A remote environmental monitoring device for environmental protection

Abstract

This invention discloses a remote environmental monitoring device for environmental protection, comprising a carrier, a sliding plate slidably connected above the carrier, a first gear meshing with the sliding plate, a bidirectional threaded rod driven by the first gear, a first stabilizing plate threaded onto the surface of the bidirectional threaded rod, and a second stabilizing plate threaded onto the end of the bidirectional threaded rod away from the first stabilizing plate. This effectively solves the problems of limited monitoring range of ground-based detection devices and data interruption of high-altitude flight equipment, improving monitoring accuracy and continuity. By combining the carrier's ground mobility with the aircraft's high-altitude and rugged terrain mobility capabilities, it achieves multi-dimensional and wide-range environmental monitoring from the ground to high altitudes, avoiding false alarms caused by incomplete monitoring at a single altitude. When encountering severe weather such as heavy rain or strong winds, the aircraft can enter the storage compartment through the meshing linkage of the first gear and the sliding plate, and be clamped and fixed by the first and second stabilizing plates, with a soft interlayer buffering to reduce vibration damage.

Description

Technical Field

[0001] This invention relates to the field of environmental protection equipment technology, and in particular to a remote environmental monitoring device for environmental protection. Background Technology

[0002] With the acceleration of industrialization and urbanization, environmental problems are becoming increasingly prominent. Air pollution, water pollution, and noise pollution pose serious threats to ecosystems and human health, urgently requiring efficient and accurate environmental monitoring methods to support environmental protection efforts. Regarding the atmospheric environment, pollutants such as sulfur dioxide, nitrogen oxides, and volatile organic compounds emitted from industrial production, as well as particulate matter from vehicle exhaust and straw burning, lead to frequent smog. This not only reduces visibility and affects transportation safety but also enters the human body through respiration, triggering various diseases such as asthma and lung cancer. According to relevant data, long-term exposure to environments with PM2.5 concentrations exceeding standards significantly increases the incidence of respiratory diseases. Simultaneously, these pollutants participate in atmospheric chemical reactions, forming acid rain, acidifying soil and water bodies, damaging forests and crop growth, and causing severe damage to ecosystems.

[0003] However, in actual environmental monitoring, many problems still need to be solved. Ground-based detection devices are limited by their monitoring range and cannot cope with the differences in environmental quality at different altitudes. When encountering regional environmental pollution, they are prone to false alarms due to incomplete monitoring, affecting the reliability of data and the accuracy of decision-making. In addition, although various types of aerial equipment are used for high-altitude environmental monitoring, they have revealed obvious shortcomings in actual use, with power supply issues being particularly prominent. Limited flight time makes it difficult to meet the needs of long-term continuous monitoring, resulting in intermittent monitoring data. Furthermore, in remote environmental monitoring scenarios, aerial equipment lacks effective protection against severe weather such as heavy rain and strong winds, making it highly susceptible to damage. This not only interrupts monitoring work but also increases maintenance costs due to equipment damage, seriously restricting the stable operation of high-altitude monitoring functions. Summary of the Invention

[0004] The purpose of this invention is to address the aforementioned technical shortcomings in the prior art by proposing a remote environmental monitoring device for environmental protection.

[0005] To achieve the above objectives, the present invention adopts the following technical solution: A remote environmental monitoring device for environmental protection includes a carrier, a sliding plate slidably connected above the carrier, a first gear meshing with the sliding plate, a bidirectional threaded rod driven by the first gear, a first stabilizing plate threaded to the surface of the bidirectional threaded rod, a second stabilizing plate threaded to the end of the bidirectional threaded rod away from the first stabilizing plate, a rotating rod driven by the bidirectional threaded rod, a first bevel gear fixedly connected to the end of the rotating rod away from the carrier, a second bevel gear meshing with the first bevel gear, a second gear fixedly connected to the side of the second bevel gear, a toothed column meshing with the second gear, the toothed column slidably connected to the carrier, a contact plate fixedly connected above the toothed column, and a detection mechanism for environmental monitoring disposed inside the carrier, the detection mechanism including a spacecraft disposed inside the carrier, a circular plate disposed at the bottom of the spacecraft.

[0006] The above technical solution further includes: The detection mechanism also includes a telescopic pull-out rod set on the side of the aircraft, a battery block fixedly connected to the bottom of the aircraft, and an environmental monitoring board and a camera board set on the side of the aircraft.

[0007] The first gear is rotatably connected to the carrier, and the first gear is driven by a first belt. The end of the first belt away from the first gear is driven by a bidirectional threaded rod, which is rotatably connected to the inner wall of the carrier. The first stabilizing plate is slidably connected to the carrier. A soft interlayer is provided on the side of the first stabilizing plate near the second stabilizing plate. The carrier is slidably connected to the second stabilizing plate. A soft interlayer is also provided on the side of the second stabilizing plate near the first stabilizing plate. The bidirectional threaded rod is driven by a second belt, and a rotating rod is driven by the end of the second belt away from the bidirectional threaded rod.

[0008] An air quality detection plate and a sound detection block are provided on the side of the carrier. An information processing box for transmitting information is provided inside the carrier. A signal receiving rod is fixedly installed on the top of the information processing box. A shooting plate is fixedly connected to the side of the carrier.

[0009] The carrier has a square compartment inside, which is rotatably connected to the second gear, and the rotating rod is rotatably connected to the square compartment.

[0010] The container provides a stable installation and rotation space for the second gear and the rotating rod, ensuring the precision of gear meshing and power transmission, guaranteeing the smoothness of mechanical transmission during the storage, fixing, and charging of the aircraft, and improving the stability and reliability of equipment operation.

[0011] The bottom of the carrier is equipped with multiple sets of rollers for movement.

[0012] Multiple sets of rollers give the carrier flexible ground mobility, enabling it to move autonomously or remotely to different monitoring areas on flat surfaces, expanding the ground monitoring range, facilitating the tracking of ground pollution sources, and providing mobile base station support for the aircraft, thus enhancing the overall mobility of the device.

[0013] The aircraft is equipped with multiple sets of support legs at its bottom.

[0014] The outriggers provide stable support during takeoff and landing, preventing the sensors, charging contacts, and other components on the bottom from being damaged by direct contact with the ground. At the same time, when the aircraft is stored inside the carrier, the outriggers can better fit into the fixed structure to ensure a firm fixation and reduce damage caused by shaking.

[0015] The aircraft is equipped with batteries at its bottom for storing energy.

[0016] The battery provides energy for the aircraft to perform monitoring tasks independently, enabling it to have sufficient endurance when detached from the carrier for monitoring in high-altitude or rugged areas. In conjunction with the carrier's charging structure, energy can be recycled, further extending the aircraft's independent working time.

[0017] The carrier is equipped with photovoltaic panels on both sides for collecting solar energy.

[0018] Photovoltaic panels can convert solar energy into electrical energy and store it in the energy storage device of the carrier, providing clean energy for the carrier's own monitoring equipment, power system and aircraft charging, reducing dependence on traditional electricity, and are especially suitable for long-term use in remote fields and other environments lacking external power sources, improving the environmental friendliness and endurance of the device.

[0019] The present invention has the following beneficial effects: 1. This invention effectively solves the problems of limited monitoring range of ground detection devices and data interruption of high-altitude flight equipment, improving the accuracy and continuity of monitoring. By combining the ground mobility of the carrier with the high-altitude and rugged area mobility of the aircraft, it achieves multi-dimensional and wide-range environmental monitoring from the ground to the high altitude, avoiding false alarms caused by incomplete monitoring at a single altitude. At the same time, the aircraft can replenish energy in time through the carrier's contact charging structure, with contact plates and circular plates, and in conjunction with the carrier's solar power supply system, significantly extending the flight time, ensuring the continuity of monitoring data, and providing a reliable basis for decision-making. 2. In this invention, the protective capability of flight equipment in complex environments is enhanced, and the operation and maintenance costs are reduced. With the help of the carrier's storage and fixing structure, when encountering severe weather such as heavy rain and strong winds, the aircraft can enter the placement compartment through the meshing linkage of the first gear and the sliding plate, and be clamped and fixed by the first stabilizing plate and the second stabilizing plate. The soft interlayer buffers and reduces vibration damage, which solves the problem of insufficient protection and easy damage of traditional flight equipment, reduces equipment failure and maintenance costs, and ensures the stable operation of high-altitude monitoring functions. Attached Figure Description

[0020] Figure 1 This is a schematic diagram of the structure of a remote environmental monitoring device for environmental protection proposed in this invention; Figure 2 This is a schematic diagram of the aircraft structure in this invention; Figure 3 for Figure 2 Enlarged view of point A in the middle; Figure 4 This is a schematic diagram of the side structure in this invention; Figure 5 for Figure 4 Enlarged view of point B in the middle; Figure 6 This is a schematic diagram of the side structure in this invention; Figure 7 for Figure 6 Enlarged view of point C in the middle; Figure 8 This is a top view of the structure in this invention.

[0021] In the diagram: 1. Carrier; 2. Air quality detection board; 3. Sound detection block; 4. Camera board; 5. Information processing box; 6. Signal receiving rod; 7. Sliding plate; 8. First gear; 9. First belt; 10. Bidirectional threaded rod; 11. First stabilizing plate; 12. Second stabilizing plate; 13. Second belt; 14. Rotating rod; 15. First bevel gear; 16. Second bevel gear; 17. Square compartment; 18. Second gear; 19. Gear column; 20. Contact plate; 21. Aircraft; 22. Telescopic extraction rod; 23. Circular plate; 24. Environmental monitoring board; 25. Camera board; 26. Battery block. Detailed Implementation

[0022] The technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of the present invention.

[0023] Please see Figures 1-8As shown, the present invention is a remote environmental monitoring device for environmental protection, comprising a carrier 1, a sliding plate 7 slidably connected above the carrier 1, a first gear 8 meshing with the sliding plate 7, a bidirectional threaded rod 10 drivingly connected to the first gear 8, a first stabilizing plate 11 threadedly connected to the surface of the bidirectional threaded rod 10, a second stabilizing plate 12 threadedly connected to the end of the bidirectional threaded rod 10 away from the first stabilizing plate 11, a rotating rod 14 drivingly connected to the bidirectional threaded rod 10, a first bevel gear 15 fixedly connected to the end of the rotating rod 14 away from the carrier 1, a second bevel gear 16 meshing with the first bevel gear 15, a second gear 18 fixedly connected to the side of the second bevel gear 16, a gear post 19 meshing with the second gear 18, the gear post 19 slidably connected to the carrier 1, a contact plate 20 fixedly connected above the gear post 19, and a detection mechanism for environmental monitoring disposed inside the carrier 1, the detection mechanism including a spacecraft 21 disposed inside the carrier 1, a circular plate 23 disposed at the bottom of the spacecraft 21.

[0024] In one embodiment, the testing mechanism further includes a telescopic pull-out rod 22 disposed on the side of the aircraft 21, a battery block 26 fixedly connected to the bottom of the aircraft 21, and an environmental monitoring board 24 and a camera board 25 disposed on the side of the aircraft 21.

[0025] In one embodiment, the first gear 8 is rotatably connected to the carrier 1, and the first gear 8 is driven by a first belt 9. The end of the first belt 9 away from the first gear 8 is driven by a bidirectional threaded rod 10. The bidirectional threaded rod 10 is rotatably connected to the inner wall of the carrier 1. The first stabilizing plate 11 is slidably connected to the carrier 1. A soft interlayer is provided on the side of the first stabilizing plate 11 near the second stabilizing plate 12. The carrier 1 is slidably connected to the second stabilizing plate 12. A soft interlayer is also provided on the side of the second stabilizing plate 12 near the first stabilizing plate 11. The bidirectional threaded rod 10 is driven by a second belt 13, and a rotating rod 14 is driven by the end of the second belt 13 away from the bidirectional threaded rod 10.

[0026] In one embodiment, for the carrier 1, an air quality detection plate 2 and a sound detection block 3 are provided on the side of the carrier 1, an information processing box 5 for transmitting information is provided inside the carrier 1, a signal receiving rod 6 is fixedly installed on the top of the information processing box 5, and a shooting plate 4 is fixedly connected to the side of the carrier 1.

[0027] In one embodiment, for the carrier 1 described above, a square compartment 17 is provided inside the carrier 1, the square compartment 17 is rotatably connected to the second gear 18, and the rotating rod 14 is rotatably connected to the square compartment 17.

[0028] In this embodiment, the container 17 provides a stable installation and rotation space for the second gear 18 and the rotating rod 14, ensuring the accuracy of gear meshing and power transmission, ensuring the smoothness of mechanical transmission during the storage, fixing and charging of the aircraft 21, and improving the stability and reliability of equipment operation.

[0029] In one embodiment, the carrier 1 described above has multiple sets of rollers at its bottom for movement.

[0030] In this embodiment, multiple sets of rollers give the carrier 1 flexible ground mobility, enabling it to move autonomously or remotely to different monitoring areas on flat surfaces, expanding the ground monitoring range, facilitating the tracking of ground pollution sources, and providing mobile base station support for the aircraft 21, thereby enhancing the overall mobility of the device.

[0031] In one embodiment, the aircraft 21 described above has multiple sets of support legs at its bottom.

[0032] In this embodiment, the outriggers can provide stable support during the take-off and landing of the aircraft 21, preventing the sensors, charging contacts and other components at its bottom from being directly damaged by the ground. At the same time, when the aircraft 21 is stored inside the carrier 1, the outriggers can better adapt to the fixed structure, ensuring a firm fixation and reducing damage caused by shaking.

[0033] In one embodiment, the aircraft 21 described above has a battery at its bottom for storing energy.

[0034] In this embodiment, the battery provides energy for the aircraft 21 to perform monitoring tasks independently, enabling it to have sufficient endurance when it is separated from the carrier 1 to conduct monitoring in high-altitude or rugged areas. In conjunction with the charging structure of the carrier 1, energy can be recycled, further improving the independent working time of the aircraft 21.

[0035] In one embodiment, for the carrier 1 described above, photovoltaic panels for collecting solar energy are provided on both sides of the carrier 1.

[0036] In this embodiment, the photovoltaic panel can convert solar energy into electrical energy and store it in the energy storage device of the carrier 1, providing clean energy for the carrier 1's own monitoring equipment, power system and the charging of the aircraft 21, reducing dependence on traditional electricity, and is especially suitable for long-term use in remote fields and other environments lacking external power sources, thereby improving the environmental friendliness and endurance of the device.

[0037] The working principle of the remote environmental monitoring device for environmental protection in this invention is as follows: Workers can move the carrier 1 to the area to be monitored remotely. Because it has wheels at the bottom, it can be moved remotely. After reaching the designated area, the surrounding environment can be observed through the imaging plates 4 around the carrier 1. Then, the air quality detection plate 2 and the sound detection block 3 begin to work, thereby monitoring the environment, such as the environment and quality near factories and regulating human environments. The air quality detection plate 2 and the sound detection block 3 play a very good role in this regard. The signal receiving rod 6 is used to receive signals to accurately determine the position of the carrier 1. The information processing box 5 is used to transmit the collected information to the cloud for easy viewing by workers. When facing rough roads, the aircraft 21 can be released for monitoring. The aircraft 21 can be used without... During use, it is in a fixed state. If it needs to be released, the first gear 8 is rotated. The rotation of the first gear 8 engages with the sliding plate 7, exposing the placement compartment inside the carrier 1, thus facilitating the movement of the aircraft 21. Then, as the first gear 8 rotates, it drives the bidirectional threaded rod 10 to rotate through the first belt 9. The rotation of the bidirectional threaded rod 10 causes the first stabilizing plate 11 and the second stabilizing plate 12 to move away from each other. At this time, the aircraft 21 is in a contact and fixed state. Then, the staff can remotely control the movement of the aircraft 21 to monitor the environment at high altitudes and on rugged roads. It is worth mentioning that the side of the aircraft 21 is equipped with an environmental monitoring plate 24, which can collect sound and gas in the environment. The camera plate 25 can monitor the surrounding environment, so that the staff can understand the overall environmental situation of the area.

[0038] When in water, the telescopic extraction rod 22 can be extended to detect the water quality in the area. Multiple samples taken upstream and downstream can determine the water quality of the area. In case of heavy rain or strong winds, the aircraft 21 is pre-controlled to enter the interior of the carrier 1. After the aircraft 21 enters the bottom of the carrier 1, the first gear 8 is controlled to rotate in the reverse direction, causing the sliding plate 7 to block the opening of the internal storage compartment of the carrier 1. Simultaneously, the reverse rotation of the first gear 8 drives the bidirectional threaded rod 10 to rotate via the first belt 9. The bidirectional threaded rod 10 further drives the first stabilizing plate 11 and the second stabilizing plate 12 to move closer together. When the first stabilizing plate 11 and the second stabilizing plate 12 move closer together, they clamp the aircraft 21. To prevent damage to the wings and other components of the aircraft 21 due to frequent shaking during movement, the first stabilizing plate 11 and the second stabilizing plate 12 are provided with a soft interlayer on the side near the aircraft 21 to provide some cushioning. Then, while the bidirectional threaded rod 10 rotates, it also drives the rotating rod 14 to rotate through the second belt 13. The rotation of the rotating rod 14 continues to utilize the meshing of the first bevel gear 15 and the second bevel gear 16 to rotate the second gear 18. After the second gear 18 rotates, it meshes with the tooth column 19, causing the contact plate 20 above the tooth column 19 to contact the circular plate 23 for contact charging. Subsequently, the aircraft 21 is in standby mode and uploads the collected information to the cloud.

[0039] Although embodiments of the invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principles and spirit of the invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A remote environmental monitoring device for environmental protection, characterized in that, The carrier (1) includes a sliding plate (7) slidably connected above the carrier (1). The sliding plate (7) is meshed with a first gear (8). The first gear (8) is driven by a bidirectional threaded rod (10). A first stabilizing plate (11) is threadedly connected to the surface of the bidirectional threaded rod (10). A second stabilizing plate (12) is threadedly connected to the end of the bidirectional threaded rod (10) away from the first stabilizing plate (11). A rotating rod (14) is driven by the bidirectional threaded rod (10). A first bevel tooth is fixedly connected to the end of the rotating rod (14) away from the carrier (1). The first bevel gear (15) is meshed with a second bevel gear (16), and a second gear (18) is fixedly connected to the side of the second bevel gear (16). The second gear (18) is meshed with a toothed column (19), which is slidably connected to the carrier (1). A contact plate (20) is fixedly connected above the toothed column (19). The carrier (1) is equipped with a detection mechanism for environmental monitoring. The detection mechanism includes an aircraft (21) installed inside the carrier (1). A circular plate (23) is installed at the bottom of the aircraft (21).

2. The remote environmental monitoring device for environmental protection according to claim 1, characterized in that, The detection mechanism also includes a telescopic extraction rod (22) set on the side of the aircraft (21), a battery block (26) fixedly connected to the bottom of the aircraft (21), and an environmental monitoring board (24) and a camera board (25) set on the side of the aircraft (21).

3. The remote environmental monitoring device for environmental protection according to claim 1, characterized in that, The first gear (8) is rotatably connected to the carrier (1). The first gear (8) is driven by a first belt (9). The end of the first belt (9) away from the first gear (8) is driven by a bidirectional threaded rod (10). The bidirectional threaded rod (10) is rotatably connected to the inner wall of the carrier (1). The first stabilizing plate (11) is slidably connected to the carrier (1). The side of the first stabilizing plate (11) near the second stabilizing plate (12) is provided with a soft interlayer. The carrier (1) is slidably connected to the second stabilizing plate (12). The side of the second stabilizing plate (12) near the first stabilizing plate (11) is also provided with a soft interlayer. The bidirectional threaded rod (10) is driven by a second belt (13). The end of the second belt (13) away from the bidirectional threaded rod (10) is driven by a rotating rod (14).

4. A remote environmental monitoring device for environmental protection according to claim 1, characterized in that, The carrier (1) is provided with an air quality detection plate (2) and a sound detection block (3) on its side. The carrier (1) is provided with an information processing box (5) for transmitting information. A signal receiving rod (6) is fixedly installed on the top of the information processing box (5). A shooting plate (4) is fixedly connected to the side of the carrier (1).

5. A remote environmental monitoring device for environmental protection according to claim 1, characterized in that, The carrier (1) has a square compartment (17) inside, the square compartment (17) is rotatably connected to the second gear (18), and the rotating rod (14) is rotatably connected to the square compartment (17).

6. A remote environmental monitoring device for environmental protection according to claim 1, characterized in that, The carrier (1) has multiple sets of rollers at its bottom for movement.

7. A remote environmental monitoring device for environmental protection according to claim 1, characterized in that, The aircraft (21) has multiple sets of support legs at its bottom.

8. A remote environmental monitoring device for environmental protection according to claim 1, characterized in that, The aircraft (21) has batteries at its bottom for storing energy.

9. A remote environmental monitoring device for environmental protection according to claim 1, characterized in that, The carrier (1) has photovoltaic panels on both sides for collecting solar energy.

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