Unmanned aerial vehicle hangar

Abstract

The unmanned aerial vehicle hangar comprises a hangar body, a bearing part, a sealing part and a transmission structure, and the hangar body is provided with a containing cavity with an opening in one side; the bearing part is arranged in the containing cavity in a liftable mode, the sealing part is rotationally arranged on the garage body, and the sealing part is suitable for rotating relative to the garage body under the action of external force so as to seal or open the opening; the transmission structure comprises a swing part and a transmission assembly, part of the transmission assembly is arranged in the containing cavity, the other part of the transmission assembly is arranged outside the containing cavity, one end of the swing part rotationally abuts against the bearing part, the other end of the swing part is connected with part of the transmission assembly arranged in the containing cavity, and part of the transmission assembly arranged outside the containing cavity is connected with the sealing part; under the action of external force, the transmission assembly is suitable for driving the bearing piece to ascend or descend in the containing cavity through the swing piece and meanwhile driving the sealing piece to rotate relative to the garage body. The unmanned aerial vehicle hangar with the structure is beneficial to improving the take-off or landing efficiency of the unmanned aerial vehicle.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicles (UAVs), and in particular to an UAV hangar. Background Art

[0002] In recent years, with the rapid development of the Internet and the Internet of Things, drone products have been widely used in many fields in modern society, such as forestry, power grid, sea area, surveying and mapping and other related industries. Drones can complete reconnaissance, detection, inspection and other tasks. For example, they can be used in scenarios where no one has visited for a long time but drone operations are needed, and can monitor and inspect fixed areas.

[0003] In the prior art, when a drone completes a task such as reconnaissance, detection or inspection, a drone hangar is needed to store the drone to ensure that the drone will not be damaged by the outside world, and the drone can monitor and inspect the surrounding area with the hangar as the center. At the same time, the hangar can realize the fully automatic take-off and landing of the drone, as well as charging, battery replacement, and load-bearing. However, in the existing drone hangar, when the drone takes off or lands, the hangar needs to open the door first, and then extend the carrying platform inside the hangar outside the hangar, so that the drone can take off from the carrying platform or land on the carrying platform, which results in low efficiency of drone take-off or landing. Summary of the invention

[0004] Therefore, the technical problem to be solved by the present invention is to overcome the defect that the existing UAV hangar needs to open the door first and then extend the carrying platform inside the hangar outside the hangar in order to allow the UAV to take off or land, resulting in low efficiency of UAV take-off or landing.

[0005] To this end, the present invention provides a drone hangar, comprising:

[0006] A storage body, wherein the storage body has a receiving cavity with an opening on one side;

[0007] A bearing member and a closing member, wherein the bearing member is movably arranged in the accommodating cavity, the closing member is rotatably arranged on the library body, and the closing member is suitable for rotating relative to the library body under the action of an external force to close or open the opening;

[0008] The transmission structure comprises a swinging member and a transmission assembly, wherein a part of the transmission assembly is arranged in the accommodating cavity, and another part of the transmission assembly is arranged outside the accommodating cavity, one end of the swinging member is rotatably abutted against the bearing member, and the other end is connected to the part of the transmission assembly arranged in the accommodating cavity, and the part of the transmission assembly arranged outside the accommodating cavity is connected to the closing member;

[0009] Under the action of external force, the transmission assembly is suitable for driving the supporting member to rise or fall in the accommodating cavity through the swinging member, and at the same time driving the closing member to rotate relative to the library body, so that when the supporting member approaches the opening, the closing member synchronously opens the opening, or when the supporting member moves away from the opening, the closing member synchronously closes the opening.

[0010] Optionally, in the above-mentioned drone hangar, the transmission assembly includes:

[0011] a first gear connected to an end of the swinging member away from the bearing member;

[0012] a second gear connected to one end of the closure member;

[0013] A transmission member is movably arranged inside and outside the accommodating cavity, and the transmission member is meshingly connected with the first gear and the second gear, so that under the action of an external force, the first gear rotates and drives the transmission member to move, and the transmission member drives the second gear to rotate synchronously.

[0014] Optionally, in the above-mentioned drone hangar, a through portion is opened on the hangar body, and one end of the transmission member is suitable for passing through the through portion, so that part of the transmission member is arranged in the accommodating cavity, and the other part of the transmission member is arranged outside the accommodating cavity.

[0015] Optionally, the above-mentioned drone hangar further includes a driving assembly, which is arranged in the accommodating cavity and on the inner wall of the hangar body, and the driving end of the driving assembly is connected to the first gear to drive the first gear to rotate.

[0016] Optionally, in the above-mentioned drone hangar, the driving assembly includes a driving member, the driving member is arranged on the inner wall of the hangar body, and the driving end of the driving member is connected to the first gear to drive the first gear to rotate.

[0017] Optionally, in the above-mentioned drone hangar, the driving assembly further includes a reduction member, the reduction member is connected to the driving end of the driving member, and the driving end of the reduction member is connected to the first gear to drive the first gear to rotate.

[0018] Optionally, in the above-mentioned drone hangar, guide parts are provided on two opposite inner side walls of the hangar body;

[0019] The transmission assembly further comprises a guide member, the guide member is connected to an end of the swing member away from the first gear, and both ends of the guide member are respectively slidably connected to one of the guide parts;

[0020] When the swinging member rotates, the guide member is adapted to slide along an extending direction of the guide portion so as to guide the swinging member through the guide portion.

[0021] Optionally, the above-mentioned drone hangar further includes a heat sink, part of which is arranged in the accommodating cavity, and another part of which is arranged outside the accommodating cavity, and the heat sink is suitable for dissipating the heat in the accommodating cavity.

[0022] Optionally, the above-mentioned drone hangar further includes an antenna component, which is arranged on the closing component and is suitable for sending a positioning signal.

[0023] Optionally, the above-mentioned drone hangar further includes a plurality of support members, one end of any of the support members is connected to the hangar body, and the other end is suitable for being set on the ground, so as to set the hangar body on the ground.

[0024] The technical solution provided by the present invention has the following advantages:

[0025] 1. The drone hangar provided by the present invention is provided with a bearing member, a closing member and a transmission structure on a hangar body, wherein the hangar body has a receiving cavity with an opening on one side, and the bearing member is arranged in a liftable manner in the receiving cavity, so that the bearing member can be lifted out of the receiving cavity or lowered into the receiving cavity through the opening, and then the bearing member can synchronously lift out of or lower into the receiving cavity with the drone thereon, and ensure the normal take-off and landing of the drone, and when the drone takes off from the bearing member or lands on the bearing member, since the bearing member is lifted out of the receiving cavity through the opening, there are no obstacles around the drone when it takes off or lands, which is conducive to lifting. In order to improve the safety of taking off or landing of the drone, the closing piece is specifically rotatably arranged on the library body, so that under the action of external force, the closing piece can rotate relative to the library body, thereby enabling the closing piece to open or close the opening, so that when the drone needs to take off or land, the closing piece can open the opening to allow the carrier to rise out of the accommodating cavity, and when the drone takes off or lands on the carrier, and the carrier brings the drone into the accommodating cavity, the closing piece can close the opening, thereby ensuring the isolation of the accommodating cavity from the outside world, and thus being beneficial to protecting the components and the drone in the accommodating cavity. The transmission structure specifically includes a swinging piece and a transmission assembly, wherein a part of the transmission assembly is arranged The closure member is arranged in the accommodating cavity, and the other part of the transmission component is arranged outside the accommodating cavity. One end of the swinging member is rotatably abutted against the bearing member, and the other end is connected to the part of the transmission component arranged in the accommodating cavity. The transmission component arranged outside the accommodating cavity is connected to the closing member. Therefore, under the action of external force, the swinging member can rotate, and when the swinging member rotates, the swinging member can drive the bearing member to rise and fall in the accommodating cavity, and can also drive the transmission component to move relative to the library body, so that the transmission component can drive the closing member to rotate relative to the library body, so that the closing member opens or closes the opening. Therefore, by rotating the swinging member, the swinging member can drive the bearing member to rise and fall and drive the closing member to move relative to the library body. The library body is rotated, so that when the carrier rises in the accommodating chamber, the closing member can rotate relative to the library body and open the opening, so that when the carrier rises to the opening, the closing member can completely open the opening, so that the carrier can immediately rise out of the accommodating chamber through the opening, and enable the drone on the carrier to take off or receive a drone that is ready to land, and when the carrier descends in the accommodating chamber, the closing member can rotate relative to the library body and close the opening, so that when the carrier descends into the accommodating chamber, the closing member can completely close the opening. This is beneficial to improving the efficiency of take-off or landing of the drone, and enables the drone to work quickly or obtain power quickly. BRIEF DESCRIPTION OF THE DRAWINGS

[0026] In order to more clearly illustrate the specific implementation methods of the present invention or the technical solutions in the prior art, the drawings required for use in the specific implementation methods or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are some implementation methods of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0027] Figure 1 A closed schematic diagram of a drone hangar provided in an embodiment of the present invention;

[0028] Figure 2 A schematic diagram of opening a drone hangar provided in an embodiment of the present invention;

[0029] Figure 3 A diagram of the opening process of a drone hangar provided in an embodiment of the present invention;

[0030] Figure 4 A fully opened diagram of a drone hangar provided in an embodiment of the present invention;

[0031] Description of reference numerals:

[0032] 1- storage body; 11- guide part;

[0033] 2-carrying member; 3-closing member;

[0034] 4-transmission structure; 41-swinging member; 42-transmission assembly; 421-first gear; 422-second gear; 423-transmission member; 424-guide member;

[0035] 5-driving assembly; 6-heat sink; 7-antenna component; 8-support component. DETAILED DESCRIPTION

[0036] The technical solution of the present invention will be described clearly and completely below in conjunction with the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0037] In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc., indicating the orientation or positional relationship, are based on the orientation or positional relationship shown in the drawings, and are only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as limiting the present invention. In addition, the terms "first" and "second" are used for descriptive purposes only and cannot be understood as indicating or implying relative importance.

[0038] In the description of the present invention, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "connected", and "connected" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be indirectly connected through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.

[0039] In addition, the technical features involved in the different embodiments of the present invention described below can be combined with each other as long as they do not conflict with each other.

[0040] Example

[0041] This embodiment provides a drone hangar, such as Figures 1 to 4 As shown, it includes a library body 1, a supporting member 2, a closing member 3 and a transmission structure 4, the library body 1 has a accommodating cavity with an opening on one side; the supporting member 2 is arranged in the accommodating cavity in a liftable manner, and the closing member 3 is rotatably arranged on the library body 1, and the closing member 3 is suitable for rotating relative to the library body 1 under the action of an external force to close or open the opening; the transmission structure 4 includes a swinging member 41 and a transmission assembly 42, part of the transmission assembly 42 is arranged in the accommodating cavity, and the other part of the transmission assembly 42 is arranged outside the accommodating cavity, one end of the swinging member 41 is rotatably abutted against the supporting member 2, and the other end is connected to the part of the transmission assembly 42 arranged in the accommodating cavity, and the part of the transmission assembly 42 arranged outside the accommodating cavity is connected to the closing member 3; under the action of an external force, the transmission assembly 42 is suitable for driving the supporting member 2 to rise or fall in the accommodating cavity through the swinging member 41, and at the same time drives the closing member 3 to rotate relative to the library body 1, so that when the supporting member 2 is close to the opening, the closing member 3 synchronously opens the opening, or when the supporting member 2 is far away from the opening, the closing member 3 synchronously closes the opening.

[0042] The drone hangar of the above structure is provided with a supporting member 2, a closing member 3 and a transmission structure 4 on the hangar body 1. The supporting member 2 and the closing member 3 are respectively a supporting plate and a closing plate in the present embodiment, wherein the hangar body 1 has a accommodating cavity with an opening on one side, and the supporting member 2 is arranged in a liftable manner in the accommodating cavity, so that the supporting member 2 can be raised out of the accommodating cavity or lowered into the accommodating cavity through the opening, thereby enabling the supporting member 2 to synchronously raise out of or lower into the accommodating cavity with the drone thereon, and ensuring the normal take-off and landing of the drone, and when the drone takes off from the supporting member 2 or lands on the supporting member 2, since the supporting member 2 is raised out of the accommodating cavity through the opening, there are no obstacles around the drone when it takes off or lands, which is beneficial to improving the safety of the drone's take-off or landing.

[0043] The closure 3 is specifically rotatably arranged on the library body 1, so that under the action of external force, the closure 3 can rotate relative to the library body 1, so that the closure 3 can open or close the opening, so that when the UAV needs to take off or land, the closure 3 can open the opening to allow the carrier 2 to rise out of the accommodating cavity, and when the UAV takes off or lands on the carrier 2, and the carrier 2 brings the UAV into the accommodating cavity, the closure 3 can close the opening, thereby ensuring the isolation of the accommodating cavity from the outside world, which is beneficial to protecting the components and the UAV in the accommodating cavity.

[0044] The transmission structure 4 specifically includes a swinging member 41 and a transmission assembly 42. The swinging member 41 is a swinging rod in the present embodiment, wherein part of the transmission assembly 42 is arranged in the accommodating cavity, and the other part of the transmission assembly 42 is arranged outside the accommodating cavity. One end of the swinging member 41 is rotatably abutted against the supporting member 2, and the other end is connected to the part of the transmission assembly 42 arranged in the accommodating cavity, and the transmission assembly 42 arranged outside the accommodating cavity is connected to the closing member 3, so that when an external force is applied, the swinging member 41 can rotate, and when the swinging member 41 rotates, the swinging member 41 can drive the supporting member 2 to rise and fall in the accommodating cavity, and can also drive the transmission assembly 42 to move relative to the library body 1, so that the transmission assembly 42 can drive the closing member 3 to rotate relative to the library body 1, so that the closing member 3 opens or closes the opening.

[0045] Therefore, by rotating the swing member 41, the swing member 41 can drive the supporting member 2 to rise and fall and drive the closing member 3 to rotate relative to the library body 1, so that when the supporting member 2 rises in the accommodating chamber, the closing member 3 can rotate relative to the library body 1 and open the opening, so that when the supporting member 2 rises to the opening, the closing member 3 can completely open the opening, so that the supporting member 2 can immediately rise out of the accommodating chamber through the opening, and enable the drone on the supporting member 2 to take off or receive the drone that is ready to land, and when the supporting member 2 descends in the accommodating chamber, the closing member 3 can rotate relative to the library body 1 and close the opening, so that when the supporting member 2 descends to the accommodating chamber, the closing member 3 can completely close the opening, which is beneficial to improving the efficiency of the drone's take-off or landing, and enables the drone to work quickly or quickly obtain power endurance.

[0046] In other optional embodiments, guide rails may be provided on the inner side walls of the library body 1, and the side walls of the carrier 2 may be connected to the guide rails, so that when the carrier 2 is lifted or lowered in the accommodating cavity, the guide rails can guide the lifting trajectory of the carrier 2 to ensure the stability of the lifting of the carrier 2.

[0047] The drone hangar provided in this embodiment is as follows: Figure 1 and Figure 2 As shown, the transmission assembly 42 includes a first gear 421, a second gear 422 and a transmission member 423. The first gear 421 is connected to one end of the swing member 41 away from the carrier 2; the second gear 422 is connected to one end of the closing member 3; the transmission member 423 is movably arranged inside and outside the accommodating cavity, and the transmission member 423 is meshedly connected with the first gear 421 and the second gear 422, so that under the action of external force, the first gear 421 rotates and drives the transmission member 423 to move, and the transmission member 423 drives the second gear 422 to rotate synchronously.

[0048] The drone hangar of the above structure is provided with a transmission assembly 42 including a first gear 421, a second gear 422 and a transmission member 423. The transmission member 423 is a transmission rod in the present embodiment, wherein the first gear 421 is connected to the end of the swinging member 41 away from the supporting member 2, the second gear 422 is connected to one end of the closing member 3, and the transmission member 423 is movably arranged inside and outside the accommodating cavity, and the transmission member 423 is also meshed and connected with the first gear 421 and the second gear 422 respectively, so that under the action of external force, the first gear 421 can rotate and drive the swinging member 41 to rotate, so that the swinging member 41 can drive the supporting member 2 to rise and fall in the accommodating cavity, and at the same time, the first gear 421 can also drive the transmission member 423 to move in the accommodating cavity, so that the transmission member 423 can drive the second gear 422 to rotate synchronously, and drive the closing member 3 to rotate relative to the library body 1 through the second gear 422, so that the closing member 3 can open or close the opening.

[0049] The drone hangar provided in this embodiment is as follows: Figures 1 to 4 As shown, a through portion is opened on the library body 1, and one end of the transmission member 423 is suitable for passing through the through portion, so that part of the transmission member 423 is arranged in the accommodating cavity, and the other part of the transmission member 423 is arranged outside the accommodating cavity.

[0050] The drone hangar of the above-mentioned structure has a through portion opened on the hangar body 1. The through portion is a through hole in this embodiment. One end of the transmission member 423 can pass through the through portion, so that part of the transmission member 423 is arranged in the accommodating cavity and the other part of the transmission member 423 is arranged outside the accommodating cavity. At the same time, the part of the transmission member 423 arranged in the accommodating cavity can be meshed and connected with the first gear 421, and the part of the transmission member 423 arranged outside the accommodating cavity can be meshed and connected with the second gear 422.

[0051] The drone hangar provided in this embodiment is as follows: Figures 1 to 4 As shown, it also includes a driving component 5, which is arranged in the accommodating cavity and on the inner wall of the library body 1. The driving end of the driving component 5 is connected to the first gear 421 to drive the first gear 421 to rotate.

[0052] The drone hangar of the above-mentioned structure is provided with a driving component 5 in the accommodating cavity, and the driving component 5 is specifically provided on the inner wall of the hangar body 1, so that the driving component 5 can be provided in the accommodating cavity, and the driving end of the driving component 5 is connected to the first gear 421, so that the driving component 5 can drive the first gear 421 to rotate, and drive the supporting member 2 to rise and fall in the accommodating cavity and drive the closing member 3 to rotate relative to the hangar body 1 through the first gear 421.

[0053] The drone hangar provided in this embodiment is as follows: Figures 1 to 4 As shown, the driving assembly 5 includes a driving member, which is arranged on the inner wall of the library body 1, and the driving end of the driving member is connected to the first gear 421 to drive the first gear 421 to rotate.

[0054] The drone hangar of the above structure includes a driving member by setting a driving component 5. The driving member in this embodiment is a driving motor. The driving member is specifically arranged on the inner wall of the hangar body 1, and the driving end of the driving member is connected to the first gear 421, so that the driving member can drive the first gear 421 to rotate.

[0055] The drone hangar provided in this embodiment is as follows: Figures 1 to 4 As shown, the driving assembly 5 further includes a reduction member, which is connected to the driving end of the driving member, and the driving end of the reduction member is connected to the first gear 421 to drive the first gear 421 to rotate.

[0056] The drone hangar of the above-mentioned structure also includes a reduction member by setting a driving component 5. The reduction member in this embodiment is a reducer, which is specifically connected to the driving end of the driving member, and the driving end of the reduction member is connected to the first gear 421, so that under the drive of the driving member, the reduction member can drive the first gear 421 to rotate, and by setting the reduction member between the driving member and the first gear 421, when the driving member drives the first gear 421 to rotate through the reduction member, the rotation of the first gear 421 can be more stable, so that the lifting and lowering of the carrier 2 and the rotation of the closing member 3 can be more stable.

[0057] The drone hangar provided in this embodiment is as follows: Figures 1 to 4 As shown, guide portions 11 are provided on two opposite inner walls of the storage body 1; the transmission assembly 42 also includes a guide member 424, which is connected to an end of the swing member 41 away from the first gear 421, and the two ends of the guide member 424 are respectively slidably connected to a guide portion 11; when the swing member 41 rotates, the guide member 424 is suitable for sliding along the extension direction of the guide portion 11 to guide the swing member 41 through the guide portion 11.

[0058] The drone hangar of the above-mentioned structure also includes a guide member 424 through the guide part 11 opened on the two inner walls opposite to each other in the hangar body 1 and the transmission assembly 42. The guide part 11 is a guide groove in the present embodiment, and the guide member 424 is a guide rod in the present embodiment. The guide member 424 is specifically connected to the end of the swing member 41 away from the first gear 421, and after the guide member 424 is connected to the swing member 41, the two ends of the guide member 424 are respectively slidably connected to a guide part 11, so that when the swing member 41 rotates, the guide member 424 can rotate synchronously with the swing member 41, and when the guide member 424 rotates, it can slide along the extension direction of the guide part 11, so that the guide member 424 can guide the rotation of the swing member 41, so that the rotation trajectory of the swing member 41 is always consistent, which is beneficial to improve the lifting stability of the carrier 2.

[0059] The drone hangar provided in this embodiment is as follows: Figure 1 As shown, a heat sink 6 is also included, part of the heat sink 6 is arranged in the accommodating cavity, and another part of the heat sink 6 is arranged outside the accommodating cavity. The heat sink 6 is suitable for dissipating the heat in the accommodating cavity.

[0060] The drone hangar of the above-mentioned structure has a heat sink 6 arranged on the hangar body 1. The heat sink 6 is an air conditioner in this embodiment. Specifically, the heat sink 6 is partially arranged in the accommodating cavity, and the other part is arranged outside the accommodating cavity. Therefore, when the drone is charging in the accommodating cavity, the heat sink 6 can dissipate the heat generated by the charging of the drone to the outside, thereby ensuring that the drone can be charged normally and also ensuring the normal operation of other components in the accommodating cavity.

[0061] The drone hangar provided in this embodiment is as follows: Figure 1 As shown, it also includes an antenna component 7, which is arranged on the closing component 3 and is suitable for sending a positioning signal.

[0062] The drone hangar of the above-mentioned structure is equipped with an antenna component 7 on the closing component 3. The antenna component 7 is an antenna in this embodiment. The antenna component 7 is specifically arranged on the closing component 3. The antenna component 7 can emit a positioning signal, so that the drone preparing to land can receive the positioning signal and fly to the position of the hangar body 1, thereby enabling the drone to land on the supporting component 2 on the hangar body 1 through the positioning signal and be driven by the supporting component 2 to be stored in the accommodating cavity.

[0063] The drone hangar provided in this embodiment is as follows: Figure 1 As shown, a plurality of support members 8 are also included, one end of any support member 8 is connected to the library body 1, and the other end is suitable for being set on the ground, so as to set the library body 1 on the ground.

[0064] The drone hangar of the above-mentioned structure is connected to the hangar body 1 through a plurality of support members 8. The support members 8 in this embodiment are brackets, one end of each bracket is connected to the hangar body 1, and the other end can be set on the ground, so that the hangar body 1 is set on the ground through all the support members 8, thereby allowing the hangar body 1 to adapt to different terrains.

[0065] The drone hangar provided by the present invention rotates the swinging member 41 so that the swinging member 41 can drive the supporting member 2 to rise and fall and drive the closing member 3 to rotate relative to the hangar body 1, so that when the supporting member 2 rises in the accommodating chamber, the closing member 3 can rotate relative to the hangar body 1 and open the opening, so that when the supporting member 2 rises to the opening, the closing member 3 can completely open the opening, so that the supporting member 2 can immediately rise out of the accommodating chamber through the opening, and enable the drone on the supporting member 2 to take off or receive the drone that is ready to land, and when the supporting member 2 descends in the accommodating chamber, the closing member 3 can rotate relative to the hangar body 1 and close the opening, so that when the supporting member 2 descends into the accommodating chamber, the closing member 3 can completely close the opening, which is beneficial to improving the efficiency of the drone's take-off or landing, and enables the drone to work quickly or obtain power quickly.

[0066] Obviously, the above embodiments are merely examples for the purpose of clear explanation, and are not intended to limit the implementation methods. For those skilled in the art, other different forms of changes or modifications can be made based on the above description. It is not necessary and impossible to list all the implementation methods here. The obvious changes or modifications derived therefrom are still within the scope of protection of the invention.

Claims

1. A drone hangar, characterized in that: include: A storage body (1), wherein the storage body (1) has a receiving cavity with an opening on one side; A carrier (2) and a closing member (3), wherein the carrier (2) is arranged in the accommodating cavity in a liftable manner, and the closing member (3) is rotatably arranged on the storage body (1), and the closing member (3) is suitable for rotating relative to the storage body (1) under the action of an external force to close or open the opening; The transmission structure (4) comprises a swinging member (41) and a transmission assembly (42), wherein a portion of the transmission assembly (42) is arranged in the accommodating cavity, and another portion of the transmission assembly (42) is arranged outside the accommodating cavity; one end of the swinging member (41) is rotatably abutted against the bearing member (2), and the other end is connected to the portion of the transmission assembly (42) arranged in the accommodating cavity, and the portion of the transmission assembly (42) arranged outside the accommodating cavity is connected to the closing member (3); Under the action of external force, the transmission assembly (42) is suitable for driving the supporting member (2) to rise or fall in the accommodating chamber through the swinging member (41), and at the same time driving the closing member (3) to rotate relative to the library body (1), so that when the supporting member (2) approaches the opening, the closing member (3) synchronously opens the opening, or when the supporting member (2) moves away from the opening, the closing member (3) synchronously closes the opening.

2. The drone hangar according to claim 1, characterized in that: The transmission assembly (42) comprises: A first gear (421), the first gear (421) being connected to an end of the swinging member (41) away from the bearing member (2); a second gear (422), the second gear (422) being connected to one end of the closing member (3); A transmission member (423), the transmission member (423) is movably arranged inside and outside the accommodating cavity, and the transmission member (423) is meshingly connected with the first gear (421) and the second gear (422), so that under the action of an external force, the first gear (421) rotates and drives the transmission member (423) to move, and the transmission member (423) drives the second gear (422) to rotate synchronously.

3. The drone hangar according to claim 2, characterized in that: The library body (1) is provided with a through portion, and one end of the transmission member (423) is suitable for passing through the through portion, so that part of the transmission member (423) is arranged in the accommodating cavity, and the other part of the transmission member (423) is arranged outside the accommodating cavity.

4. The drone hangar according to claim 3, characterized in that: It also includes a driving component (5), which is arranged in the accommodating cavity and on the inner wall of the library body (1), and the driving end of the driving component (5) is connected to the first gear (421) to drive the first gear (421) to rotate.

5. The drone hangar according to claim 4, characterized in that: The driving assembly (5) comprises a driving member, which is arranged on the inner side wall of the storage body (1), and the driving end of the driving member is connected to the first gear (421) to drive the first gear (421) to rotate.

6. The drone hangar according to claim 5, characterized in that: The driving assembly (5) further comprises a reduction member, wherein the reduction member is connected to a driving end of the driving member, and the driving end of the reduction member is connected to the first gear (421) to drive the first gear (421) to rotate.

7. The drone hangar according to any one of claims 2-6, characterized in that: The two opposite inner side walls of the storage body (1) are both provided with guide parts (11); The transmission assembly (42) further comprises a guide member (424), wherein the guide member (424) is connected to an end of the swing member (41) away from the first gear (421), and both ends of the guide member (424) are respectively slidably connected to one of the guide portions (11); When the swinging member (41) rotates, the guide member (424) is adapted to slide along the extension direction of the guide portion (11) so as to guide the swinging member (41) through the guide portion (11).

8. The drone hangar according to claim 7, characterized in that: It also comprises a heat sink (6), part of which is arranged in the accommodating cavity, and another part of which is arranged outside the accommodating cavity, and the heat sink (6) is suitable for dissipating heat in the accommodating cavity.

9. The drone hangar according to claim 8, characterized in that: It also comprises an antenna component (7), wherein the antenna component (7) is arranged on the closing component (3), and the antenna component (7) is suitable for sending a positioning signal.

10. The drone hangar according to claim 1, characterized in that: It also comprises a plurality of support members (8), one end of any of the support members (8) is connected to the library body (1), and the other end is suitable for being arranged on the ground, so as to arrange the library body (1) on the ground.

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