Unmanned aerial vehicle inspection system

Abstract

The technical problem to be solved by the utility model is to provide the unmanned aerial vehicle inspection system, which effectively improves the inspection efficiency, can realize fixed-line inspection and task inspection, is more comprehensive in inspection range, can timely find hidden dangers, and effectively reduces the labor intensity of inspection and the risk of serious accidents. The unmanned aerial vehicle inspection system comprises an unmanned aerial vehicle, an automatic airport, an unmanned aerial vehicle nest, a server and an operation terminal, the unmanned aerial vehicle is provided with a multifunctional holder mount, and the multifunctional holder mount is used for carrying shooting equipment or a thermal infrared imager. Video inspection and temperature detection are carried out on equipment in a photovoltaic plant area through the arranged unmanned aerial vehicle carrying shooting equipment and the thermal infrared imager, the inspection efficiency is improved, different task instructions are issued to the unmanned aerial vehicle through the operation terminal, fixed-line inspection and task inspection can be achieved, the inspection range is more comprehensive, key parts can be inspected more accurately, and the inspection efficiency is improved. Hidden dangers can be found in time, and the risk of serious accidents is effectively reduced.

Description

Technical Field

[0001] The utility model relates to the technical field of photovoltaic power generation, and in particular to an unmanned aerial vehicle inspection system. Background Art

[0002] The operation and maintenance of photovoltaic power stations has emerged with the development of the photovoltaic industry. It is mainly to ensure the normal promotion of power generation. The operation and maintenance of photovoltaic power stations is of great significance in ensuring the normal operation of power stations and improving power generation efficiency. In order to meet the existing challenges, the photovoltaic industry needs to continuously explore new operation and maintenance management models and improve the level of operation and maintenance management to achieve safe and efficient operation of photovoltaic power stations. At present, the operation and maintenance of photovoltaic power stations mainly adopts periodic inspections and periodic equipment performance tests. This operation and maintenance model has periodic restrictions and equipment limitations, requires a lot of manpower and material resources, has a long inspection time and relatively low inspection efficiency, and is prone to inspection blind spots. Utility Model Content

[0003] The technical problem to be solved by the utility model is to provide a drone inspection system, which effectively improves the inspection efficiency, can realize line inspection and task inspection, has a more comprehensive inspection range, can discover hidden dangers in time, and effectively reduces the labor intensity of inspection and the risk of serious accidents.

[0004] The technical solution adopted by the utility model to solve the above technical problems is: the unmanned aerial vehicle inspection system includes a unmanned aerial vehicle, an automated airport, an unmanned aerial vehicle nest, a server, and an operation terminal;

[0005] The automated airport is connected to the server through a wired network, a firewall is provided between the automated airport and the server, and the operation terminal is connected to the server through an intranet;

[0006] The automated airport is provided with a 4 / 5G network, and the drone is connected to the automated airport through the 4 / 5G network;

[0007] The UAV is provided with a multifunctional gimbal mount, and the multifunctional gimbal mount is used to carry a shooting device or an infrared thermal imager;

[0008] The drone nest is arranged in an automated airport, and is used for parking and charging drones.

[0009] Furthermore, the drone nest comprises a first shell with an open upper end;

[0010] The upper end of the first shell is provided with a fixed cover plate and a movable cover plate, the fixed cover plate is provided at the rear end of the opening of the first shell through a detachable structure, and the movable cover plate is provided at the front end of the opening of the first shell through a sliding structure and the two are in sliding contact;

[0011] A partition plate is provided in the first shell, and the partition plate divides the inner cavity of the first shell into an energy compartment and a storage and charging compartment;

[0012] A storage battery is arranged in the energy warehouse, and the storage battery is electrically connected to the photovoltaic power generation system through a charge and discharge controller;

[0013] The storage and charging compartment is provided with a plurality of drone storage platforms, and the drone storage platforms are used for parking drones and charging them.

[0014] Furthermore, each drone storage platform includes a second shell with an open rear end;

[0015] A wireless charging seat is embedded on the upper side wall of the second housing, and the wireless charging seat is electrically connected to the battery via a retractable wire;

[0016] The second housing is provided with a GPS locator, and the GPS locator is used for accurate positioning of the UAV upon return;

[0017] An electric push rod is arranged on the front side wall of the partition plate and is located in the corresponding second housing, the rod head of the electric push rod is fixedly connected to the center position of the front side wall of the second housing, and the electric push rod is electrically connected to the battery;

[0018] Telescopic rods are symmetrically arranged on the left and right sides of the electric push rod, the base of the telescopic rod is arranged on the partition plate, the rod head of the telescopic rod is fixedly connected to the surface of the front side wall of the second shell, and the extension distance of the telescopic rod is greater than the distance between the front side wall of the second shell and the front side wall of the first shell;

[0019] It also includes a controller, which is arranged in the energy bin through a mounting plate and is located above the storage battery; the controller is electrically connected to the storage battery;

[0020] The electric push rod is connected with the controller signal.

[0021] Furthermore, the sliding structure includes two driving components symmetrically arranged on the left and right sides of the first housing;

[0022] Each driving assembly includes a movable plate, the movable plate includes a transverse plate, a first vertical plate, and a second vertical plate, the first vertical plate and the second vertical plate are respectively vertically arranged at the front and rear ends of the transverse plate, and the length of the transverse plate is equal to the front and rear width of the housing;

[0023] The horizontal plate is fixedly connected to the movable cover plate and the upper surfaces of the two are flush, and the horizontal plate is in sliding contact with the fixed cover plate;

[0024] A multi-stage electric cylinder is provided at the middle front portion of the upper end of the side wall of the first shell and is located below the horizontal plate on the corresponding side, the end of the multi-stage electric cylinder is connected to the rear surface of the first vertical plate, the multi-stage electric cylinder is electrically connected to the battery, and the multi-stage electric cylinder is connected to the controller signal;

[0025] A fixing plate is provided in the middle of the upper end of the side wall of the first shell, a sliding rod is provided on the rear surface of the fixing plate, a sliding hole matched with the sliding rod is provided on the second vertical plate, and the second vertical plate is sleeved on the sliding rod through the sliding hole. When the second vertical plate contacts the fixing plate, the movable cover is in a fully open state.

[0026] Furthermore, a limiting plate is arranged between the two first vertical plates, the upper end of the limiting plate is fixedly connected to the front end of the movable cover plate and the two are perpendicular to each other, the left and right ends of the limiting plate are respectively connected to the first vertical plate and the second vertical plate, and when the limiting plate contacts the front side surface of the first shell, the movable cover plate is completely closed.

[0027] Furthermore, a guard plate is arranged on the outer side of the horizontal plate, the upper end of the guard plate is connected to the horizontal plate, and the front and rear ends of the guard plate are respectively connected to the first vertical plate and the second vertical plate on the corresponding side.

[0028] Furthermore, a temperature regulating device is provided in the first housing, and the temperature regulating device includes a temperature sensor, a refrigerator, a heater, and a fan;

[0029] The refrigerator and the heater are respectively arranged on the left and right side walls of the first shell and are located in the storage and charging compartment, the fan is arranged in the middle of the front surface of the partition plate, and the temperature sensor is arranged on the front surface of the partition plate and is located above the fan;

[0030] The temperature sensor, refrigerator, heater and fan are electrically connected to the battery respectively, and the temperature sensor, refrigerator, heater and fan are signal-connected to the controller respectively.

[0031] The beneficial effects of the utility model are as follows:

[0032] 1. Use drones equipped with shooting equipment and infrared thermal imagers to conduct video inspections and temperature detection of equipment in photovoltaic plants. The inspection efficiency is improved by combining the two different inspection methods.

[0033] 2. By issuing different task instructions to the unmanned aerial vehicle through the operating terminal, fixed-line inspection and task inspection can be realized. The inspection scope is more comprehensive, and more accurate inspection of key areas can be carried out to timely discover hidden dangers, effectively reducing the risk of serious accidents. BRIEF DESCRIPTION OF THE DRAWINGS

[0034] Figure 1It is a structural block diagram of the unmanned aerial vehicle inspection system described in the utility model;

[0035] Figure 2 This is a schematic diagram of the structure of the drone nest described in the utility model;

[0036] Figure 3 It is a structural schematic diagram of the combination of the movable cover plate, movable plate, limit plate and guard plate described in the utility model;

[0037] Figure 4 It is a right side view of the drone nest structure described in the utility model;

[0038] Figure 5 It is a schematic diagram of the internal structure of the first shell of the utility model;

[0039] Figure 6 It is a top view of the internal structure of the first shell of the utility model;

[0040] Figure 7 It is a structural schematic diagram of the partition plate and the drone storage platform combination of the utility model;

[0041] Figure 8 This is a schematic diagram of the state in which the drone storage platform of the utility model is pushed out;

[0042] Markings in the figure: first shell 1, fixed cover plate 2, movable cover plate 3, partition plate 4, energy compartment 5, storage charging compartment 6, second shell 7, wireless charging seat 8, electric push rod 9, telescopic rod 10, controller 11, movable plate 12, horizontal plate 1201, first vertical plate 1202, second vertical plate 1203, multi-stage electric cylinder 13, fixed plate 14, sliding rod 15, limit plate 16, guard plate 17, temperature sensor 18, refrigerator 19, heater 20, fan 21, charge and discharge controller 22. DETAILED DESCRIPTION

[0043] The specific implementation of the utility model is further described below in conjunction with the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the present application, rather than all the embodiments. Based on the embodiments in the present application, all other embodiments obtained by ordinary technicians in the field without creative work are within the scope of protection of the present application.

[0044] It should be noted that the directions or positional relationships indicated by all directional indication terms in the embodiments of the present application, such as "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside" and "outside", are based on the directions or positional relationships shown in the accompanying drawings. They are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific direction, be constructed and operated in a specific direction. Therefore, they cannot be understood as limitations on the present invention. They are only used to explain the relative positional relationship, movement status, etc. between the components in a certain specific posture. If the specific posture changes, the directional indication will also change accordingly.

[0045] In this application, unless otherwise clearly specified and limited, the terms "connection", "fixation", etc. should be understood in a broad sense. For example, "fixation" can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium, it can be the internal connection of two elements or the interaction relationship between two elements, unless otherwise clearly defined. For ordinary technicians in this field, the specific meanings of the above terms in this application can be understood according to specific circumstances.

[0046] In addition, if there are descriptions involving "first", "second", etc. in the embodiments of the present application, the descriptions of "first", "second", etc. are only used for descriptive purposes and cannot be understood as indicating or implying their relative importance or implicitly indicating the number of technical features indicated. Therefore, the features defined as "first" and "second" may explicitly or implicitly include at least one of the features. In addition, the meaning of "and / or" appearing in the full text includes three parallel schemes. Taking "A and / or B" as an example, it includes scheme A, or scheme B, or a scheme that satisfies both A and B. In addition, the technical solutions between the various embodiments can be combined with each other, but it must be based on the ability of ordinary technicians in the field to implement. When the combination of technical solutions is contradictory or cannot be implemented, it should be considered that such a combination of technical solutions does not exist and is not within the scope of protection required by this application.

[0047] like Figure 1-8 As shown, the unmanned aerial vehicle inspection system includes a unmanned aerial vehicle, an automated airport, an unmanned aerial vehicle nest, a server, and an operation terminal;

[0048] The automated airport is connected to the server through a wired network. A firewall is provided between the automated airport and the server. The operation terminal is connected to the server through an intranet. Task instructions can be issued remotely through the operation terminal. Autonomous inspections can be carried out according to pre-planned routes, or tasks can be issued to conduct fixed-point inspections of a certain part. The inspection methods are diversified. In addition, since the photovoltaic plant area is relatively large, the number of drones is generally multiple, which is not limited here. It can be selected according to actual needs. Multiple drones can be divided into regions and functional categories, such as video inspections, infrared thermal imager inspections, etc.;

[0049] The automated airport is provided with a 4G / 5G network, and the drone is connected to the automated airport through the 4G / 5G network. The inspection data information of the drone can be synchronously transmitted to the automated airport through the 4G / 5G network, and then transmitted to the server through the automated airport for data analysis, processing, generating reports and storing them. The data can be retrieved and viewed through the operation terminal, and the operation terminal can be a portable device equipped with a flight control APP, such as a smart phone, or a computer equipped with a flight control system;

[0050] The drone is provided with a multifunctional gimbal mount, which is used to carry a shooting device or an infrared thermal imager. The shooting device carried by the drone can be used to carry out aerial photography inspections of the equipment in the photovoltaic plant, and the aerial photography information can be transmitted back to the server. The infrared thermal imager carried by the drone can measure the temperature of the surface of the equipment, effectively discover overheated equipment or equipment that has caught fire, and deal with safety hazards in the first place. By combining the shooting device and the infrared thermal imager, various equipment in the photovoltaic plant can be inspected more comprehensively, thereby improving the inspection efficiency.

[0051] The drone nest is arranged in an automated airport, and is used for parking and charging drones.

[0052] like Figure 2-8 As shown, in this embodiment, as a preference, the drone nest comprises a first shell 1 with an open upper end;

[0053] A fixed cover plate 2 and a movable cover plate 3 are arranged at the upper open end of the first shell 1. The fixed cover plate 2 is arranged at the rear end of the opening of the first shell 1 and is generally fixed in a detachable manner, such as screws, etc., to facilitate subsequent maintenance. The movable cover plate 3 is arranged at the front end of the opening of the first shell 1 through a sliding structure and the two are in sliding contact. The sliding structure is used to make the movable cover plate 3 slide back and forth along the upper end surface of the first shell 1. When the rear end of the movable cover plate 3 contacts the front end of the fixed cover plate 2, the upper open end of the first shell 1 is completely sealed by the fixed cover plate 2 and the movable cover plate 3. A layer of sealing rubber gasket can be arranged on the rear end surface of the movable cover plate 3. The rear end of the movable cover plate 3 contacts the front end of the fixed cover plate 2. The gap between the two can be completely sealed by the sealing rubber gasket, thereby further improving the sealing performance.

[0054] A partition plate 4 is provided in the first shell 1, and the partition plate 4 divides the inner cavity of the first shell 1 into an energy compartment 5 and a storage and charging compartment 6;

[0055] The energy warehouse 5 is provided with a storage battery, which is electrically connected to the photovoltaic power generation system through a charge and discharge controller 22, and is charged by photovoltaic power generation, and the storage battery provides power to various electrical components to enable them to work normally;

[0056] The storage and charging compartment 6 is provided with a plurality of drone storage platforms, and the number of drones is selected according to actual needs. The drone storage platforms are used to park drones and charge them.

[0057] like Figure 5-8 As shown, in this embodiment, as a preference, each drone storage platform includes a second shell 7 with an open rear end;

[0058] A wireless charging seat 8 is embedded on the upper side wall of the second housing 7, and the wireless charging seat 8 is electrically connected to the battery through a retractable wire. The drone can be wirelessly charged when it lands on the upper side wall of the second housing 7. Wireless charging is a prior art and will not be described in detail here.

[0059] The second housing 7 is provided with a GPS locator, which is used for accurate positioning of the drone when returning. The GPS locator enables the drone to accurately land on the upper side wall of the second housing 7 when returning.

[0060] An electric push rod 9 is provided on the front side wall of the partition plate 4 and is located in the corresponding second shell 7. The rod head of the electric push rod 9 is fixedly connected to the center position of the front side wall of the second shell 7. The electric push rod 9 is electrically connected to the battery. The second shell 7 is pushed out by extending the electric push rod 9 to make it contact with the front side wall of the first shell 1. At this time, the second shell 7 is completely located in the open area where the movable cover plate 3 is located, ensuring that the drone falls onto the second shell 7 through the opening;

[0061] Telescopic rods 10 are symmetrically arranged on the left and right sides of the electric push rod 9, the base of the telescopic rod 10 is arranged on the partition plate 4, the rod head of the telescopic rod 10 is fixedly connected to the surface of the front side wall of the second shell 7, and the extension distance of the telescopic rod 10 is greater than the distance between the front side wall of the second shell 7 and the front side wall of the first shell 1. The telescopic rods 10 on the left and right sides can ensure that the corresponding second shell 7 can run smoothly when it is pushed out or pulled back, and at the same time play a supporting role to ensure that the drone will not move downward with the increase of weight after landing;

[0062] It also includes a controller 11, which is arranged in the energy bin 5 and above the battery through a mounting plate; the controller 11 is electrically connected to the battery;

[0063] The electric push rod 9 and the sliding structure are respectively connected to the controller 11 by signal, and the controller 11 is connected to the automated airport communication. When receiving a signal that a drone is about to return, the controller 11 controls the start of the sliding structure to push the movable cover 3 forward, so that the upper end of the first shell 1 is opened, and then the controller 11 controls the start of the electric push rod 9 to extend and push the second shell 7 out so that it contacts the front side wall of the first shell 1. The drone is accurately positioned by the set GPS locator and falls onto the corresponding extended second shell 7. Then the controller 11 controls the electric push rod 9 to retract and pull the second shell 7 back until it is connected to the partition plate 4. Then the sliding structure is controlled to pull the movable cover 3 back in the opposite direction until the rear end of the movable cover 3 contacts the front end of the fixed cover 2.

[0064] like Figure 2-4 As shown, in this embodiment, as a preference, the sliding structure includes two driving components symmetrically arranged on the left and right sides of the first housing 1;

[0065] Each driving assembly includes a movable plate 12, and the movable plate 12 includes a horizontal plate 1201, a first vertical plate 1202, and a second vertical plate 1203. The first vertical plate 1202 and the second vertical plate 1203 are respectively vertically arranged at the front and rear ends of the horizontal plate 1201, and the length of the horizontal plate 1201 is equal to the front and rear width of the housing;

[0066] The horizontal plate 1201 is fixedly connected to the movable cover plate 3 and the upper surfaces of the two are flush, and the horizontal plate 1201 is in sliding contact with the fixed cover plate 2;

[0067] A multi-stage electric cylinder 13 is provided at the middle front part of the upper end of the side wall of the first shell 1 and is located below the horizontal plate 1201 on the corresponding side. The end of the multi-stage electric cylinder 13 is connected to the rear surface of the first vertical plate 1202. The multi-stage electric cylinder 13 is electrically connected to the battery. The multi-stage electric cylinder 13 is connected to the controller 1 by signal. When the movable cover plate 3 needs to be opened, the controller 11 controls the start of the two multi-stage electric cylinders 13 to extend at the same time. During the extension of the multi-stage electric cylinder 13, the movable plate 12 can be pushed forward. Since the horizontal plate 1201 is fixedly connected to the movable cover plate 3, the movable plate 12 can be driven to move forward, thereby opening the upper end of the first shell 1.

[0068] A fixing plate 14 is provided in the middle of the upper end of the side wall of the first shell 1, and a sliding rod 15 is provided on the rear surface of the fixing plate 14. A sliding hole matched with the sliding rod 15 is provided on the second vertical plate 1203, and the second vertical plate 1203 is sleeved on the sliding rod 15 through the sliding hole. When the second fixing plate 1203 contacts the fixing plate 14, the movable cover 3 is in a fully open state. Through the cooperation of the set sliding rod 15 and the second vertical plate 1203, the movable cover 3 is relatively stable during the movement. In addition, through the cooperation of the fixing plate 14 and the second vertical plate 1203, the limiting function can be realized to prevent the movable cover 3 from completely separating from the upper end of the first shell 1.

[0069] like Figure 2 , Figure 3 As shown, in the present embodiment, in order to prevent the movable cover plate 3 from excessively squeezing the fixed cover plate 2, a limiting plate 16 is arranged between the two first vertical plates 1202, and the upper end of the limiting plate 16 is fixedly connected to the front end of the movable cover plate 3 and the two are perpendicular to each other, and the left and right ends of the limiting plate 16 are respectively connected to the first vertical plate 1202 and the second vertical plate 1203, when the limiting plate 16 contacts the front surface of the shell, the movable cover plate 3 is completely closed, and the limiting plate 16 is arranged so that the movable cover plate 3 contacts the fixed cover plate 2.

[0070] like Figure 2 , Figure 3 As shown, in this embodiment, in order to protect the multi-stage electric cylinder 13 and related components, a guard plate 17 is provided on the outer side of the horizontal plate 1201, and the upper end of the guard plate 17 is connected to the horizontal plate 1201, and the front and rear ends of the guard plate 17 are respectively connected to the first vertical plate 1202 and the second vertical plate 1203 on the corresponding side. The guard plate 17 and the movable plate 12 jointly form a structure with a lower opening, and the multi-stage electric cylinder 13 and related components are located inside the structure, which effectively avoids wind and rain, protects them and prolongs their service life.

[0071] like Figure 5 , Figure 6As shown, in this embodiment, in order to avoid the influence of charging heat and high and low temperatures of the external environment on the battery in the first shell 1 and the charging of the drone, a temperature regulating device is provided in the first shell 1, and the temperature regulating device includes a temperature sensor 18, a refrigerator 19, a heater 20, and a fan 21;

[0072] The refrigerator 19 and the heater 20 are respectively arranged on the left and right side walls of the first housing 1 and are located in the storage and charging compartment 6. The fan 21 is arranged in the middle of the front surface of the partition plate 4. The temperature sensor 18 is arranged on the front surface of the partition plate 4 and is located above the fan 21.

[0073] The temperature sensor 18, refrigerator 19, heater 20, and fan 21 are electrically connected to the battery respectively, and the temperature sensor 18, refrigerator 19, heater 20, and fan 21 are respectively connected to the controller 1 signal. The heater 20 is preferably a heating rod, and the number of heating rods is selected according to actual needs. The refrigerator 19 is preferably a semiconductor refrigeration plate, and the hot end of the semiconductor refrigeration plate is located on the outside of the first shell 1, and the cold end is located inside the first shell 1. The temperature of the first shell 1 is monitored in real time by the temperature sensor 18. When the monitored temperature is lower than the preset value range, the controller 11 controls the heater 20 to start working, and at the same time starts the fan 21 to accelerate the air circulation in the first shell 1, so that its heat distribution is more uniform, and heats it to restore it to the preset temperature range. When the monitored temperature is higher than the preset value range, the controller 11 controls the refrigerator 19 to start cooling, and at the same time starts the fan 21 to accelerate the air circulation in the first shell 1, so that the cold air quickly diffuses into the entire first shell 1 to avoid local overcooling.

[0074] The above are only preferred embodiments of the present application, and are not intended to limit the patent scope of the present application. Any equivalent structure or equivalent process transformation made using the contents of the present application specification and drawings, or directly or indirectly applied in other related technical fields, are also included in the patent protection scope of the present application.

Claims

1. A drone inspection system, characterized by: Including drones, automated airports, drone nests, servers, and operating terminals; The automated airport is connected to the server through a wired network, a firewall is provided between the automated airport and the server, and the operation terminal is connected to the server through an intranet; The automated airport is provided with a 4 / 5G network, and the drone is connected to the automated airport through the 4 / 5G network; The UAV is provided with a multifunctional gimbal mount, and the multifunctional gimbal mount is used to carry a shooting device or an infrared thermal imager; The drone nest is arranged in an automated airport, and is used for parking and charging drones.

2. The unmanned aerial vehicle inspection system according to claim 1, characterized in that: The drone nest comprises a first shell (1) with an open upper end; The upper end of the first shell (1) is provided with a fixed cover plate (2) and a movable cover plate (3), the fixed cover plate (2) being arranged at the rear end of the opening of the first shell (1) through a detachable structure, and the movable cover plate (3) being arranged at the front end of the opening of the first shell (1) through a sliding structure, and the two are in sliding contact; A partition plate (4) is provided inside the first shell (1), and the partition plate (4) divides the inner cavity of the first shell (1) into an energy compartment (5) and a storage and charging compartment (6); A storage battery is arranged in the energy warehouse (5), and the storage battery is electrically connected to the photovoltaic power generation system through a charge and discharge controller (22); The storage and charging compartment (6) is provided with a plurality of drone storage platforms, and the drone storage platforms are used for parking drones and charging them.

3. The unmanned aerial vehicle inspection system according to claim 2, characterized in that: Each drone storage platform comprises a second shell (7) with an open rear end; A wireless charging seat (8) is embedded on the upper side wall of the second shell (7), and the wireless charging seat (8) is electrically connected to the battery via a retractable wire; The second housing (7) is provided with a GPS locator, which is used for accurate positioning of the drone when it returns; An electric push rod (9) is provided on the front side wall of the partition plate (4) and is located in the corresponding second housing (7); the rod head of the electric push rod (9) is fixedly connected to the center position of the front side wall of the second housing (7); and the electric push rod (9) is electrically connected to a storage battery; Telescopic rods (10) are symmetrically arranged on the left and right sides of the electric push rod (9), the base of the telescopic rod (10) is arranged on the partition plate (4), the rod head of the telescopic rod (10) is fixedly connected to the surface of the front side wall of the second shell (7), and the extension distance of the telescopic rod (10) is greater than the distance between the front side wall of the second shell (7) and the front side wall of the first shell (1); It also includes a controller (11), which is arranged in the energy bin (5) through a mounting plate and is located above the storage battery; the controller (11) is electrically connected to the storage battery; The electric push rod (9) is connected to the controller (11) via signals.

4. The unmanned aerial vehicle inspection system according to claim 3, characterized in that: The sliding structure comprises two driving components symmetrically arranged on the left and right sides of the first housing (1); Each driving assembly comprises a movable plate (12), wherein the movable plate (12) comprises a transverse plate (1201), a first vertical plate (1202), and a second vertical plate (1203), wherein the first vertical plate (1202) and the second vertical plate (1203) are respectively arranged vertically at the front and rear ends of the transverse plate (1201), and the length of the transverse plate (1201) is equal to the front and rear width of the first housing (1); The transverse plate (1201) is fixedly connected to the movable cover plate (3) and the upper surfaces of the two are flush, and the transverse plate (1201) is in sliding contact with the fixed cover plate (2); A multi-stage electric cylinder (13) is provided at the middle front portion of the upper end of the side wall of the first shell (1) and is located below the horizontal plate (1201) on the corresponding side, the end of the multi-stage electric cylinder (13) is connected to the rear surface of the first vertical plate (1202), the multi-stage electric cylinder (13) is electrically connected to a battery, and the multi-stage electric cylinder (13) is signal-connected to a controller (11); A fixing plate (14) is provided in the middle of the upper end of the side wall of the first shell (1), a sliding rod (15) is provided on the rear surface of the fixing plate (14), a sliding hole matched with the sliding rod (15) is provided on the second vertical plate (1203), and the second vertical plate (1203) is sleeved on the sliding rod (15) through the sliding hole. When the second vertical plate (1203) is in contact with the fixing plate (14), the movable cover (3) is in a fully open state.

5. The unmanned aerial vehicle inspection system according to claim 4, characterized in that: A limiting plate (16) is arranged between the two first vertical plates (1202); the upper end of the limiting plate (16) is fixedly connected to the front end of the movable cover plate (3) and the two are perpendicular to each other; the left and right ends of the limiting plate (16) are respectively connected to the first vertical plate (1202) and the second vertical plate (1203); when the limiting plate (16) contacts the front side surface of the first shell (1), the movable cover plate (3) is completely closed.

6. The unmanned aerial vehicle inspection system according to claim 5, characterized in that: A guard plate (17) is arranged on the outer side of the transverse plate (1201), the upper end of the guard plate (17) is connected to the transverse plate (1201), and the front and rear ends of the guard plate (17) are respectively connected to the first vertical plate (1202) and the second vertical plate (1203) on the corresponding side.

7. The unmanned aerial vehicle inspection system according to claim 6, characterized in that: A temperature regulating device is arranged in the first housing (1), and the temperature regulating device comprises a temperature sensor (18), a refrigerator (19), a heater (20), and a fan (21); The refrigerator (19) and the heater (20) are respectively arranged on the left and right side walls of the first shell (1) and are located in the storage and charging compartment (6); the fan (21) is arranged in the middle of the front surface of the partition plate (4); and the temperature sensor (18) is arranged on the front surface of the partition plate (4) and is located above the fan (21); The temperature sensor (18), refrigerator (19), heater (20), and fan (21) are respectively electrically connected to the battery, and the temperature sensor (18), refrigerator (19), heater (20), and fan (21) are respectively signal-connected to the controller (11).

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