Unmanned aerial vehicle garage equipment

Abstract

The invention discloses unmanned aerial vehicle garage equipment which comprises a plurality of garage bodies and a heat dissipation structure, all the garage bodies are arranged at intervals, any garage body is provided with a containing cavity and a mounting cavity which are arranged at intervals, and the containing cavity is suitable for containing an unmanned aerial vehicle; the heat dissipation structure comprises a heat dissipation piece and a plurality of communicating assemblies, the heat dissipation piece is arranged on one side of the warehouse body, any communicating assembly is arranged in the corresponding mounting cavity, and any communicating assembly is provided with an air supply channel and an air outlet channel which communicate with the corresponding containing cavity; the air supply channels and the air outlet channels of all the communicating assemblies are arranged in a communicating mode, and the air supply channel and the air outlet channel of at least one communicating assembly are communicated with the heat dissipation piece, so that the heat dissipation piece sends cold air into the containing cavities of all the warehouse bodies through all the air supply channels. And hot air in the containing cavities of all the warehouse bodies is pumped out to the outside through all the air outlet channels. The unmanned aerial vehicle garage equipment with the structure is beneficial to improving the maintenance efficiency of the unmanned aerial vehicle garage.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicles, and in particular to unmanned aerial vehicle hangar equipment. 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. When the drone completes the task and returns to the drone hangar, the drone will generate heat during operation, so when it returns to the drone hangar, it will bring the heat back to the hangar. At the same time, the drone will also generate heat when charging in the hangar. The heat accumulated in the hangar will affect the charging efficiency of the drone. Therefore, a heat dissipation module needs to be set in the drone hangar to dissipate the heat in the hangar to the outside world.

[0004] However, existing drone hangars are all equipped with heat dissipation modules, and when encountering a site where multiple drones are required to operate, multiple drone hangars are required to accommodate these drones, which requires maintenance of all drone hangars, resulting in low maintenance efficiency. Summary of the invention

[0005] Therefore, the technical problem to be solved by the present invention is to overcome the defect that when multiple drone hangars are used to store drones, all drone hangars need to be maintained, resulting in low maintenance efficiency.

[0006] To this end, the present invention provides an unmanned aerial vehicle hangar device, comprising:

[0007] A plurality of storage bodies, all of which are arranged at intervals, and any of which has a receiving cavity and an installation cavity arranged at intervals, wherein the receiving cavity is suitable for storing a drone;

[0008] The heat dissipation structure comprises a heat dissipation element and a plurality of connecting components, wherein the heat dissipation element is arranged on one side of the storage body, any of the connecting components is arranged in one of the installation chambers, and any of the connecting components has an air supply channel and an air outlet channel connected to the accommodating chamber;

[0009] Among them, the air supply channels and the air outlet channels of all the connected components are connected, and the air supply channel and the air outlet channel of at least one of the connected components are connected to the heat sink, so that the heat sink can send cold air into the accommodating cavities of all the storage bodies through all the air supply channels, and draw hot air in the accommodating cavities of all the storage bodies to the outside through all the air outlet channels.

[0010] Optionally, in the above-mentioned unmanned aerial vehicle hangar equipment, all of the hangar bodies include a first body and a plurality of second bodies, the heat sink is arranged on one side of the first body, all of the second bodies are arranged in sequence at intervals, and at least one of the second bodies is arranged on the side of the first body away from the heat sink, and all of the connecting components are arranged in series.

[0011] Optionally, in the above-mentioned unmanned aerial hangar equipment, any of the air supply channels has a first interface, a second interface and a third interface, the first interface is suitable for communicating with the heat sink or the second interface of the adjacent air supply channel, the second interface is suitable for communicating with the heat sink or the first interface of the adjacent air supply channel, and the third interface is suitable for connecting with the accommodating cavity to connect the air supply channel and the accommodating cavity.

[0012] Optionally, in the above-mentioned unmanned aerial hangar equipment, any of the air outlet channels has a fourth interface, a fifth interface and a sixth interface, the fourth interface is suitable for communicating with the fifth interface of the heat sink or the adjacent air supply channel, the fifth interface is suitable for communicating with the fourth interface of the heat sink or the adjacent air supply channel, and the sixth interface is suitable for connecting with the accommodating cavity to connect the air outlet channel and the accommodating cavity.

[0013] Optionally, in the above-mentioned unmanned aerial vehicle hangar equipment, in the second body at the end, the first interface or the second interface of the air supply channel of the connecting component is in a blocked state, and the fourth interface or the fifth interface of the air outlet channel of the connecting component is in a blocked state.

[0014] Optionally, in the above-mentioned unmanned aerial vehicle hangar equipment, all of the hangar bodies include a first body and a plurality of second bodies, the heat sink is arranged on one side of the first body, all of the second body arrays are arranged on the surrounding side of the first body, and all of the connecting components in the second bodies are arranged in parallel with the connecting components in the first body.

[0015] Optionally, in the above-mentioned unmanned aerial vehicle hangar equipment, any one of the air supply channels has a seventh interface and several eighth interfaces, the seventh interface is connected to the accommodating cavity, one of the eighth interfaces of the air supply channel in the first body is connected to the heat sink, and all of the eighth interfaces are connected to an eighth interface of the adjacent air supply channel.

[0016] Optionally, in the above-mentioned unmanned aerial vehicle hangar equipment, any one of the air outlet channels has a ninth interface and several tenth interfaces, the ninth interface is connected to the accommodating cavity, one of the tenth interfaces of the air outlet channels in the first body is connected to the heat sink, and all of the tenth interfaces are connected to a tenth interface of an adjacent air outlet channel.

[0017] Optionally, in the above-mentioned unmanned aerial vehicle hangar equipment, in each of the second bodies at the end, at least one of the eighth interfaces of the air supply channel of the connecting component is in a blocked state, and at least one of the tenth interfaces of the air outlet channel of the connecting component is in a blocked state.

[0018] Optionally, in the above-mentioned unmanned aerial vehicle hangar equipment, the connecting component includes an air supply piece and an air outlet piece, the air supply channel is opened on the air supply piece, the air outlet channel is opened on the air outlet piece, and each of the interfaces is a port on the air supply piece and the air outlet piece.

[0019] The technical solution provided by the present invention has the following advantages:

[0020] 1. The drone hangar equipment provided by the present invention has a heat dissipation structure arranged on a hangar body, wherein a plurality of hangar bodies are arranged at intervals, and each hangar body has a storage cavity and an installation cavity arranged at intervals, and the storage cavity can be used to store the drone, thereby protecting the drone through the hangar body; the heat dissipation structure specifically includes a heat sink and a plurality of connecting components, wherein the heat sink is arranged on one side of one of the hangar bodies and is connected to the hangar body, and each connecting component is arranged in the installation cavity of a hangar body, and at the same time, each connecting component has an air supply channel and an air outlet channel connected to the storage cavity, and the air supply channels of all the connecting components are connected to each other, and the air outlet channels are connected to each other, so that all the storage cavities of the hangar bodies are connected together through the air supply channel and the air outlet channel, and in addition, the air supply channel and the air outlet channel of one of the connecting components are connected to the heat sink, so that the heat sink can send cold air into the storage cavities of all hangar bodies through the air supply channels of all the connecting components, so that the cold air can cool the air in the storage cavity, and the air cooled in the storage cavity is cooled by the cold air. The air is used to cool the drone that has completed the operation and is charging in the storage chamber to ensure that the charging efficiency of the drone will not be affected by the heat generated during the operation and charging of the drone, and it is beneficial to improve the charging efficiency of the drone. While the heat sink delivers cold air to the storage chamber through all the air supply channels, the heat sink can also extract the hot air in the storage chamber to the outside through the air outlet channels of all the connected components. The hot air is specifically the heat generated when the drone is operating, the heat generated when the drone is charging, and the heat neutralized with the cold air, so that the cooling efficiency of the air in the storage chamber can be effectively guaranteed, and the circulation of the air in the storage chamber can be realized; in summary, the storage chambers of multiple library bodies are connected together through the air supply channels and air outlet channels of multiple connected components, and the air in the storage chambers of all library bodies is cooled by a heat sink, so that there is no need to install a heat sink on each library body, thereby effectively avoiding waste of resources. At the same time, when the heat sink fails, only the library body installed with the heat sink needs to be repaired, and there will be no failure of the heat sinks in multiple library bodies, which is beneficial to improving the maintenance efficiency of the drone hangar. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] 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.

[0022] Figure 1It is a plan schematic diagram of the drone hangar equipment provided in an embodiment of the present invention;

[0023] Figure 2 It is a structural schematic diagram of the drone hangar equipment provided in an embodiment of the present invention;

[0024] Description of reference numerals:

[0025] 1-First body; 2-Second body;

[0026] 3-heat dissipation structure; 31-heat dissipation component; 32-connecting component; 321-air supply component; 322-air outlet component. DETAILED DESCRIPTION

[0027] 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.

[0028] 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.

[0029] 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.

[0030] 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.

[0031] Example

[0032] This embodiment provides a drone hangar device, such as Figure 1 and Figure 2As shown, it includes a plurality of library bodies and a heat dissipation structure 3, all of the library bodies are arranged at intervals, and any of the library bodies has a storage cavity and an installation cavity arranged at intervals, and the storage cavity is suitable for storing a drone; the heat dissipation structure 3 includes a heat sink 31 and a plurality of connecting components 32, the heat sink 31 is arranged on one side of a library body, any of the connecting components 32 is arranged in an installation cavity, and any of the connecting components 32 has an air supply channel and an air outlet channel connected to the storage cavity; wherein the air supply channels and air outlet channels of all the connecting components 32 are connected, and the air supply channel and air outlet channel of at least one connecting component 32 are connected with the heat sink 31, so that the heat sink 31 sends cold air into the storage cavities of all the library bodies through all the air supply channels, and extracts the hot air in the storage cavities of all the library bodies to the outside through all the air outlet channels.

[0033] The drone hangar device of the above structure is provided with a heat dissipation structure 3 on the hangar body, wherein a plurality of hangar bodies are provided and all hangar bodies are spaced apart from each other. At the same time, each hangar body has a storage cavity and an installation cavity spaced apart from each other, and the storage cavity can be used to store the drone, thereby protecting the drone through the hangar body.

[0034] The heat dissipation structure 3 specifically includes a heat sink 31 and a plurality of connecting components 32. The heat sink 31 is an air conditioner in this embodiment, wherein the heat sink 31 is arranged on one side of one of the library bodies and is connected to the library body, and each connecting component 32 is arranged in an installation cavity of a library body. At the same time, each connecting component 32 has an air supply channel and an air outlet channel connected to the accommodating cavity, and the air supply channels of all the connecting components 32 are interconnected, and the air outlet channels are interconnected, so that all the accommodating cavities of the library bodies are connected together through the air supply channel and the air outlet channel.

[0035] In addition, among all the connected components 32, the air supply channel and the air outlet channel of one connected component 32 are connected to the heat sink 31, so that the heat sink 31 can send cold air into the receiving chambers of all the storage bodies through the air supply channels of all the connected components 32, and then the cold air can cool the air in the receiving chamber, and the cooled air in the receiving chamber can be used to cool the drone that has completed the operation and is charging in the receiving chamber, so as to ensure that the charging efficiency of the drone will not be affected by the heat generated during the operation of the drone and the heat generated during charging, and it is beneficial to improve the charging efficiency of the drone.

[0036] While the heat sink 31 delivers cold air to the accommodating chamber through all the air supply channels, the heat sink 31 can also extract the hot air in the accommodating chamber to the outside through the air outlet channels of all the connecting components 32. The hot air specifically includes the heat generated during the operation of the drone, the heat generated during the charging of the drone, and the heat neutralized by the cold air, thereby effectively ensuring the cooling efficiency of the air in the accommodating chamber and realizing the circulation of the air in the accommodating chamber.

[0037] In summary, the accommodating cavities of multiple library bodies are connected together through the air supply channels and air outlet channels of multiple connecting components 32, and the air in the accommodating cavities of all library bodies is cooled by a heat sink 31, so there is no need to install the heat sink 31 on each library body, thereby effectively avoiding waste of resources. At the same time, when the heat sink 31 fails, only the library body installed with the heat sink 31 needs to be repaired, and there will be no failure of the heat sinks 31 in multiple library bodies, which is beneficial to improving the maintenance efficiency of the unmanned aerial vehicle hangar.

[0038] The drone hangar device provided in this embodiment is as follows: Figure 1 and Figure 2 As shown, all the library bodies include a first body 1 and several second bodies 2, the heat sink 31 is arranged on one side of the first body 1, all the second bodies 2 are arranged in sequence at intervals, and at least one second body 2 is arranged on the side of the first body 1 away from the heat sink 31, and all the connecting components 32 are arranged in series.

[0039] The drone hangar equipment of the above structure is configured such that all hangar bodies include a first body 1 and a plurality of second bodies 2, wherein a heat sink 31 is disposed on one side of the first body 1 and is connected to the first body 1, and all second bodies 2 are disposed in sequence at intervals, and one of the second bodies 2 is disposed on the side of the first body 1 away from the heat sink 31. In this way, the connecting component 32 in the first body 1 and the connecting components 32 in all the second bodies 2 can be connected in series, so that the heat sink 31 disposed on one side of the first body 1 can simultaneously cool the air in the accommodating cavities of all hangar bodies through all the connecting components 32, and the first body 1 and a plurality of second bodies 2 can be connected together through the connecting components 32 connected in series, so as to respectively accommodate a plurality of operating drones through these hangar bodies.

[0040] The drone hangar device provided in this embodiment is as follows: Figure 2 As shown, any air supply channel has a first interface, a second interface and a third interface, the first interface is suitable for connecting with the heat sink 31 or the second interface of the adjacent air supply channel, the second interface is suitable for connecting with the first interface of the heat sink 31 or the adjacent air supply channel, and the third interface is suitable for connecting with the accommodating cavity to connect the air supply channel and the accommodating cavity.

[0041] The unmanned aerial hangar equipment of the above-mentioned structure is configured such that each air supply channel has a first interface, a second interface and a third interface, the first interface and the second interface are arranged relatively to each other, and the third interface is arranged between the first interface and the second interface. At the same time, the third interfaces of all the air supply channels can be connected with a receiving cavity of a hangar body, so that the receiving cavity can be connected with the air supply channel, the first interface of the air supply channel of the connecting component 32 in the first body 1 can be connected with the heat sink 31, and the first interface of the air supply channel of the connecting component 32 in the second body 2 can be connected with the second interface of the air supply channel of the adjacent connecting component 32. In this way, the heat sink 31 can be connected with the air supply channels of all the connecting components 32, so that the heat sink 31 can transport cold air to the receiving cavity of the hangar body through all the air supply channels.

[0042] Of course, the second interface of the air supply channel of the connecting component 32 in the first body 1 can also be connected to the heat sink 31. Then the second interface of the air supply channel of the connecting component 32 in the second body 2 needs to be connected to the first interface of the air supply channel of the adjacent connecting component 32. In this way, the heat sink 31 can be connected to the air supply channels of all the connecting components 32, and the heat sink 31 can deliver cold air to the accommodating cavity of the storage body through all the air supply channels.

[0043] The drone hangar device provided in this embodiment is as follows: Figure 2 As shown, any air outlet channel has a fourth interface, a fifth interface and a sixth interface, the fourth interface is suitable for connecting with the fifth interface of the heat sink 31 or the adjacent air supply channel, the fifth interface is suitable for connecting with the fourth interface of the heat sink 31 or the adjacent air supply channel, and the sixth interface is suitable for connecting with the accommodating cavity to connect the air outlet channel and the accommodating cavity.

[0044] The unmanned aerial hangar equipment of the above-mentioned structure is configured such that each air outlet channel has a fourth interface, a fifth interface and a sixth interface, wherein the fourth interface and the fifth interface are relatively arranged, and the sixth interface is arranged between the first interface and the second interface. At the same time, the sixth interfaces of all the air outlet channels can be connected to the accommodating cavity of a hangar body, so that the accommodating cavity can be connected to the air outlet channel, the fourth interface of the air outlet channel of the connecting component 32 in the first body 1 can be connected to the heat sink 31, and the fourth interface of the air outlet channel of the connecting component 32 in the second body 2 can be connected to the fifth interface of the air supply channel of the adjacent connecting component 32.

[0045] In this way, the heat sink 31 can be connected to the air outlet channels of all the connecting components 32, so that the heat sink 31 can draw the hot air in the containing cavity of the storage body to the outside through all the air outlet channels; of course, the fifth interface of the air outlet channel of the connecting component 32 in the first body 1 can also be connected to the heat sink 31, then the fifth interface of the air outlet channel of the connecting component 32 in the second body 2 needs to be connected to the fourth interface of the air supply channel of the adjacent connecting component 32. In this way, the heat sink 31 can also be connected to the air outlet channels of all the connecting components 32, and the heat sink 31 can draw the hot air in the containing cavity of the storage body to the outside through all the air outlet channels.

[0046] The drone hangar device provided in this embodiment is as follows: Figure 2 As shown, in the second body 2 at the end, the first interface or the second interface of the air supply channel of the connecting component 32 is in a blocked state, and the fourth interface or the fifth interface of the air outlet channel of the connecting component 32 is in a blocked state.

[0047] The unmanned aerial vehicle hangar equipment of the above-mentioned structure is configured such that the first interface of the air supply channel of the connecting component 32 in the second body 2 at the end and the fourth interface of the air outlet channel are in a blocked state, so that after the connecting component 32 completes the connection between all the second bodies 2 and the first body 1, all the air supply channels and air outlet channels can be blocked, and the cold air in the air supply channel and the hot air in the air outlet channel will not flow out to the outside through other outlets except the heat sink 31, thereby enabling the air in the containing cavity of all the hangar bodies to circulate between all the air supply channels and the air outlet channels.

[0048] The drone hangar device provided in this embodiment is as follows: Figure 1 and Figure 2 As shown, all the library bodies include a first body 1 and several second bodies 2, the heat sink 31 is arranged on one side of the first body 1, all the second bodies 2 are arranged in array on the surrounding side of the first body 1, and all the connecting components 32 in the second bodies 2 are arranged in parallel with the connecting components 32 in the first body 1.

[0049] The drone hangar equipment of the above structure is provided with all hangar bodies including a first body 1 and a plurality of second bodies 2, wherein a heat sink 31 is provided on one side of the first body 1 and connected to the first body 1, and all the second bodies 2 are arranged in an array on the surrounding side of the first body 1. In this way, the connecting component 32 in the first body 1 and the connecting components 32 in all the second bodies 2 can be connected in parallel, so that the heat sink 31 provided on one side of the first body 1 can cool the air in the accommodating cavity of all the hangar bodies through all the connecting components 32, and the first body 1 can be connected to all the second bodies 2 through the parallel connecting components 32, so as to respectively store multiple operating drones through these hangar bodies.

[0050] The drone hangar device provided in this embodiment is as follows: Figure 1 and Figure 2 As shown, any air supply channel has a seventh interface and several eighth interfaces, the seventh interface is connected to the accommodating cavity, one of the eighth interfaces of the air supply channel in the first body 1 is connected to the heat sink 31, and all the eighth interfaces are connected to an eighth interface of the adjacent air supply channel.

[0051] The unmanned aerial hangar equipment of the above-mentioned structure is configured so that each air supply channel has a seventh interface and several eighth interfaces, wherein the seventh interface is arranged between all the eighth interfaces, and at the same time, the seventh interfaces of all the air supply channels can be connected with the accommodating cavity of a hangar body, so that the accommodating cavity can be connected with the air supply channel, one of the eighth interfaces of the air supply channel of the connecting component 32 in the first body 1 can be connected with the heat sink 31, and the other eighth interface can be connected with one of the eighth interfaces of the air supply channel of the connecting component 32 in the adjacent second body 2, and the other eighth interface of the air supply channel of the connecting component 32 in the second body 2 can be connected with one of the eighth interfaces of the air supply channel of the connecting component 32 in the adjacent second body 2. In this way, the heat sink 31 can be connected with the air supply channels of all the connecting components 32, so that the heat sink 31 can transport cold air to the accommodating cavities of all hangar bodies through all the air supply channels.

[0052] The drone hangar device provided in this embodiment is as follows: Figure 1 and Figure 2 As shown, any air outlet channel has a ninth interface and several tenth interfaces, the ninth interface is connected to the accommodating cavity, one of the tenth interfaces of the air outlet channel in the first body 1 is connected to the heat sink 31, and all the tenth interfaces are connected to a tenth interface of the adjacent air outlet channel.

[0053] The unmanned aerial hangar equipment of the above-mentioned structure is configured so that each air outlet channel has a ninth interface and several tenth interfaces, wherein the ninth interface is arranged between all the tenth interfaces, and at the same time, the ninth interfaces of all the air outlet channels can be connected to the containing cavity of a hangar body, so that the containing cavity can be connected to the air supply channel, one of the tenth interfaces of the air outlet channel of the connecting component 32 in the first body 1 can be connected to the heat sink 31, and the other tenth interface can be connected to one of the tenth interfaces of the air outlet channel of the connecting component 32 in the adjacent second body 2, and the other tenth interface of the air outlet channel of the connecting component 32 in the second body 2 can be connected to one of the tenth interfaces of the air outlet channel of the connecting component 32 in the adjacent second body 2. In this way, the heat sink 31 can be connected to the air outlet channels of all the connecting components 32, so that the heat sink 31 can extract the hot air in the containing cavity of all the hangar bodies to the outside through all the air outlet channels.

[0054] The drone hangar device provided in this embodiment is as follows: Figure 1 and Figure 2 As shown, in each second body 2 at the end, at least one eighth interface of the air supply channel of the connecting component 32 is in a blocked state, and at least one tenth interface of the air outlet channel of the connecting component 32 is in a blocked state.

[0055] The unmanned aerial hangar equipment of the above-mentioned structure is configured such that the eighth interface of the air supply channel of the connecting component 32 in each second body 2 at the end and the tenth interface of the air outlet channel that are not involved in the connection are in a blocked state, so that after the connecting component 32 completes the connection between all the second bodies 2 and the first body 1, all the air supply channels and the air outlet channels can be blocked, and the cold air in the air supply channel and the hot air in the air outlet channel will not flow out to the outside through other outlets except the heat sink 31, thereby enabling the air in the containing cavity of all the hangar bodies to circulate between all the air supply channels and the air outlet channels.

[0056] The drone hangar device provided in this embodiment is as follows: Figure 2 As shown, the connecting component 32 includes an air supply member 321 and an air outlet member 322 , the air supply channel is opened on the air supply member 321 , the air outlet channel is opened on the air outlet member 322 , and each interface is a port on the air supply member 321 and the air outlet member 322 .

[0057] The unmanned aerial vehicle hangar equipment of the above structure includes an air supply member 321 and an air outlet member 322 by setting a connecting component 32. The air supply member 321 and the air outlet member 322 are respectively an air supply duct and an air outlet duct in the present embodiment, wherein the air supply member 321 and the air outlet member 322 are arranged in the installation cavity at intervals, and at the same time, the air supply channel is opened on the air supply member 321, and the air outlet channel is opened on the air outlet member 322, and the interfaces on the air supply channel and the air outlet channel are respectively ports on the air supply member 321 and the air outlet member 322. When the first body 1 and all the second bodies 2 are connected through the connecting component 32, one port between all the air supply members 321 and the air outlet members 322 can be connected. In this way, the first body 1 and all the second bodies 2 can be connected together through the connecting component 32.

[0058] The drone hangar device provided by the present invention is provided with a heat dissipation structure 3 on the hangar body, wherein a plurality of hangar bodies are provided, and all hangar bodies are arranged at intervals, and at the same time, each hangar body has a receiving cavity and an installation cavity arranged at intervals, and the receiving cavity can be used to store the drone, so as to protect the drone through the hangar body; the heat dissipation structure 3 specifically includes a heat dissipation element 31 and a plurality of connecting components 32, wherein the heat dissipation element 31 is provided on one side of one hangar body and connected to the hangar body, and each connecting component 32 is provided in the installation cavity of a hangar body, and at the same time, each connecting component Each of the components 32 has an air supply channel and an air outlet channel connected to the accommodating chamber, and the air supply channels of all the connecting components 32 are connected to each other, and the air outlet channels are connected to each other, so that all the accommodating chambers of the storage body are connected together through the air supply channel and the air outlet channel. In addition, the air supply channel and the air outlet channel of one connecting component 32 among all the connecting components 32 are connected to the heat sink 31, so that the heat sink 31 can send cold air into the accommodating chambers of all the storage bodies through the air supply channels of all the connecting components 32, so that the cold air can cool the air in the accommodating chamber and pass through the accommodating chamber. The cooled air cools the drone that has completed the operation and is charging in the accommodating chamber, so as to ensure that the charging efficiency of the drone will not be affected by the heat generated during the operation of the drone and the heat generated during charging, and is conducive to improving the charging efficiency of the drone. While the heat sink 31 delivers cold air to the accommodating chamber through all the air supply channels, the heat sink 31 can also extract the hot air in the accommodating chamber to the outside through the air outlet channels of all the connecting components 32. The hot air specifically includes the heat generated during the operation of the drone, the heat generated when the drone is charging, and the heat neutralized with the cold air, thereby effectively ensuring the accommodating chamber. The cooling efficiency of the air in the cavity is improved, and the circulation of the air in the accommodating cavity can be realized; in summary, the accommodating cavities of multiple library bodies are connected together through the air supply channels and air outlet channels of multiple connecting components 32, and the air in the accommodating cavities of all library bodies is cooled by a heat sink 31, so that there is no need to install a heat sink 31 on each library body, thereby effectively avoiding the waste of resources. At the same time, when the heat sink 31 fails, only the library body installed with the heat sink 31 needs to be repaired, and there will be no failure of the heat sinks 31 in multiple library bodies, which is beneficial to improving the maintenance efficiency of the unmanned aerial vehicle hangar.

[0059] 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 equipment, characterized in that: include: A plurality of storage bodies, all of which are arranged at intervals, and any of which has a receiving cavity and an installation cavity arranged at intervals, wherein the receiving cavity is suitable for storing a drone; The heat dissipation structure (3) comprises a heat dissipation element (31) and a plurality of connecting components (32), wherein the heat dissipation element (31) is arranged on one side of the storage body, any one of the connecting components (32) is arranged in one of the installation chambers, and any one of the connecting components (32) has an air supply channel and an air outlet channel connected to the accommodating chamber; Among them, the air supply channels and the air outlet channels of all the connecting components (32) are connected, and the air supply channel and the air outlet channel of at least one of the connecting components (32) are connected to the heat sink (31), so that the heat sink (31) can send cold air into the containing chambers of all the storage bodies through all the air supply channels, and draw hot air in the containing chambers of all the storage bodies to the outside through all the air outlet channels.

2. The drone hangar equipment according to claim 1, characterized in that: All of the library bodies include a first body (1) and a plurality of second bodies (2); the heat sink (31) is arranged on one side of the first body (1); all of the second bodies (2) are arranged in sequence and spaced apart; and at least one of the second bodies (2) is arranged on a side of the first body (1) away from the heat sink (31); and all of the connecting components (32) are arranged in series.

3. The drone hangar equipment according to claim 2, characterized in that: Any of the air supply channels has a first interface, a second interface and a third interface, the first interface is suitable for communicating with the heat sink (31) or the second interface of an adjacent air supply channel, the second interface is suitable for communicating with the heat sink (31) or the first interface of an adjacent air supply channel, and the third interface is suitable for connecting with the accommodating cavity to connect the air supply channel and the accommodating cavity.

4. The drone hangar equipment according to claim 3, characterized in that: Any of the air outlet channels has a fourth interface, a fifth interface and a sixth interface, the fourth interface is suitable for communicating with the heat sink (31) or the fifth interface of the adjacent air supply channel, the fifth interface is suitable for communicating with the heat sink (31) or the fourth interface of the adjacent air supply channel, and the sixth interface is suitable for connecting with the accommodating cavity to connect the air outlet channel and the accommodating cavity.

5. The drone hangar equipment according to claim 4, characterized in that: In the second body (2) at the end, the first interface or the second interface of the air supply channel of the connecting component (32) is in a blocked state, and the fourth interface or the fifth interface of the air outlet channel of the connecting component (32) is in a blocked state.

6. The drone hangar equipment according to claim 1, characterized in that: All of the library bodies include a first body (1) and a plurality of second bodies (2); the heat sink (31) is arranged on one side of the first body (1); all of the second bodies (2) are arranged in an array around the first body (1); and the connecting components (32) in all of the second bodies (2) are arranged in parallel with the connecting components (32) in the first body (1).

7. The drone hangar equipment according to claim 6, characterized in that: Any of the air supply channels has a seventh interface and several eighth interfaces, the seventh interface is connected to the accommodating cavity, one of the eighth interfaces of the air supply channel in the first body (1) is connected to the heat sink (31), and all of the eighth interfaces are connected to an eighth interface of an adjacent air supply channel.

8. The drone hangar equipment according to claim 7, characterized in that: Any of the air outlet channels has a ninth interface and a plurality of tenth interfaces, the ninth interface is connected to the accommodating cavity, one of the tenth interfaces of the air outlet channels in the first body (1) is connected to the heat sink (31), and all of the tenth interfaces are connected to a tenth interface of an adjacent air outlet channel.

9. The drone hangar equipment according to claim 8, characterized in that: In each of the second bodies (2) at the end, at least one of the eighth interfaces of the air supply channel of the connecting component (32) is in a blocked state, and at least one of the tenth interfaces of the air outlet channel of the connecting component (32) is in a blocked state.

10. The drone hangar equipment according to claim 5 or 9, characterized in that: The connecting component (32) comprises an air supply member (321) and an air outlet member (322); the air supply channel is provided on the air supply member (321); the air outlet channel is provided on the air outlet member (322); and each of the interfaces is a port on the air supply member (321) and the air outlet member (322).

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