Substation inspection unmanned aerial vehicle carrying platform

Abstract

The invention discloses a transformer substation inspection unmanned aerial vehicle carrier platform, which comprises a protection box, a sealing door plate and two carrier platforms, two bottom plates are horizontally and fixedly connected in the protection box, the two bottom plates are vertically and uniformly distributed, a ventilation mechanism is arranged in the protection box, four corners of the bottom of the protection box are fixedly connected with supporting legs, and the number of the carrier platforms is two. Sliding mechanisms for sliding the two aerial carrier platforms are arranged in the two bottom plates, stabilizing mechanisms are arranged at the tops of the two aerial carrier platforms, the two sealing door plates are rotationally connected to one end of the surface of the protection box, and rotating mechanisms for rotating the two sealing door plates are arranged on the surfaces of the two aerial carrier platforms. According to the unmanned aerial vehicle protection device, the two aerial vehicle carrying platforms are arranged in the device, the unmanned aerial vehicle can be parked during use, meanwhile, the unmanned aerial vehicle can be parked in the protection box, the two aerial vehicle carrying platforms are obliquely arranged, water stains on the surface of the unmanned aerial vehicle are rapidly discharged in cooperation with the arrangement of a fan, and therefore the protection effect on the unmanned aerial vehicle is improved.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicle (UAV) carrier platforms, and in particular to a substation inspection UAV carrier platform. Background Art

[0002] A drone is an aircraft that does not require a pilot in the aircraft and is usually controlled by a remote control device or an automatic control system. Drones have a wide range of applications, covering multiple fields. Substation inspection drones are unmanned aerial vehicles specially designed for inspection and monitoring of substations. This type of drone uses advanced sensors, high-definition cameras and thermal imaging technology to effectively perform a variety of tasks. With the development of drone technology, substation inspection drones are being used more and more widely in the power industry and have become an important tool for modern power operation and maintenance. With the development of technology, the performance and application scenarios of drones are constantly expanding, making it one of the indispensable tools in modern society.

[0003] When using a substation inspection drone, it is usually necessary to use it in conjunction with a drone carrier platform. However, the existing drone carrier platforms are mostly used to park the drone better in actual use, but this will result in low practicality and failure to better protect the drone. At the same time, when parking the drone, most of them are parked on the surface parking platform, which cannot actively make the drone more stable. When the carrier platform shakes, the drone is not parked stably enough, which can easily cause damage. At the same time, the existing drone carrier platform does not have any protective equipment for the drone, which will reduce the use effect. Therefore, the above problems need to be solved. Summary of the invention

[0004] Based on the technical problems existing in the background technology, the present invention proposes a substation inspection drone carrier platform.

[0005] The substation inspection drone carrier platform proposed by the present invention comprises a protection box, a sealed door panel and a carrier platform, two inspection doors are symmetrically installed on both sides of the surface of the protection box, and lock bodies are installed on the surfaces of the four inspection doors. Fixing strips are vertically fixedly connected to both sides of one end of the surface of the protection box, and two bottom plates are horizontally fixedly connected inside the protection box. The two bottom plates are evenly distributed vertically. A ventilation mechanism is arranged inside the protection box, and support legs are fixedly connected to the four corners of the bottom of the protection box. The carrier platform is provided with two, and the two carrier platforms are horizontally slidably connected to the top of the two bottom plates. Two sliding carrier platforms are arranged inside the two bottom plates. The sliding mechanism of the platform, the top of the two aircraft carrier platforms are provided with a stabilizing mechanism, the two sealing door panels are provided with two, the two sealing door panels are rotatably connected to one end of the surface of the protection box, the two sealing door panels are rotatably connected between the two fixing strips, and the surfaces of the two aircraft carrier platforms are provided with a rotating mechanism for rotating the two sealing door panels. Two aircraft carrier platforms are arranged inside the device, and the drone can be parked when in use. At the same time, through the setting of the two aircraft carrier platforms, the drone can be parked inside the protection box, and the two aircraft carrier platforms are placed at an angle. Combined with the setting of the fan, water stains on the surface of the drone can be quickly discharged, thereby improving the protection effect on the drone.

[0006] Preferably, the ventilation mechanism includes a connecting box, which is fixedly connected to one end of the interior of the protective box away from the sealing door panel, the bottom end of the connecting box is fixedly connected to the top of the bottom base plate, the connecting box is inserted into the surface of the top base plate, and the top of the connecting box is fixedly connected to the top of the protective box. Two connecting compartments are provided inside the connecting box, and the two connecting compartments are respectively arranged on the top of two aircraft carrier platforms. Fans are installed inside the two connecting compartments, and a cavity is provided inside the connecting box. A protective box is vertically fixedly connected to one end of the surface of the protective box away from the sealing door panel, and the two connecting compartments are communicated with the interior of the protective box. Multiple air inlets are provided at the bottom and one side of the protective box for limiting the operation of the two fans, thereby facilitating the air flow inside the protective box and drying the parked drones.

[0007] Furthermore, the sliding mechanism includes a support rod, a first slide track is horizontally provided on the top of the bottom plate, and two second slide grooves are horizontally provided on the top of the bottom plate, the two second slide grooves are respectively arranged on both sides of the two first slide tracks, and multiple conveying rollers are rotatably connected on opposite sides of the two second slide grooves, and the multiple conveying rollers are arranged in a double-layer manner, and the support rods are provided with two, the two support rods are respectively slidably connected to the inside of the two second slide grooves, the two support rods are respectively arranged between the multiple conveying rollers, the bottoms of the two support rods are fixedly connected to limiting plates, and the two limiting plates are respectively arranged between the double-layer conveying rollers, the tops of the two support rods close to the sealing door panel are fixedly connected to the second fixed blocks, and the tops of the two support rods away from the sealing door panel are provided with a first arc groove, the bottom of the carrier platform close to the sealing door panel is fixedly connected to the two first fixed blocks, the two first fixed blocks are respectively hinged inside the two second fixed blocks, and the carrier platform is away from the sealing door panel. The two ends are fixedly connected with two arc columns, and the two arc columns are respectively slidably connected to the two first arc grooves, and the first slide is horizontally slidably connected inside the first slide, and the top of the first slide is hinged with a second connecting rod, and the bottom of the carrier platform is provided with a first connecting groove at one end away from the sealing door panel, and the top of the second connecting rod is rotatably connected to the inside of the first connecting groove, and the first slide is rotatably connected to the inside of the first slide, and the first screw rod is horizontally arranged, and one end of the first screw rod is sleeved inside the connecting box, and the first slider is sleeved on the surface of the first screw rod, and the first slider cooperates with the first screw rod, and a motor is installed inside the cavity, and the output end of the motor is fixedly connected to one end of the first screw rod, used to limit the horizontal sliding of the first slider, and under the support of the two support rods, the carrier platform slides horizontally. At the same time, after the carrier platform slides into the protective box, one end of the carrier platform will be tilted upward, so that the carrier platform is arranged in an inclined state, which will make the water stains on the drone and the carrier platform flow out more quickly.

[0008] Preferably, the stabilizing mechanism comprises a fixing box, the top of the carrier platform is horizontally provided with four third slide grooves, the four third slide grooves are arranged in pairs in the same straight line, the fixing box is provided with four, the four fixing boxes are all slidably connected to the top of the carrier platform, the four fixing boxes are respectively slidably connected to the surfaces of the four third slide grooves, the four third slide grooves are slidably connected to the second sliding blocks, the four second sliding blocks are respectively fixedly connected to the bottoms of the four fixing boxes, two slide plates are horizontally slidably connected to the inside of the carrier platform, the four second sliding blocks are respectively fixedly connected to the two ends of the tops of the two slide plates, a second screw rod is rotatably connected to the inside of the carrier platform, the second screw rod is horizontally arranged, the two ends of the second screw rod are respectively inserted through the symmetrical sides of the carrier platform surface, the second screw rod is sleeved in the two slide plates, the two slide plates are matched with the second screw rod, the symmetrical sides of the carrier platform surface are rotatably connected with gears, the two second screw rods are respectively fixedly connected to the two ends of the second screw rod, four racks are arranged inside the protective box, and four The racks are fixedly connected to both sides of the top of the two bottom plates, and the two gears are respectively meshed with two of the racks. The four fixed box surfaces are each provided with a second connecting groove, and the four second connecting grooves are each horizontally fixedly connected with two sliding rods, and the four second connecting grooves are each horizontally slidably connected with a clamping block, and the four clamping block surfaces are symmetrically fixedly connected with a second limit strip, and multiple second limit strips are respectively slidably connected to the opposite sides of the four second connecting grooves, and the four clamping blocks are respectively sleeved on the surfaces of multiple sliding rods, and the surfaces of multiple sliding rods are sleeved with springs, and multiple springs are respectively arranged on the surfaces of four clamping blocks, and the surfaces of four clamping blocks are provided with a second arc groove, which is used for rotating the two gears through the two racks during the sliding of the carrier platform, so that the four fixed boxes and the clamping blocks are close to each other in pairs, so that the parking rack at the bottom of the parked drone can be restricted, thereby making the parking of the drone more stable, and also facilitating the adjustment of the parking position of the drone, so that the parking position of the drone is more centered.

[0009] Furthermore, the rotating mechanism includes a first connecting rod, and the surface of the aircraft carrier platform is symmetrically fixedly connected with first connecting columns on both sides near one end of the sealing door panel. The first connecting rod is provided with two, and the two first connecting rods are respectively arranged on both sides of the surface of the aircraft carrier platform symmetrically, and the bottom ends of the two first connecting rods are respectively sleeved on the surfaces of the two first connecting columns, and two first limit strips are vertically fixedly connected to one side of the surface of the sealing door panel, and the surfaces of the two first limit strips are penetrated by limiting grooves, and the top ends of the two first connecting rods are respectively slidably connected to the surfaces of the two first limit strips, and the top ends of the two first connecting rods are fixedly connected to the limiting columns, and the two limiting columns are respectively slidably connected to the inside of the two limiting grooves, which are used to drive the two sealing door panels to rotate while sliding the two aircraft carrier platforms, so that the protection effect of the drone is better when it is parked, thereby improving the use effect of the device.

[0010] In the present invention, when the device is in use, the two aircraft carrier platforms are slid horizontally, so that the UAV can be parked on top of the two aircraft carrier platforms, and the UAV can be parked inside the protection box, so that the UAV can be better protected.

[0011] When the device is in use, when the drone is parked, the parking frame at the bottom of the drone can be clamped, so that the drone can be parked more stably, thereby improving the protection effect of the drone.

[0012] When the drone is parked, one end of the carrier platform is lifted up. When it rains, the rainwater on the surface of the drone can be quickly removed. At the same time, the fan can be set to quickly dry the rainwater on the surface of the drone, thereby effectively preventing the drone from being damaged. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 This is a front view of the substation inspection drone carrier platform proposed by the present invention;

[0014] Figure 2 This is a cross-sectional view of the surface structure of the substation inspection drone carrier platform proposed by the present invention;

[0015] Figure 3 This is a cross-sectional view of the internal structure of the protective box of the substation inspection drone carrier platform proposed by the present invention;

[0016] Figure 4 This is a schematic diagram of the sliding mechanism of the substation inspection UAV carrier platform proposed by the present invention;

[0017] Figure 5 This is a schematic diagram of the rotating mechanism of the substation inspection UAV carrier platform proposed by the present invention;

[0018] Figure 6 for Figure 5 A magnified image of point A;

[0019] Figure 7 A cross-sectional view of the internal structure of the carrier platform of the substation inspection UAV carrier platform proposed by the present invention;

[0020] Figure 8 A cross-sectional view of the bottom structure of the carrier platform of the substation inspection UAV carrier platform proposed by the present invention;

[0021] Fig. 9 A schematic diagram of the stabilizing mechanism of the substation inspection UAV carrier platform proposed by the present invention;

[0022] Fig.10 for Fig. 9 Enlarged view of point B.

[0023] In the figure: 1. protection box; 11. inspection door; 12. protection box; 13. air inlet; 14. support leg; 15. lock body; 16. fixing bar; 17. bottom plate; 18. first slideway; 19. second slideway; 110. conveying roller; 111. connection box; 112. connection compartment; 113. cavity; 114. fan; 115. rack; 2. sealing door panel; 21. first limit bar; 22. limit slot; 3. aircraft carrier platform; 31. third slideway; 32. first connecting column; 33. first connecting rod ; 34. Limiting column; 35. First fixed block; 36. Arc column; 37. First connecting groove; 4. First screw rod; 41. Motor; 42. First slider; 43. Second connecting rod; 5. Support rod; 51. Limiting plate; 52. First arc groove; 53. Second fixed block; 6. Slide plate; 61. Second screw rod; 62. Gear; 63. Second slider; 64. Fixed box; 65. Second connecting groove; 66. Slide rod; 7. Clamp block; 71. Second limiting strip; 72. Second arc groove; 73. Spring. DETAILED DESCRIPTION

[0024] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all the embodiments.

[0025] Reference Figure 1 - Fig.10 The substation inspection drone carrier platform includes a protection box 1, a sealing door panel 2 and a carrier platform 3. Two inspection doors 11 are symmetrically installed on both sides of the surface of the protection box 1. Lock bodies 15 are installed on the surfaces of the four inspection doors 11. Fixing strips 16 are vertically fixedly connected to both sides of one end of the surface of the protection box 1. Two bottom plates 17 are horizontally fixedly connected inside the protection box 1. The two bottom plates 17 are evenly distributed vertically. A ventilation mechanism is arranged inside the protection box 1. Support legs 14 are fixedly connected to the four corners of the bottom of the protection box 1. Two carrier platforms 3 are provided. The two carrier platforms 3 are horizontally slidably connected to the tops of the two bottom plates 17. Two sliding carrier platforms 3 are arranged inside the two bottom plates 17. A sliding mechanism is provided, and a stabilizing mechanism is provided on the top of each of the two aircraft carrier platforms 3. Two sealing door panels 2 are provided, and both sealing door panels 2 are rotatably connected to one end of the surface of the protective box 1. Both sealing door panels 2 are rotatably connected between two fixing strips 16. A rotating mechanism for rotating the two sealing door panels 2 is provided on the surfaces of the two aircraft carrier platforms 3. Two aircraft carrier platforms 3 are provided inside the device, and the drone can be parked when in use. At the same time, through the setting of the two aircraft carrier platforms 3, the drone can be parked inside the protective box 1, and the two aircraft carrier platforms 3 are placed at an angle. Combined with the setting of the fan 114, water stains on the surface of the drone can be quickly discharged, thereby improving the protection effect on the drone.

[0026] Reference Figure 1 - Figure 3 In a preferred embodiment, the ventilation mechanism includes a connection box 111, which is fixedly connected to the end of the protective box 1 away from the sealing door panel 2, the bottom end of the connection box 111 is fixedly connected to the top of the bottom plate 17, the connection box 111 is inserted into the surface of the top bottom plate 17, and the top of the connection box 111 is fixedly connected to the top of the protective box 1, and two connection chambers 112 are opened inside the connection box 111, and the two connection chambers 112 are respectively arranged on the top of the two aircraft carrier platforms 3, and fans 114 are installed inside the two connection chambers 112, and a cavity 113 is arranged inside the connection box 111, and a protective box 12 is vertically fixedly connected to the end of the surface of the protective box 1 away from the sealing door panel 2, and the two connection chambers 112 are connected to the inside of the protective box 12, and a plurality of air inlets 13 are arranged on the bottom and one side of the protective box 12 for limiting the operation of the two fans 114, so as to facilitate the air flow inside the protective box 1 and dry the parked drone at the same time.

[0027] Reference Figure 3 , Figure 4 , Figure 7 and Figure 8In a preferred embodiment, the sliding mechanism includes a support rod 5, a first slide 18 is horizontally opened on the top of the bottom plate 17, two second slide grooves 19 are horizontally opened on the top of the bottom plate 17, the two second slide grooves 19 are respectively arranged on both sides of the two first slide grooves 18, and the two second slide grooves 19 are rotatably connected to the opposite sides of the multiple conveying rollers 110, and the multiple conveying rollers 110 are arranged in double layers, and the support rod 5 is provided with two, and the two support rods 5 are respectively slidably connected to the inside of the two second slide grooves 19, and the two support rods 5 are respectively arranged on the multiple conveying rollers 1 10, the bottoms of the two support rods 5 are fixedly connected to the limit plates 51, and the two limit plates 51 are respectively arranged between the double-layer conveying rollers 110, the tops of the two support rods 5 are fixedly connected to the second fixed blocks 53 at one end close to the sealing door plate 2, and the tops of the two support rods 5 are provided with first arc grooves 52 at one end away from the sealing door plate 2, and the bottom of the carrier platform 3 is fixedly connected to the end close to the sealing door plate 2. The two first fixed blocks 35 are respectively hinged to the inside of the two second fixed blocks 53, and the carrier platform 3 is away from the sealing door plate 2. Two arc columns 36 are fixedly connected, and the two arc columns 36 are respectively slidably connected to the inside of the two first arc grooves 52. The first slide 18 is horizontally slidably connected to the first slider 42, and the top of the first slider 42 is hinged with a second connecting rod 43. The bottom of the carrier platform 3 is far away from the sealing door panel 2. The top of the second connecting rod 43 is rotatably connected to the inside of the first connecting groove 37. The first slide 18 is rotatably connected to the first screw rod 4, which is horizontally arranged, and one end of the first screw rod 4 is sleeved inside the connection box 111. The first slider 42 is sleeved on the surface of the first screw rod 4, the first slider 42 cooperates with the first screw rod 4, a motor 41 is installed inside the connecting box 111, and the output end of the motor 41 is fixedly connected to one end of the first screw rod 4, which is used to limit the horizontal sliding of the first slider 42. Under the support of the two support rods 5, the carrier platform 3 slides horizontally. At the same time, after the carrier platform 3 slides into the protective box 1, one end of the carrier platform 3 will be tilted upward, so that the carrier platform 3 is set in an inclined state, which will make the water stains on the drone and the carrier platform 3 flow out more quickly.

[0028] Reference Figure 3 , Figure 7 , Fig. 9 and Fig.10In a preferred embodiment, the stabilizing mechanism includes a fixed box 64, four third slide grooves 31 are horizontally opened on the top of the carrier platform 3, and the four third slide grooves 31 are arranged in pairs in the same straight line. There are four fixed boxes 64, and the four fixed boxes 64 are slidably connected to the top of the carrier platform 3. The four fixed boxes 64 are respectively slidably connected to the surfaces of the four third slide grooves 31. The insides of the four third slide grooves 31 are slidably connected to the second sliders 63, and the four second sliders 63 are respectively fixedly connected to the bottoms of the four fixed boxes 64. There are two horizontal sliding connections inside the carrier platform 3. The slide plate 6, four second sliders 63 are respectively fixedly connected to the two ends of the top of the two slide plates 6, the second screw rod 61 is rotatably connected inside the aircraft carrier platform 3, the second screw rod 61 is horizontally arranged, the two ends of the second screw rod 61 are respectively inserted on the symmetrical sides of the surface of the aircraft carrier platform 3, the second screw rod 61 is sleeved inside the two slide plates 6, the two slide plates 6 are matched with the second screw rod 61, the two symmetrical sides of the surface of the aircraft carrier platform 3 are rotatably connected with gears 62, the two second screw rods 61 are respectively fixedly connected to the two ends of the second screw rod 61, and four racks 115 are arranged inside the protective box 1, and the four gears The racks 115 are respectively fixedly connected to the two sides of the top of the two bottom plates 17, and the two gears 62 are respectively meshed with two of the racks 115. The surfaces of the four fixed boxes 64 are each provided with a second connecting groove 65, and the inside of the four second connecting grooves 65 are both horizontally fixedly connected with two sliding rods 66. The inside of the four second connecting grooves 65 are both horizontally slidably connected with clamping blocks 7, and the surfaces of the four clamping blocks 7 are both symmetrically fixedly connected with second limiting bars 71 on both sides, and the plurality of second limiting bars 71 are respectively slidably connected to the opposite sides of the inside of the four second connecting grooves 65, and the four clamping blocks 7 are respectively sleeved on the plurality of sliding bars. The surface of the rod 66 and the surfaces of the multiple sliding rods 66 are all sleeved with springs 73, and the multiple springs 73 are respectively arranged on the surfaces of the four clamping blocks 7. The surfaces of the four clamping blocks 7 are all provided with second arc grooves 72, which are used to rotate the two gears 62 through the two racks 115 during the sliding process of the carrier platform 3, so that the four fixed boxes 64 and the clamping blocks 7 are close to each other in pairs, so as to limit the parking frame at the bottom of the parked drone, so that the parking of the drone is more stable, and it is also convenient to adjust the parking position of the drone, so that the parking position of the drone is more centered.

[0029] Reference Figure 1 , Figure 5 and Figure 6In a preferred embodiment, the rotating mechanism includes a first connecting rod 33, and the first connecting columns 32 are fixedly connected to the symmetrical sides of the surface of the aircraft carrier platform 3 near one end of the sealing door panel 2. The first connecting rods 33 are provided with two, and the two first connecting rods 33 are respectively arranged on the symmetrical sides of the surface of the aircraft carrier platform 3. The bottom ends of the two first connecting rods 33 are respectively sleeved on the surfaces of the two first connecting columns 32. One side of the surface of the sealing door panel 2 is vertically fixedly connected with two first limit strips 21, and the surfaces of the two first limit strips 21 are penetrated by limiting grooves 22. The top ends of the two first connecting rods 33 are respectively slidably connected to the surfaces of the two first limit strips 21, and the top ends of the two first connecting rods 33 are fixedly connected to the limiting columns 34. The two limiting columns 34 are respectively slidably connected to the inside of the two limiting grooves 22, and are used for driving the two sealing door panels 2 to rotate while sliding the two aircraft carrier platforms 3, so that the protection effect of the drone is better when it is parked, thereby improving the use effect of the device.

[0030] In the present invention, two aircraft carrier platforms 3 are arranged inside the device in actual use, and the drone can be parked when in use. At the same time, through the arrangement of the two aircraft carrier platforms 3, the drone can be parked inside the protective box 1, so that the two aircraft carrier platforms 3 are placed at an angle, and the fan 114 is arranged to quickly blow out the water stains on the surface of the drone, thereby improving the protection effect of the drone. When in use, the device can be installed in a suitable position, and the drone can be temporarily parked during use. When the drone needs to be parked, the motor 41 inside the protective box 1 can be driven to drive the first screw rod 4 to rotate, thereby driving the first slider 42 When the carrier platform 3 slides outwards, the two support rods 5 and the limit plate 51 are connected, and the carrier platform 3 is mechanically supported. When the carrier platform 3 slides outwards, one of the sealed door panels 2 is rotated under the connection of the two first connecting rods 33, and the limit column 34 at one end of the first connecting rod 33 slides inside the limit groove 22, so that the sealed door panel 2 is opened while the carrier platform 3 slides without blocking the drone. Then the drone is parked by mistake. When the drone is parked on the top of the carrier platform 3, it is driven in the reverse direction. The motor 41 drives the first screw rod 4 to rotate, causing the first slider 42 to slide into the protective box 1, thereby driving the carrier platform 3 and the drone to slide into the protective box 1 together. During the sliding of the carrier platform 3, the gears 62 at both ends of the carrier platform 3 will contact the two racks 115 respectively, and cause the two gears 62 to rotate, and also drive the second screw rod 61 to rotate. At this time, the two slides 6 will approach each other, and at the same time, the four fixed boxes 64 on the top of the carrier platform 3 will approach each other in pairs, thereby limiting the parking rack at the bottom of the drone, making the drone more centered. It will also make the drone more stable, and then the sealing door panel 2 will be closed through the two first connecting rods 33, and then the first slider 42 will continue to slide. Under the connection of the second connecting rod 43, the carrier platform 3 will be tilted upward away from one end of the sealing door panel 2, and in conjunction with the driving fan 114, dust or rainwater on the surface of the drone will be removed and leak out along the two first slides 18. During this process, when it rains, the sewage on the surface of the drone can be quickly discharged, which can better protect the drone and also make the drone more safely parked, thereby improving the use effect of the device.

[0031] The above description is only a preferred specific implementation manner of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can make equivalent replacements or changes according to the technical scheme and inventive concept of the present invention within the technical scope disclosed by the present invention, which should be covered by the protection scope of the present invention.

Claims

1. A substation inspection drone carrier platform, comprising a protective box (1), a sealing door panel (2) and a carrier platform (3), characterized in that: Two inspection doors (11) are symmetrically installed on both sides of the surface of the protection box (1), and lock bodies (15) are installed on the surfaces of the four inspection doors (11). Fixing strips (16) are vertically fixedly connected to both sides of one end of the surface of the protection box (1). Two bottom plates (17) are horizontally fixedly connected inside the protection box (1), and the two bottom plates (17) are evenly distributed vertically. A ventilation mechanism is arranged inside the protection box (1), and support legs (14) are fixedly connected to the four corners of the bottom of the protection box (1); Two aircraft carrier platforms (3) are provided, and the two aircraft carrier platforms (3) are horizontally slidably connected to the tops of the two bottom plates (17), and the insides of the two bottom plates (17) are provided with sliding mechanisms for sliding the two aircraft carrier platforms (3), and the tops of the two aircraft carrier platforms (3) are provided with stabilizing mechanisms; Two sealing door panels (2) are provided, and the two sealing door panels (2) are both rotatably connected to one end of the surface of the protection box (1), and the two sealing door panels (2) are both rotatably connected between two fixing strips (16), and the surfaces of the two aircraft carrier platforms (3) are provided with a rotating mechanism for rotating the two sealing door panels (2).

2. The substation inspection drone carrier platform according to claim 1 is characterized in that: The ventilation mechanism comprises a connection box (111), wherein the connection box (111) is fixedly connected to one end of the protective box (1) away from the sealing door plate (2), the bottom end of the connection box (111) is fixedly connected to the top of the bottom base plate (17), the connection box (111) is inserted into the surface of the top base plate (17), the top of the connection box (111) is fixedly connected to the top of the protective box (1), two connection chambers (112) are provided inside the connection box (111), the two connection chambers (112) are respectively arranged on the tops of two aircraft carrier platforms (3), fans (114) are installed inside the two connection chambers (112), and a cavity (113) is arranged inside the connection box (111).

3. The substation inspection drone carrier platform according to claim 2 is characterized in that: A protective box (12) is vertically fixedly connected to one end of the surface of the protective box (1) away from the sealing door plate (2), the two connecting compartments (112) are both connected to the inside of the protective box (12), and a plurality of air inlets (13) are provided at the bottom and one side of the protective box (12).

4. The substation inspection drone carrier platform according to claim 1 is characterized in that: The sliding mechanism comprises a support rod (5), a first slideway (18) is horizontally provided on the top of the bottom plate (17), two second slide grooves (19) are horizontally provided on the top of the bottom plate (17), the two second slide grooves (19) are respectively arranged on both sides of the two first slideways (18), a plurality of conveying rollers (110) are rotatably connected on opposite sides inside the two second slide grooves (19), the plurality of conveying rollers (110) are arranged in double layers, two support rods (5) are provided, the two support rods (5) are respectively slidably connected inside the two second slide grooves (19), the two support rods (5) are respectively arranged between the plurality of conveying rollers (110), the bottoms of the two support rods (5) are fixedly connected to limit plates (51), the two limit plates (51) are respectively arranged between the double-layer conveying rollers (110).

5. The substation inspection drone carrier platform according to claim 4 is characterized in that: The tops of the two support rods (5) are fixedly connected to one end close to the sealing door panel (2) with a second fixed block (53); the tops of the two support rods (5) are opened to one end away from the sealing door panel (2) with a first arc groove (52); the bottom of the aircraft carrier platform (3) is fixedly connected to one end close to the sealing door panel (2) with two first fixed blocks (35); the two first fixed blocks (35) are respectively hinged to the inside of the two second fixed blocks (53); the end of the aircraft carrier platform (3) away from the sealing door panel (2) is fixedly connected to two arc columns (36); the two arc columns (36) are respectively slidably connected to the inside of the two first arc grooves (52).

6. The substation inspection drone carrier platform according to claim 5 is characterized in that: The first slideway (18) is horizontally slidably connected to a first slider (42), the top of the first slider (42) is hinged to a second connecting rod (43), a first connecting groove (37) is provided at one end of the bottom of the carrier platform (3) away from the sealing door panel (2), the top of the second connecting rod (43) is rotatably connected to the inside of the first connecting groove (37), the first slideway (18) is rotatably connected to a first screw rod (4), the first screw rod (4) is horizontally arranged, one end of the first screw rod (4) is sleeved inside the connecting box (111), the first slider (42) is sleeved on the surface of the first screw rod (4), the first slider (42) cooperates with the first screw rod (4), a motor (41) is installed inside the cavity (113), and the output end of the motor (41) is fixedly connected to one end of the first screw rod (4).

7. The substation inspection drone carrier platform according to claim 1 is characterized in that: The stabilizing mechanism comprises a fixed box (64), four third slide grooves (31) are horizontally opened on the top of the aircraft carrier platform (3), and the four third slide grooves (31) are arranged in pairs in the same straight line. There are four fixed boxes (64), and the four fixed boxes (64) are all slidably connected to the top of the aircraft carrier platform (3). The four fixed boxes (64) are respectively slidably connected to the surfaces of the four third slide grooves (31). The four third slide grooves (31) are slidably connected to the inside of the second sliders (63), and the four second sliders (63) are respectively fixedly connected to the bottom of the four fixed boxes (64). Two slide plates (6) are horizontally slidably connected inside the aircraft carrier platform (3), and the four second sliders (63) are respectively fixedly connected to the two ends of the top of the two slide plates (6).

8. The substation inspection drone carrier platform according to claim 7 is characterized in that: The carrier platform (3) is rotatably connected to a second screw rod (61) inside. The second screw rod (61) is horizontally arranged. The two ends of the second screw rod (61) are respectively inserted into the symmetrical sides of the surface of the carrier platform (3). The second screw rod (61) is sleeved inside two slide plates (6). The two slide plates (6) are matched with the second screw rod (61). The symmetrical sides of the surface of the carrier platform (3) are rotatably connected to gears (62). The two second screw rods (61) are respectively fixedly connected to the two ends of the second screw rod (61). Four racks (115) are arranged inside the protective box (1). The four racks (115) are respectively fixedly connected to the two sides of the top of the two bottom plates (17). The two gears (62) are respectively meshed with two of the racks (115).

9. The substation inspection drone carrier platform according to claim 8 is characterized in that: The surfaces of the four fixed boxes (64) are each provided with a second connecting groove (65), the inside of the four second connecting grooves (65) are each horizontally fixedly connected with two sliding rods (66), the inside of the four second connecting grooves (65) are each horizontally slidably connected with a clamping block (7), the surfaces of the four clamping blocks (7) are symmetrically fixedly connected with second limiting strips (71) on both sides, and a plurality of the second limiting strips (71) are respectively slidably connected to the opposite sides of the inside of the four second connecting grooves (65), the four clamping blocks (7) are respectively sleeved on the surfaces of a plurality of sliding rods (66), the surfaces of the plurality of sliding rods (66) are each sleeved with a spring (73), and a plurality of the springs (73) are respectively arranged on the surfaces of the four clamping blocks (7), and the surfaces of the four clamping blocks (7) are each provided with a second arc groove (72).

10. The substation inspection drone carrier platform according to claim 1, characterized in that: The rotating mechanism comprises a first connecting rod (33), and first connecting columns (32) are fixedly connected to the two symmetrical sides of the surface of the aircraft carrier platform (3) near one end of the sealing door plate (2). Two first connecting rods (33) are provided, and the two first connecting rods (33) are respectively arranged on the two symmetrical sides of the surface of the aircraft carrier platform (3). The bottom ends of the two first connecting rods (33) are respectively sleeved on the surfaces of the two first connecting columns (32). Two first limiting strips (21) are vertically fixedly connected to one side of the surface of the sealing door plate (2). The surfaces of the two first limiting strips (21) are penetrated by limiting grooves (22). The top ends of the two first connecting rods (33) are respectively slidably connected to the surfaces of the two first limiting strips (21). The top ends of the two first connecting rods (33) are fixedly connected to the limiting columns (34), and the two limiting columns (34) are respectively slidably connected to the inside of the two limiting grooves (22).

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