrared thermometer is directed towards the inner metal tube to collect the temperature, thereby obtaining a second temperature value.

[0047] S3. Process the first and second temperature values ​​to obtain the vacuum degree.

[0048] The system uses a preset algorithm to calculate the vacuum level of the target solar collector tube based on the first and second temperature values. After completing the calculation for the current collector tube, the system controls the flight vehicle to fly to the next high-temperature solar collector tube, using it as the next target collector tube for temperature acquisition and vacuum level calculation.

[0049] The preset algorithm here can either look up the vacuum level from the temperature-vacuum MAP based on the first and second temperature values, or it can calculate the vacuum level based on the first and second temperature values ​​using a pre-trained neural network model. The temperature-vacuum MAP is obtained by calibrating a standard solar collector tube; the neural network model is obtained by measuring the standard solar collector tube under different temperature and vacuum conditions to obtain training samples, and then training the constructed neural network based on these training samples.

[0050] As can be seen from the above technical solution, this embodiment provides a detection and control method applied to a solar collector tube vacuum degree detection system. Specifically, the method involves sequentially selecting the target solar collector tubes and hovering the flight vehicle above them; using a temperature detection device to collect a first temperature value and a second temperature value of the target solar collector tube; and using a preset algorithm to calculate the vacuum degree of the target solar collector tube based on the first and second temperature values. This method allows the vacuum detection system to sequentially detect the vacuum degree of high-temperature solar collector tubes, enabling users to address issues such as repair or replacement when the vacuum degree of a particular collector tube fails to meet standards, thereby preventing significant heat loss to the system due to a decrease in vacuum degree.

[0051] The flowcharts and block diagrams in the accompanying drawings illustrate the architecture, functionality, and operation of possible implementations of systems, methods, and computer program products according to various embodiments of this disclosure. In this regard, each block in a flowchart or block diagram may represent a module, segment, or portion of code containing one or more executable instructions for implementing a specified logical function. It should also be noted that in some alternative implementations, the functions indicated in the blocks may occur in a different order than those indicated in the drawings. For example, two consecutively indicated blocks may actually be executed substantially in parallel, and they may sometimes be executed in reverse order, depending on the functions involved. It should also be noted that each block in the block diagrams and / or flowcharts, and combinations of blocks in the block diagrams and / or flowcharts, can be implemented using a dedicated hardware-based system that performs the specified function or operation, or using a combination of dedicated hardware and computer instructions.

[0052] Although the operations are described in a specific order, this should not be construed as requiring these operations to be performed in the specific order shown or in a sequential order. In certain environments, multitasking and parallel processing may be advantageous.

[0053] It should be understood that the steps described in the method embodiments of this disclosure may be performed in different orders and / or in parallel. Furthermore, the method embodiments may include additional steps and / or omit the steps shown. The scope of this disclosure is not limited in this respect.

[0054] Computer program code for performing the operations of this disclosure can be written in one or more programming languages ​​or a combination thereof, including but not limited to object-oriented programming languages ​​such as Java, Smalltalk, and C++, as well as conventional procedural programming languages ​​such as C or similar languages. The program code can be executed entirely on the user's computer, partially on the user's computer, as a standalone software package, partially on the user's computer and partially on a remote computer, or entirely on a remote computer or server. In cases involving remote computers, the remote computer can be connected to the user's computer via any type of network—including a local area network (LAN) or a wide area network (WAN)—or can be connected to an external computer.

[0055] Figure 3 This is a block diagram of an electronic device according to an embodiment of this application.

[0056] The following is for reference. Figure 3 This document illustrates a structural diagram suitable for implementing the electronic device in the embodiments of this disclosure. The terminal device in the embodiments of this disclosure may include, but is not limited to, mobile terminals such as mobile phones, laptops, digital broadcast receivers, PDAs (personal digital assistants), PADs (tablet computers), PMPs (portable multimedia players), in-vehicle terminals (e.g., in-vehicle navigation terminals), and fixed terminals such as digital TVs and desktop computers. This electronic device is merely an example and should not impose any limitations on the functionality and scope of use of the embodiments of this disclosure.

[0057] The electronic device may include a processing unit (e.g., a central processing unit, a graphics processing unit, etc.) 301, which can perform various appropriate actions and processes according to a program stored in a read-only memory (ROM) 302 or a program loaded from an input device 306 into a random access memory (RAM) 303. The RAM also stores various programs and data required for the operation of the electronic device. The processing unit, ROM, and RAM are interconnected via a bus 304. An input / output (I / O) interface 305 is also connected to the bus 304.

[0058] Typically, the following devices can be connected to the I / O interface: input devices including, for example, touchscreens, touchpads, keyboards, mice, cameras, microphones, accelerometers, gyroscopes, etc.; output devices 307 including, for example, liquid crystal displays (LCDs), speakers, vibrators, etc.; storage devices 308 including, for example, magnetic tapes, hard disks, etc.; and communication devices 309. Communication device 309 allows the electronic device to communicate wirelessly or wiredly with other devices to exchange data. Although electronic devices with various devices are shown in the figures, it should be understood that it is not required to implement or possess all of the devices shown. More or fewer devices may be implemented or possessed alternatively.

[0059] This application also provides an embodiment of a computer-readable storage medium.

[0060] The aforementioned computer-readable storage medium is used in an electronic device and carries one or more computer programs. When the electronic device executes these programs, it sequentially selects the target solar collector tubes and hovers the flight vehicle above them. A temperature detection device collects a first temperature value and a second temperature value of the target solar collector tube. A preset algorithm is used to calculate the vacuum level of the target solar collector tube based on the first and second temperature values. This method allows the vacuum detection system to sequentially detect the vacuum level of high-temperature solar collector tubes, enabling users to address issues such as repair or replacement when the vacuum level of a particular collector tube fails to meet standards, thereby preventing significant heat loss to the system due to a decrease in vacuum level.

[0061] It should be noted that the computer-readable medium described above in this disclosure can be a computer-readable signal medium or a computer-readable storage medium, or any combination of the two. A computer-readable storage medium can be, for example,—but not limited to—an electrical, magnetic, optical, electromagnetic, infrared, or semiconductor system, apparatus, or device, or any combination thereof. More specific examples of a computer-readable storage medium may include, but are not limited to: an electrical connection having one or more wires, a portable computer disk, a hard disk, random access memory (RAM), read-only memory (ROM), erasable programmable read-only memory (EPROM or flash memory), optical fiber, portable compact disk read-only memory (CD-ROM), optical storage device, magnetic storage device, or any suitable combination thereof.

[0062] In this disclosure, a computer-readable storage medium can be any tangible medium that contains or stores a program that can be used by or in connection with an instruction execution system, apparatus, or device. In this disclosure, a computer-readable signal medium can include a data signal propagated in baseband or as part of a carrier wave, carrying computer-readable program code. Such propagated data signals can take various forms, including but not limited to electromagnetic signals, optical signals, or any suitable combination thereof. A computer-readable signal medium can also be any computer-readable medium other than a computer-readable storage medium, which can send, propagate, or transmit a program for use by or in connection with an instruction execution system, apparatus, or device. The program code contained on the computer-readable medium can be transmitted using any suitable medium, including but not limited to: wires, optical fibers, RF (radio frequency), etc., or any suitable combination thereof.

[0063] The various embodiments in this specification are described in a progressive manner, with each embodiment focusing on the differences from other embodiments. The same or similar parts between the various embodiments can be referred to each other.

[0064] Although preferred embodiments of the present invention have been described, those skilled in the art, upon learning the basic inventive concept, can make other changes and modifications to these embodiments. Therefore, the appended claims are intended to be interpreted as including the preferred embodiments as well as all changes and modifications falling within the scope of the embodiments of the present invention.

[0065] Finally, it should be noted that in this document, relational terms such as "first" and "second" are used only to distinguish one entity or operation from another, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Furthermore, the terms "comprising," "including," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or terminal device that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such a process, method, article, or terminal device. Without further limitations, an element defined by the phrase "comprising one..." does not exclude the presence of other identical elements in the process, method, article, or terminal device that includes said element.

[0066] The technical solution provided by the present invention has been described in detail above. Specific examples have been used to illustrate the principle and implementation of the present invention. The description of the above embodiments is only for the purpose of helping to understand the method and core idea of ​​the present invention. At the same time, for those skilled in the art, there will be changes in the specific implementation and application scope based on the idea of ​​the present invention. Therefore, the content of this specification should not be construed as a limitation of the present invention.

Claims

1. A vacuum detection system for solar collector tubes, used for real-time detection of the vacuum level of high-temperature solar collector tubes in a linear concentrating solar thermal power generation system, characterized in that, The vacuum detection system for the solar collector tube includes a flight vehicle and a temperature detection device mounted on the flight vehicle, and also includes a data processing device wirelessly connected to the temperature detection device, wherein: The flight vehicle is used to move in the collector tube array of the linear concentrating solar thermal power generation system according to a preset pattern, and to make the temperature detection device sequentially face the target collector tubes selected sequentially from the collector tube array; The temperature detection device is used to collect the temperature of the glass tube of the target heat collector tube to obtain a first temperature value, and is also used to collect the temperature of the metal inner tube of the target heat collector tube to obtain a second temperature value. The data processing device is used to calculate the first temperature value and the second temperature value based on a predetermined algorithm to obtain the vacuum degree of the target heat collection tube.

2. The vacuum detection system for solar collector tubes as described in claim 1, characterized in that, The flight vehicle is equipped with a satellite positioning module, which is used to provide positioning signals for the flight control of the flight vehicle.

3. The vacuum detection system for solar collector tubes as described in claim 1, characterized in that, The temperature detection device includes a first temperature sensor for detecting the temperature of the glass tube and a second temperature sensor for detecting the temperature of the inner metal tube.

4. The vacuum detection system for solar collector tubes as described in claim 3, characterized in that, The first temperature sensor is an infrared thermal imager.

5. The vacuum detection system for solar collector tubes as described in claim 3, characterized in that, The second temperature sensor is a low emissivity infrared thermometer.

6. A detection and control method, applied to the vacuum detection system for solar collector tubes as described in any one of claims 1 to 5, characterized in that, The detection and control method includes the following steps: The target solar collector tubes are selected in sequence, and the flight vehicle is hovered above the target solar collector tubes. The first and second temperature values ​​of the target solar collector tube are collected using a temperature detection device. The vacuum degree of the target heat collector tube is obtained by calculating the first temperature value and the second temperature value using a preset algorithm.

7. The detection and control method as described in claim 6, characterized in that, The step of acquiring the first and second temperature values ​​of the target solar collector using a temperature detection device includes the following steps: The flight vehicle is controlled to hover directly above the target heat collection tube, and the temperature of the glass tube is detected based on an infrared thermal imager to obtain the first temperature value; The flight vehicle is controlled to hover directly above the target heat collection tube, and the lens of the low emissivity infrared thermometer is controlled to maintain a distance of 0.1 to 1 m from the glass tube. The low emissivity infrared thermometer is then controlled to collect temperature data from the inner metal tube to obtain the second temperature value.

8. The detection and control method as described in claim 6, characterized in that, The vacuum degree of the target solar collector tube is obtained by calculating the first and second temperature values ​​using a preset algorithm, including the following steps: The vacuum level is obtained by looking up the temperature-vacuum level MAP based on the first temperature value and the second temperature value. Alternatively, the vacuum level can be obtained by calculating the first temperature value and the second temperature value based on a pre-trained neural network model.

9. An electronic device, characterized in that, The electronic device includes at least one processor and a memory connected to the processor, wherein: The memory is used to store computer programs or instructions; The processor is used to execute the computer program or instructions to enable the electronic device to implement the detection and control method as described in any one of claims 6 to 8.

10. A computer-readable storage medium for use in electronic devices, characterized in that, The storage medium carries one or more computer programs that can be executed by the electronic device, thereby enabling the electronic device to implement the detection and control method as described in any one of claims 6 to 8.

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