Distribution network monitoring data transmission system and device based on distributed wireless communication technology

Abstract

The present invention discloses a distribution network monitoring data transmission system based on distributed wireless communication technology, including: the distribution network is interconnected with a plurality of distribution terminals through cables. The data acquisition module is used to collect the power distribution of the distribution network. The processing module is used to receive the information collected by the data acquisition module. The monitoring main station is used to receive the information processed by the processing module. The protection module is used to protect the distribution network. The early warning module is used to monitor the alarm of the main station. The inspection module is a drone equipped with a probe. The inspection module starts the inspection through the processing module, and feeds back the inspection content to the processing module through wireless communication technology. Finally, the data is stored and analyzed by the monitoring main station. The inspection equipment designed by the present invention, by stripping the blades in the traditional drone, does not involve the blades during normal use, thereby preventing safety accidents caused by the breakage and scattering of high-speed rotating blades in advance.

Description

Technical Field

[0001] The present invention relates to the field of power distribution network monitoring, and in particular to a power distribution network monitoring data transmission system and device based on distributed wireless communication technology. Background Art

[0002] The distribution network monitoring data transmission system is a system that uses modern communication technology to monitor and transmit data to the distribution network. Such a system usually includes components such as sensors, communication equipment, data acquisition and processing units, and monitoring centers. The following are the main features and functions of the system.

[0003] Sensor network: The distribution network monitoring system deploys a series of sensors to measure various parameters in the distribution network, such as current, voltage, frequency, temperature, etc. These sensors are responsible for collecting real-time grid operation data.

[0004] Communication technology: Using distributed wireless communication technology, the system can achieve data transmission between sensor nodes. Common communication technologies include wireless sensor networks, IoT communication protocols, and possible cellular networks or satellite communications.

[0005] Data collection and processing: The collected data is processed by the local processing unit, which may include steps such as data filtering, compression and conversion. The processed data is sent to the monitoring center or cloud platform for further analysis and storage.

[0006] Remote monitoring and management: The system allows remote monitoring and management, and operation and maintenance personnel can view the operating status of the distribution network in real time through the monitoring center. This helps to quickly identify problems, perform fault diagnosis and implement remote control.

[0007] Real-time alarm and fault inspection: The system has a real-time alarm function, which can immediately notify the operation and maintenance personnel when a grid anomaly or fault is detected. This helps to take timely measures to prevent potential problems.

[0008] Visual interface: The monitoring center usually provides an intuitive visual interface to display the topology of the distribution network and the real-time data of each node. This helps operation and maintenance personnel quickly understand the overall status of the power grid.

[0009] Security: Since it involves the power system, the system design should take security into consideration. Encryption technology is used to ensure the confidentiality of data, and access rights are set up to ensure the safe operation of the system.

[0010] Historical data storage and analysis: The system may store historical data in a database for subsequent analysis, report generation, and long-term monitoring of grid performance.

[0011] The whole system mostly uses drones in the inspection module. Drones are unmanned aerial vehicles with no pilot on board, and can be controlled remotely using radio waves. Unlike ordinary aircraft, drones do not have separate space and safety devices for the pilot, so they can be miniaturized and lightweight, and can be used for information collection and reconnaissance in places that are difficult for humans to reach, and can also be used for various industrial purposes. Especially with the popularity of small drones, drones are used as hobby tools for ordinary people.

[0012] A conventional UAV includes a main body formed by an aircraft skeleton, a propulsion support frame radially protruding from the main body, and a plurality of propellers. The motor on the propeller is directly connected to the propulsion support frame so that the blades rotate at high speed to propel the main body.

[0013] As a result, propellers composed of blades and motors with high-speed rotating blades are generally arranged in large numbers at the outermost edge of the drone body. There is a risk of the propeller motor being damaged due to collisions with other drones and external obstacles, or the high-speed rotating blades breaking and scattering, causing safety accidents, and increasing the drone maintenance cost due to damage to the expensive propeller motor. Summary of the invention

[0014] The purpose of the present invention is to provide a distribution network monitoring data transmission system and device based on distributed wireless communication technology to solve the above technical problems.

[0015] In order to solve the above technical problems, the present invention adopts the following technical solutions:

[0016] The distribution network monitoring data transmission system based on distributed wireless communication technology is characterized by including:

[0017] A power distribution network is interconnected with a plurality of power distribution terminals through cables, and is used to distribute electricity for use by the power distribution terminals.

[0018] A data acquisition module is used to collect power distribution information of the power distribution network.

[0019] The processing module is used to receive the information collected by the data collection module and process the information.

[0020] The monitoring main station is used to receive the information processed by the processing module and send processing instructions to the processing module.

[0021] A protection module is used to protect the power distribution network, and the protection module is started through the wireless communication of the processing module.

[0022] An early warning module is activated by the processing module and is used to monitor the alarm of the main station.

[0023] Inspection module, the inspection module is a drone equipped with a probe. The inspection module starts the inspection through the processing module, and feeds back the inspection content to the processing module through wireless communication technology. Finally, the data is stored and analyzed by the monitoring main station.

[0024] A patrol module, comprising:

[0025] The shell has a groove inside, and the groove is used for air flow.

[0026] The propulsion mechanism is located at the edge of the shell and is fixedly connected to the shell, and is used to push the shell to rise.

[0027] An air bleed mechanism is located inside the groove and fixedly connected to the groove, and is used to transport gas to the inside of the propulsion mechanism.

[0028] The supporting mechanism is located below the shell and is fixedly connected to the shell, and is used to support the shell.

[0029] The regulating mechanism is located inside the shell and is used to adjust the air flow conveying size of the air bleed mechanism.

[0030] The air bleed mechanism comprises a support seat, the support seat is located inside a groove on the shell, the support seat is fixedly connected to the shell, and a mounting shaft is fixedly connected to the top of the support seat.

[0031] The portion of the installation shaft located in the groove is in a truncated cone shape.

[0032] An upper compressed air blower is installed on the installation shaft, a lower compressed air blower is arranged below the upper compressed air blower, and the lower compressed air blower is fixedly connected to the installation shaft.

[0033] A fixed propeller is located between the upper compressed air blower and the lower compressed air blower, and the fixed propeller is fixedly connected to the shell.

[0034] Preferably, the propulsion mechanism comprises:

[0035] The propeller has two truncated cone-shaped grooves arranged inside, and the two truncated cone-shaped grooves are connected.

[0036] A spiral hole is provided inside the propeller, one end of the spiral hole is connected to the groove of the shell, and the other end of the spiral hole is tilted downward and aligned with the truncated cone-shaped groove located above.

[0037] Deflection plates, a plurality of said deflection plates are located inside the truncated cone-shaped groove and are fixedly connected to the propeller.

[0038] Preferably, the supporting mechanism comprises:

[0039] A support tube is located below the shell and is fixedly connected to the shell, and the support tube is L-shaped.

[0040] The mounting plate is located inside the support tube and is fixedly connected to the support plate.

[0041] A dual-axis motor is located between two mounting plates and is fixedly connected to the mounting plates.

[0042] One-way components, two of which are located at two ends of the dual-axis motor and are fixedly connected to the dual-axis motor.

[0043] Preferably, the one-way component comprises:

[0044] A connecting frame, the connecting frame located below the dual-axis motor is fixedly connected to the power output shaft of the dual-axis motor, and the connecting frame located above the dual-axis motor is fixedly connected to the adjustment mechanism.

[0045] A ratchet ring is fixedly connected to the connecting frame.

[0046] The second rotating shaft, the second rotating shaft located below the dual-axis motor is rotatably connected to the support tube, and the second rotating shaft located above the dual-axis motor is fixedly connected to the power output shaft of the dual-axis motor.

[0047] A toggle plate, wherein the toggle plate is located inside the ratchet ring, the toggle plate is fixedly connected to the second rotating shaft, and the toggle plate is used to drive the ratchet ring to rotate.

[0048] A rotating ring is located above the dual-axis motor, the rotating ring is fixedly connected to the housing, and the rotating ring is rotatably connected to the ratchet ring.

[0049] Preferably, the adjustment mechanism comprises:

[0050] The first rotating shaft penetrates the shell and extends into the groove, the first rotating shaft is rotatably connected to the shell, and the first rotating shaft is fixedly connected to the connecting frame.

[0051] A fixed spherical shell is located inside the groove and fixedly connected to the housing, and the fixed spherical shell is communicated with the spiral hole on the propeller.

[0052] A sealing ball is located inside the fixed ball shell, a through hole is formed through the sealing ball, and the sealing ball is fixedly connected to the first rotating shaft.

[0053] Preferably, the hollow tube is fixedly connected to the support tube.

[0054] An installation cover is located above the hollow tube and is fixedly connected to the hollow tube.

[0055] A third rotating shaft is located inside the hollow tube and is rotatably connected to the hollow tube.

[0056] The two pulleys are fixedly mounted on the second rotating shaft and the third rotating shaft respectively.

[0057] A connecting belt is installed on two pulleys, and the connecting belt is matched with the pulleys to make the second rotating shaft and the third rotating shaft rotate synchronously.

[0058] The partition is located inside the support tube and is fixedly connected to the support tube. The partition is used to block the support tube. A groove is provided on the partition, and the groove is used to place the connecting belt.

[0059] Preferably, the connecting ring is fixedly mounted on the third rotating shaft.

[0060] The first wing is fixedly connected to the connecting ring, and the first wing is fixedly connected to a fourth rotating shaft.

[0061] The second wing is fixedly connected with a fourth rotating shaft, and the second wing is rotatably connected with the fourth rotating shaft on the first wing.

[0062] The third wing is fixedly connected with a fourth rotating shaft, and the third wing is rotationally connected with the fourth rotating shaft on the second wing.

[0063] A fourth wing is rotatably connected to a fourth rotating shaft on the third wing.

[0064] The beneficial effects of the present invention are:

[0065] 1. The inspection equipment designed by the present invention can prevent safety accidents caused by the breakage and scattering of high-speed rotating blades by stripping the blades of the traditional drone in normal use. The present invention can improve the lift generated by the propeller by discharging high-pressure and high-speed air to the outside through the propeller, and can improve the lift generated by the propeller and the driving efficiency relative to the driving force of the compressed air generating part by compressing the external air sucked by the compressed air generating part to a predetermined pressure and supplying it to the propeller.

[0066] 2. By setting up a support tube, the support tube itself can not only play a supporting role, but also be used to store the driving source. By using the driving source, the driving source can act on the blocking ball, so that the blocking ball controls the amount of gas entering each thruster. Due to the change in the intake volume, the propulsion force will also change, so that the UAV body can rotate and move stably in a horizontal state, and when the propulsion gas volume is balanced, the flight stability can also be improved.

[0067] 3. Through the one-way component, the driving mode of the driving source can be changed, so that the driving source can effectively act on the first wing, the second wing, the third wing, and the fourth wing without affecting the blocking ball. The first wing, the second wing, the third wing, and the fourth wing can effectively play an auxiliary flight role, and the second wing can be stretched by centrifugal force during flight. Even if the wing hits an object during flight, the second wing can be rotated and folded through the hinge part to minimize damage to the wing or the object. In addition, the second wing can be folded through the hinge part for easy storage. BRIEF DESCRIPTION OF THE DRAWINGS

[0068] Figure 1 This is a schematic diagram of the principle of the power distribution network monitoring data transmission system of the present invention;

[0069] Figure 2 It is a structural schematic diagram of the inspection module of the present invention;

[0070] Figure 3 It is a schematic diagram of the internal structure of the housing of the present invention;

[0071] Figure 4 for Figure 3 A magnified schematic diagram of part A;

[0072] Figure 5 Schematic diagram of the internal structure of the propeller of the present invention;

[0073] Figure 6 It is a structural schematic diagram of the regulating mechanism of the present invention;

[0074] Figure 7 It is a schematic diagram of the internal structure of the support tube of the present invention;

[0075] Figure 8 for Figure 7 An enlarged schematic diagram of part B;

[0076] Fig. 9 for Figure 8 An enlarged schematic diagram of the C portion;

[0077] Fig.10 It is a schematic diagram of the structure of the one-way component of the present invention;

[0078] Fig.11 is a schematic diagram of the connection between the first wing and the fourth wing of the present invention;

[0079] Fig.12 It is a top view of the inspection module of the present invention.

[0080] 1. Shell; 2. Propeller; 3. Support tube; 4. Support seat; 6. Mounting shaft; 7. Upper compressed air blower; 8. Fixed propeller; 9. Lower compressed air blower; 10. Deflection plate; 11. Spiral hole; 12. Fixed ball shell; 13. Sealing ball; 14. First rotating shaft; 15. Mounting plate; 16. Dual-axis motor; 17. Pulley; 18. Second rotating shaft; 19. Connecting belt; 20. Hollow tube; 21. Mounting cover; 22. Third rotating shaft; 23. Partition; 25. Connecting frame; 26. Ratchet ring; 28. Paddle plate; 29. ​​First wing; 30. Second wing; 31. Fourth rotating shaft; 32. Third wing; 33. Fourth wing; 34. Connecting ring; 35. Rotating ring. DETAILED DESCRIPTION

[0081] In order to make the technical means, creative features, objectives and effects of the present invention easy to understand, the present invention is further described below in conjunction with specific embodiments and drawings, but the following embodiments are only preferred embodiments of the present invention, not all. Based on the embodiments in the implementation mode, other embodiments obtained by those skilled in the art without creative work are all within the scope of protection of the present invention.

[0082] The specific embodiments of the present invention are described below with reference to the accompanying drawings.

[0083] Embodiment 1:

[0084] like Figure 1-11 As shown;

[0085] Distributed wireless communication technology covers a variety of wireless communication technologies used to build distributed systems.

[0086] The distribution network monitoring data transmission system based on distributed wireless communication technology includes:

[0087] Distribution network: The distribution network is interconnected with several distribution terminals through cables. The distribution network is used to distribute electricity for use by the distribution terminals.

[0088] The data acquisition module is used to collect the power distribution situation of the distribution network.

[0089] The processing module is used to receive the information collected by the data collection module and process the information.

[0090] The monitoring master station is used to receive information processed by the processing module and send processing instructions to the processing module.

[0091] The protection module is used to protect the power distribution network, and the protection module is activated through the wireless communication of the processing module.

[0092] The early warning module is started by the processing module, and the early warning module is used to monitor the alarm of the main station.

[0093] The inspection module is a drone equipped with a probe. The inspection module starts the inspection through the processing module and feeds back the inspection content to the processing module through wireless communication technology. Finally, the data is stored and analyzed by the monitoring main station.

[0094] Wireless sensor network (WSN) is a network consisting of distributed sensor nodes that can communicate with each other through wireless communication protocols. WSN is usually used to monitor various parameters in the environment, such as temperature, humidity, pressure, etc.

[0095] IoT is a technology that connects various physical devices and objects through the Internet. It covers a variety of wireless communication technologies, including Wi-Fi, Bluetooth, Zigbee, LoRa, etc., which are used to achieve communication and data transmission between devices.

[0096] Mesh network is a topology in which each node can communicate directly with other nodes to form a self-organizing network. This network structure enhances coverage and reliability and is often used in large-scale sensor networks and Internet of Things applications.

[0097] Zigbee is a low-power, short-range communication protocol that is particularly suitable for the Internet of Things and sensor networks. It supports self-organizing networks and enables reliable communication between devices.

[0098] LoRa is a low-power, long-distance communication technology suitable for long-distance sensor networks. It is mainly used in low-data-rate applications such as urban intelligence and agricultural monitoring.

[0099] NB-IoT is a cellular network technology designed for the Internet of Things. It provides low power consumption, wide coverage, and a large number of connections, and is suitable for communication between remote sensors and devices.

[0100] 5G technology is not only used to provide high-speed mobile communications, but also supports large-scale IoT connections. 5G IoT has the characteristics of low latency, high reliability and large capacity, and is suitable for a variety of application scenarios, including industrial automation, smart cities, etc.

[0101] The combination of the above-mentioned multiple modules enables the distribution network and the monitoring main station to transmit signals through different wireless network transmission methods, thereby achieving effective monitoring effects.

[0102] Embodiment 2:

[0103] like Figure 1-11 As shown, when other parts are the same as those in Example 1, the difference between this embodiment and Example 1 is: a patrol module, including:

[0104] A groove is provided inside the housing 1 for air flow.

[0105] The propulsion mechanism is located at the edge of the shell 1 and is fixedly connected to the shell 1 . The propulsion mechanism is used to push the shell 1 to rise.

[0106] The air bleed mechanism is located inside the groove and is fixedly connected to the groove, and the air bleed mechanism is used to transport gas to the inside of the propulsion mechanism.

[0107] The supporting mechanism is located below the shell 1 and is fixedly connected to the shell 1 , and is used to support the shell 1 .

[0108] The regulating mechanism is located inside the housing 1 and is used to adjust the air flow conveying size of the air bleed mechanism.

[0109] The air bleed mechanism includes a support seat 4 , which is located inside a groove on the shell 1 , and is fixedly connected to the shell 1 , and a mounting shaft 6 is fixedly connected to the top of the support seat 4 .

[0110] The portion of the mounting shaft 6 located in the groove is in the shape of a truncated cone.

[0111] An upper compressed air blower 7 is installed on the installation shaft 6 , and a lower compressed air blower 9 is arranged below the upper compressed air blower 7 . The lower compressed air blower 9 is fixedly connected to the installation shaft 6 .

[0112] The fixed propeller 8 is located between the upper compressed air blower 7 and the lower compressed air blower 9 , and the fixed propeller 8 is fixedly connected to the housing 1 .

[0113] The promotion agencies include:

[0114] The propeller 2 has two truncated cone-shaped grooves disposed inside the propeller 2, and the two truncated cone-shaped grooves are connected.

[0115] A spiral hole 11 is provided inside the propeller 2 , one end of the spiral hole 11 is connected to the groove of the housing 1 , and the other end of the spiral hole 11 is tilted downward and aligned with the truncated cone-shaped groove located above.

[0116] The deflection plates 10 , wherein a plurality of deflection plates 10 are located inside the truncated cone-shaped groove and are fixedly connected to the propeller 2 .

[0117] By arranging the upper compressed air blower 7, the lower compressed air blower 9 and the fixed propeller 8, the external gas can be sucked into the shell 1 with the help of the blower, and because the groove at the shell 1 gradually becomes smaller, the gas can be better compressed.

[0118] The compressed gas will enter the propeller 2, flow along the spiral hole 11 in the propeller 2, and be ejected downward at the highest point, thereby providing an upward lift, which can effectively make it fly and effectively prevent the propeller from breaking.

[0119] Embodiment 3:

[0120] like Figure 1-11 As shown, when other parts are the same as those in Example 1, the difference between this embodiment and Example 1 is that: the supporting mechanism:

[0121] The support tube 3 is located below the shell 1 and is fixedly connected to the shell 1 . The support tube 3 is L-shaped.

[0122] The mounting plate 15 is located inside the support tube 3 and is fixedly connected to the support plate.

[0123] The dual-axis motor 16 is located between the two mounting plates 15 , and the dual-axis motor 16 is fixedly connected to the mounting plates 15 .

[0124] The two one-way components are respectively located at two ends of the dual-axis motor 16 and are fixedly connected to the dual-axis motor 16 .

[0125] One-way components include:

[0126] The connecting frame 25 , which is located below the dual-axis motor 16 , is fixedly connected to the power output shaft of the dual-axis motor 16 , and the connecting frame 25 which is located above the dual-axis motor 16 is fixedly connected to the adjusting mechanism.

[0127] The ratchet ring 26 is fixedly connected to the connecting frame 25 .

[0128] The second rotating shaft 18 located below the dual-axis motor 16 is rotatably connected to the support tube 3 , and the second rotating shaft 18 located above the dual-axis motor 16 is fixedly connected to the power output shaft of the dual-axis motor 16 .

[0129] The paddle plate 28 is located inside the ratchet ring 26 . The paddle plate 28 is fixedly connected to the second rotating shaft 18 . The paddle plate 28 is used to drive the ratchet ring 26 to rotate.

[0130] The rotating ring 35 is located above the dual-axis motor 16 . The rotating ring 35 is fixedly connected to the housing 1 . The rotating ring 35 is rotatably connected to the ratchet ring 26 .

[0131] The first rotating shaft 14 passes through the housing 1 and extends to the inside of the groove. The first rotating shaft 14 is rotatably connected to the housing 1 , and the first rotating shaft 14 is fixedly connected to the connecting frame 25 .

[0132] The fixed spherical shell 12 is located inside the groove and is fixedly connected to the housing 1 . The fixed spherical shell 12 is communicated with the spiral hole 11 on the propeller 2 .

[0133] The blocking ball 13 is located inside the fixed ball shell 12 . A through hole is formed through the blocking ball 13 . The blocking ball 13 is fixedly connected to the first rotating shaft 14 .

[0134] By starting the dual-axis motor 16, the dual-axis motor 16 reverses, so that the top end of the dual-axis motor 16 will drive the third rotating shaft 22 to rotate, and the third rotating shaft 22 will drive the ratchet ring 26 to rotate through the paddle plate 28, so that the ratchet ring 26 will drive the first rotating shaft 14 to rotate through the connecting frame 25, and the first rotating shaft 14 will drive the blocking ball 13 to rotate, so that the blocking ball 13 will change the space inside the fixed shell 1, so that the size of the gap through which the gas can pass will change, and the flow size of the gas will also change.

[0135] When the size of the gas flow gaps at points b and c is reduced, the airflow at points a and d will be greater than that at points b and c, and the entire device will rotate counterclockwise.

[0136] When the size of the gas flow gaps at a and d is reduced, the airflow inflow at b and c will be greater than that at a and d, and the entire device will rotate clockwise.

[0137] When the size of the gas flow gaps at a and c is reduced, the airflow inflow at b and d is made greater than that at a and c, and the entire device will move to the left.

[0138] When the size of the gas flow gaps at b and d is reduced, the airflow inflow at a and c is greater than that at b and d, and the entire device will move to the right.

[0139] Embodiment 4:

[0140] like Figure 1-11 As shown, when other parts are the same as those in Example 1, the difference between this embodiment and Example 1 lies in: a hollow tube 20, and the hollow tube 20 is fixedly connected to the support tube 3.

[0141] The mounting cover 21 is located above the hollow tube 20 and is fixedly connected to the hollow tube 20 .

[0142] The third rotating shaft 22 is located inside the hollow tube 20 and is rotatably connected to the hollow tube 20 .

[0143] The two pulleys 17 are fixedly mounted on the second rotating shaft 18 and the third rotating shaft 22 respectively.

[0144] The connecting belt 19 is installed on the two pulleys 17 , and the connecting belt 19 cooperates with the pulleys 17 to make the second rotating shaft 18 and the third rotating shaft 22 rotate synchronously.

[0145] The partition 23 is located inside the support tube 3 and is fixedly connected to the support tube 3 . The partition 23 is used to block the support tube 3 . A groove is provided on the partition 23 , and the groove is used to place the connecting belt 19 .

[0146] The connecting ring 34 is fixedly mounted on the third rotating shaft 22 .

[0147] The first wing 29 is fixedly connected to the connecting ring 34 , and a fourth rotating shaft 31 is fixedly connected to the first wing 29 .

[0148] A fourth rotating shaft 31 is fixedly connected to the second wing 30 , and the second wing 30 is rotatably connected to the fourth rotating shaft 31 on the first wing 29 .

[0149] The third wing 32 is fixedly connected with the fourth rotating shaft 31 , and the third wing 32 is rotatably connected with the fourth rotating shaft 31 on the second wing 30 .

[0150] The fourth wing 33 is rotatably connected to the fourth rotating shaft 31 on the third wing 32 .

[0151] When the dual-axis motor 16 rotates forward, the dual-axis motor 16 does not act on the first rotating shaft 14, but drives the ratchet ring 26 through the connecting frame 25, so that the ratchet ring 26 drives the second rotating shaft 18 to rotate through the paddle plate 28, and the second rotating shaft 18 drives the third rotating shaft 22 to rotate through the connecting belt 19 and the pulley 17, and the third rotating shaft 22 drives the first wing 29, the second wing 30, the third wing 32, and the fourth wing 33 to rotate.

[0152] The second wing 30 can be stretched by centrifugal force during flight, and even if the wing hits an object during flight, the second wing 30 can be rotated and folded by the hinge portion to minimize damage to the wing or the object. In addition, the second wing 30 can be folded by the hinge portion for easy storage.

[0153] The above shows and describes the basic principles, main features and advantages of the present invention. Those skilled in the art should understand that the present invention is not limited by the above embodiments. The above embodiments and descriptions are only preferred examples of the present invention and are not intended to limit the present invention. Without departing from the spirit and scope of the present invention, the present invention may have various changes and improvements, which fall within the scope of the present invention. The scope of protection of the present invention is defined by the attached claims and their equivalents.

Claims

1. The distribution network monitoring data transmission system based on distributed wireless communication technology is characterized by ,include: A distribution network, the distribution network is interconnected with a plurality of distribution terminals through cables, and the distribution network is used to distribute electricity for use by the distribution terminals; A data acquisition module, wherein the data acquisition module is used to collect information about power distribution in the power distribution network; A processing module, the processing module is used to receive the information collected by the data collection module and process the information; A monitoring main station, the monitoring main station is used to receive information processed by the processing module and send processing instructions to the processing module; A protection module, the protection module is used to protect the power distribution network, and the protection module is activated through wireless communication of the processing module; An early warning module, which is activated by the processing module and is used to monitor the alarm of the master station; Inspection module, which is a drone equipped with a probe. The inspection module starts inspection through the processing module and feeds back the inspection content to the processing module through wireless communication technology. Finally, the data is stored and analyzed by the monitoring master station; The inspection module comprises: A housing (1), wherein a groove is provided inside the housing (1), and the groove is used for airflow; A propulsion mechanism, the propulsion mechanism being located at an edge of the shell (1) and fixedly connected to the shell (1), the propulsion mechanism being used to propel the shell (1) upward; An air entrainment mechanism, the air entrainment mechanism is located inside the groove and fixedly connected to the groove, and the air entrainment mechanism is used to transport gas into the propulsion mechanism; A supporting mechanism, the supporting mechanism being located below the shell (1) and fixedly connected to the shell (1), the supporting mechanism being used to support the shell (1); An adjusting mechanism, the adjusting mechanism being located inside the housing (1) and being used to adjust the airflow conveying size of the air bleed mechanism; The air entrainment mechanism comprises a support seat (4), the support seat (4) is located inside a groove on the shell (1), the support seat (4) is fixedly connected to the shell (1), and a mounting shaft (6) is fixedly connected to the top of the support seat (4); The portion of the installation shaft (6) located in the groove is in the shape of a truncated cone; An upper compressed air blower (7) is mounted on the mounting shaft (6), a lower compressed air blower (9) is arranged below the upper compressed air blower (7), and the lower compressed air blower (9) is fixedly connected to the mounting shaft (6); a fixed propeller (8), the fixed propeller (8) being located between the upper compressed air blower (7) and the lower compressed air blower (9), and the fixed propeller (8) being fixedly connected to the housing (1); The propulsion mechanism comprises: A propeller (2), wherein two truncated cone-shaped grooves are provided inside the propeller (2), and the two truncated cone-shaped grooves are connected; A spiral hole (11) is provided inside the propeller (2), one end of the spiral hole (11) is connected to the groove of the housing (1), and the other end of the spiral hole (11) is tilted downward and aligned with the truncated cone-shaped groove located above; Deflection plates (10), a plurality of the deflection plates (10) being located inside the truncated cone-shaped groove and fixedly connected to the propeller (2); The supporting mechanism comprises: A support tube (3), the support tube (3) being located below the shell (1) and fixedly connected to the shell (1), and the support tube (3) being L-shaped; A mounting plate (15), the mounting plate (15) being located inside the support tube (3) and fixedly connected to the support plate; A dual-axis motor (16), the dual-axis motor (16) being located between two mounting plates (15), the dual-axis motor (16) being fixedly connected to the mounting plates (15); One-way components, two of the one-way components are respectively located at two ends of the dual-axis motor (16) and are fixedly connected to the dual-axis motor (16); The one-way component comprises: A connecting frame (25), the connecting frame (25) located below the dual-axis motor (16) is fixedly connected to the power output shaft of the dual-axis motor (16), and the connecting frame (25) located above the dual-axis motor (16) is fixedly connected to the adjustment mechanism; A ratchet ring (26), wherein the ratchet ring (26) is fixedly connected to the connecting frame (25); a second rotating shaft (18), the second rotating shaft (18) located below the dual-axis motor (16) being rotationally connected to the support tube (3), and the second rotating shaft (18) located above the dual-axis motor (16) being fixedly connected to the power output shaft of the dual-axis motor (16); a toggle plate (28), the toggle plate (28) being located inside the ratchet ring (26), the toggle plate (28) being fixedly connected to the second rotating shaft (18), and the toggle plate (28) being used to drive the ratchet ring (26) to rotate; A rotating ring (35), the rotating ring (35) being located above the dual-axis motor (16), the rotating ring (35) being fixedly connected to the housing (1), and the rotating ring (35) being rotatably connected to the ratchet ring (26); The regulating mechanism comprises: a first rotating shaft (14), the first rotating shaft (14) passing through the housing (1) and extending into the interior of the groove, the first rotating shaft (14) being rotatably connected to the housing (1), and the first rotating shaft (14) being fixedly connected to the connecting frame (25); a fixed spherical shell (12), the fixed spherical shell (12) being located inside the groove and fixedly connected to the housing (1), the fixed spherical shell (12) being connected to the spiral hole (11) on the propeller (2); A blocking ball (13), the blocking ball (13) being located inside the fixed ball shell (12), a through hole being formed through the blocking ball (13), and the blocking ball (13) being fixedly connected to the first rotating shaft (14).

2. The distribution network monitoring data transmission system based on distributed wireless communication technology according to claim 1 is characterized in that: The inspection module also includes: A hollow tube (20), wherein the hollow tube (20) is fixedly connected to the support tube (3); A mounting cover (21), the mounting cover (21) being located above the hollow tube (20) and fixedly connected to the hollow tube (20); a third rotating shaft (22), the third rotating shaft (22) being located inside the hollow tube (20) and being rotatably connected to the hollow tube (20); Pulleys (17), wherein the two pulleys (17) are fixedly mounted on the second rotating shaft (18) and the third rotating shaft (22), respectively; A connecting belt (19), wherein the connecting belt (19) is mounted on two pulleys (17), and the connecting belt (19) cooperates with the pulleys (17) to enable the second rotating shaft (18) and the third rotating shaft (22) to rotate synchronously; A partition (23), the partition (23) being located inside the support tube (3) and fixedly connected to the support tube (3), the partition (23) being used to seal the support tube (3), the partition (23) being provided with a groove, the groove being used to place the connection belt (19).

3. The distribution network monitoring data transmission system based on distributed wireless communication technology according to claim 2 is characterized in that: The inspection module also includes: a connecting ring (34), wherein the connecting ring (34) is fixedly mounted on the third rotating shaft (22); A first wing (29), the first wing (29) being fixedly connected to a connecting ring (34), and a fourth rotating shaft (31) being fixedly connected to the first wing (29); a second wing (30), wherein a fourth rotating shaft (31) is fixedly connected to the second wing (30), and the second wing (30) is rotatably connected to the fourth rotating shaft (31) on the first wing (29); a third wing (32), the third wing (32) being fixedly connected to a fourth rotating shaft (31), the third wing (32) being rotationally connected to the fourth rotating shaft (31) on the second wing (30); A fourth wing (33), the fourth wing (33) being rotationally connected to a fourth rotating shaft (31) on the third wing (32).

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