A high-altitude storage cabin for unmanned aerial vehicles

Abstract

The application relates to a high-altitude storage cabin of a UAV, belonging to the technical field of UAV storage, which comprises a lifting assembly, the lifting assembly is connected with two chain assembly, the ends of the two chain assemblies away from the lifting assembly are connected with two transmission assemblies respectively, the top portions of the two transmission assemblies are connected with two cover plate assemblies respectively, the ends of the two cover plate assemblies away from each other are provided with a plurality of limiting assemblies, when the UAV needs to be parked, two electric push cylinders drive the parking platform to ascend, the parking platform pulls four chains and synchronously drives two lifting plates to ascend when ascending, so that four sleeves ascend and press the springs in the sleeves, until the four springs can drive four jacks and make the four jacks drive two cover plates, the two cover plates rotate around the connecting shafts fixedly connected with the cover plates, so that a space for the parking platform to pass through is formed between the two connecting shafts, until the parking platform ascends to the outside of the cabin body, and the UAV can be smoothly parked on the parking platform.

Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of unmanned aerial vehicle storage, in particular to an unmanned aerial vehicle high-altitude storage cabin. BACKGROUND

[0002] The power transmission line tower and the surrounding power facilities are exposed to the outdoors for a long time, and their various components will age or be damaged due to the influence of the external environment. Therefore, professional personnel need to regularly maintain the power transmission line tower and the surrounding power facilities. However, the power transmission line often passes through complex terrains such as mountains, forests, and rivers, and the towers are distributed in a scattered manner with a long distance (usually hundreds of meters). Relying on personnel to personally inspect requires a lot of time, and using unmanned aerial vehicles to replace manual inspection can avoid the above situation.

[0003] The current unmanned aerial vehicles cannot meet the requirements of long-distance and long-time operation due to small battery capacity. Therefore, an unmanned aerial vehicle storage device needs to be installed on the power transmission line tower to temporarily store the unmanned aerial vehicle and charge it. Chinese Patent No. CN216468426 U discloses a lifting mechanism of an unmanned aerial vehicle storage device and an unmanned aerial vehicle storage device, which relates to the technical field of unmanned aerial vehicles. It solves the technical problems of existing unmanned aerial vehicle storage equipment, such as large size, inability to automatically store, poor storage and charging, and complex overall structure. The device includes a driving structure, a guide structure, and a scissor arm. The driving structure is connected to the guide structure through a push-pull piece. The scissor arm is hinged to the guide structure and connected to the bearing platform of the unmanned aerial vehicle storage device. The driving structure drives the guide structure to reciprocate through the push-pull piece. The angle between the scissor arm and the guide structure changes, causing the bearing platform to move up and down.

[0004] The above-mentioned storage device allows the unmanned aerial vehicle to be parked on the base. The power transmission line tower is exposed to the outdoors for a long time, and the storage device installed on the power transmission line tower is also exposed to the outdoors in a place rarely visited by people. The lifting mechanism in the above-mentioned storage device is located inside the storage device. When the unmanned aerial vehicle is parked, the storage device needs to be provided with an opening for the base and the unmanned aerial vehicle to pass through, so that the unmanned aerial vehicle can normally enter the inside of the storage device. However, the opening of the above-mentioned storage device is not controlled by a power device and needs to be manually opened or closed, which cannot realize the automation of unmanned aerial vehicle storage. In addition, when the opening of the storage device is in a constant open state, the storage device cannot protect the unmanned aerial vehicle in adverse weather such as strong winds and rain. SUMMARY

[0005] Technical problems to be solved

[0006] The unmanned aerial vehicle high-altitude storage cabin of the present application comprises a lifting assembly, which is connected with two chain assemblies; the ends of the two chain assemblies away from the lifting assembly are connected with two transmission assemblies respectively; the top portions of the two transmission assemblies are connected with two cover plate assemblies respectively; the ends of the two cover plate assemblies away from each other are provided with a plurality of limiting assemblies, and the limiting assemblies are fixedly connected with the outer upper end of the cabin body;

[0007] Technical scheme

[0008] In order to achieve the object of the present application, the technical scheme adopted by the present application is as follows:

[0009] The unmanned aerial vehicle high-altitude storage cabin of the present application comprises a lifting assembly, which is connected with two chain assemblies; the ends of the two chain assemblies away from the lifting assembly are connected with two transmission assemblies respectively; the top portions of the two transmission assemblies are connected with two cover plate assemblies respectively; the ends of the two cover plate assemblies away from each other are provided with a plurality of limiting assemblies, and the limiting assemblies are fixedly connected with the outer upper end of the cabin body;

[0010] The cover plate assembly comprises a cover plate, one end of which is fixedly connected with a connecting shaft, and the cover plate and the connecting shaft are rotatably connected with the top of the cabin body; a plurality of upper solar panels are uniformly installed on the top of the cover plate;

[0011] The lifting assembly comprises a parking platform for parking the unmanned aerial vehicle, the bottom of the parking platform is fixedly connected with a connecting plate at the middle of both ends; the bottom of the two connecting plates is fixedly connected with the telescopic rods of two electric push cylinders respectively; a wireless charging platform is embedded in the middle of the top of the parking platform; four connecting pieces one are fixedly connected with the bottom of the parking platform uniformly, and two connecting pieces one located at the same end are respectively located on both sides of the electric push cylinder;

[0012] The transmission assembly comprises a lifting plate, the top of which is fixedly connected with a sleeve at both ends; a top column is coaxially arranged in the inner side of the sleeve; a circular hole is arranged on the top of the sleeve for the top column to pass through; the bottom of the end of the cover plate close to the connecting shaft is rotatably connected with the top of the two top columns; the bottom of the two top columns is coaxially fixedly connected with a baffle, the diameter of which is larger than that of the circular hole on the top of the sleeve; the top of both ends of the lifting plate is fixedly connected with a connecting piece two;

[0013] The chain assembly comprises two chains, one end of each chain is connected with two connecting pieces one at one end of the parking platform; the end of each chain away from the parking platform is connected with two connecting pieces two respectively; the inner side of the lower corner of each chain is engaged with a lower sprocket; the inner side of the upper corner of each chain is engaged with an upper sprocket; the two upper sprockets are coaxially fixedly connected with an upper shaft, and the two lower sprockets are coaxially fixedly connected with a lower shaft.

[0014] As a further technical scheme of the present application, the bottom of the cover plate is provided with a backing plate, and the top of the backing plate is attached to the bottom of the cover plate; the backing plate is located on the inner side of the top of the cabin body, and both ends of the backing plate are fixedly connected with the inner wall of the cabin body; the top of the cabin body is provided with a space for the cover plate to move.

[0015] As a further technical scheme of the present application, the stop platform is located in the middle of the inside of the cabin body, and the size of the cabin body is larger than that of the unmanned aerial vehicle; the bottoms of the two electric push cylinders are fixedly connected with the inner bottom of the cabin body; the wireless charging platform corresponds to the position of the unmanned aerial vehicle; an electric battery is arranged between the two electric push cylinders, and the bottom of the electric battery is fixedly connected with the inner bottom of the cabin body; the electric battery is electrically connected with the wireless charging platform and the electric push cylinders.

[0016] As a further technical scheme of the present application, the inside of each of the two sleeves is provided with a spring, the bottom of each of the two springs is attached to the inner bottom of each of the two sleeves, and the top of each of the two springs is attached to the bottom of each of the two baffles; the diameter of the spring is smaller than that of the baffle.

[0017] As a further technical scheme of the present application, the top of the lifting plate is symmetrically provided with two placing grooves, and two counterweights are arranged in the two placing grooves; the two counterweights are located between the two sleeves; one end of each of the two jacks away from the sleeve is slidably connected with a positioning piece, and one end of each of the two positioning pieces away from the jack is fixedly connected with the inner wall of the cabin body.

[0018] As a further technical scheme of the present application, the upper shaft and the lower shaft are located in the inside of the cabin body, and the two ends of the upper shaft and the two ends of the lower shaft are provided with bearing seats, and the plurality of bearing seats are fixedly connected with the inner wall of the cabin body.

[0019] As a further technical scheme of the present application, the limiting assembly comprises a limiting block for limiting the cover plate, and one end of the limiting block away from the cover plate is embedded in a connecting frame; one end of the connecting frame away from the limiting block is integrally connected with a mounting seat; one side of the mounting seat away from the connecting frame is fixedly connected with the outer upper end of the cabin body.

[0020] As a further technical scheme of the present application, the bottom of the cabin body is fixedly connected with a support frame, the support frame is L-shaped, one side of the support frame away from the cabin body is fixedly connected with a power transmission line tower and other power facilities, and the outer sides of both ends of the cabin body are provided with inclined side solar panels, and the bottoms of the two side solar panels are fixedly connected with two supports respectively, and one side of each of the two supports is fixedly connected with the outer sides of both ends of the cabin body.

[0021] Advantages:

[0022] 1、The unmanned aerial vehicle is parked on the parking platform, and the two electric push cylinders drive the parking platform to rise, and the parking platform pulls the four chains and synchronously drives the two lifting plates to rise, so that the four sleeves rise and press the springs in the respective interiors, until the four springs can drive the four jacks and make the two cover plates rotate around the connecting shafts fixedly connected with the cover plates, so that a space is formed between the two connecting shafts for the parking platform to pass through, until the parking platform rises to the outside of the cabin body, ensuring that the unmanned aerial vehicle can be smoothly parked on the parking platform; the rising of the parking platform and the rotation of the two cover plates are synchronous and controlled by the two electric push cylinders, without the need for additional power devices or manual control of the opening of the two cover plates.

[0023] 2、After the unmanned aerial vehicle is parked, the two electric push cylinders drive the parking platform to descend and reset, and the two lifting plates synchronously descend and reset; under the action of the spring force of the four springs, the four sleeves first descend with the two lifting plates, and the descending speed of the four jacks is less than that of the four sleeves, so that the descending speed of the parking platform is greater than that of the reverse rotation of the two cover plates, so that the two cover plates do not block the descent of the parking platform and the unmanned aerial vehicle during the resetting process, ensuring that the parking platform and the unmanned aerial vehicle can normally enter the cabin body.

[0024] 3、The four counterweights can increase the weight and stability of the two lifting plates, prevent the two lifting plates from shaking during vertical movement, and ensure the stability of the four sleeves and the four jacks; the four positioning pieces fix the positions of the four jacks, allowing the four jacks to only move vertically without affecting the movement of the four jacks, preventing the jacks from tilting, and ensuring that the four jacks can smoothly drive the two cover plates to rotate.

[0025] 4、The two backing plates support the two cover plates, so that the positions of the two cover plates in the closed state correspond to each other, ensuring that the two cover plates can wrap the unmanned aerial vehicle together with the cabin body, preventing the unmanned aerial vehicle from being negatively affected by the external harsh environment; the multiple limiting blocks and the multiple connecting frames limit the two cover plates, and when the two cover plates are in an open state, the multiple limiting blocks can support the two cover plates, preventing the two cover plates from rotating excessively due to their own gravity, and avoiding affecting the movement of the parking platform and the two lifting plates.

[0026] 5、The batteries can supply power to the two electric push cylinders and the wireless charging platform, and the wireless charging platform can wirelessly charge the unmanned aerial vehicle, so that the storage cabin can protect and charge the unmanned aerial vehicle at the same time; the multiple upper solar panels and the two side solar panels are distributed on the top and both ends of the cabin body, have a large area for receiving light, and can provide sufficient power for the batteries, ensuring that the wireless charging platform and the two electric push cylinders can work for a long time. Attached Figure Description

[0027] Figure 1 This is a three-dimensional structural diagram of the present invention;

[0028] Figure 2 In this invention Figure 1 Another perspective view;

[0029] Figure 3 In this invention Figure 2 Another perspective view;

[0030] Figure 4 In this invention Figure 1 Top view;

[0031] Figure 5 In this invention Figure 4 AA section view;

[0032] Figure 6 In this invention Figure 1 Partial structural diagram;

[0033] Figure 7 In this invention Figure 6 The main view;

[0034] Figure 8 In this invention Figure 6 Another perspective view;

[0035] Figure 9 This is a schematic diagram showing the connection between the cover plate assembly and the transmission assembly of the present invention;

[0036] Figure 10 In this invention Figure 9 Another perspective view;

[0037] Figure 11 This is a schematic diagram showing the connection between the lifting assembly and the chain assembly of the present invention;

[0038] Figure 12 In this invention Figure 11 Another perspective view;

[0039] Figure 13 In this invention Figure 11 The main view;

[0040] Figure 14 This is a schematic diagram showing the connection between the chain assembly and the transmission assembly of the present invention.

[0041] Figure 15 This is a schematic diagram of the internal structure of the transmission component of the present invention.

[0042] Figure 16 In this invention Figure 1 A magnified view of a portion of the image.

[0043] In the drawings:

[0044] 1 - cabin body,

[0045] 2 - support frame,

[0046] 3 - cover plate assembly, 31 - cover plate, 32 - backing plate, 33 - connecting shaft,

[0047] 4 - limiting assembly, 41 - limiting block, 42 - connecting frame, 43 - mounting seat,

[0048] 5 - upper solar panel,

[0049] 6 - side solar panel,

[0050] 7 - chain assembly, 71 - chain, 72 - upper sprocket, 73 - upper shaft, 74 - lower sprocket, 75 - lower shaft, 76 - bearing seat,

[0051] 8 - lifting assembly, 81 - stop platform, 82 - wireless charging platform, 83 - electric push cylinder, 84 - connecting plate, 85 - connecting piece one,

[0052] 9 - transmission assembly, 91 - lifting plate, 92 - counterweight, 93 - connecting piece two, 94 - sleeve, 95 - jacking column, 96 - positioning piece, 97 - spring, 98 - baffle,

[0053] 10 - support,

[0054] 11 - unmanned aerial vehicle,

[0055] 12 - battery. DETAILED DESCRIPTION

[0056] Please refer to Figures 1-15 The unmanned aerial vehicle high-altitude storage cabin comprises a lifting assembly 8, the lifting assembly 8 is connected with two chain assemblies 7; the ends of the two chain assemblies 7 away from the lifting assembly 8 are connected with two transmission assemblies 9 respectively; the top portions of the two transmission assemblies 9 are connected with two cover plate assemblies 3 respectively, the ends of the two cover plate assemblies 3 away from each other are provided with a plurality of limiting assemblies 4, and the plurality of limiting assemblies 4 are fixedly connected with the outer upper end of the cabin body 1.

[0057] The cover plate assembly 3 comprises a cover plate 31, one end of the cover plate 31 is fixedly connected with a connecting shaft 33, and the cover plate 31 and the connecting shaft 33 are rotatably connected with the top of the cabin body 1; a plurality of upper solar panels 5 are uniformly installed on the top of the cover plate 31;

[0058] The lifting assembly 8 comprises a parking platform 81 for parking the unmanned aerial vehicle 11, the bottom of the parking platform 81 is fixedly connected with a connecting plate 84 at the middle of both ends, the bottom of the two connecting plates 84 is fixedly connected with the telescopic rods of two electric push cylinders 83 respectively, the top of the parking platform 81 is embedded with a wireless charging platform 82, and the bottom of the parking platform 81 is fixedly connected with four connecting pieces one 85, wherein the two connecting pieces one 85 at the same end are located on the two sides of the electric push cylinder 83 respectively.

[0059] The transmission assembly 9 comprises a lifting plate 91, the top of the lifting plate 91 is fixedly connected with a sleeve 94 at both ends, the inner side of the two sleeves 94 is coaxially provided with a jackscrew 95, and the top of the sleeve 94 is provided with a circular hole for the jackscrew 95 to pass through, the top of the two jackscrews 95 is rotatably connected with the bottom of one end of the cover plate 31 close to the connecting shaft 33, the bottom of the two jackscrews 95 is coaxially fixedly connected with a baffle 98, the diameter of the baffle 98 is greater than that of the circular hole at the top of the sleeve 94, and the top of both ends of the lifting plate 91 is fixedly connected with a connecting piece two 93.

[0060] The chain assembly 7 comprises two chains 71, one end of the two chains 71 is connected with the two connecting pieces one 85 at one end of the parking platform 81 respectively, the end of the two chains 71 away from the parking platform 81 is connected with the two connecting pieces two 93 respectively, the lower corner inner side of the two chains 71 is engaged with a lower sprocket 74, and the upper corner inner side of the two chains 71 is engaged with an upper sprocket 72, the two upper sprockets 72 are coaxially fixedly connected with an upper shaft 73, and the two lower sprockets 74 are coaxially fixedly connected with a lower shaft 75.

[0061] The upper shaft 73 and the lower shaft 75 are located inside the cabin 1, the two ends of the upper shaft 73 and the two ends of the lower shaft 75 are provided with a bearing seat 76, and the plurality of bearing seats 76 are fixedly connected with the inner wall of the cabin 1.

[0062] When the unmanned aerial vehicle 11 needs to be parked, the two electric push cylinders 83 drive the parking platform 81 to rise, the parking platform 81 pulls the four chains 71 and synchronously drives the two lifting plates 91 to rise at the same time, so that the four sleeves 94 rise and press the springs 97 in the respective interiors, until the four springs 97 can drive the four jackscrews 95 and make the four jackscrews 95 drive the two cover plates 31, the two cover plates 31 rotate around the connecting shaft 33 fixedly connected with the cover plates 31 as the center, so that the space between the two connecting shafts 33 for the parking platform 81 to pass through is generated, until the parking platform 81 rises to the outside of the cabin 1, ensuring that the unmanned aerial vehicle 11 can be smoothly parked on the parking platform 81, the rising of the parking platform 81 and the rotation of the two cover plates 31 are synchronous and controlled by the two electric push cylinders 83, without the need of using an additional power device or manually controlling the opening of the two cover plates 31.

[0063] Please refer to Figures 5-10In the embodiment, the parking platform 81 is located in the middle of the cabin 1, and the size of the cabin 1 is larger than that of the unmanned aerial vehicle 11; the bottoms of the two electric push cylinders 83 are fixedly connected with the inner bottom of the cabin 1; the wireless charging platform 82 corresponds to the position of the unmanned aerial vehicle 11; the battery 12 is arranged between the two electric push cylinders 83, and the bottom of the battery 12 is fixedly connected with the inner bottom of the cabin 1; the battery 12 is electrically connected with the wireless charging platform 82 and the electric push cylinder 83.

[0064] The two sleeves 94 are internally provided with springs 97, the bottoms of the two springs 97 are respectively attached to the inner bottoms of the two sleeves 94, and the tops of the two springs 97 are respectively attached to the bottoms of the two baffles 98; the diameter of the spring 97 is smaller than that of the baffle 98.

[0065] By adopting the above technical scheme, after the unmanned aerial vehicle 11 is parked, the two electric push cylinders 83 drive the parking platform 81 to descend and reset, and the two lifting plates 91 are synchronously lowered and reset; under the action of the elasticity of the four springs 97, the four sleeves 94 first descend with the two lifting plates 91, the descending speed of the four jacks 95 is smaller than that of the four sleeves 94, so that the descending speed of the parking platform 81 is greater than the speed of reverse rotation and resetting of the two cover plates 31, the two cover plates 31 cannot block the descent of the parking platform 81 and the unmanned aerial vehicle 11 in the process of resetting, and the parking platform 81 and the unmanned aerial vehicle 11 can normally enter the cabin 1.

[0066] Please refer to Figures 9-10 、 Figures 14-15 In the embodiment, the top of the lifting plate 91 is symmetrically provided with two placing grooves, and the two placing grooves are respectively arranged with a counterweight 92; the two counterweights 92 are located between the two sleeves 94; the ends of the two jacks 95 away from the sleeves 94 are slidably connected with positioning members 96, and the ends of the two positioning members 96 away from the jacks 95 are fixedly connected with the inner wall of the cabin 1.

[0067] By adopting the above technical scheme, the four counterweights 92 can increase the weight of the two lifting plates 91, increase the stability of the two lifting plates 91, prevent the two lifting plates 91 from shaking in the process of vertical movement, and further ensure the stability of the four sleeves 94 and the four jacks 95; the four positioning members 96 respectively fix the positions of the four jacks 95, do not affect the movement of the four jacks 95, make the four jacks 95 only be able to move vertically, prevent the jacks 95 from tilting, and ensure that the four jacks 95 can smoothly jack the two cover plates 31 to rotate.

[0068] Please refer to Figures 7-10 、 Figure 16In the embodiment, the bottom of the cover plate 31 is provided with a backing plate 32, and the top of the backing plate 32 is attached to the bottom of the cover plate 31; the backing plate 32 is located on the inner side of the upper end of the cabin body 1, and both ends of the backing plate 32 are fixedly connected with the inner wall of the cabin body 1; the top of the cabin body 1 is provided with a space for the cover plate 31 to move.

[0069] The limiting assembly 4 comprises a limiting block 41 for limiting the cover plate 31, and one end of the limiting block 41 away from the cover plate 31 is embedded in the connecting frame 42; one end of the connecting frame 42 away from the limiting block 41 is integrally connected with the mounting seat 43; one side of the mounting seat 43 away from the connecting frame 42 is fixedly connected with the outer side of the upper end of the cabin body 1.

[0070] By adopting the above technical scheme, the two backing plates 32 play a supporting role for the two cover plates 31, so that the positions of the two cover plates 31 in the closed state correspond to each other, ensuring that the two cover plates 31 can wrap the unmanned aerial vehicle 11 together with the cabin body 1, preventing the unmanned aerial vehicle 11 from being affected by the harsh external environment; the multiple limiting blocks 41 cooperate with the multiple connecting frames 42 to limit the two cover plates 31, when the two cover plates 31 are in an open state, the multiple limiting blocks 41 can support the two cover plates 31, preventing the two cover plates 31 from rotating excessively due to their own gravity, and avoiding affecting the movement of the parking platform 81 and the two lifting plates 91.

[0071] Please refer to Figures 1-8 、 Figures 11-12 In the embodiment, the bottom of the cabin body 1 is fixedly connected with the support frame 2, the support frame 2 is L-shaped, and one side of the support frame 2 away from the cabin body 1 is fixedly connected with the power transmission line tower and other power facilities; the outer sides of both ends of the cabin body 1 are provided with inclined side solar panels 6, and the bottoms of the two side solar panels 6 are fixedly connected with two brackets 10, and one side of each of the two brackets 10 is fixedly connected with the outer sides of both ends of the cabin body 1.

[0072] By adopting the above technical scheme, the storage cabin can supply power to the two electric push cylinders 83 and the wireless charging platform 82, and the wireless charging platform 82 can wirelessly charge the unmanned aerial vehicle 11, so that the storage cabin can charge the unmanned aerial vehicle 11 while protecting it; the multiple upper solar panels 5 and the two side solar panels 6 are distributed on the top and both ends of the cabin body 1, and have a large area to receive light, which can provide sufficient power for the storage battery 12, ensuring that the wireless charging platform 82 and the two electric push cylinders 83 can work for a long time.

[0073] The embodiments of the present application disclose the preferred embodiments, but are not limited thereto, and those skilled in the art can easily understand the spirit of the present application according to the above embodiments, and make different inferences and changes, as long as they do not deviate from the spirit of the present application, which are within the protection scope of the present application.

Claims

1. A high-altitude storage compartment for unmanned aerial vehicles (UAVs), characterized in that: It includes a lifting assembly (8), which is connected to two chain assemblies (7); the ends of the two chain assemblies (7) away from the lifting assembly (8) are respectively connected to two transmission assemblies (9); the tops of the two transmission assemblies (9) are respectively connected to two cover plate assemblies (3); the ends of the two cover plate assemblies (3) away from each other are provided with multiple limiting components (4), and the multiple limiting components (4) are fixedly connected to the upper outer side of the cabin (1); The cover plate assembly (3) includes a cover plate (31), one end of which is fixedly connected to a connecting shaft (33), and the cover plate (31) is rotatably connected to the top of the cabin (1) through the connecting shaft (33); a plurality of upper solar panels (5) are evenly installed on the top of the cover plate (31). The lifting assembly (8) includes a landing platform (81) for parking the drone (11), with connecting plates (84) fixedly connected to the middle of both ends of the bottom of the landing platform (81); the bottom of the two connecting plates (84) is fixedly connected to the telescopic rods of the two electric push cylinders (83); a wireless charging platform (82) is embedded in the middle of the top of the landing platform (81); four connectors (85) are evenly fixedly connected to the bottom of the landing platform (81), with two connectors (85) located at the same end located on both sides of the electric push cylinder (83). The transmission assembly (9) includes a lifting plate (91), with sleeves (94) fixedly connected to both ends of the top of the lifting plate (91). The inner sides of the two sleeves (94) are coaxially provided with top posts (95), and the top of the sleeves (94) is provided with a round hole for the top posts (95) to pass through. The tops of the two top posts (95) are rotatably connected to the bottom of the end of the cover plate (31) near the connecting shaft (33). The bottoms of the two top posts (95) are coaxially fixedly connected with baffles (98), the diameter of which is larger than the diameter of the round hole at the top of the sleeves (94). Connecting parts two (93) are fixedly connected to the tops of both ends of the lifting plate (91). The chain assembly (7) includes two chains (71), one end of each chain (71) is connected to two connectors (85) at one end of the stop platform (81); the ends of each chain (71) away from the stop platform (81) are connected to two connectors (93); the inner side of the lower corner of each chain (71) is engaged with a lower sprocket (74), and the inner side of the upper corner of each chain (71) is engaged with an upper sprocket (72); the two upper sprockets (72) are coaxially fixedly connected to the upper shaft (73), and the two lower sprockets (74) are coaxially fixedly connected to the lower shaft (75).

2. The UAV high-altitude storage cabin as described in claim 1, characterized in that: The bottom of the cover plate (31) is provided with a pad plate (32), and the top of the pad plate (32) is attached to the bottom of the cover plate (31); the pad plate (32) is located on the inner side of the upper end of the cabin (1), and both ends of the pad plate (32) are fixedly connected to the inner wall of the cabin (1); the top of the cabin (1) is provided with space for the cover plate (31) to move.

3. The UAV high-altitude storage cabin as described in claim 1, characterized in that: The landing platform (81) is located in the middle of the cabin (1), and the size of the cabin (1) is larger than the size of the drone (11); the bottom of the two electric thrust cylinders (83) is fixedly connected to the bottom of the inner side of the cabin (1); the wireless charging platform (82) corresponds to the position of the drone (11); a battery (12) is provided between the two electric thrust cylinders (83), and the bottom of the battery (12) is fixedly connected to the bottom of the inner side of the cabin (1); the battery (12) is electrically connected to the wireless charging platform (82) and the electric thrust cylinders (83).

4. The UAV high-altitude storage cabin as described in claim 1, characterized in that: Both sleeves (94) are equipped with springs (97) inside. The bottom of the two springs (97) is in contact with the bottom of the inner side of the two sleeves (94), and the top of the two springs (97) is in contact with the bottom of the two baffles (98). The diameter of the springs (97) is smaller than the diameter of the baffles (98).

5. The UAV high-altitude storage cabin as described in claim 1, characterized in that: The top of the lifting plate (91) is symmetrically provided with two placement slots, and a counterweight (92) is placed in each of the two placement slots; the two counterweights (92) are located between the two sleeves (94); the ends of the two top columns (95) away from the sleeves (94) are slidably connected with positioning parts (96), and the ends of the two positioning parts (96) away from the top columns (95) are fixedly connected to the inner wall of the cabin (1).

6. The UAV high-altitude storage cabin as described in claim 1, characterized in that: The upper shaft (73) and the lower shaft (75) are both located inside the cabin (1). Bearing seats (76) are installed at both ends of the upper shaft (73) and the lower shaft (75). Multiple bearing seats (76) are fixedly connected to the inner wall of the cabin (1).

7. The UAV high-altitude storage cabin as described in claim 1, characterized in that: The limiting component (4) includes a limiting block (41) for limiting the cover plate (31). The end of the limiting block (41) away from the cover plate (31) is embedded in the connecting frame (42). The end of the connecting frame (42) away from the limiting block (41) is integrally connected to the mounting base (43). The side of the mounting base (43) away from the connecting frame (42) is fixedly connected to the upper outer side of the cabin (1).

8. The UAV high-altitude storage cabin as described in claim 3, characterized in that: The bottom of the cabin (1) is fixedly connected to the support frame (2), which is L-shaped, and the side of the support frame (2) away from the cabin (1) is fixedly connected to the power facilities of the transmission line tower; both ends of the cabin (1) are provided with inclined side solar panels (6), and the bottom of the two side solar panels (6) is fixedly connected to two brackets (10) respectively, and one side of the two brackets (10) is fixedly connected to both ends of the cabin (1).

Images