An unmanned aerial vehicle hangar

Abstract

The utility model belongs to the technical field of unmanned plane, disclose a kind of unmanned plane hangar, comprising: warehouse body subassembly has parking platform;Top cover subassembly is in closed state, first top cover, second top cover and parking platform form parking cavity by surrounding;Paddle collection subassembly includes first elastic paddle collection board and second elastic paddle collection board, along respective length direction, first elastic paddle collection board one end is connected in the inner side wall of first top cover, and end towards second top cover extends, second elastic paddle collection board one end is connected in the inner side wall of second top cover, and end towards first top cover extends;In first elastic paddle collection board and second elastic paddle collection board, the end of one of them extends bending towards the direction of inner side wall away from corresponding, and / or, the end of another extends bending towards the direction of inner side wall close to corresponding, in closed state, first elastic paddle collection board end and second elastic paddle collection board end staggered coincidence. The above-mentioned setting improves the safety and reliability of the unmanned plane hangar folding paddle.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, and in particular to a UAV hangar. Background Technology

[0002] A drone (unmanned aerial vehicle) is an aircraft that can complete flight missions through remote control or autonomous program control without a pilot operating it from inside the aircraft. It can be applied in various industries. A drone hangar is a device that provides shelter from wind and rain and power replenishment for drones conducting unmanned inspections. The hangar has a parking platform for drones to land and a rotating, opening and closing cover. After the cover is opened, the drone can land on the platform, and then the cover can be rotated to close. Because the drone's propellers may be extended beyond the parking platform when landing, the rotating cover can collide with and damage the propellers.

[0003] Existing technology provides a drone hangar with two opposing, closing covers. Each cover has four extending, flexible propeller retracting plates on its two sides. These four plates correspond to the four propeller blades of the drone. During the rotation and closing process of the covers, the flexible retracting plates first abut against the propeller blades, pushing them to rotate and retract into the cover. The elasticity of the retracting plates reduces damage to the propeller blades. However, to align the corresponding propeller blades, the two flexible retracting plates on the same side of the two covers are installed in the same position on their respective covers. This leads to interference and collision between the two plates during the rotation and closing process. If the installation positions of the two plates on their corresponding covers are staggered, it will be difficult to cover the corresponding propeller blades, posing a risk that the propeller blades cannot be retracted. Utility Model Content

[0004] The purpose of this utility model is to provide a drone hangar that can solve the problem of interference between the installation positions of the flexible propeller retraction plates in existing drone hangars, or the difficulty of covering the corresponding propellers by staggering the installation positions, which makes it impossible to retract the propellers.

[0005] To achieve this objective, the present invention adopts the following technical solution:

[0006] A drone hangar is provided, comprising:

[0007] The hangar components include a parking platform for carrying drones;

[0008] The top cover assembly includes a first top cover and a second top cover disposed opposite to each other. The first top cover and the second top cover are rotatably connected to the garage body assembly. In the closed state where the first top cover and the second top cover are closed above the parking platform, the first top cover, the second top cover and the parking platform together form a parking cavity.

[0009] The paddle recovery assembly includes a first elastic paddle recovery plate and a second elastic paddle recovery plate. Along their respective length directions, one end of the first elastic paddle recovery plate is connected to the inner sidewall of the first top cover, and the end extends toward the second top cover. One end of the second elastic paddle recovery plate is connected to the inner sidewall of the second top cover, and the end extends toward the first top cover.

[0010] In the closed state, the ends of the first elastic reaming plate and the second elastic reaming plate are bent and extended away from the corresponding inner sidewall, and / or the ends of the other elastic reaming plate are bent and extended closer to the corresponding inner sidewall.

[0011] In one embodiment, the top cover assembly further includes:

[0012] A first mounting block is disposed on the first inner sidewall of the first top cover. One end of the first elastic paddle retractor is connected to the first mounting block and is spaced apart from the first inner sidewall. The end of the first elastic paddle retractor is bent and extended away from the first inner sidewall.

[0013] The second mounting block is disposed on the second inner sidewall of the second top cover. One end of the second elastic paddle retractor is connected to the second mounting block and is spaced apart from the second inner sidewall. The end of the second elastic paddle retractor is bent and extended toward the second inner sidewall.

[0014] In one embodiment, the first top cover further includes a first connecting sidewall disposed between the two first inner sidewalls, and the first mounting block has a first extending arc surface that extends from the first inner sidewall to the first connecting sidewall.

[0015] And / or, the second top cover further includes a second connecting sidewall disposed between the two second inner sidewalls, the second mounting block having a second extending arc surface extending from the second inner sidewall to the second connecting sidewall.

[0016] In one embodiment, the drone hangar further includes:

[0017] An air conditioning unit includes a main unit and an air outlet that are interconnected. The air conditioning unit is connected to the garage body assembly. The air outlet of the air outlet faces upwards from the parking platform. The air conditioning unit is configured to blow cold or hot air toward the parking cavity.

[0018] In one embodiment, the garage assembly includes an outer shell, a parking platform disposed on top of the outer shell, an installation space within the outer shell, a main unit disposed in the installation space, one end of an air outlet connected to the main unit, and the other end extending above the parking platform, the main unit having a second air outlet facing the installation space.

[0019] In one embodiment, a partition plate is provided inside the outer casing, which divides the installation space into a first installation space above and a second installation space below. The second air outlet faces the second installation space. The parking platform is provided with a first flow hole and a second flow hole that are spaced apart, and both the first flow hole and the second flow hole are connected to the first installation space.

[0020] In one embodiment, the paddle recovery assembly is provided in two sets, the first top cover having two opposing first inner sidewalls, the second top cover having two opposing second inner sidewalls, the two first elastic paddle recovery plates of the two sets of paddle recovery assemblies being disposed opposite to the two first inner sidewalls, and the two second elastic paddle recovery plates of the two sets of paddle recovery assemblies being disposed opposite to the two second inner sidewalls; and / or,

[0021] The end of the first elastic throttle plate is provided with a first flexible protective part; and / or,

[0022] The second flexible sprue plate has a second flexible protective part at its end.

[0023] In one embodiment, the first top cover and / or the second top cover are provided with functional modules. The drone hangar also includes a control module and a cable drag chain. The hangar body component includes an outer shell. The parking platform is disposed on the top of the outer shell. The outer shell has an installation space. The control module is disposed in the installation space. The fixed end of the cable drag chain is fixedly connected to the hangar body component. The cable drag chain has a free end. The control module and the functional module are connected by a wire harness. The wire harness passes through the cable drag chain.

[0024] In one embodiment, the top cover assembly further includes a first seal, the first top cover having a first closed edge and the second top cover having a second closed edge, the first seal being disposed on either the first closed edge or the second closed edge, wherein in the closed state, the first closed edge abuts against the second closed edge, and the first seal is used to seal the gap between the first closed edge and the second closed edge; and / or,

[0025] The top cover assembly further includes a second seal. The first top cover has a first opening. In the closed state, the library body assembly is fitted into the first opening. The second seal is disposed around the periphery of the first opening and abuts against the outer surface of the library body assembly. The second seal is configured to seal the gap between the library body assembly and the first top cover; and / or,

[0026] The top cover assembly further includes a third seal. The second top cover has a second opening. In the closed state, the library body assembly is embedded in the second opening. The third seal is disposed on the periphery of the second opening and abuts against the outer surface of the library body assembly. The third seal is configured to seal the gap between the library body assembly and the second top cover.

[0027] In one embodiment, the top cover assembly further includes a first drive member and a first rotating shaft. The output end of the first drive member is connected to the first rotating shaft. The length of the first rotating shaft extends along a first direction, and both ends of the first rotating shaft are respectively connected to the two sides of the first top cover. The first rotating shaft is used to drive the first top cover to rotate. A first torsion spring is fitted around the first rotating shaft. One end of the first torsion spring is fixedly connected to the output end of the first drive member, and the other end of the first torsion spring is connected to the first rotating shaft and rotates with the first rotating shaft. The first torsion spring applies torque to the first rotating shaft, and the torque drives the first rotating shaft to always have a tendency to rotate in the opposite direction; and / or,

[0028] The top cover assembly further includes a second drive member and a second rotating shaft. The output end of the second drive member is connected to the second rotating shaft. The length of the second rotating shaft extends along a first direction. The two ends of the second rotating shaft are respectively connected to the two sides of the second top cover. The second rotating shaft is used to drive the second top cover to rotate. A second torsion spring is fitted around the second rotating shaft. One end of the second torsion spring is fixedly connected to the output end of the second drive member. The other end of the second torsion spring is connected to the second rotating shaft and rotates with the second rotating shaft. The second torsion spring applies torque to the second rotating shaft. The torque drives the second rotating shaft to always have a tendency to rotate in the opposite direction.

[0029] The beneficial effects of this utility model are:

[0030] The drone hangar provided by this utility model includes a propeller retraction assembly comprising a first elastic propeller retraction plate and a second elastic propeller retraction plate. Along their respective lengths, one end of the first elastic propeller retraction plate is connected to the inner wall of the first top cover, and its end extends toward the second top cover. One end of the second elastic propeller retraction plate is connected to the inner wall of the second top cover, and its end extends toward the first top cover. After the drone lands on the parking platform, during the rotation and closing of the first and second top covers, the first elastic propeller retraction plate extending from the first top cover and the second elastic propeller retraction plate extending from the second top cover each correspond to one propeller blade on the drone. Through elastic contact, they retract the propeller blade into the parking cavity, preventing the first and second top covers from colliding with the propeller blade. Specifically, one of the first and second elastic propeller retraction plates can have its end bent away from the corresponding inner wall, or its end bent toward the corresponding inner wall, or both ends can be bent away from the corresponding inner wall and toward the corresponding inner wall. For example, the end of the first elastic rotor blade installed on the inner wall of the first top cover is bent and extended away from the inner wall. Correspondingly, the end of the second elastic rotor blade installed on the inner wall of the second top cover is bent and extended closer to the inner wall. In this way, after the first and second top covers are rotated and closed, the ends of the bent and extended first and second elastic rotor blades avoid each other, forming an overlapping state. This arrangement avoids the risk that the installation area may not be able to cover the corresponding rotor blades and the rotor blades may not be able to be retracted due to misaligned installation of the first and second elastic rotor blades. It also avoids the risk of interference and collision between the first and second elastic rotor blades, thus improving the safety and reliability of the UAV hangar. Attached Figure Description

[0031] Figure 1 This is a schematic diagram of the structure of the drone hangar described in this embodiment of the utility model;

[0032] Figure 2 This is a front view of the unmanned aerial vehicle hangar in the closed state according to an embodiment of this utility model;

[0033] Figure 3 yes Figure 2 A cross-sectional view along the AA direction;

[0034] Figure 4 yes Figure 2 A cross-sectional view along the BB direction;

[0035] Figure 5 yes Figure 3 A magnified view of part C in the diagram.

[0036] In the picture:

[0037] 1. Garage body assembly; 11. Parking platform; 12. Parking cavity; 13. Outer shell; 14. Divider plate; 141. First installation space; 142. Second installation space; 151. First flow hole; 152. Second flow hole; 16. Casters; 17. Support legs;

[0038] 2. Top cover assembly; 21. First top cover; 211. First inner sidewall; 212. First connecting sidewall; 22. Second top cover; 221. Second inner sidewall; 222. Second connecting sidewall; 23. First mounting block; 231. First extended arc surface; 24. Second mounting block; 241. Second extended arc surface; 251. First driving component; 252. First rotating shaft; 253. First torsion spring;

[0039] 3. Paddle recovery assembly; 31. First elastic paddle recovery plate; 32. Second elastic paddle recovery plate;

[0040] 4. Air conditioning components; 41. Main unit; 411. Second air outlet; 42. Air outlet section; 421. Air outlet; 51. Camera; 52. Wind vane; 53. Cable chain; 6. First centering component; 61. First push rod; 7. Second centering component; 71. Second push rod; 81. First seal; 82. Second seal; 9. Charging component. Detailed Implementation

[0041] The technical solution of this utility model will now be clearly and completely described with reference to the accompanying drawings. Obviously, the described embodiments are only some, not all, of the embodiments of this utility model. Based on the embodiments of this utility model, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of this utility model.

[0042] In the description of this utility model, it should be noted that the terms "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," and "outer," etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are used only for the convenience of describing this utility model and for simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model. Furthermore, the terms "first" and "second" are used for descriptive purposes only and should not be construed as indicating or implying relative importance. The terms "first position" and "second position" refer to two different positions. Moreover, "above," "on top of," and "over" the first feature in relation to the second feature includes the first feature directly above and diagonally above the second feature, or simply indicates that the first feature is at a higher horizontal level than the second feature. "Below," "under," and "below" the first feature in relation to the second feature includes the first feature directly below and diagonally below the second feature, or simply indicates that the first feature is at a lower horizontal level than the second feature.

[0043] In the description of this utility model, it should be noted that, unless otherwise explicitly specified and limited, the terms "installation," "connection," and "joining" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; and they can refer to the internal connection of two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0044] The embodiments of this utility model are described in detail below. Examples of these embodiments are shown in the accompanying drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary and are only used to explain this utility model, and should not be construed as limiting this utility model.

[0045] The technical solution of this utility model will be further described below with reference to the accompanying drawings and specific embodiments.

[0046] like Figures 1 to 5 As shown, this utility model provides a drone hangar, which includes a hangar body assembly 1, a top cover assembly 2, and a propeller retraction assembly 3. The hangar body assembly 1 includes a parking platform 11 for carrying drones, and drones in flight can land on the parking platform 11. The top cover assembly 2 includes a first top cover 21 and a second top cover 22 disposed opposite to each other. Both the first top cover 21 and the second top cover 22 are rotatably connected to the hangar body assembly 1. In the closed state, with the first top cover 21 and the second top cover 22 closed on the parking platform 11, the first top cover 21, the second top cover 22, and the parking platform 11 together form a parking cavity 12, which provides a safe and enclosed space for the drone.

[0047] The propeller retraction assembly 3 includes a first elastic retraction plate 31 and a second elastic retraction plate 32. Along their respective length directions, one end of the first elastic retraction plate 31 is connected to the inner wall of the first top cover 21, and the other end extends toward the second top cover 22. One end of the second elastic retraction plate 32 is connected to the inner wall of the second top cover 22, and the other end extends toward the first top cover 21. After the drone lands on the parking platform 11, during the rotation and closing of the first top cover 21 and the second top cover 22, the first elastic retraction plate 31 extending from the first top cover 21 and the second elastic retraction plate 32 extending from the second top cover 22 each correspond to one propeller blade on the drone. Through elastic contact, the propeller blade is retracted into the parking cavity 12, preventing the first top cover 21 and the second top cover 22 from colliding with the propeller blade. In this configuration, of the first elastic reaming plate 31 and the second elastic reaming plate 32, one end is bent and extends away from the corresponding inner wall, and / or the other end is bent and extends closer to the corresponding inner wall. In the closed state, the ends of the first elastic reaming plate 31 and the second elastic reaming plate 32 overlap. That is, of the first elastic reaming plate 31 and the second elastic reaming plate 32, one end may be bent and extends away from the corresponding inner wall, or the other end may be bent and extends closer to the corresponding inner wall, or one end may be bent and extends away from the corresponding inner wall while the other end is bent and extends closer to the corresponding inner wall.

[0048] like Figure 3 and Figure 5 As shown, the end of the first elastic rotor blade 31, installed on the inner wall of the first top cover 21, bends and extends away from the inner wall. Correspondingly, the end of the second elastic rotor blade 32, installed on the inner wall of the second top cover 22, bends and extends closer to the inner wall. Thus, after the first top cover 21 and the second top cover 22 are rotated and closed, the ends of the bent-extended first elastic rotor blade 31 and the second elastic rotor blade 32 avoid each other, forming an overlapping staggered state. This arrangement avoids the risk that misaligned installation of the first elastic rotor blade 31 and the second elastic rotor blade 32 might result in the installation area not covering the corresponding rotor blades, thus preventing the rotor blades from being retracted. It also avoids the risk of interference and collision between the first elastic rotor blade 31 and the second elastic rotor blade 32, improving the safety and reliability of the UAV hangar. Moreover, compared to a planar structure, the bent-extended first elastic rotor blade 31 and the second elastic rotor blade 32 have better structural strength and are less prone to deformation.

[0049] In one embodiment, the inner wall on the first top cover 21 where the first elastic paddle catcher 31 is mounted is defined as the first inner wall 211, and the inner wall on the second top cover 22 where the second elastic paddle catcher 32 is mounted is defined as the second inner wall 221. The top cover assembly 2 also includes a first mounting block 23 and a second mounting block 24. The first mounting block 23 is disposed on the first inner wall 211, one end of the first elastic paddle catcher 31 is connected to the first mounting block 23 and spaced apart from the first inner wall 211, and the end of the first elastic paddle catcher 31 is bent and extended away from the first inner wall 211. The second mounting block 24 is disposed on the second inner wall 221, one end of the second elastic paddle catcher 32 is connected to the second mounting block 24 and spaced apart from the second inner wall 221, and the end of the second elastic paddle catcher 32 is bent and extended closer to the second inner wall 221. After the first top cover 21 and the second top cover 22 are rotated and closed, the end of the second elastic retractable paddle plate 32 is inserted between the first elastic retractable paddle plate 31 and the first inner sidewall 211. The end of the first elastic retractable paddle plate 31 is located on the side of the second elastic retractable paddle plate 32 opposite to the second inner sidewall 221. Figure 3 The sectional view is shown in the figure.

[0050] The first top cover 21 also includes a first connecting sidewall 212 disposed between two first inner sidewalls 211. The first mounting block 23 has a first extending arc surface 231, which extends from the first inner sidewall 211 to the first connecting sidewall 212. The first extending arc surface 231 causes the right-angle connection between the first inner sidewall 211 and the first connecting sidewall 212 to form an arc-shaped connection. The first extending arc surface 231 guides the position of the blades, making the blades more concentrated.

[0051] Similarly, the second top cover 22 also includes a second connecting sidewall 222 disposed between the two second inner sidewalls 221, and the second mounting block 24 has a second extending arc surface 241, which extends from the second inner sidewall 221 to the second connecting sidewall 222. The second extending arc surface 241 forms an arc-shaped connection at the right-angle connection between the second inner sidewall 221 and the second connecting sidewall 222, and guides the position of the blades, making the blades more concentrated.

[0052] To provide a safer parking environment for drones, the drone hangar also includes an air conditioning component 4. The air conditioning component 4 includes a main unit 41 and an air outlet 42 connected to each other. The air conditioning component 4 is connected to the hangar body component 1. The air outlet 421 of the air outlet 42 faces upwards towards the parking platform 11. The air conditioning component 4 is configured to blow cold or hot air towards the parking cavity 12, maintaining a suitable temperature in the parking cavity 12 compared to the outside environment. This prevents damage to the drone or the internal structural components of the drone hangar from high or low temperatures. For example, when the outside temperature is low, the hot air delivered by the air conditioning component 4 helps maintain the drone's battery life. The specific structure and working principle of the main unit 41 can be set with reference to existing technology, and will not be elaborated here.

[0053] Specifically, the garage assembly 1 includes an outer shell 13, a parking platform 11 disposed on top of the outer shell 13, and an installation space within the outer shell 13. The main unit 41 is disposed within the installation space. One end of the air outlet 42 is connected to the main unit 41, and the other end extends above the parking platform 11. The main unit 41 has a second air outlet 411 facing the installation space, thereby ensuring a suitable ambient temperature in both the installation space and the parking chamber 12.

[0054] In one embodiment, two sets of air conditioning components 4 are provided, with the two types of air conditioning components 4 respectively located at both ends of the parking platform 11 along its length to improve temperature regulation capability.

[0055] In one embodiment, the drone hangar is equipped with a backup battery to provide charging power for the drone when there is no external power supply, and to provide operating power for the electrical structural components of the drone hangar. A partition 14 is provided inside the outer shell 13, dividing the installation space into an upper first installation space 141 and a lower second installation space 142. The first installation space 141 is used to store electrical structural components, and the second installation space 142 is used to store the backup battery; this partitioned storage improves safety. A second air outlet 411 faces the second installation space 142, directly providing cool or hot air to the second installation space 142. The parking platform 11 has a first flow hole 151 and a second flow hole 152 spaced apart, both of which are connected to the first installation space 141. Through the first flow hole 151 and the second flow hole 152, airflow circulates between the first installation space 141 and the parking cavity 12 above the parking platform 11, enabling temperature regulation within the first installation space 141 and improving temperature uniformity through airflow.

[0056] In one embodiment, the UAV is equipped with four propellers, and two sets of propeller retraction assemblies 3 are provided. The first top cover 21 has two opposing first inner sidewalls 211, and the second top cover 22 has two opposing second inner sidewalls 221. The two first elastic retraction plates 31 of the two sets of propeller retraction assemblies 3 are oppositely disposed on the two first inner sidewalls 211, and the two second elastic retraction plates 32 of the two sets of propeller retraction assemblies 3 are oppositely disposed on the two second inner sidewalls 221. The ends of the two opposing first elastic retraction plates 31 are bent and extended in a direction away from each other, and the ends of the two opposing second elastic retraction plates 32 are bent and extended in a direction close to each other, forming a cross-avoidance.

[0057] To improve the safety of retracting the propeller blades, a first flexible protective part is provided at the end of the first elastic retractor plate 31. For example, a rubber sheet is fitted at the end of the first elastic retractor plate 31 to form the first flexible protective part. The first flexible protective part directly contacts the propeller blade. The body of the first elastic retractor plate 31 has a slightly higher rigidity to ensure that thrust can be applied to the propeller blade, so as to safely retract the propeller blade without damaging it.

[0058] Similarly, the end of the second elastic blade 32 is provided with a second flexible protective part. For example, the end of the second elastic blade 32 is fitted with a rubber sheet to form the second flexible protective part, which directly contacts the blade. The body of the second elastic blade 32 has a slightly higher rigidity to ensure that it can apply thrust to the blade and will not damage the blade while safely retracting it.

[0059] Functional modules are provided on the first top cover 21 and / or the second top cover 22. The drone hangar also includes a control module and a cable drag chain 53. The hangar body component 1 includes an outer shell 13, a parking platform 11 is located on top of the outer shell 13, and the control module is located within the installation space, which can be located in the first installation space 141. The fixed end of the cable drag chain 53 is fixedly connected to the hangar body component 1. The cable drag chain 53 has a free end. The control module and the functional module are connected by a wire harness, which passes through the cable drag chain 53. During the rotation of the first top cover 21 and the second top cover 22, the functional module will move, and the wire harness will move accordingly. Through the cable drag chain 53, the cable harness is protected while also allowing it to follow the movement, preventing the wire harness from being dragged. The functional modules include, but are not limited to, a camera 51 and a wind vane 52.

[0060] The top cover assembly 2 also includes a first sealing element 81. The first top cover 21 has a first closed edge, and the second top cover 22 has a second closed edge. The first sealing element 81 is disposed on either the first or the second closed edge. In the closed state, the first closed edge abuts against the second closed edge, and the first sealing element 81 is used to seal the gap between the first and second closed edges. The first sealing element 81 can be disposed on the first top cover 21 or the second top cover 22, for example, as shown in... Figure 3 and Figure 5 As shown, the first sealing element 81 is fitted onto the second closed edge of the second top cover 22. After the first top cover 21 and the second top cover 22 are closed, the first sealing element 81 abuts against the first top cover 21 to seal the gap between the first closed edge and the second closed edge. The first sealing element 81 is a rubber sealing strip, and this application does not limit the cross-sectional shape of the first sealing element 81.

[0061] The top cover assembly 2 also includes a second seal 82. The first top cover 21 has a first opening. In the closed state, the vault body assembly 1 is embedded in the first opening. The second seal 82 is disposed inside the periphery of the first opening. After the first top cover 21 is rotated to close, the second seal 82 abuts against the outer surface of the vault body assembly 1. The second seal 82 is configured to seal the gap between the vault body assembly 1 and the first top cover 21. The second seal 82 is a rubber sealing strip, and this application does not limit the cross-sectional shape of the second seal 82.

[0062] Similarly, the top cover assembly 2 also includes a third seal. The second top cover 22 has a second opening. In the closed state, the storage body assembly 1 is embedded in the second opening. The third seal is disposed inside the periphery of the second opening. After the second top cover 22 is rotated to close, the third seal abuts against the outer side of the storage body assembly 1. The third seal is configured to seal the gap between the storage body assembly 1 and the second top cover 22, improving the sealing performance of the storage cavity 12. The third seal is also a rubber sealing strip. This application does not limit the cross-sectional shape of the second seal 82.

[0063] The top cover assembly 2 also includes a first drive element 251 and a first rotating shaft 252. The first drive element 251 is a motor, and its output end is connected to the first rotating shaft 252. The length of the first rotating shaft 252 extends along a first direction, and its two ends are respectively connected to the two sides of the first top cover 21. The first rotating shaft 252 is used to drive the first top cover 21 to rotate. For ease of understanding, the width direction of the storage body assembly 1 is defined as the first direction, and the length direction of the storage body assembly 1 is defined as the second direction. The first rotating shaft 252 is connected to one end of the first top cover 21 through a rod structure, applying torque to the first top cover 21 and controlling its rotation. As the first top cover 21 rotates and opens, the lever arm between the center of gravity of the open first top cover 21 and the first rotating shaft 252 increases, requiring a larger starting torque when the first top cover 21 is rotated in the opposite direction to close it. A first torsion spring 253 is fitted around the first rotating shaft 252. One end of the first torsion spring 253 is fixedly connected to the output end of the first driving member 251, and the other end of the first torsion spring 253 is connected to the first rotating shaft 252 and rotates with the first rotating shaft 252. The first torsion spring 253 applies torque to the first rotating shaft 252, and the torque drives the first rotating shaft 252 to always have a tendency to rotate in the opposite direction. During the process of the first rotating shaft 252 rotating and opening the first top cover 21, the first torsion spring 253 is twisted. The elastic force generated by the twisting of the first torsion spring 253 is applied to the first top cover 21, which can reduce the starting torque required for the first top cover 21 to rotate and close, and the closing speed is faster.

[0064] Similarly, the top cover assembly 2 also includes a second drive unit and a second rotating shaft. The second drive unit is a motor, and its output end is connected to the second rotating shaft. The length of the second rotating shaft extends along a first direction, and its two ends are respectively connected to the two sides of the second top cover 22. The second rotating shaft is used to drive the second top cover 22 to rotate. A second torsion spring is fitted around the second rotating shaft. One end of the second torsion spring is fixedly connected to the output end of the second drive unit, and the other end of the second torsion spring is connected to the second rotating shaft and rotates with it. The second torsion spring applies torque to the second rotating shaft, and the torque drives the second rotating shaft to always have a tendency to rotate in the opposite direction. By setting the second torsion spring, the starting torque required for the rotation and closing of the second top cover 22 can be reduced, resulting in a faster closing speed.

[0065] The parking platform 11 has a charging position at its center. Since the landing position of the drone may be inaccurate, in one embodiment, the drone hangar also includes a first centering component 6. The first centering component 6 includes two first push rods 61 that are spaced apart on both sides of the parking platform 11 along a first direction. The first push rods 61 can reciprocate along the first direction. The two first push rods 61 move towards each other to push the drone on the parking platform 11 to move to the charging position.

[0066] The drone hangar also includes a second centering component 7, which includes two second push rods 71 ​​spaced apart at both ends of the parking platform 11 along a second direction. The second push rods 71 ​​can reciprocate along the second direction, and the two push rods 71 ​​move towards each other to push the drone on the parking platform 11 to the charging position. The reciprocating movement structure of the first centering component 6 and the second centering component 7 can be configured with reference to existing technology, and this embodiment is not limited thereto. The drone that has moved to the charging position can dock with the charging unit 9 to achieve charging.

[0067] The bottom of the outer casing 13 is equipped with four casters 16 and four liftable support legs 17. The casters 16 enable the drone hangar to move, and when it moves to the required position, the support legs 17 lower to support the drone hangar and keep it in a stable position.

[0068] Obviously, the above embodiments of this utility model are merely examples for clearly illustrating the present utility model, and are not intended to limit the implementation of the present utility model. Those skilled in the art can make other variations or modifications based on the above description. It is neither necessary nor possible to exhaustively list all possible implementations here. Any modifications, equivalent substitutions, and improvements made within the spirit and principles of this utility model should be included within the protection scope of the claims of this utility model.

Claims

1. A hangar for unmanned aerial vehicles (UAVs), characterized in that, include: The storage component (1) includes a parking platform (11) for carrying the drone; The top cover assembly (2) includes a first top cover (21) and a second top cover (22) disposed opposite to each other. The first top cover (21) and the second top cover (22) are rotatably connected to the garage body assembly (1). In the closed state where the first top cover (21) and the second top cover (22) are closed over the parking platform (11), the first top cover (21), the second top cover (22) and the parking platform (11) together form a parking cavity (12). The paddle retraction assembly (3) includes a first elastic paddle retraction plate (31) and a second elastic paddle retraction plate (32). Along their respective length directions, one end of the first elastic paddle retraction plate (31) is connected to the inner wall of the first top cover (21), and the end extends toward the second top cover (22). One end of the second elastic paddle retraction plate (32) is connected to the inner wall of the second top cover (22), and the end extends toward the first top cover (21). In the closed state, the ends of the first elastic reaming plate (31) and the second elastic reaming plate (32) are bent and extended away from the corresponding inner wall, and / or the ends of the other are bent and extended closer to the corresponding inner wall.

2. The drone hangar according to claim 1, characterized in that, The top cover assembly (2) also includes: The first mounting block (23) is disposed on the first inner sidewall (211) of the first top cover (21). One end of the first elastic paddle retractor (31) is connected to the first mounting block (23) and is spaced apart from the first inner sidewall (211). The end of the first elastic paddle retractor (31) is bent and extended away from the first inner sidewall (211). The second mounting block (24) is disposed on the second inner sidewall (221) of the second top cover (22). One end of the second elastic paddle retractor (32) is connected to the second mounting block (24) and is spaced apart from the second inner sidewall (221). The end of the second elastic paddle retractor (32) is bent and extended toward the second inner sidewall (221).

3. The drone hangar according to claim 2, characterized in that, The first top cover (21) further includes a first connecting sidewall (212) disposed between the two first inner sidewalls (211), and the first mounting block (23) has a first extending arc surface (231) extending from the first inner sidewall (211) to the first connecting sidewall (212). And / or, the second top cover (22) further includes a second connecting sidewall (222) disposed between the two second inner sidewalls (221), and the second mounting block (24) has a second extending arc surface (241) extending from the second inner sidewall (221) to the second connecting sidewall (222).

4. The drone hangar according to claim 1, characterized in that, The drone hangar also includes: An air conditioning unit (4) includes a main unit (41) and an air outlet (42) connected to each other. The air conditioning unit (4) is connected to the garage assembly (1). The air outlet (421) of the air outlet (42) faces upwards toward the parking platform (11). The air conditioning unit (4) is configured to blow cold or hot air toward the parking cavity (12).

5. The drone hangar according to claim 4, characterized in that, The garage assembly (1) includes an outer shell (13), the parking platform (11) is disposed on the top of the outer shell (13), the outer shell (13) has an installation space inside, the main unit (41) is disposed in the installation space, one end of the air outlet (42) is connected to the main unit (41), and the other end extends above the parking platform (11), the main unit (41) has a second air outlet (411), the second air outlet (411) faces the installation space.

6. The drone hangar according to claim 5, characterized in that, A partition plate (14) is provided inside the outer shell (13). The partition plate (14) divides the installation space into a first installation space (141) above and a second installation space (142) below. The second air outlet (411) faces the second installation space (142). The parking platform (11) is provided with a first flow hole (151) and a second flow hole (152) spaced apart. The first flow hole (151) and the second flow hole (152) are both connected to the first installation space (141).

7. The unmanned aerial vehicle hangar according to any one of claims 1-6, characterized in that, The paddle-catching assembly (3) is provided in two sets. The first top cover (21) has two opposing first inner sidewalls (211), and the second top cover (22) has two opposing second inner sidewalls (221). The two first elastic paddle-catching plates (31) of the two sets of paddle-catching assemblies (3) are oppositely arranged on the two first inner sidewalls (211), and the two second elastic paddle-catching plates (32) of the two sets of paddle-catching assemblies (3) are oppositely arranged on the two second inner sidewalls (221); and / or, The end of the first elastic throttle plate (31) is provided with a first flexible protective part; and / or, The second flexible protective part is provided at the end of the second elastic sprue plate (32).

8. The unmanned aerial vehicle hangar according to any one of claims 1-6, characterized in that, The first top cover (21) and / or the second top cover (22) are provided with functional modules. The UAV hangar also includes a control module and a cable drag chain (53). The hangar body component (1) includes an outer shell (13). The parking platform (11) is located on the top of the outer shell (13). The outer shell (13) has an installation space. The control module is located in the installation space. The fixed end of the cable drag chain (53) is fixedly connected to the hangar body component (1). The cable drag chain (53) has a free end. The control module and the functional module are connected by a wire harness. The wire harness is passed through the cable drag chain (53).

9. The unmanned aerial vehicle hangar according to any one of claims 1-6, characterized in that, The top cover assembly (2) further includes a first seal (81), the first top cover (21) having a first closed edge, and the second top cover (22) having a second closed edge. The first seal (81) is disposed on either the first closed edge or the second closed edge. In the closed state, the first closed edge abuts against the second closed edge, and the first seal (81) is used to seal the gap between the first closed edge and the second closed edge; and / or, The top cover assembly (2) further includes a second seal (82). The first top cover (21) has a first opening. In the closed state, the library body assembly (1) is fitted into the first opening. The second seal (82) is disposed around the periphery of the first opening and abuts against the outer surface of the library body assembly (1). The second seal (82) is configured to seal the gap between the library body assembly (1) and the first top cover (21); and / or, The top cover assembly (2) further includes a third seal, the second top cover (22) having a second opening, the body assembly (1) being fitted into the second opening in the closed state, the third seal being disposed on the periphery of the second opening, the third seal abutting against the outer side of the body assembly (1), the third seal being configured to seal the gap between the body assembly (1) and the second top cover (22).

10. The unmanned aerial vehicle hangar according to any one of claims 1-6, characterized in that, The top cover assembly (2) further includes a first drive member (251) and a first rotating shaft (252). The output end of the first drive member (251) is connected to the first rotating shaft (252). The length of the first rotating shaft (252) extends along a first direction. The two ends of the first rotating shaft (252) are respectively connected to the two sides of the first top cover (21). The first rotating shaft (252) is used to drive the first top cover (21) to rotate. A first torsion spring (253) is fitted around the first rotating shaft (252). One end of the first torsion spring (253) is fixedly connected to the output end of the first drive member (251). The other end of the first torsion spring (253) is connected to the first rotating shaft (252) and rotates with the first rotating shaft (252). The first torsion spring (253) applies torque to the first rotating shaft (252). The torque drives the first rotating shaft (252) to always have a tendency to rotate in the opposite direction; and / or, The top cover assembly (2) further includes a second drive member and a second rotating shaft. The output end of the second drive member is connected to the second rotating shaft. The length of the second rotating shaft extends along a first direction. The two ends of the second rotating shaft are respectively connected to the two sides of the second top cover (22). The second rotating shaft is used to drive the second top cover (22) to rotate. A second torsion spring is fitted on the outside of the second rotating shaft. One end of the second torsion spring is fixedly connected to the output end of the second drive member. The other end of the second torsion spring is connected to the second rotating shaft and rotates with the second rotating shaft. The second torsion spring applies torque to the second rotating shaft. The torque drives the second rotating shaft to always have a tendency to rotate in the opposite direction.

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