CN117354346A - Remote monitoring system for solar aviation obstruction lights - Google Patents
Remote monitoring system for solar aviation obstruction lights Download PDFInfo
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- CN117354346A CN117354346A CN202311646483.8A CN202311646483A CN117354346A CN 117354346 A CN117354346 A CN 117354346A CN 202311646483 A CN202311646483 A CN 202311646483A CN 117354346 A CN117354346 A CN 117354346A
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- 238000012544 monitoring process Methods 0.000 title claims abstract description 132
- 238000004891 communication Methods 0.000 claims abstract description 69
- 230000002159 abnormal effect Effects 0.000 claims abstract description 9
- 238000007537 lampworking Methods 0.000 claims abstract description 4
- 238000000034 method Methods 0.000 claims abstract description 4
- 230000008569 process Effects 0.000 claims abstract description 4
- 238000005286 illumination Methods 0.000 claims description 28
- 238000004146 energy storage Methods 0.000 claims description 23
- 238000001514 detection method Methods 0.000 claims description 16
- 238000013500 data storage Methods 0.000 claims description 9
- 230000004044 response Effects 0.000 claims description 9
- 238000005070 sampling Methods 0.000 claims description 7
- 230000007613 environmental effect Effects 0.000 claims description 6
- 238000009434 installation Methods 0.000 claims description 5
- 238000004458 analytical method Methods 0.000 claims description 4
- 238000012545 processing Methods 0.000 claims description 3
- 230000035939 shock Effects 0.000 claims description 3
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- 230000008859 change Effects 0.000 description 3
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- 230000000694 effects Effects 0.000 description 3
- 238000011084 recovery Methods 0.000 description 3
- 238000012986 modification Methods 0.000 description 2
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- 239000012080 ambient air Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000007405 data analysis Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000007726 management method Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
Classifications
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L67/00—Network arrangements or protocols for supporting network services or applications
- H04L67/01—Protocols
- H04L67/12—Protocols specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L67/00—Network arrangements or protocols for supporting network services or applications
- H04L67/01—Protocols
- H04L67/10—Protocols in which an application is distributed across nodes in the network
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04Q—SELECTING
- H04Q9/00—Arrangements in telecontrol or telemetry systems for selectively calling a substation from a main station, in which substation desired apparatus is selected for applying a control signal thereto or for obtaining measured values therefrom
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B47/00—Circuit arrangements for operating light sources in general, i.e. where the type of light source is not relevant
- H05B47/10—Controlling the light source
- H05B47/175—Controlling the light source by remote control
- H05B47/19—Controlling the light source by remote control via wireless transmission
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B47/00—Circuit arrangements for operating light sources in general, i.e. where the type of light source is not relevant
- H05B47/20—Responsive to malfunctions or to light source life; for protection
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B20/00—Energy efficient lighting technologies, e.g. halogen lamps or gas discharge lamps
- Y02B20/40—Control techniques providing energy savings, e.g. smart controller or presence detection
Abstract
The invention relates to a remote monitoring system for a solar aviation obstruction lamp, which belongs to the technical field of remote monitoring of aviation obstruction lamps, wherein the monitoring system can monitor the state and the performance of the lamp in real time by arranging a monitoring module and collecting working parameters of the aviation obstruction lamp, and a cloud service module receives and processes monitoring data, and can conveniently know the working state of the aviation obstruction lamp by comparing with a set threshold value, so that abnormal conditions can be found in time and the monitoring system can be processed and maintained in time. The monitoring modules are constructed into a netlike topological structure through the second communication units, the structure can realize mutual communication among the monitoring modules, the selection of communication lines between the monitoring modules and the cloud service module is increased, and the stability and the reliability of the system are improved. The electric signal of the solar power supply circuit and the electric signal of the aviation obstruction lamp working circuit are sampled and monitored to monitor whether the solar power supply module can normally supply power for the aviation obstruction lamp.
Description
Technical Field
The invention belongs to the technical field of remote monitoring of aviation obstruction lights, and particularly relates to a remote monitoring system for a solar aviation obstruction light.
Background
Aviation obstruction lights are commonly used to identify high-rise buildings, power lines, communication towers, and other airborne obstructions, and automatically adjust the brightness according to different weather conditions to ensure that the aircraft can identify and avoid such obstructions during night or low visibility conditions. However, most of the installation positions of the aviation obstruction lights are high-altitude, mountain areas or other dangerous places, patrol personnel may face high-risk working environments, real-time monitoring and fault investigation are difficult to realize, and particularly, under the conditions of wide distribution range and numerous problems are found and handled with a certain delay.
Disclosure of Invention
In order to solve the problems in the prior art, the invention provides a remote monitoring system for a solar aviation obstruction lamp.
The aim of the invention can be achieved by the following technical scheme:
a remote monitoring system for solar aviation obstruction lights comprises a cloud service module and a plurality of monitoring modules;
the cloud service module is used for receiving and processing the data acquired by the monitoring module, comparing the acquired data with a threshold value and executing a corresponding instruction according to a comparison result; the user accesses the cloud service module to remotely check the monitoring data in a mode of collecting the application or the webpage;
the monitoring module comprises a communication module and an acquisition module;
the communication module comprises a first communication unit and a second communication unit;
the first communication unit is used for communication between the monitoring module and the cloud service module, and the second communication unit is used for communication inside the monitoring module and communication between the monitoring module and other monitoring modules;
the monitoring module is also provided with a controller, and the controller is communicated with the acquisition module through a second communication unit and records the data acquired by the acquisition module; the controller is communicated with the cloud service module through the first communication unit, transmits the data acquired by the acquisition module to the cloud service module and receives an instruction of the cloud service module;
before the controller communicates with the cloud service module, a detection signal is sent to the cloud service module through the first communication unit, and if the response of the cloud service module to the detection signal is received within a set time, the data acquired by the acquisition module is sent to the cloud service module through the first communication unit; if the response of the cloud service module to the detection signal cannot be received within the set time, the data acquired by the acquisition module is transmitted to other monitoring modules through the second communication unit and then transmitted to the cloud service module;
wherein the remote monitoring comprises the steps of:
s1: a monitoring module is arranged at the position of the navigation obstacle lamp;
s2: the monitoring module is used for collecting working parameters of the aviation obstruction lights through the collecting module;
s3: the monitoring module transmits the data acquired by the acquisition module to the cloud service module through the communication module;
s4: and after the cloud service module receives the data transmitted by the monitoring module, the actual data is compared with the threshold value in real time, and corresponding instructions are executed according to the comparison result.
Preferably, the first communication unit is a 2G/3G/4G/5G module, the second communication unit is a ZigBee module, and the controller is connected with the acquisition module through the second control module and is also connected with other monitoring modules to construct a mesh topology structure.
Preferably, before the controller communicates with the cloud service module, the controller sends a detection signal to the cloud service module through the first communication unit, and if a response of the cloud service module to the detection signal is received within a set time, the controller sends the data acquired by the acquisition module to the cloud service module through the first communication unit; if the response of the cloud service module to the detection signal cannot be received within the set time, the data acquired by the acquisition module are transmitted to other detection modules through the second communication unit, and then are transmitted to the cloud service module.
Preferably, the acquisition module comprises a first acquisition unit, a second acquisition unit and a third acquisition unit;
the first acquisition unit is used for acquiring the electric signals of the solar power supply circuit and the electric signals of the aviation obstruction lamp working circuit;
the second acquisition unit is used for acquiring working parameters of the aviation obstruction lights;
the third acquisition unit is used for acquiring environmental parameters of the working environment where the aviation obstruction lights are located.
Preferably, the first collecting unit samples and monitors the electric signals of the solar power supply circuit and the electric signals of the aviation obstruction light working circuit to respectively monitor the working states of the solar power supply device and the aviation obstruction light;
the cloud service module analyzes and compares the working states of the solar power supply devices in the same area to judge whether the solar power supply devices are in a normal working state or not.
Preferably, the third acquisition unit monitors environmental parameters of the working environment where the aviation obstruction lights are located through a plurality of sensors, and the third acquisition unit comprises: a temperature sensor, a humidity sensor, an air pressure sensor, a wind speed sensor, a rainfall sensor and a second illumination sensor; the second illumination sensor is used for monitoring the environment illumination intensity of the position where the aviation obstruction light is located, which is not illuminated by the aviation obstruction light.
Preferably, the second acquisition unit monitors the working parameters of the aviation obstruction lights through a plurality of sensors, and the second acquisition unit comprises: a battery power sensor, a tilt sensor, a shock sensor, and a first illumination sensor;
the inclination sensor is used for monitoring whether the aviation obstruction lights are kept vertical at the installation position;
the vibration sensor is used for monitoring whether abnormal vibration occurs to the aviation obstruction lights or not;
the first illumination sensor is used for monitoring illumination intensity under the irradiation of the aviation obstruction lights when the aviation obstruction lights work;
the cloud service module determines the actual illumination intensity of the aviation obstruction lamp during working according to the difference value between the data acquired by the first illumination intensity sensor and the data acquired by the second illumination sensor;
the battery electric quantity sensor is used for monitoring whether an energy storage battery of the solar power supply device can be charged and discharged normally or not, judging the actual capacity of the energy storage battery by monitoring the electric quantity of the energy storage battery in a full-power state, and further obtaining the service life of the energy storage battery.
Preferably, the cloud service module further comprises a data storage unit, an alarm unit and a remote control unit;
the data storage unit is used for storing the data acquired by the monitoring module and used for subsequent analysis and inquiry;
the alarm unit is used for monitoring the comparison result of the acquired data and the threshold value, triggering an alarm when the comparison result exceeds the set threshold value and reminding related staff to process;
the remote control unit is used for receiving the instruction of the user, transmitting the instruction to the corresponding monitoring module, realizing remote control operation of the aviation obstruction lights, and realizing remote control of the aviation obstruction lights by the user sending the instruction in a mode of collecting applications or webpages, such as turning on/off the aviation obstruction lights, adjusting the light brightness and the like.
The beneficial effects of the invention are as follows:
1. through setting up monitoring module and gathering the operating parameter of aviation obstruction light, state and the performance that can real-time supervision lamp, cloud service module receives and handles monitoring data, through comparing with the threshold value that sets for, conveniently knows the operating condition of aviation obstruction light, can in time discover abnormal conditions, in time handles and maintains.
2. The monitoring modules are constructed into a netlike topological structure through the second communication units, the structure can realize mutual communication among the monitoring modules, the selection of communication lines between the monitoring modules and the cloud service module is increased, and the stability and the reliability of the system are improved.
3. Through sampling monitoring to the signal of telecommunication of solar energy power supply circuit and aviation obstruction lamp work circuit, whether monitoring solar energy power supply module can normally be the aviation obstruction lamp power supply, simultaneously, through the continuous control to energy storage battery, in time acquire energy storage battery's life condition.
Drawings
The present invention is further described below with reference to the accompanying drawings for the convenience of understanding by those skilled in the art.
Fig. 1 is a system configuration diagram provided in embodiment 1 of the present invention;
FIG. 2 is a flow chart of monitoring provided in an embodiment of the invention
FIG. 3 is a system configuration diagram provided in embodiment 2 of the present invention;
FIG. 4 is a system configuration diagram provided in embodiment 3 of the present invention;
Detailed Description
In order to further describe the technical means and effects adopted by the invention for achieving the preset aim, the following detailed description is given below of the specific implementation, structure, characteristics and effects according to the invention with reference to the attached drawings and the preferred embodiment.
Example 1
Referring to fig. 1-2, a remote monitoring system for solar aviation obstruction lights provided in this embodiment includes a cloud service module and a plurality of monitoring modules;
the solar aviation obstruction lights are respectively provided with a monitoring module;
the cloud service module is used for receiving and processing the data acquired by the monitoring module, comparing the acquired data with a threshold value and executing corresponding instructions according to a comparison result; the user accesses the cloud service module to remotely check the monitoring data and modify the threshold value by collecting the application or the webpage;
the monitoring module comprises a communication module and an acquisition module;
the communication module comprises a first communication unit and a second communication unit;
the first communication unit is used for communication between the monitoring module and the cloud service module, and the die communication unit is used for communication inside the monitoring module and communication of quality inspection between the monitoring module and other monitoring modules;
the monitoring module is also provided with a controller, and the controller is communicated with the acquisition module through a second communication unit and records the data acquired by the acquisition module; the controller is communicated with the cloud service module through the first communication unit, transmits the data acquired by the acquisition module to the cloud service module and receives an instruction of the cloud service module;
before the controller communicates with the cloud service module, a detection signal is sent to the cloud service module through the first communication unit, and if the response of the cloud service module to the detection signal is received within a set time, the data acquired by the acquisition module is sent to the cloud service module through the first communication unit; if the response of the cloud service module to the detection signal cannot be received within the set time, the data acquired by the acquisition module is transmitted to other monitoring modules through the second communication unit and then transmitted to the cloud service module;
wherein the remote monitoring comprises the steps of:
s1: a monitoring module is arranged at the position of the navigation obstacle lamp;
s2: the monitoring module is used for collecting working parameters of the aviation obstruction lights through the collecting module;
s3: the monitoring module transmits the data acquired by the acquisition module to the cloud service module through the communication module;
s4: and after the cloud service module receives the data transmitted by the monitoring module, the actual data is compared with the threshold value in real time, and corresponding instructions are executed according to the comparison result.
In this embodiment, through setting up monitoring module and gathering aviation obstruction light's operating parameter, state and the performance that can real-time supervision lamp, cloud service module receives and handles monitoring data, through carrying out the contrast with the threshold value that sets for, conveniently knows aviation obstruction light's operating condition, can in time discover the abnormal situation, in time handles and maintains.
Example 2
Referring to fig. 3, according to the remote monitoring system for a solar aviation obstruction light provided in embodiment 1, the first communication unit is a 2G/3G/4G/5G module, the second communication unit is a ZigBee module, and the controller is connected with the acquisition module through the second communication unit and is also connected with other monitoring modules, so as to construct a mesh topology structure, so that data transmission is more flexible and reliable.
Before communicating with the cloud service module, the controller sends a detection signal to the cloud service module through the first communication unit, if the response of the cloud service module to the detection signal is received within a set time, the controller responds to the detection signal to the cloud service module through the first communication unit, and after the data acquired by the acquisition module are transmitted to other monitoring modules through the second communication unit, the data are transmitted to the cloud service module.
In this embodiment, the monitoring modules are constructed into a mesh topology structure through the second communication unit, and this structure can realize mutual communication between the monitoring modules, increase the selection of communication lines between the monitoring modules and the cloud service module, and improve the stability and reliability of the system.
Example 3
Referring to fig. 4, a remote monitoring system for a solar aviation obstruction beacon according to embodiment 1 is provided, wherein the acquisition module includes a first acquisition unit, a second acquisition unit, and a third acquisition unit;
the first acquisition unit is used for sampling the electric signals of the solar power supply circuit and the electric signals of the aviation obstruction lamp working circuit;
the second acquisition unit is used for acquiring working parameters of the aviation obstruction lights;
the third acquisition unit is used for acquiring environmental parameters of the working environment where the aviation obstruction lights are located.
The first acquisition unit is used for respectively monitoring the working states of the solar power supply device and the aviation obstruction lights by sampling and monitoring the electric signals of the solar power supply circuit and the electric signals of the aviation obstruction lights working circuit;
the cloud service module analyzes and compares the working states of the solar power supply devices in the same area to judge whether the solar power supply devices are in a normal working state or not.
The third acquisition unit monitors environmental parameters of the working environment where the aviation obstruction lights are located through a plurality of sensors, and the third acquisition unit comprises: a temperature sensor, a humidity sensor, an air pressure sensor, a wind speed sensor, a rainfall sensor and a second illumination sensor; the second illumination sensor is used for monitoring the environment illumination intensity of the position where the aviation obstruction light is located, which is not illuminated by the aviation obstruction light.
The temperature sensor and the humidity sensor are respectively used for monitoring the temperature and the humidity of the environment where the aviation obstruction lights are located. The temperature and the humidity of environment all have certain influence to aviation obstruction light's normal operating and life-span, can real-time supervision ambient temperature with through temperature sensor, in time take measures protection aviation obstruction light.
Air pressure sensor: the device is used for monitoring the air pressure of the environment where the aviation obstruction lights are located. The change of air pressure can influence the light brightness and the stability of aviation obstruction lights, can real-time supervision ambient air pressure through the air pressure sensor, in time adjusts aviation obstruction lights's operating condition.
Wind speed sensor: the device is used for monitoring the wind speed of the environment where the aviation obstruction lights are located. The stability and wind resistance of the aviation obstruction lights can be influenced by the change of the wind speed, the ambient wind speed can be monitored in real time through a wind speed sensor, the working state of the aviation obstruction lights can be adjusted in time, and the normal operation of the aviation obstruction lights is ensured.
Rain sensor: the device is used for monitoring rainfall conditions of the environment where the aviation obstruction lights are located. The rainfall can influence the visibility and stability of the aviation obstruction lights, and the rainfall condition of the environment can be monitored in real time through the rainfall sensor, and measures are taken in time to protect the aviation obstruction lights.
The second acquisition unit monitors the working parameters of the aviation obstruction lights through a plurality of sensors, and comprises: a battery power sensor, a tilt sensor, a shock sensor, and a first illumination sensor;
the inclination sensor is used for monitoring whether the aviation obstruction lights are kept vertical at the installation position; if the aviation obstruction lights are tilted, the normal operation and lighting effects thereof may be affected, and even the risk of unstable installation or collapse may result. Therefore, the monitoring of the inclination sensor can help to find and repair the inclination problem in time, and ensure the normal operation and safety of the aviation obstruction lamp.
The vibration sensor is used for monitoring whether abnormal vibration occurs to the aviation obstruction lights or not; by monitoring the vibration condition of the aviation obstruction lights, whether abnormal conditions occur or not can be timely found, such as damage, collision or loosening of the aviation obstruction lights.
The first illumination sensor is used for monitoring illumination intensity under the irradiation of the aviation obstruction lights when the aviation obstruction lights work;
the cloud service module determines the actual illumination intensity of the aviation obstruction lamp during working according to the difference value between the data acquired by the first illumination sensor and the data acquired by the second illumination sensor;
meanwhile, according to the change condition in the data acquired by the first illumination sensor, the flicker frequency of the aviation obstruction light is monitored so as to ensure that the aviation obstruction light can effectively attract the attention of an aircraft.
The battery electric quantity sensor is used for monitoring whether the energy storage battery of the solar power supply device can be charged and discharged normally or not, judging the actual capacity of the energy storage battery by monitoring the electric quantity of the energy storage battery in a full-power state, and further obtaining the residual service life of the energy storage battery.
The solar energy aviation obstruction light built-in battery is charged by solar energy in daytime and automatically supplies power at night, whether the solar energy power supply module charges the energy storage battery or not is judged by sampling and monitoring the electric signals of the solar energy power supply circuit and the electric signals of the aviation obstruction light working circuit, whether the energy storage battery is in a charging or discharging state is further judged, and whether the energy storage battery can be normally charged or discharged is monitored by combining the data acquired by the battery electric quantity sensor. Meanwhile, the actual capacity of the energy storage battery is judged by monitoring the electric quantity of the energy storage battery in a full-power state through the battery electric quantity sensor, and the residual service life of the energy storage battery is obtained by the loss rate of the electric quantity when the energy storage battery supplies power to the aviation obstruction light.
In this embodiment, through sampling the monitoring to the signal of telecommunication of solar energy power supply circuit and aviation obstruction light work circuit, whether monitoring solar energy power supply module can normally be for aviation obstruction light power supply, simultaneously, through the continuous control to energy storage battery, in time acquire energy storage battery's life condition.
Example 4
According to the remote monitoring system for the solar aviation obstruction lights provided in the embodiment 1, the cloud service module further comprises a data storage unit, an alarm unit and a remote control unit;
the data storage unit is used for storing the data acquired by the monitoring module and used for subsequent analysis and inquiry; the stored data can comprise parameters such as working state, brightness, electric quantity and the like of the aviation obstruction lights, and the data can be conveniently analyzed and inquired later by storing the data in the data storage unit. The user can access the data in the data storage unit through the remote control unit or other terminal equipment, and perform data analysis and query operations. Therefore, the user can be helped to know the working condition of the aviation obstruction lights, discover problems in time and take corresponding measures. Meanwhile, the data storage unit can be provided with a data backup and recovery mechanism so as to ensure the safety and reliability of the data. The backup data can be used for disaster recovery or recovery operation when the data is lost, and the integrity and usability of the data are ensured. In addition, different storage strategies can be set according to requirements, such as storage according to time, storage according to geographic positions and the like. Thus, the user can conveniently inquire and analyze the data according to different requirements. The user can inquire the aviation obstruction light data of a specific time period or a specific place through the conditions such as a designated time range or a geographic position so as to perform relevant analysis and decision.
The alarm unit is used for monitoring the comparison result of the acquired data and the threshold value, triggering an alarm when the comparison result exceeds the set threshold value, and reminding related personnel to process;
when the data collected by the monitoring module exceeds a set threshold, the alarm unit can send out alarm signals such as sound, light flashing and the like to draw the attention of related personnel. Therefore, abnormal conditions such as faults, abnormal vibration or inclination of the aviation obstruction lights can be found in time, and measures can be taken in time to repair or treat the aviation obstruction lights, so that the normal operation and the safety of the aviation obstruction lights are ensured. The setting of alarm unit can be adjusted according to actual demand to satisfy the needs of different monitoring requirements and alarm level.
The remote control unit is used for receiving the instruction of the user, transmitting the instruction to the corresponding monitoring module, realizing remote control operation of the aviation obstruction lights, and enabling the user to send the instruction in a mode of mobile phone application or webpage, such as turning on/off the aviation obstruction lights, adjusting the light brightness and the like, so as to realize remote control of the aviation obstruction lights.
In this embodiment, the cloud service module may trigger an alarm in time by comparing with the threshold value, so as to remind relevant personnel to take corresponding measures. This helps to prevent and solve problems that may occur, ensuring proper operation of the aviation obstruction lights. Meanwhile, the cloud service module is provided with a remote control unit, and a user can send instructions through a mobile phone application or a webpage mode, such as turning on/off an aviation obstruction light, adjusting the light brightness and the like, so that remote control of the aviation obstruction light is achieved. This provides a convenient way of management, which can reduce labor costs and maintenance work.
The present invention is not limited to the above embodiments, but is not limited to the above embodiments, and any technical modifications, equivalents and modifications made to the above embodiments according to the technical principles of the present invention can be made by those skilled in the art without departing from the scope of the invention.
Claims (7)
1. The remote monitoring system for the solar aviation obstruction lights is characterized by comprising a cloud service module and a plurality of monitoring modules;
the cloud service module is used for receiving and processing the data acquired by the monitoring module, comparing the acquired data with a threshold value and executing a corresponding instruction according to a comparison result; the user accesses the cloud service module to remotely check the monitoring data in a mode of mobile phone application or webpage;
the monitoring module comprises a communication module and an acquisition module;
the communication module comprises a first communication unit and a second communication unit;
the first communication unit is used for communication between the monitoring module and the cloud service module, and the second communication unit is used for communication inside the monitoring module and communication between the monitoring module and other monitoring modules;
the monitoring module is also provided with a controller, and the controller is communicated with the acquisition module through a second communication unit and records the data acquired by the acquisition module; the controller is communicated with the cloud service module through the first communication unit, transmits the data acquired by the acquisition module to the cloud service module and receives an instruction of the cloud service module;
before the controller communicates with the cloud service module, a detection signal is sent to the cloud service module through the first communication unit, and if the response of the cloud service module to the detection signal is received within a set time, the data acquired by the acquisition module is sent to the cloud service module through the first communication unit; if the response of the cloud service module to the detection signal cannot be received within the set time, the data acquired by the acquisition module is transmitted to other monitoring modules through the second communication unit and then transmitted to the cloud service module;
wherein the remote monitoring comprises the steps of:
s1: a monitoring module is arranged at the position of the navigation obstacle lamp;
s2: the monitoring module is used for collecting working parameters of the aviation obstruction lights through the collecting module;
s3: the monitoring module transmits the data acquired by the acquisition module to the cloud service module through the communication module;
s4: and after the cloud service module receives the data transmitted by the monitoring module, the actual data is compared with the threshold value in real time, and corresponding instructions are executed according to the comparison result.
2. The remote monitoring system for solar aviation obstruction lights according to claim 1, wherein the first communication unit is a 2G/3G/4G/5G module, the second communication unit is a ZigBee module, and the controller is connected with the acquisition module through the second communication unit and is also connected with other monitoring modules to construct a mesh topology structure.
3. The remote monitoring system for a solar energy aircraft obstruction beacon of claim 1, wherein the acquisition module comprises a first acquisition unit, a second acquisition unit, and a third acquisition unit;
the first acquisition unit is used for sampling the electric signals of the solar power supply circuit and the electric signals of the aviation obstruction lamp working circuit;
the second acquisition unit is used for acquiring working parameters of the aviation obstruction lights;
the third acquisition unit is used for acquiring environmental parameters of the working environment where the aviation obstruction lights are located.
4. A remote monitoring system for solar energy aviation obstruction lights according to claim 3, wherein the first collection unit monitors the working states of the solar energy power supply device and the aviation obstruction lights by sampling and monitoring the electric signals of the solar energy power supply circuit and the electric signals of the aviation obstruction lights working circuit;
the cloud service module analyzes and compares the working states of the solar power supply devices in the same area to judge whether the solar power supply devices are in a normal working state or not.
5. A remote monitoring system for solar energy avionic obstruction lights according to claim 3, wherein the third acquisition unit monitors environmental parameters of the operating environment in which the avionic obstruction lights are located via a plurality of sensors, comprising: a temperature sensor, a humidity sensor, an air pressure sensor, a wind speed sensor, a rainfall sensor and a second illumination sensor; the second illumination sensor is used for monitoring the environment illumination intensity of the position where the aviation obstruction light is located, which is not illuminated by the aviation obstruction light.
6. The remote monitoring system for solar energy avionic obstruction lights according to claim 5, wherein said second acquisition unit monitors operating parameters of the avionic obstruction lights by a plurality of sensors, comprising: a battery power sensor, a tilt sensor, a shock sensor, and a first illumination sensor;
the inclination sensor is used for monitoring whether the aviation obstruction lights are kept vertical at the installation position;
the vibration sensor is used for monitoring whether abnormal vibration occurs to the aviation obstruction lights or not;
the first illumination sensor is used for monitoring illumination intensity under the irradiation of the aviation obstruction lights when the aviation obstruction lights work;
the cloud service module determines the actual illumination intensity of the aviation obstruction lamp during working according to the difference value between the data acquired by the first illumination sensor and the data acquired by the second illumination sensor;
the battery electric quantity sensor is used for monitoring whether the energy storage battery of the solar power supply device can be charged and discharged normally or not, judging the actual capacity of the energy storage battery by monitoring the electric quantity of the energy storage battery in a full-power state, and further obtaining the service life of the energy storage battery.
7. The remote monitoring system for solar energy aviation obstruction lights according to claim 1, wherein the cloud service module further comprises a data storage unit, an alarm unit, and a remote control unit;
the data storage unit is used for storing the data acquired by the monitoring module and used for subsequent analysis and inquiry;
the alarm unit is used for monitoring the comparison result of the acquired data and the threshold value, triggering an alarm when the comparison result exceeds the set threshold value, and reminding related personnel to process;
the remote control unit is used for receiving the instruction of the user, transmitting the instruction to the corresponding monitoring module, realizing remote control operation of the aviation obstruction lights, and sending the instruction by the user through a mobile phone application or a webpage mode, wherein the instruction comprises the steps of switching on/off the aviation obstruction lights and adjusting the light brightness.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202311646483.8A CN117354346B (en) | 2023-12-04 | 2023-12-04 | Remote monitoring system for solar aviation obstruction lights |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202311646483.8A CN117354346B (en) | 2023-12-04 | 2023-12-04 | Remote monitoring system for solar aviation obstruction lights |
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| Publication Number | Publication Date |
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| CN117354346A true CN117354346A (en) | 2024-01-05 |
| CN117354346B CN117354346B (en) | 2024-02-20 |
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| CN202311646483.8A Active CN117354346B (en) | 2023-12-04 | 2023-12-04 | Remote monitoring system for solar aviation obstruction lights |
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