Compound wing unmanned aerial vehicle hangar

Abstract

The utility model belongs to the technical field of unmanned plane equipment, disclose a kind of composite wing unmanned plane hangar, it includes support mechanism and hatch assembly.Support mechanism is used to carry and park unmanned plane;Hatch assembly includes first hatch and second hatch, first hatch and second hatch are movably arranged on support mechanism, first hatch and second hatch can be respectively in horizontal direction mutually close to abut, and with support mechanism form sealed containing cavity, to cover unmanned plane, first hatch and second hatch are respectively provided with first containing portion and second containing portion that protrude outward, first containing portion and second containing portion are used to accommodate the wing of unmanned plane, first hatch and second hatch can also be respectively in horizontal direction mutually away, to completely expose unmanned plane.The volume of the composite wing unmanned plane hangar is smaller, realizes lightweight and miniaturization design, meets the use demand of user.

Description

Technical Field

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

[0002] Unmanned aerial vehicles (UAVs), also known as drones, are unmanned aircraft controlled by electronic remote control equipment and onboard program control devices. Due to their advantages such as small size, low cost, and ease of use, they are widely used in aerial photography, surveying, disaster relief, and express delivery.

[0003] Drones can perform tasks such as reconnaissance, detection, and inspection. For example, they can be used in scenarios where there is no one to visit for extended periods but drone operations are still required, enabling monitoring and inspection of fixed areas. Therefore, drone hangars are needed for these scenarios, allowing drones to monitor and inspect the surrounding area from the hangar's center. However, current drone hangars on the market are quite large, especially those for fixed-wing or hybrid-wing drones. Their large size and weight not only make transportation and storage difficult but also limit their functionality, hindering drone deployment.

[0004] Therefore, there is an urgent need for a composite-wing UAV hangar to solve the above problems. Utility Model Content

[0005] According to one aspect of the present invention, a composite-wing UAV hangar is provided, which has a small volume and achieves lightweight and miniaturized design to meet the user's needs.

[0006] To achieve this objective, the present invention adopts the following technical solution:

[0007] The compound-wing drone hangar includes:

[0008] Support structure, used to support and park drones;

[0009] The hatch assembly includes a first hatch and a second hatch, both of which are movably mounted on the support mechanism. The first hatch and the second hatch can approach and abut against each other in the horizontal direction, forming a sealed accommodating cavity with the support mechanism to cover the drone. The first hatch and the second hatch are respectively provided with an outwardly protruding first accommodating portion and a second accommodating portion for accommodating the wings of the drone. The first hatch and the second hatch can also move away from each other in the horizontal direction to completely expose the drone.

[0010] Optionally, the support mechanism includes a landing pad and a lifting assembly. The landing pad is used to carry and park the UAV, and the lifting assembly can drive the landing pad to switch between a first height and a second height in the vertical direction when the UAV is fully exposed.

[0011] Optionally, the compound-wing UAV hangar further includes an opening and closing drive mechanism, which includes an opening and closing drive component and a slide rail. The slide rail is disposed on the support mechanism. The first hatch and the second hatch are respectively movably disposed on the slide rail. The output end of the opening and closing drive component is respectively connected to the first hatch and the second hatch. The opening and closing drive component can drive the first hatch and the second hatch to move closer to or further away from each other.

[0012] Optionally, the compound-wing UAV hangar further includes a sealing element, wherein a first sealing groove is provided on the side of the first door facing the second door, and a corresponding second sealing groove is provided on the second door. When the first door and the second door approach and abut against each other, the sealing element is sandwiched between the bottom of the first sealing groove and the bottom of the second sealing groove.

[0013] Optionally, the height of the top surface of the first hatch gradually decreases along the direction away from the second hatch;

[0014] Along the direction away from the first hatch, the height of the top surface of the second hatch gradually decreases.

[0015] Optionally, the support structure includes a helipad, on which the UAV is parked;

[0016] The compound-wing UAV hangar also includes a centering mechanism, which is located on the landing pad and is used to drive the UAV to a designated position on the landing pad.

[0017] Optionally, the centering mechanism includes a first centering component, which includes a first centering rod and a second centering rod. The first centering rod and the second centering rod are respectively disposed on both sides of the helipad and can move closer to or further away from each other along a first direction; and / or,

[0018] The centering mechanism further includes a second centering component, which includes a third centering rod and a fourth centering rod. The third centering rod and the fourth centering rod are respectively located on both sides of the parking apron and can move closer to or further away from each other along a second direction, which is perpendicular to the first direction.

[0019] Optionally, the first centering component further includes a first transmission belt, a first slider, and a second slider. The first transmission belt is disposed parallel to a first direction on the apron. The first transmission belt has a first belt and a second belt connected end-to-end and moving in opposite directions. The first slider is connected to the first belt, and the second slider is connected to the second belt. Rotation of the first transmission belt can cause the first slider and the second slider to move closer to or further away from each other. The first centering rod is connected to the first slider, and the second centering rod is connected to the second slider; and / or,

[0020] The second centering component further includes a second transmission belt, a third slider, and a fourth slider. The second transmission belt is arranged parallel to the second direction on the apron. The second transmission belt has a third belt and a fourth belt that are connected end to end and move in opposite directions. The third slider is connected to the third belt, and the fourth slider is connected to the fourth belt. When the second transmission belt rotates, it can drive the third slider and the fourth slider to move closer to or further away from each other. The third centering rod is connected to the third slider, and the fourth centering rod is connected to the fourth slider.

[0021] Optionally, the compound-wing UAV hangar further includes a charging mechanism, which includes a charging component and a protective cover. The charging component is disposed on the support mechanism and is used to charge the UAV. The protective cover is disposed outside the charging component.

[0022] Optionally, the compound-wing UAV hangar also includes an environmental meteorological monitoring mechanism located outside the housing cavity, which is used to monitor environmental and meteorological information outside the compound-wing UAV hangar.

[0023] The beneficial effects of this utility model are:

[0024] This utility model provides a composite-wing UAV hangar, with a support mechanism for supporting and parking the UAV, thus providing support points for UAV takeoff and landing. The door assembly includes a first door and a second door, both movably mounted on the support mechanism. The first and second doors can approach each other horizontally, forming a sealed accommodating cavity with the support mechanism to cover the UAV; they can also move horizontally away from each other to fully expose the UAV. In other words, when the first and second doors are abutting, the door assembly, in cooperation with the support mechanism, enables the UAV to be stored and housed; when the first and second doors are separated, the UAV can be released. The first and second doors each have outwardly protruding first and second accommodating portions for accommodating the UAV's wings. The door assembly conforms to the UAV's shape, has a small overall size, and high space utilization, contributing to lightweight and miniaturized design and meeting user needs. Attached Figure Description

[0025] To more clearly illustrate the technical solutions in the embodiments of this utility model, the drawings used in the description of the embodiments of this utility model will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on the content of the embodiments of this utility model and these drawings without creative effort.

[0026] Figure 1 This is a schematic diagram of the structure of the composite-wing UAV hangar provided in this embodiment of the utility model;

[0027] Figure 2 This is a schematic diagram of the structure of the first hatch provided in this embodiment of the utility model;

[0028] Figure 3 This is a schematic diagram of the structure of the second hatch provided in this embodiment of the utility model;

[0029] Figure 4 This is a bottom view of the hangar section structure of the compound-wing UAV provided in this embodiment of the utility model;

[0030] Figure 5 This is a partial structural schematic diagram of the hangar for the composite-wing unmanned aerial vehicle provided in this embodiment of the utility model;

[0031] Figure 6 This is a top view of the hangar section structure of the compound-wing UAV provided in this embodiment of the utility model;

[0032] Figure 7 This is a top view of the helipad provided in this embodiment of the utility model;

[0033] Figure 8 This is a partial structural schematic diagram of the centering mechanism provided in this embodiment of the utility model;

[0034] Figure 9 yes Figure 8 A magnified view of a section at point A in the middle;

[0035] Figure 10 This is a schematic diagram of the structure of the environmental meteorological monitoring agency provided in this embodiment of the utility model.

[0036] In the picture:

[0037] 100. Drones;

[0038] 1. Support mechanism; 11. Helipad; 111. First through channel; 112. Second through channel; 113. Third through channel; 114. Fourth through channel; 12. Lifting assembly; 13. First dustproof component; 14. Second dustproof component;

[0039] 2. Door assembly; 21. First door; 211. First receiving portion; 212. First sealing groove; 22. Second door; 221. Second receiving portion; 222. Second sealing groove;

[0040] 31. Opening and closing drive component; 32. Slide rail;

[0041] 4. Centering mechanism; 41. First centering component; 411. First centering rod; 412. Second centering rod; 413. First transmission belt; 4131. First strip belt; 4132. Second strip belt; 414. First slider; 415. Second slider; 416. First driving component; 4171. First transmission rod; 4172. First support; 418. First guide rail; 42. Second centering component; 421. Third centering rod; 422. Fourth centering rod; 423. Second transmission belt; 424. Third slider; 425. Fourth slider; 426. Second driving component; 4271. Second transmission rod; 428. Third guide rail; 43. Dust cover;

[0042] 5. Charging mechanism;

[0043] 6. Environmental meteorological monitoring agencies; 61. Wind speed measuring devices; 62. Rainfall measuring devices; 63. Cameras. Detailed Implementation

[0044] The technical solution of this utility model will be further described below with reference to the accompanying drawings and specific embodiments.

[0045] To make the objectives, technical solutions, and advantages of the embodiments of this utility model clearer, the technical solutions of the embodiments of this utility model will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this utility model, and not all embodiments. The components of the embodiments of this utility model described and shown in the accompanying drawings can generally be arranged and designed in various different configurations.

[0046] Therefore, the following detailed description of the embodiments of the present invention provided in the accompanying drawings is not intended to limit the scope of the claimed invention, but merely to illustrate selected embodiments of the invention. All other embodiments obtained by those skilled in the art based on the embodiments of the present invention without inventive effort are within the scope of protection of the present invention.

[0047] It should be noted that similar labels and letters in the following figures indicate similar items. Therefore, once an item is defined in one figure, it does not need to be further defined and explained in subsequent figures.

[0048] In the description of this utility model, it should be noted that the terms "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, or the orientation or positional relationship commonly used when the product of this utility model is in use. 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," "second," and "third," etc., are used only to distinguish descriptions and should not be construed as indicating or implying relative importance. In the description of this utility model, unless otherwise stated, "a plurality of" means two or more.

[0049] In the description of this utility model, it should also be noted that, unless otherwise explicitly specified and limited, the terms "set" and "connection" 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. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0050] In this invention, unless otherwise explicitly specified and limited, "above" or "below" the second feature can include direct contact between the first and second features, or contact between the first and second features through another feature between them. Furthermore, "above," "over," and "on top" of the second feature includes the first feature directly above or diagonally above the second feature, or simply indicates that the first feature is at a higher horizontal level than the second feature. "Below," "below," and "under" the second feature includes the first feature directly below or diagonally below the second feature, or simply indicates that the first feature is at a lower horizontal level than the second feature.

[0051] In the description of this utility model, the term "and / or" is merely a description of the relationship between related objects, indicating that three relationships can exist. For example, A and / or B can represent: A existing alone, A and B existing simultaneously, or B existing alone. Additionally, in this utility model, the character " / " generally indicates that the preceding and following related objects have an "or" relationship.

[0052] 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.

[0053] This embodiment provides a hybrid-wing drone hangar, which can be used for drone storage and recharging. In this embodiment, the hybrid-wing drone hangar is specifically used for the storage and retrieval of hybrid-wing drones. Of course, in other embodiments, the hybrid-wing drone hangar can also accommodate other types of drones; this is not a limitation. Figure 1 As shown, the hangar for the composite wing unmanned aerial vehicle includes a support structure 1 and a door assembly 2.

[0054] The support mechanism 1 is used to support and park the drone 100, thereby providing a support point for the takeoff and landing of the drone 100. The door assembly 2 includes a first door 21 and a second door 22. The first door 21 and the second door 22 are movably mounted on the support mechanism 1. The first door 21 and the second door 22 can approach and abut against each other in the horizontal direction, forming a sealed receiving cavity with the support mechanism 1 to cover the drone 100; the first door 21 and the second door 22 can also move away from each other in the horizontal direction to completely expose the drone 100. That is, when the first door 21 and the second door 22 abut against each other, the door assembly 2 cooperates with the support mechanism 1 to realize the storage and retrieval of the drone 100; when the first door 21 and the second door 22 separate, the drone 100 can be released. The first door 21 and the second door 22 are respectively provided with an outwardly protruding first receiving portion 211 and a second receiving portion 221, which are used to accommodate the wings of the drone 100. The hatch assembly 2 fits the shape of the UAV 100, with a small overall size and high space utilization, which helps to achieve lightweight and miniaturized design and meet the user's needs.

[0055] In this embodiment, the shapes of the first receiving portion 211 and the second receiving portion 221 are adapted to the wing shape of the UAV 100, and the lengths of the first receiving portion 211 and the second receiving portion 221 are designed according to the longest wingspan of the UAV 100. Meanwhile, both the first door 21 and the second door 22 are made of aluminum, which is lightweight and rust-resistant, effectively utilizing hangar space, reducing the hangar's external dimensions and weight.

[0056] Optionally, such as Figures 1-3 As shown, the top surface height of the first door 21 gradually decreases along the direction away from the second door 22. Simultaneously, the top surface height of the second door 22 gradually decreases along the direction away from the first door 21. This arrangement ensures that when the first door 21 and the second door 22 abut, the height of the middle position between them is the highest. This not only enhances the visual appeal and increases the aesthetics but also facilitates rapid drainage of rainwater, preventing rainwater from accumulating on the top of the doors for extended periods and preventing rainwater from seeping into the hangar of the composite-wing UAV through the gap between the first door 21 and the second door 22.

[0057] Furthermore, the hangar for the compound-wing UAV also includes seals (not shown). (See reference...) Figure 2 and Figure 3The first hatch 21 has a first sealing groove 212 on the side facing the second hatch 22, and the second hatch 22 has a corresponding second sealing groove 222. When the first hatch 21 and the second hatch 22 approach and abut against each other, a sealing element is sandwiched between the bottom of the first sealing groove 212 and the bottom of the second sealing groove 222. For example, the sealing element can be a sealing ring or a sealing strip, etc., to ensure the sealing performance of the gap between the first hatch 21 and the second hatch 22.

[0058] Optionally, continue to refer to Figure 1 The hangar for the compound-wing UAV also includes an opening and closing drive mechanism. This mechanism includes an opening and closing drive component 31 and a slide rail 32. The slide rail 32 is mounted on the support mechanism 1, and the first hatch 21 and the second hatch 22 are movably mounted on the slide rail 32. The output end of the opening and closing drive component 31 is connected to the first hatch 21 and the second hatch 22, respectively. The opening and closing drive component 31 can drive the first hatch 21 and the second hatch 22 to move closer or further apart, thereby enabling the storage or release of the UAV 100.

[0059] In this embodiment, the opening and closing drive component 31 is a three-stage push rod, and the slide rail 32 is a heavy-duty telescopic slide rail. The three-stage push rod has stable efficiency and low operating cost, while the heavy-duty telescopic slide rail is stable and provides good support.

[0060] Specifically, the slide rail 32 is provided in two sets, and the two sets of slide rail 32 are along the first direction ( Figure 1 (Extended setting in the x direction). There are two opening and closing drive components 31, which are respectively located on both sides of the support mechanism 1. By opening the output end of the drive mechanism, the first hatch 21 or the second hatch 22 can be pushed to move along the corresponding set of slide rails 32.

[0061] More specifically, the two slide rails 32 in each group are set in parallel and spaced apart, which can ensure the stability of the first hatch 21 or the second hatch 22 during the movement.

[0062] like Figure 1 and Figure 4 As shown, the support mechanism 1 includes a landing pad 11 and a lifting assembly 12. The landing pad 11 is used to support and park the drone 100. The lifting assembly 12 is capable of driving the landing pad 11 vertically when the drone 100 is fully exposed. Figure 1 (Z-direction) Switching between the first altitude and the second altitude. When the drone 100 lands, the lifting assembly 12 drives the landing pad 11 to rise to the highest point (second altitude) to facilitate the landing of the drone 100; after the drone 100 lands, the lifting assembly 12 drives the landing pad 11 to fall to the lowest point (first altitude) to facilitate the closing of the first door 21 and the second door 22 to store the drone 100.

[0063] Optionally, the support mechanism 1 also includes a housing. The housing has an opening at the top, the lifting assembly 12 is housed inside the housing, and the landing pad 11 is vertically and flexibly positioned at the opening of the housing. The housing provides installation space for the lifting assembly 12 and protects the lifting assembly 12 from damage caused by external dust or moisture.

[0064] In this embodiment, the lifting assembly 12 is a scissor lift structure as used in the prior art. The helipad 11 is made of sheet metal and plastic materials, which effectively reduces the weight of the helipad 11, reduces the load on the lifting assembly 12, and thus better ensures the stability of the helipad 11 during lifting.

[0065] Continue to refer to Figures 5-9 The hangar for the composite-wing UAV also includes a centering mechanism 4. The centering mechanism 4 is used to push and clamp the UAV 100 in the middle position of the parking apron 11.

[0066] Specifically, the centering mechanism 4 includes a first centering component 41. The first centering component 41 includes a first centering rod 411 and a second centering rod 412. The first centering rod 411 and the second centering rod 412 are respectively located on both sides of the apron 11 and can move along a first direction ( Figure 1 (in the x-direction) moving closer or further apart. The first centering rod 411 and the second centering rod 412 can push the drone 100 to the center of the landing pad 11 in the first direction.

[0067] Similarly, the centering mechanism 4 also includes a second centering component 42. The second centering component 42 includes a third centering rod 421 and a fourth centering rod 422. The third centering rod 421 and the fourth centering rod 422 are respectively located on both sides of the apron 11 and can move along the second direction ( Figure 1 The first and second directions are set perpendicular to each other. The third centering rod 421 and the fourth centering rod 422 can push the drone 100 to the middle of the landing pad 11 in the second direction, so that the drone 100 will eventually stop in the middle position of the landing pad 11.

[0068] More specifically, the first centering component 41 further includes a first transmission belt 413, a first slider 414, and a second slider 415. The first transmission belt 413 is arranged parallel to the first direction on the apron 11. The first transmission belt 413 has a first belt 4131 and a second belt 4132 connected end to end and moving in opposite directions. The first slider 414 is connected to the first belt 4131, the second slider 415 is connected to the second belt 4132, the first centering rod 411 is connected to the first slider 414, and the second centering rod 412 is connected to the second slider 415. When the first transmission belt 413 rotates, it can drive the first slider 414 and the second slider 415 to move closer or further apart, thereby realizing the movement of the first centering rod 411 and the second centering rod 412 closer or further apart.

[0069] Furthermore, such as Figure 9 As shown, the first centering assembly 41 further includes a first driving member 416, a first transmission rod 4171, and a first support 4172. Two first supports 4172 are provided, spaced apart along a first direction on the helipad 11. Correspondingly, two first transmission rods 4171 are provided, extending parallel to a second direction. Each first transmission rod 4171 is rotatably mounted on one of the two first supports 4172 around its own axis, and a first transmission belt 413 is wound around the two first transmission rods 4171. The fixed end of the first driving member 416 is located on the helipad 11, and the output end of the first driving member 416 is connected to one of the first transmission rods 4171. The output end of the first driving member 416 can drive the first transmission rod 4171 to rotate around its own axis, thereby driving the first transmission belt 413 to rotate. Since the first transmission belt 413 moves in opposite directions before and after passing the first transmission rod 4171, by placing the first slider 414 and the second slider 415 on opposite sides of the first transmission belt 413, the first transmission belt 413 can drive the first slider 414 and the second slider 415 to move toward or away from each other. This arrangement ensures, on the one hand, the synchronization of the movement of the first slider 414 and the second slider 415, thereby ensuring that the first centering assembly 41 can stably center the UAV 100 in the first direction; on the other hand, it eliminates the need for two first drive members 416 to drive the first slider 414 and the second slider 415 respectively, simplifying the structure of the first centering assembly 41 and thus reducing the manufacturing cost of the entire compound-wing UAV hangar.

[0070] Preferably, the first driving component 416 is a servo motor. Using a servo motor as the first driving component 416 can improve the motion accuracy of the first slider 414 and the second slider 415.

[0071] Furthermore, the first centering component 41 also includes a first guide rail 418 and a second guide rail. Both the first guide rail 418 and the second guide rail are arranged parallel to the first direction on the landing pad 11. The first slider 414 slides in engagement with the first guide rail 418, and the second slider 415 slides in engagement with the second guide rail. This arrangement restricts the movement of the first slider 414 and the second slider 415 to only the first direction, thereby preventing the UAV 100 from accurately centering in the first direction due to the misalignment of the first centering rod 411 and the second centering rod 412.

[0072] Similarly, continue to refer to Figures 5-8The second centering assembly 42 further includes a second transmission belt 423, a third slider 424, and a fourth slider 425. The second transmission belt 423 is arranged parallel to the second direction on the apron 11. The second transmission belt 423 has a third belt and a fourth belt connected end-to-end and moving in opposite directions. The third slider 424 is connected to the third belt, and the fourth slider 425 is connected to the fourth belt. The third centering rod 421 is connected to the third slider 424, and the fourth centering rod 422 is connected to the fourth slider 425. Rotation of the second transmission belt 423 can cause the third slider 424 and the fourth slider 425 to move closer or further apart, thereby causing the third centering rod 421 and the fourth centering rod 422 to move closer or further apart.

[0073] Furthermore, the second centering assembly 42 also includes a second drive member 426, a second transmission rod 4271, and a second support. Two second supports are provided, spaced apart along a second direction on the helipad 11. Correspondingly, two second transmission rods 4271 are provided, extending parallel to the first direction. Each second transmission rod 4271 is rotatably mounted on one of the two second supports around its own axis, and a second transmission belt 423 is wound around the two second transmission rods 4271. The fixed end of the second drive member 426 is located on the helipad 11, and the output end of the second drive member 426 is connected to one of the second transmission rods 4271. The output end of the second drive member 426 can drive the second transmission rod 4271 to rotate around its own axis, thereby driving the second transmission belt 423 to rotate. Since the second transmission belt 423 moves in opposite directions before and after passing the second transmission rod 4271, the third slider 424 and the fourth slider 425 are respectively positioned on opposite sides of the second transmission belt 423. This allows the second transmission belt 423 to drive the third slider 424 and the fourth slider 425 to move towards or away from each other. This arrangement ensures, on the one hand, the synchronous movement of the third slider 424 and the fourth slider 425, thereby ensuring that the second centering assembly 42 can stably center the UAV 100 in the second direction; on the other hand, it eliminates the need for two second drive members 426 to drive the third slider 424 and the fourth slider 425 respectively, simplifying the structure of the second centering assembly 42 and reducing the manufacturing cost of the entire compound-wing UAV hangar.

[0074] Preferably, the second driving element 426 is a servo motor. Using a servo motor as the second driving element 426 can improve the motion accuracy of the third slider 424 and the fourth slider 425.

[0075] Furthermore, the second centering component 42 also includes a third guide rail 428 and a fourth guide rail. Both the third and fourth guide rails are arranged parallel to the second direction on the landing pad 11. The third slider 424 slides in engagement with the third guide rail 428, and the fourth slider 425 slides in engagement with the fourth guide rail. This arrangement restricts the movement of the third slider 424 and the fourth slider 425 to only the second direction, thus preventing the UAV 100 from accurately centering in the second direction due to the misalignment of the third centering rod 421 and the fourth centering rod 422.

[0076] More specifically, such as Figure 7 As shown, the helipad 11 is provided with a first through groove 111 and a second through groove 112 extending along a first direction. A portion of the first centering rod 411 passes through the first through groove 111 and connects to the first slider 414, and a portion of the second centering rod 412 passes through the second through groove 112 and connects to the second slider 415. In this embodiment, the first centering rod 411 and the second centering rod 412 are disposed above the helipad 11, while the first transmission belt 413, the first slider 414, the second slider 415, the first driving member 416, the first transmission rod 4171, the first support 4172, the first guide rail 418, and the second guide rail are all disposed below the helipad 11. This arrangement can make reasonable use of the installation space, simplify the number of components on the upper surface of the helipad 11, and avoid interference.

[0077] Furthermore, the walls of both the first through groove 111 and the second through groove 112 are provided with a first dust-proof element 13. The first dust-proof element 13 can prevent sand and dust from entering the internal structure. For example, the first dust-proof element 13 can be a soft bristle strip.

[0078] Furthermore, the first centering component 41 also includes a dust cover 43. The dust cover 43 is installed on the first guide rail 418 and the second guide rail, and the dust cover 43 can protect the slider and guide rail from dust contamination, which could lead to blockage or other issues.

[0079] Similarly, the helipad 11 is provided with a third through groove 113 and a fourth through groove 114 extending along the second direction. A portion of the third centering rod 421 passes through the third through groove 113 and connects to the third slider 424, and a portion of the fourth centering rod 422 passes through the fourth through groove 114 and connects to the fourth slider 425. In this embodiment, the third centering rod 421 and the fourth centering rod 422 are disposed above the helipad 11, while the second transmission belt 423, the third slider 424, the fourth slider 425, the second drive member 426, the second transmission rod 4271, the second support, the third guide rail 428, and the fourth guide rail are all disposed below the helipad 11. This arrangement can make reasonable use of the installation space, simplify the number of components on the upper surface of the helipad 11, and avoid interference.

[0080] Furthermore, the walls of both the third channel 113 and the fourth channel 114 are provided with second dust-proof elements 14. The first dust-proof element 13 prevents sand and dust from entering the internal structure. For example, the first dust-proof element 13 may be a soft bristle strip.

[0081] Furthermore, the second centering component 42 also includes a dust cover 43. The dust cover 43 is installed on the third guide rail 428 and the fourth guide rail, and can protect the slider and guide rail from dust contamination and blockage.

[0082] It is understood that the centering mechanism 4 in this embodiment adopts a synchronous belt structure. In other embodiments, the centering mechanism 4 may also adopt a ball screw structure or a gear rack structure, etc., and there is no limitation here.

[0083] Optionally, the compound-wing UAV hangar also includes a charging mechanism 5. The charging mechanism 5 includes a charging component and a protective cover. The charging component is mounted on the support mechanism 1 and is used to charge the UAV 100. The protective cover covers the charging component. This configuration allows for the release and retrieval of the UAV 100 even in rainy weather, while also protecting the charging component in case of emergencies such as rain.

[0084] Optionally, such as Figure 10 As shown, the hangar for the compound-wing UAV also includes an environmental meteorological monitoring unit 6. Located outside the housing, the environmental meteorological monitoring unit 6 is used to monitor environmental and meteorological information outside the hangar.

[0085] Specifically, the environmental meteorological monitoring device 6 includes a wind speed detector 61, a rainfall detector 62, and a camera 63. For example, the wind speed detector 61 can be a wind speed sensor, the rainfall detector 62 can be a rainfall sensor, and the camera 63 is a waterproof camera. This composite-wing UAV hangar, by integrating wind speed and rainfall sensors and using an external waterproof camera 63, can achieve meteorological function monitoring and external situation observation.

[0086] 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 a compound-wing unmanned aerial vehicle (UAV), characterized in that, include: Support mechanism (1) for carrying and parking drone (100); The hatch assembly (2) includes a first hatch (21) and a second hatch (22). The first hatch (21) and the second hatch (22) are movably mounted on the support mechanism (1). The first hatch (21) and the second hatch (22) can approach and abut against each other in the horizontal direction and form a sealed receiving cavity with the support mechanism (1) to cover the drone (100). The first hatch (21) and the second hatch (22) are respectively provided with an outwardly protruding first receiving part (211) and a second receiving part (221). The first receiving part (211) and the second receiving part (221) are used to accommodate the wings of the drone (100). The first hatch (21) and the second hatch (22) can also move away from each other in the horizontal direction to completely expose the drone (100).

2. The composite-wing UAV hangar according to claim 1, characterized in that, The support mechanism (1) includes a landing pad (11) and a lifting assembly (12). The landing pad (11) is used to carry and park the UAV (100). The lifting assembly (12) can drive the landing pad (11) to switch between a first height and a second height in the vertical direction when the UAV (100) is fully exposed.

3. The composite-wing UAV hangar according to claim 1, characterized in that, The compound-wing UAV hangar also includes an opening and closing drive mechanism, which includes an opening and closing drive component (31) and a slide rail (32). The slide rail (32) is mounted on the support mechanism (1). The first hatch (21) and the second hatch (22) are respectively movably mounted on the slide rail (32). The output end of the opening and closing drive component (31) is connected to the first hatch (21) and the second hatch (22) respectively. The opening and closing drive component (31) can drive the first hatch (21) and the second hatch (22) to move closer to or further away from each other.

4. The composite-wing UAV hangar according to claim 1, characterized in that, The composite wing UAV hangar also includes a sealing element. The first door (21) is provided with a first sealing groove (212) on the side facing the second door (22), and the second door (22) is provided with a corresponding second sealing groove (222). When the first door (21) and the second door (22) approach and abut against each other, the sealing element is sandwiched between the bottom of the first sealing groove (212) and the bottom of the second sealing groove (222).

5. The composite-wing UAV hangar according to claim 1, characterized in that, Along the direction away from the second hatch (22), the height of the top surface of the first hatch (21) gradually decreases; Along the direction away from the first hatch (21), the height of the top surface of the second hatch (22) gradually decreases.

6. The composite-wing UAV hangar according to claim 1, characterized in that, The support structure (1) includes a helipad (11), on which the drone (100) is parked; The compound-wing UAV hangar also includes a centering mechanism (4), which is located on the parking apron (11) and is used to drive the UAV (100) to a designated position on the parking apron (11).

7. The composite-wing UAV hangar according to claim 6, characterized in that, The centering mechanism (4) includes a first centering component (41), which includes a first centering rod (411) and a second centering rod (412). The first centering rod (411) and the second centering rod (412) are respectively located on both sides of the helipad (11) and can move closer to or further away from each other along a first direction; and / or, The centering mechanism (4) further includes a second centering component (42), which includes a third centering rod (421) and a fourth centering rod (422). The third centering rod (421) and the fourth centering rod (422) are respectively located on both sides of the parking apron (11) and can move closer to or further away from each other along a second direction, which is perpendicular to the first direction.

8. The composite-wing UAV hangar according to claim 7, characterized in that, The first centering component (41) further includes a first transmission belt (413), a first slider (414), and a second slider (415). The first transmission belt (413) is arranged parallel to a first direction on the parking apron (11). The first transmission belt (413) has a first strip (4131) and a second strip (4132) connected end to end and moving in opposite directions. The first slider (414) is connected to the first strip (4131), and the second slider (415) is connected to the second strip (4132). When the first transmission belt (413) rotates, it can drive the first slider (414) and the second slider (415) to move closer to or further away from each other. The first centering rod (411) is connected to the first slider (414), and the second centering rod (412) is connected to the second slider (415); and / or, The second centering component (42) further includes a second transmission belt (423), a third slider (424), and a fourth slider (425). The second transmission belt (423) is arranged parallel to the second direction on the parking apron (11). The second transmission belt (423) has a third belt and a fourth belt that are connected end to end and move in opposite directions. The third slider (424) is connected to the third belt, and the fourth slider (425) is connected to the fourth belt. When the second transmission belt (423) rotates, it can drive the third slider (424) and the fourth slider (425) to move closer to or further away from each other. The third centering rod (421) is connected to the third slider (424), and the fourth centering rod (422) is connected to the fourth slider (425).

9. The composite-wing UAV hangar according to claim 1, characterized in that, The compound-wing UAV hangar also includes a charging mechanism (5), which includes a charging component and a protective cover. The charging component is disposed on the support mechanism (1) and is used to charge the UAV (100). The protective cover is disposed outside the charging component.

10. The composite-wing unmanned aerial vehicle hangar according to any one of claims 1-9, characterized in that, The composite wing UAV hangar also includes an environmental meteorological monitoring unit (6), which is located outside the housing cavity and is used to detect environmental and meteorological information outside the composite wing UAV hangar.

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