Multifunctional inspection unmanned aerial vehicle composite airport

Abstract

The invention discloses a multifunctional inspection unmanned aerial vehicle combined type airport, and relates to the technical field of unmanned aerial vehicle industrial grade inspection, the multifunctional inspection unmanned aerial vehicle combined type airport comprises a cabin, an automatic door, a pull box, a weather detector and a humidity monitoring assembly, the automatic door is installed on the outer wall of the cabin, and the pull box is installed on the outer wall of the cabin in a penetrating mode; a weather detector is installed at the top of the cabin, a drying assembly is installed at the top of the cabin in a penetrating mode, and a humidity monitoring assembly is installed on the outer wall of the drying assembly. Air is heated through a heating block, the heated air is blown to the unmanned aerial vehicle to adjust the humidity of the unmanned aerial vehicle, a pneumatic head moves to drive a first clamping rod to move, the first clamping rod moves to drive a first spring to move, and the first spring moves to enable the first clamping rod to drive a first sliding barrel to move; and a first sliding barrel moves to enable a first clamping rod to move out of a first clamping groove, and the function that the humidity in the cabin is rapidly reduced to prevent the unmanned aerial vehicle from being damaged by too high humidity is achieved.

Description

Technical Field

[0001] The present invention relates to the technical field of industrial inspection of unmanned aerial vehicles, and specifically to a multi-functional inspection unmanned aerial vehicle composite airport. Background Art

[0002] With the rapid development of unmanned aerial vehicle technology, the application demand in fields such as industrial inspection, emergency rescue, and urban management is increasing day by day. However, the traditional unmanned aerial vehicle inspection mode faces problems such as low operation efficiency, insufficient endurance, and excessive manual intervention, and it is difficult to meet the inspection requirements of large scale, high frequency, and long endurance. In this context, the multi-functional inspection unmanned aerial vehicle composite airport emerges as the times require. By integrating functions such as automatic takeoff and landing, intelligent charging, data transmission, and remote control of unmanned aerial vehicles, it realizes the automation, intelligence, and high efficiency of unmanned aerial vehicle inspection. In industrial factories, there are many chemical finished products and raw material equipment in production reserves, and the area is wide, and the manual efficiency is low, consuming time and effort. The application of unmanned aerial vehicle technology can greatly reduce the manual work intensity. However, the humidity in the cabin of the existing inspection unmanned aerial vehicle composite airport cannot be quickly reduced, resulting in too high humidity and damage to the unmanned aerial vehicle.

[0003] The defects existing in the existing inspection unmanned aerial vehicle composite airport are as follows:

[0004] 1. The patent document CN113682489A discloses a new type of unmanned aerial vehicle airport, "including a tarmac 1, a logistics operation center 2, a fixed-wing unmanned transport aircraft hangar 31, and a vertical takeoff and landing unmanned aerial vehicle hangar 32. The logistics operation center 2 is respectively connected to the tarmac 1, the fixed-wing unmanned transport aircraft hangar 31, and the vertical takeoff and landing unmanned aerial vehicle hangar 32. The fixed-wing unmanned transport aircraft hangar 31 and the vertical takeoff and landing unmanned aerial vehicle hangar 32 are also both connected to the tarmac 1. The tarmac 1 is connected to the main runway area 4 through a taxiway 41. The present invention has the characteristics of meeting the needs of simultaneous takeoff and landing of multiple types of unmanned aerial vehicles, realizing rapid logistics distribution and intelligent management", but the humidity in the cabin of the existing inspection unmanned aerial vehicle composite airport cannot be quickly reduced, resulting in too high humidity and damage to the unmanned aerial vehicle;

[0005] 2. The patent document CN221835566U discloses an unmanned aerial vehicle airport, "The unmanned aerial vehicle airport includes: an airport body provided with a tarmac; a propeller rod blocking mechanism arranged on the airport body and capable of extending to one side of the airport body where the tarmac is located, for folding the propellers of the unmanned aerial vehicle staying on the tarmac so that the orthographic projection of the propellers on the plane where the tarmac is located is within the tarmac. The unmanned aerial vehicle airport of the present application can reduce the damage of the propellers, improve the service life of the unmanned aerial vehicle, and reduce costs", but the existing inspection unmanned aerial vehicle composite airport is prone to generate static electricity, causing short circuits in precision circuit failure equipment or fogging of the lens;

[0006] 3. The patent document CN212195963U discloses an unmanned aerial vehicle (UAV) airport, "which can achieve synchronous opening / closing and lifting. The UAV airport of the present utility model includes: a frame, on which orthogonal guide rails and guide rods are provided; a hatch cover, which can reciprocate along the guide rails through a slider fixedly connected to the hatch cover; a landing pad, on which the UAV can park and can reciprocate along the guide rods through a guide block fixedly connected to the landing pad; a driving part, the telescopic rod of which is hinged to the landing pad, so as to drive the landing pad to move along the guide rods; and a transmission member, which transmits the movement of the landing pad to the hatch cover to make the hatch cover and the landing pad move synchronously", but the UAVs of the existing inspection UAV composite airport cannot be stably fixed, reducing stability.

[0007] 4. The patent document CN216684892U discloses an unmanned aerial vehicle (UAV) airport, "including a housing mechanism, a lifting mechanism, a centering mechanism and a opening / closing door mechanism. The housing mechanism includes a protective box, and brake wheels are fixedly connected to the lower surface of the protective box. Its beneficial effect is that, for this UAV airport, by setting a first motor, a threaded rod, a gear, a first toothed plate and a second toothed plate, when adjusting the height of the UAV body, people control the first motor to operate through a control switch, thereby driving the threaded rod to rotate and simultaneously driving the first box body to rise. The rise of the first box body drives the gear to rotate, and under the cooperation of the second toothed plate and the first toothed plate, the second box body and the UAV body are driven to move upward. Under the action of the first motor, the threaded rod, the gear, the first toothed plate and the second toothed plate, it is more convenient for people to adjust the height of the UAV body. At the same time, the telescopic stroke of this device is larger, saving more space", but the dirt on the UAV lens of the existing inspection UAV composite airport cannot be automatically cleaned, reducing the use efficiency of the inspection UAV composite airport. Summary of the Invention

[0008] The purpose of the present invention is to provide a multi-functional inspection UAV composite airport to solve the technical problem in the above-mentioned background technology that the humidity in the cabin of the inspection UAV composite airport cannot be quickly reduced, resulting in too high humidity and damaging the UAV.

[0009] To achieve the above purpose, the present invention provides the following technical solution: A multi-functional inspection UAV composite airport, including a cabin, an automatic door, a pull box, a weather detector and a humidity monitoring component. An automatic door is installed on the outer wall of the cabin, a pull box is installed through the outer wall of the cabin, a weather detector is installed on the top of the cabin, a drying component is installed through the top of the cabin, a humidity monitoring component is installed on the outer wall of the drying component, a placement area is opened on the inner wall of the cabin, and the drying component penetrates through the top of the placement area.

[0010] The drying component includes a support box, a fan, a heating block, a filter screen, a pull plate, a first clamping rod, and a first spring. The support box is installed through the top of the engine room. The fan is located on the inner wall of the support box, the heating block is located on the inner wall of the support box, the pull plate penetrates the outer wall of the support box, and the filter screen is located on the outer wall of the pull plate. A first opening is provided on the outer wall of the support box, and a second opening is provided on the outer wall of the support box. A first spring is installed on the inner wall of the second opening. A pneumatic head is installed on the inner wall of the support box. A first sliding rod is installed on the inner wall of the pull plate. A first sliding cylinder is installed on the outer wall of the first sliding rod. The first clamping rod is installed through the inner wall of the second opening, and the outer wall of the first clamping rod is connected to the outer wall of the first spring. The output end of the pneumatic head is connected to the outer wall of the first clamping rod, and the outer wall of the first sliding cylinder is connected to the outer wall of the first clamping rod. A first clamping groove is provided on the inner wall of the pull plate.

[0011] Preferably, the fan is located above the heating block, the filter screen is located above the fan, the first opening is located above the filter screen, the first clamping rod is inserted into the first clamping groove, and the first sliding cylinder moves by the support of the first sliding rod.

[0012] Preferably, the humidity monitoring component includes a humidity sensor and a processing module. The humidity sensor is located at the bottom of the support box, and the processing module is located on the outer wall of the engine room. The processing module is electrically connected to the humidity sensor and the drying component. The humidity sensor is used to detect the real-time humidity data in the engine room. The processing module stores the appropriate humidity data in the engine room, and the appropriate humidity is 35%-65%.

[0013] Preferably, the real-time humidity data in the engine room is transmitted to the processing module. The processing module compares the real-time humidity data in the engine room with the appropriate humidity data in the engine room. When the real-time humidity data in the engine room is greater than the appropriate humidity data in the engine room, it is set as the high humidity state. When the real-time humidity data in the engine room is less than the appropriate humidity data in the engine room, it is set as the low humidity state. When the real-time humidity data in the engine room is within the appropriate humidity data in the engine room, it is set as the appropriate humidity state.

[0014] Preferably, a fixing component is installed on the inner wall of the placement area, and a cleaning component is installed on the inner wall of the engine room. The cleaning component penetrates the outer wall of the placement area.

[0015] Preferably, the fixing component includes a placement net, a placement table, a second card slot, a first friction pad, and a first motor. The placement net is located on the inner wall of the placement area. The placement table is located on the top of the placement net. The second card slot is opened on the top of the placement table. The first friction pad is located on the inner wall of the second card slot. A second support rod is installed on the inner wall of the placement table. One end of the second support rod is installed with a third cylinder. A first frame is installed through the inner wall of the third cylinder. A fourth cylinder is installed through the outer wall of the second card slot. And one end of the first frame extends into the fourth cylinder. A second friction pad is installed at one end of the first frame. A first toothed rod is installed on the outer wall of the first frame. The first motor is located on the inner wall of the placement table. The output end of the first motor is installed with a gear, and the gear meshes with the first toothed rod.

[0016] Preferably, the first frame moves through the support of the third cylinder and the fourth cylinder. The placement net is located above the pulling box.

[0017] Preferably, the cleaning component includes a fifth box, a first slideway, a third spring, a fifth motor, a collecting wheel, a pulling rope, a spray head, and a water pump. The fifth box is located on the outer wall of the placement area. The first slideway is located on the inner wall of the fifth box. A water tank is installed on the inner wall of the fifth box. The water pump penetrates through the top of the water tank. A pulley is installed on the inner wall of the first slideway. A fourth frame body is installed on the outer wall of the pulley. The third spring is installed on the top of the water tank, and the outer wall of the third spring is connected to the outer wall of the fourth frame body. The output end of the water pump is installed with a spring tube. The spray head is installed on the outer wall of the spring tube, and the outer wall of the fourth frame body is connected to the outer wall of the spray head. A sixth opening is opened on the outer walls of the fifth box and the placement area, and the spray head penetrates through the inner wall of the sixth opening. One end of the pulling rope is connected to the outer wall of the fourth frame body. A water source is provided in the water tank.

[0018] Preferably, the pulley moves through the support of the first slideway. The spring tube moves the spray head.

[0019] Preferably, the usage method of the drone composite airport includes the following steps:

[0020] Step S1: The fan is started to generate suction, and the wind enters the support box through the first opening. The air is filtered through the filter screen, and the air is heated through the heating block. The heated air blows towards the drone to adjust its humidity. The pneumatic head moves to drive the first clamping rod to move. The first clamping rod moves to drive the first spring to move. The first spring moves to make the first clamping rod drive the first sliding cylinder to move. The first sliding cylinder moves to make the first clamping rod move out of the first card slot. At this time, the pulling plate is pulled to drive the filter screen to move, and the filter screen is pulled out of the support box for cleaning, realizing the function of quickly reducing the humidity in the cabin to prevent damage to the drone caused by excessive humidity.

[0021] Step S2: When the processing module detects a state of excessive humidity, the processing module controls the drying component to start. After the drying component starts, the humidity sensor continuously detects the real-time humidity data in the cabin until the processing module detects a state of appropriate humidity or a state of excessive low humidity. When the processing module detects a state of excessive low humidity, the processing module controls the drying component not to start. After the drying component does not start, the humidity sensor continuously detects the real-time humidity data in the cabin until the processing module detects a state of appropriate humidity or a state of excessive humidity. When the processing module detects a state of appropriate humidity, the processing module controls the drying component not to start. After the drying component does not start, the humidity sensor continuously detects the real-time humidity data in the cabin until the processing module detects a state of excessive low humidity or a state of excessive humidity, realizing the functions of not easily generating static electricity to protect precision circuits, preventing metal corrosion, equipment short circuits or lens fogging;

[0022] Step S3: The function of the second strut is to provide support for the third cylinder. The rotation of the first motor drives the gear to rotate, the rotation of the gear drives the first rack to move, the movement of the first rack drives the first frame to move, the movement of the first frame drives the second friction pad to move, and the movement of the second friction pad presses the wheels of the drone against the first friction pad to fix it, realizing the function of the drone composite airport to stably fix the drone and improve stability;

[0023] Step S4: The water pump starts to suck water from the water source into the spring tube. The water source enters the nozzle through the spring tube, and the water source is sprayed onto the surface of the drone through the nozzle for rapid cleaning. At this time, the fifth motor rotates to drive the collection wheel to rotate, the rotation of the collection wheel drives the pull rope to move, the movement of the pull rope drives the fourth frame body to move, the movement of the fourth frame body drives the pulley to move, the movement of the pulley makes the fourth frame body drive the third spring to move, and the movement of the third spring makes the fourth frame body drive the nozzle to adjust the spraying position to increase the cleaning range, realizing the function of automatically cleaning the dirt on the drone lens and improving the use efficiency of the inspection drone composite airport.

[0024] Compared with the prior art, the beneficial effects of the present invention are:

[0025] 1. In the present invention, the blower is installed to start generating suction, and the wind enters the support box through the first port. The air is filtered through the filter screen, the air is heated through the heating block, and the heated air blows towards the drone to adjust its humidity. The pneumatic head moves to drive the first clamping rod to move, the movement of the first clamping rod drives the first spring to move, and the movement of the first spring makes the first clamping rod drive the first sliding cylinder to move. The movement of the first sliding cylinder makes the first clamping rod move out of the first clamping groove. At this time, the pull plate is pulled to drive the filter screen to move, and the filter screen is pulled out of the support box for cleaning, realizing the function of quickly reducing the humidity in the cabin to prevent damage to the drone caused by excessive humidity;

[0026] 2. When the processing module detects a state of excessive humidity through installation, it controls the drying component to start. After the drying component starts, the humidity sensor continuously detects the real-time humidity data in the cabin until the processing module detects a suitable humidity state or a state of excessive low humidity. When the processing module detects a state of excessive low humidity, it controls the drying component not to start. After the drying component does not start, the humidity sensor continuously detects the real-time humidity data in the cabin until the processing module detects a suitable humidity state or a state of excessive high humidity. When the processing module detects a suitable humidity state, it controls the drying component not to start. After the drying component does not start, the humidity sensor continuously detects the real-time humidity data in the cabin until the processing module detects a state of excessive low humidity or a state of excessive high humidity, realizing the functions of not easily generating static electricity to protect precision circuits, preventing metal corrosion, equipment short circuits or lens fogging;

[0027] 3. The function of the second strut installed in the present invention is to provide support for the third cylinder. The first motor rotates to drive the gear to rotate, the gear rotates to drive the first rack to move, the first rack moves to drive the first frame to move, the first frame moves to drive the second friction pad to move, and the second friction pad moves to press the wheels of the drone against the first friction pad to fix it, realizing the function of the composite airport of the drone to stably fix the drone and improve the stability;

[0028] 4. In the present invention, the water pump is started to suck water into the spring tube. The water source enters the nozzle through the spring tube, and the water source is sprayed onto the surface of the drone through the nozzle for rapid cleaning. At this time, the fifth motor rotates to drive the collecting wheel to rotate, the collecting wheel rotates to drive the pull rope to move, the pull rope moves to drive the fourth frame body to move, the fourth frame body moves to drive the pulley to move, the pulley moves to make the fourth frame body drive the third spring to move, and the third spring moves to make the fourth frame body drive the nozzle to adjust the spraying position to increase the cleaning range, realizing the function of automatically cleaning the dirt on the lens of the drone and improving the use efficiency of the inspection drone composite airport. BRIEF DESCRIPTION OF THE DRAWINGS

[0029] Figure 1 is the front view structural schematic diagram of the present invention;

[0030] Figure 2 is the front structural schematic diagram of the present invention;

[0031] Figure 3 is the structural schematic diagram of the support box of the present invention;

[0032] Figure 4 is of the present invention Figure 3 structural schematic diagram of B;

[0033] Figure 5 is of the present invention Figure 3 structural schematic diagram of A;

[0034] Figure 6 Schematic diagram of the drying process of the present invention;

[0035] Figure 7 Schematic diagram of the structure of the second friction pad of the present invention;

[0036] Figure 8 Schematic diagram of the structure of the nozzle of the present invention;

[0037] Figure 9 For the present invention Figure 8 Schematic diagram of the C structure.

[0038] In the figure: 1, engine room; 2, automatic door; 3, suitcase; 4, processing module; 5, weather detector; 8, heating block; 9, fan; 10, support box; 11, filter screen; 12, pull plate; 13, first card slot; 14, first slide bar; 15, first slide cylinder; 16, second port; 17, first spring; 18, pneumatic head; 19, first clamping rod; 20, humidity sensor; 21, placement net; 22, placement table; 23, second support rod; 24, third cylinder; 25, first rack; 26, fourth cylinder; 27, second card slot; 28, second friction pad; 29, first friction pad; 30, first motor; 31, gear; 32, first toothed rod; 33, fifth box; 34, first slideway; 35, pulley; 36, fifth motor; 37, collecting wheel; 38, pull rope; 39, sixth port; 40, third spring; 41, water tank; 42, water pump; 43, fourth frame; 44, nozzle; 45, spring tube. Detailed implementation manners

[0039] Next, the technical solutions in the embodiments of the present invention will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present invention without making creative efforts shall fall within the protection scope of the present invention.

[0040] In the description of the present invention, it should be noted that the orientation or positional relationship indicated by the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end", etc. is based on the orientation or positional relationship shown in the accompanying drawings. It is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation of the present invention. In addition, the terms "first" and "second" are only used for descriptive purposes and cannot be understood as indicating or implying relative importance.

[0041] In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, terms such as "installation", "provided with", "connection", etc. should be understood in a broad sense. For example, "connection" 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 directly connected or indirectly connected through an intermediate medium, and it can be the communication inside two components. For those of ordinary skill in the art, it can be understood according to specific circumstances.

[0042] Example 1: Please refer to Figure 1 , Figure 2 , Figure 3 and Figure 4, an embodiment provided by the present invention: a multifunctional inspection unmanned aerial vehicle composite airport, which includes a cabin 1, an automatic door 2, a suitcase 3, a weather detector 5 and a humidity monitoring component. An automatic door 2 is installed on the outer wall of the cabin 1, a suitcase 3 is installed through the outer wall of the cabin 1, a weather detector 5 is installed on the top of the cabin 1, a drying component is installed through the top of the cabin 1, a humidity monitoring component is installed on the outer wall of the drying component, a placement area is provided on the inner wall of the cabin 1, the drying component penetrates through the top of the placement area, a fixing component is installed on the inner wall of the placement area, a cleaning component is installed on the inner wall of the cabin 1, and the cleaning component penetrates through the outer wall of the placement area. The automatic door 2 automatically opens electrically to let the unmanned aerial vehicle fly out. The suitcase 3 collects water sources. The processing module 4 has an intelligent platform AI data analysis to mark abnormal situations. The intelligent platform AI data analysis includes thermal imaging image temperature analysis, sound data analysis, and image and video analysis. The weather detector 5 monitors bad weather, and the bad weather includes wind speed monitoring, rainfall monitoring, temperature and humidity monitoring to ensure the safety of the unmanned aerial vehicle leaving the warehouse. The cabin 1 is equipped with a wireless charging module, which wirelessly charges the unmanned aerial vehicle. A camera is installed in the cabin 1, and the camera is electrically connected to the processing module 4. The camera is used to detect whether the wings of the unmanned aerial vehicle are damaged, whether the lens is covered with dirt, and whether the gas detection airway is blocked. Multiple unmanned aerial vehicles can be placed in the cabin 1. The drying component includes a support box 10, a fan 9, a heating block 8, a filter screen 11, a pull plate 12, a first clamping rod 19, and a first spring 17. The support box 10 is installed through the top of the cabin 1. The fan 9 is located inside the support box 10, the heating block 8 is located inside the support box 10, the pull plate 12 penetrates through the outer wall of the support box 10, the filter screen 11 is located on the outer wall of the pull plate 12. A first opening is provided on the outer wall of the support box 10, a second opening 16 is provided on the outer wall of the support box 10, a first spring 17 is installed on the inner wall of the second opening 16, a pneumatic head 18 is installed on the inner wall of the support box 10, a first sliding rod 14 is installed on the inner wall of the pull plate 12, a first sliding cylinder 15 is installed on the outer wall of the first sliding rod 14, the first clamping rod 19 is installed through the inner wall of the second opening 16, and the outer wall of the first clamping rod 19 is connected to the outer wall of the first spring 17. The output end of the pneumatic head 18 is connected to the outer wall of the first clamping rod 19, and the outer wall of the first sliding cylinder 15 is connected to the outer wall of the first clamping rod 19. A first clamping groove 13 is provided on the inner wall of the pull plate 12. The fan 9 is located above the heating block 8, the filter screen 11 is located above the fan 9, the first opening is located above the filter screen 11. The first clamping rod 19 is clamped into the first clamping groove 13. The first sliding cylinder 15 moves through the support of the first sliding rod 14. When the fan 9 starts, it generates suction, and the wind enters the support box 10 through the first opening. The air is filtered through the filter screen 11 and heated through the heating block 8. The heated air blows on the unmanned aerial vehicle to adjust its humidity. When the pneumatic head 18 moves, it drives the first clamping rod 19 to move, and the first clamping rod 19 drives the first spring 17 to move.The movement of the first spring 17 causes the first latch rod 19 to drive the first sliding cylinder 15 to move. The movement of the first sliding cylinder 15 causes the first latch rod 19 to move out of the first card slot 13. At this time, pulling the pull plate 12 drives the filter screen 11 to move. The movement of the filter screen 11 pulls it out of the support box 10 for cleaning, realizing the function of quickly reducing the humidity in the cabin 1 to prevent damage to the drone caused by excessive humidity.

[0043] Embodiment 2: Please refer to Figure 2 、 Figure 3 、 Figure 5 and Figure 6 ,An embodiment provided by the present invention: The humidity monitoring component includes a humidity sensor 20 and a processing module 4. The humidity sensor 20 is located at the bottom of the support box 10, and the processing module 4 is located on the outer wall of the cabin 1. The processing module 4 is electrically connected to the humidity sensor 20, and the processing module 4 is electrically connected to the drying component. The humidity sensor 20 is used to detect the real-time humidity data in the cabin 1. The processing module 4 stores the appropriate humidity data in the cabin 1, and the appropriate humidity is 35%-65%. The real-time humidity data in the cabin 1 is transmitted into the processing module 4. The processing module 4 compares the real-time humidity data in the cabin 1 with the appropriate humidity data in the cabin 1. When the real-time humidity data in the cabin 1 is greater than the appropriate humidity data in the cabin 1, it is set as the state of excessive humidity. When the real-time humidity data in the cabin 1 is less than the appropriate humidity data in the cabin 1, it is set as the state of low humidity. When the real-time humidity data in the cabin 1 is within the appropriate humidity data in the cabin 1, it is set as the state of appropriate humidity. When the processing module 4 detects the state of excessive humidity, the processing module 4 controls the drying component to start. After the drying component starts, the humidity sensor 20 continuously detects the real-time humidity data in the cabin 1 until the processing module 4 detects the state of appropriate humidity or the state of low humidity. When the processing module 4 detects the state of low humidity, the processing module 4 controls the drying component not to start. After the drying component does not start, the humidity sensor 20 continuously detects the real-time humidity data in the cabin 1 until the processing module 4 detects the state of appropriate humidity or the state of excessive humidity. When the processing module 4 detects the state of appropriate humidity, the processing module 4 controls the drying component not to start. After the drying component does not start, the humidity sensor 20 continuously detects the real-time humidity data in the cabin 1 until the processing module 4 detects the state of low humidity or the state of excessive humidity, realizing the function of not easily generating static electricity to protect the precision circuit, preventing metal corrosion, equipment short circuit or lens fogging.

[0044] Embodiment 3: Please refer to Figure 2 and Figure 7, An embodiment provided by the present invention: The fixing component includes a placement net 21, a placement table 22, a second card slot 27, a first friction pad 29, and a first motor 30. The placement net 21 is located on the inner wall of the placement area, the placement table 22 is located on the top of the placement net 21, the second card slot 27 is opened on the top of the placement table 22, the first friction pad 29 is located on the inner wall of the second card slot 27, a second support rod 23 is installed on the inner wall of the placement table 22, one end of the second support rod 23 is installed with a third cylinder 24, a first frame 25 is installed through the inner wall of the third cylinder 24, a fourth cylinder 26 is installed through the outer wall of the second card slot 27, and one end of the first frame 25 extends into the fourth cylinder 26. A second friction pad 28 is installed at one end of the first frame 25, a first toothed rod 32 is installed on the outer wall of the first frame 25, the first motor 30 is located on the inner wall of the placement table 22, and a gear 31 is installed at the output end of the first motor 30, and the gear 31 meshes with the first toothed rod 32. The first frame 25 moves through the support of the third cylinder 24 and the fourth cylinder 26. The placement net 21 is located above the pulling box 3. The function of the second support rod 23 is to provide support for the third cylinder 24. The first motor 30 rotates to drive the gear 31 to rotate, the gear 31 rotates to drive the first toothed rod 32 to move, the first toothed rod 32 moves to drive the first frame 25 to move, the first frame 25 moves to drive the second friction pad 28 to move, and the second friction pad 28 moves to press the wheels of the drone against the first friction pad 29 to fix it, realizing the function of the drone composite airport to stably fix the drone and improve stability.

[0045] Embodiment 4: Please refer to Figure 2 , Figure 8 and Figure 9, an embodiment provided by the present invention: The cleaning component includes a fifth box 33, a first slideway 34, a third spring 40, a fifth motor 36, a collecting wheel 37, a pulling rope 38, a nozzle 44, and a water pump 42. The fifth box 33 is located on the outer wall of the placement area. The first slideway 34 is located inside the fifth box 33. A water tank 41 is installed on the inner wall of the fifth box 33. The water pump 42 penetrates through the top of the water tank 41. A pulley 35 is installed on the inner wall of the first slideway 34. A fourth frame 43 is installed on the outer wall of the pulley 35. The third spring 40 is installed on the top of the water tank 41, and the outer wall of the third spring 40 is connected to the outer wall of the fourth frame 43. The output end of the water pump 42 is installed with a spring tube 45. The nozzle 44 is installed on the outer wall of the spring tube 45, and the outer wall of the fourth frame 43 is connected to the outer wall of the nozzle 44. A sixth opening 39 is formed on the outer walls of the fifth box 33 and the placement area, and the nozzle 44 penetrates through the inner wall of the sixth opening 39. One end of the pulling rope 38 is connected to the outer wall of the fourth frame 43. A water source is provided in the water tank 41. The pulley 35 moves through the support of the first slideway 34. The spring tube 45 moves the nozzle 44. The water pump 42 is started to suck the water source into the spring tube 45. The water source enters the nozzle 44 through the spring tube 45. The water source is sprayed onto the surface of the drone through the nozzle 44 to quickly clean it. At this time, the fifth motor 36 rotates to drive the collecting wheel 37 to rotate. The collecting wheel 37 rotates to drive the pulling rope 38 to move. The pulling rope 38 moves to drive the fourth frame 43 to move. The fourth frame 43 moves to drive the pulley 35 to move. The pulley 35 moves to drive the fourth frame 43 to drive the third spring 40 to move. The third spring 40 moves to drive the fourth frame 43 to drive the nozzle 44 to adjust the spraying position to improve the cleaning range, realizing the function of automatically cleaning the dirt on the drone lens and improving the use efficiency of the inspection drone in the compound airport.

[0046] The usage method of this drone compound airport includes the following steps:

[0047] Step S1, the fan 9 is started to generate suction, and the wind enters the support box 10 through the first opening. The air is filtered through the filter screen 11, and the air is heated by the heating block 8. The heated air blows towards the drone to adjust its humidity. The pneumatic head 18 moves to drive the first clamping rod 19 to move. The first clamping rod 19 moves to drive the first spring 17 to move. The first spring 17 moves to drive the first clamping rod 19 to drive the first sliding cylinder 15 to move. The first sliding cylinder 15 moves to drive the first clamping rod 19 to move out of the first clamping groove 13. At this time, the pull plate 12 is pulled to drive the filter screen 11 to move. The filter screen 11 moves to pull it out of the support box 10 for cleaning, realizing the function of quickly reducing the humidity in the cabin 1 to prevent damage to the drone caused by excessive humidity.

[0048] Step S2: When the processing module 4 detects a state of excessive humidity, the processing module 4 controls the drying component to start. After the drying component starts, the humidity sensor 20 continuously detects the real-time humidity data in the cabin 1 until the processing module 4 detects a state of appropriate humidity or a state of excessive low humidity. When the processing module 4 detects a state of excessive low humidity, the processing module 4 controls the drying component not to start. After the drying component does not start, the humidity sensor 20 continuously detects the real-time humidity data in the cabin 1 until the processing module 4 detects a state of appropriate humidity or a state of excessive humidity. When the processing module 4 detects a state of appropriate humidity, the processing module 4 controls the drying component not to start. After the drying component does not start, the humidity sensor 20 continuously detects the real-time humidity data in the cabin 1 until the processing module 4 detects a state of excessive low humidity or a state of excessive humidity, achieving the functions of not easily generating static electricity to protect precision circuits, preventing metal corrosion, equipment short circuits or lens fogging;

[0049] Step S3: The function of the second support rod 23 is to provide support for the third cylinder 24. The first motor 30 rotates to drive the gear 31 to rotate. The gear 31 rotates to drive the first toothed rod 32 to move. The first toothed rod 32 moves to drive the first frame 25 to move. The first frame 25 moves to drive the second friction pad 28 to move. The second friction pad 28 moves to press the wheels of the unmanned aerial vehicle against the first friction pad 29 to fix it, achieving the function of the unmanned aerial vehicle composite airport stably fixing the unmanned aerial vehicle to improve stability;

[0050] Step S4: The water pump 42 starts to suck water from the water source into the spring tube 45. The water source enters the nozzle 44 through the spring tube 45. The water source is sprayed onto the surface of the unmanned aerial vehicle through the nozzle 44 for rapid cleaning. At this time, the fifth motor 36 rotates to drive the collection wheel 37 to rotate. The collection wheel 37 rotates to drive the pull rope 38 to move. The pull rope 38 moves to drive the fourth frame body 43 to move. The fourth frame body 43 moves to drive the pulley 35 to move. The pulley 35 moves to make the fourth frame body 43 drive the third spring 40 to move. The third spring 40 moves to make the fourth frame body 43 drive the nozzle 44 to adjust the spraying position to increase the cleaning range, achieving the function of automatically cleaning the dirt on the lens of the unmanned aerial vehicle and improving the use efficiency of the inspection unmanned aerial vehicle composite airport.

[0051] Working principle: Fan 9 starts to generate suction, and its wind enters the support box 10 through the first port. The air is filtered through the filter screen 11, heated by the heating block 8, and the heated air blows towards the drone to adjust its humidity. The pneumatic head 18 moves to drive the first clamping rod 19 to move. The movement of the first clamping rod 19 drives the first spring 17 to move. The movement of the first spring 17 causes the first clamping rod 19 to drive the first sliding cylinder 15 to move. The movement of the first sliding cylinder 15 makes the first clamping rod 19 move out of the first clamping groove 13. At this time, pulling the pull plate 12 drives the filter screen 11 to move, and the movement of the filter screen 11 pulls it out of the support box 10 for cleaning, realizing the function of quickly reducing the humidity in the cabin 1 to prevent excessive humidity from damaging the drone. When the processing module 4 detects a state of excessive humidity, the processing module 4 controls the drying component to start. After the drying component starts, the humidity sensor 20 continuously detects the real-time humidity data in the cabin 1 until the processing module 4 detects a suitable humidity state or a state of too low humidity. When the processing module 4 detects a state of too low humidity, the processing module 4 controls the drying component not to start. After the drying component does not start, the humidity sensor 20 continuously detects the real-time humidity data in the cabin 1 until the processing module 4 detects a suitable humidity state or a state of excessive humidity. When the processing module 4 detects a suitable humidity state, the processing module 4 controls the drying component not to start. After the drying component does not start, the humidity sensor 20 continuously detects the real-time humidity data in the cabin 1 until the processing module 4 detects a state of too low humidity or a state of excessive humidity, realizing the function of not easily generating static electricity to protect the precision circuit, preventing metal corrosion, equipment short circuit or lens fogging. The function of the second support rod 23 is to provide support for the third cylinder 24. The first motor 30 rotates to drive the gear 31 to rotate. The rotation of the gear 31 drives the first toothed rod 32 to move. The movement of the first toothed rod 32 drives the first frame 25 to move. The movement of the first frame 25 drives the second friction pad 28 to move. The movement of the second friction pad 28 presses the wheels of the drone against the first friction pad 29 to fix it, realizing the function of the drone composite airport to stably fix the drone and improve stability. The water pump 42 starts to suck water into the spring tube 45. The water source enters the nozzle 44 through the spring tube 45. The water source is sprayed from the nozzle 44 onto the surface of the drone for quick cleaning. At this time, the fifth motor 36 rotates to drive the collection wheel 37 to rotate. The rotation of the collection wheel 37 drives the pull rope 38 to move. The movement of the pull rope 38 drives the fourth frame body 43 to move. The movement of the fourth frame body 43 drives the pulley 35 to move. The movement of the pulley 35 makes the fourth frame body 43 drive the third spring 40 to move. The movement of the third spring 40 makes the fourth frame body 43 drive the nozzle 44 to adjust the spraying position to improve the cleaning range, realizing the function of automatically cleaning the dirt on the drone lens and improving the use efficiency of the inspection drone composite airport.

[0052] It is obvious to those skilled in the art that the present invention is not limited to the details of the above-described exemplary embodiments, and the present invention can be implemented in other specific forms without departing from the spirit or essential characteristics of the present invention. Therefore, from any point of view, the embodiments should be regarded as exemplary and non-limiting. The scope of the present invention is defined by the appended claims rather than the above description. Therefore, all changes falling within the meaning and scope of the equivalent elements of the claims are intended to be embraced within the present invention. Any reference signs in the claims should not be construed as limiting the claims involved.

Claims

1. A multi-functional inspection UAV composite airport, comprising a cabin (1), an automatic door (2), a suitcase (3), a weather detector (5) and a humidity monitoring component, characterized in that: An automatic door (2) is installed on the outer wall of the engine room (1), a suitcase (3) is installed through the outer wall of the engine room (1), a weather detector (5) is installed on the top of the engine room (1), a drying component is installed through the top of the engine room (1), a humidity monitoring component is installed on the outer wall of the drying component, a placement area is provided on the inner wall of the engine room (1), and the drying component penetrates through the top of the placement area; The drying component includes a support box (10), a fan (9), a heating block (8), a filter screen (11), a pull plate (12), a first clamping rod (19), and a first spring (17). The support box (10) is installed through the top of the engine room (1). The fan (9) is located inside the support box (10), the heating block (8) is located inside the support box (10), the pull plate (12) penetrates through the outer wall of the support box (10), the filter screen (11) is located on the outer wall of the pull plate (12). A first opening is provided on the outer wall of the support box (10), a second opening (16) is provided on the outer wall of the support box (10), a first spring (17) is installed on the inner wall of the second opening (16), a pneumatic head (18) is installed inside the support box (10), a first sliding rod (14) is installed on the inner wall of the pull plate (12), a first sliding cylinder (15) is installed on the outer wall of the first sliding rod (14), a first clamping rod (19) is installed through the inner wall of the second opening (16), and the outer wall of the first clamping rod (19) is connected to the outer wall of the first spring (17). The output end of the pneumatic head (18) is connected to the outer wall of the first clamping rod (19), and the outer wall of the first sliding cylinder (15) is connected to the outer wall of the first clamping rod (19). A first clamping groove (13) is provided on the inner wall of the pull plate (12).

2. The multifunctional inspection unmanned aerial vehicle composite airport according to claim 1, wherein: The fan (9) is located above the heating block (8), the filter screen (11) is located above the fan (9), the first opening is located above the filter screen (11), the first clamping rod (19) is clamped into the first clamping groove (13), and the first sliding cylinder (15) moves by the support of the first sliding rod (14).

3. A multifunctional inspection UAV composite airport according to claim 1, characterized in that: The humidity monitoring component includes a humidity sensor (20) and a processing module (4). The humidity sensor (20) is located at the bottom of the support box (10), the processing module (4) is located on the outer wall of the engine room (1), the processing module (4) is electrically connected to the humidity sensor (20), the processing module (4) is electrically connected to the drying component. The humidity sensor (20) is used to detect the real-time humidity data inside the engine room (1), the processing module (4) stores the appropriate humidity data inside the engine room (1), and the appropriate humidity is 35% - 65%.

4. The multi-functional inspection unmanned aerial vehicle composite airport according to claim 3, characterized in that: The real-time humidity data in the engine room (1) is transmitted to the processing module (4). The processing module (4) compares the real-time humidity data in the engine room (1) with the appropriate humidity data in the engine room (1). When the real-time humidity data in the engine room (1) is greater than the appropriate humidity data in the engine room (1), it is set as the high humidity state. When the real-time humidity data in the engine room (1) is less than the appropriate humidity data in the engine room (1), it is set as the low humidity state. When the real-time humidity data in the engine room (1) is equal to the appropriate humidity data in the engine room (1), it is set as the appropriate humidity state.

5. The multifunctional inspection unmanned aerial vehicle composite airport according to claim 1, characterized in that: A fixing component is installed on the inner wall of the placement area, and a cleaning component is installed on the inner wall of the engine room (1). The cleaning component penetrates the outer wall of the placement area.

6. The multifunctional inspection unmanned aerial vehicle composite airport according to claim 5, characterized in that: The fixing component includes a placement net (21), a placement table (22), a second card slot (27), a first friction pad (29), and a first motor (30). The placement net (21) is located on the inner wall of the placement area. The placement table (22) is located on the top of the placement net (21). The second card slot (27) is opened on the top of the placement table (22). The first friction pad (29) is located on the inner wall of the second card slot (27). A second support rod (23) is installed on the inner wall of the placement table (22). One end of the second support rod (23) is installed with a third cylinder (24). A first frame (25) is installed through the inner wall of the third cylinder (24). A fourth cylinder (26) is installed through the outer wall of the second card slot (27). One end of the first frame (25) extends into the fourth cylinder (26). A second friction pad (28) is installed at one end of the first frame (25). A first toothed rod (32) is installed on the outer wall of the first frame (25). The first motor (30) is located on the inner wall of the placement table (22). The output end of the first motor (30) is installed with a gear (31), and the gear (31) meshes with the first toothed rod (32).

7. A multi-functional inspection UAV composite airport according to claim 6, characterized in that: The first frame (25) moves through the support of the third cylinder (24) and the fourth cylinder (26). The placement net (21) is located above the pull box (3).

8. A multi-functional inspection UAV composite airport according to claim 5, characterized in that: The cleaning component includes a fifth box (33), a first slideway (34), a third spring (40), a fifth motor (36), a collecting wheel (37), a pulling rope (38), a spray head (44), and a water pump (42). The fifth box (33) is located on the outer wall of the placement area. The first slideway (34) is located on the inner wall of the fifth box (33). A water tank (41) is installed on the inner wall of the fifth box (33). The water pump (42) penetrates through the top of the water tank (41). A pulley (35) is installed on the inner wall of the first slideway (34). A fourth frame body (43) is installed on the outer wall of the pulley (35). The third spring (40) is installed on the top of the water tank (41), and the outer wall of the third spring (40) is connected to the outer wall of the fourth frame body (43). The output end of the water pump (42) is installed with a spring tube (45). The spray head (44) is installed on the outer wall of the spring tube (45), and the outer wall of the fourth frame body (43) is connected to the outer wall of the spray head (44). A sixth opening (39) is formed on the outer walls of the fifth box (33) and the placement area, and the spray head (44) penetrates through the inner wall of the sixth opening (39). One end of the pulling rope (38) is connected to the outer wall of the fourth frame body (43). A water source is provided in the water tank (41).

9. The multifunctional inspection UAV composite airport according to claim 8, wherein: The pulley (35) moves by the support of the first slideway (34), and the spring tube (45) moves the spray head (44).

10. A method for using a multi-functional inspection UAV composite airport, applicable to the multi-functional inspection UAV composite airport described in any one of claims 1-9, characterized in that, The usage method of the drone composite airport includes the following steps: Step S1: The heated air blows towards the drone to adjust its humidity. The pneumatic head (18) moves to drive the first clamping rod (19) to move. The first clamping rod (19) moves to drive the first spring (17) to move. The first spring (17) moves to make the first clamping rod (19) drive the first sliding cylinder (15) to move. The first sliding cylinder (15) moves to make the first clamping rod (19) move out of the first clamping groove (13). At this time, the pulling plate (12) is pulled to drive the filter screen (11) to move. The filter screen (11) moves to pull it out of the support box (10) for cleaning; Step S2: When the processing module (4) detects a state of too low humidity, the processing module (4) controls the drying component not to start. After the drying component does not start, the humidity sensor (20) continuously detects the real-time humidity data in the cabin (1) until the processing module (4) detects a state of appropriate humidity or too high humidity. When the processing module (4) detects a state of appropriate humidity, the processing module (4) controls the drying component not to start. After the drying component does not start, the humidity sensor (20) continuously detects the real-time humidity data in the cabin (1) until the processing module (4) detects a state of too low humidity or too high humidity; Step S3: The function of the second support rod (23) is to provide support for the third cylinder (24). The first motor (30) rotates to drive the gear (31) to rotate. The gear (31) rotates to drive the first toothed rod (32) to move. The first toothed rod (32) moves to drive the first frame (25) to move. The first frame (25) moves to drive the second friction pad (28) to move. The second friction pad (28) moves to press the wheels of the drone against the first friction pad (29) to fix it; Step S4: The water pump (42) starts to suck water from the water source into the bourdon tube (45). The water source enters the nozzle (44) through the bourdon tube (45), and is sprayed onto the surface of the drone through the nozzle (44) for rapid cleaning. At this time, the fifth motor (36) rotates to drive the collection wheel (37) to rotate. The rotation of the collection wheel (37) drives the movement of the pull rope (38). The movement of the pull rope (38) drives the movement of the fourth frame (43). The movement of the fourth frame (43) drives the movement of the pulley (35). The movement of the pulley (35) causes the fourth frame (43) to drive the movement of the third spring (40). The movement of the third spring (40) causes the fourth frame (43) to drive the nozzle (44) to adjust the spraying position and improve the cleaning range.

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