Unmanned aerial vehicle hangar, temperature control method and device, medium and vehicle

Abstract

The invention discloses an unmanned aerial vehicle hangar, a temperature control method, equipment, a medium and a vehicle, relates to the technical field of vehicles, and aims to solve the problem that the service life of an unmanned aerial vehicle is affected by too high temperature of the unmanned aerial vehicle hangar when the unmanned aerial vehicle is arranged in the unmanned aerial vehicle hangar. The unmanned aerial vehicle hangar is used for a vehicle, the unmanned aerial vehicle hangar comprises a hangar body and a ventilation assembly, the hangar body comprises a containing cavity, the containing cavity is used for containing an unmanned aerial vehicle, the ventilation assembly comprises an air inlet and an air outlet, and the air inlet and the air outlet are both formed in the hangar body and are arranged at intervals in the first direction; the air inlet and the air outlet are both communicated with the containing cavity and the external environment, when the vehicle runs, the air inlet is located on the windward side, and the air outlet is located on the leeward side. Therefore, the air inlet and the air outlet are matched to ventilate the accommodating cavity, so that the temperature of the unmanned aerial vehicle arranged in the accommodating cavity is reduced, and the service life of the unmanned aerial vehicle is prolonged.

Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of vehicles, in particular to a UAV hangar, a temperature control method, equipment, a medium and a vehicle. BACKGROUND

[0002] In recent years, the unmanned aerial vehicle industry has developed rapidly, and vehicle-mounted unmanned aerial vehicles, as an inevitable product of technological development, have a more and more extensive application market. The unmanned aerial vehicle hangar, as a take-off and landing platform for unmanned aerial vehicles, can be arranged on vehicles, ships and building walls, etc. With the increasing size of unmanned aerial vehicles, the corresponding unmanned aerial vehicle hangars are also becoming larger and larger.

[0003] In the related art, the unmanned aerial vehicle is placed in the unmanned aerial vehicle cabin, and the unmanned aerial vehicle cabin is installed on the roof of the vehicle and is exposed to the sun, so that the temperature in the cabin is very high, even exceeding the normal working temperature of the unmanned aerial vehicle, thereby affecting the service life of the unmanned aerial vehicle. SUMMARY

[0004] The present application discloses a UAV hangar, a temperature control method, equipment, a medium and a vehicle, and relates to the technical field of vehicles, aiming to solve the problem of how to avoid the temperature of the UAV hangar being too high when the UAV is arranged in the UAV hangar, thereby affecting the service life of the UAV.

[0005] To achieve the above-mentioned purpose, the present application adopts the following technical solutions:

[0006] The present application provides a UAV hangar for a vehicle, comprising:

[0007] a hangar main body, the hangar main body comprising a containing cavity, the containing cavity being used for containing a UAV,

[0008] a ventilation assembly comprising an air inlet and an air outlet, the air inlet and the air outlet being arranged on the hangar main body and being spaced apart along a first direction, the air inlet and the air outlet both communicating the containing cavity and an external environment, the air inlet being located on a windward side and the air outlet being located on a leeward side when the vehicle is running.

[0009] In the UAV hangar of the present application, the UAV hangar is used for a vehicle, and the UAV hangar comprises a hangar main body and a ventilation assembly, the hangar main body comprises a containing cavity, the containing cavity is used for arranging a UAV, the ventilation assembly comprises an air inlet and an air outlet, the air inlet and the air outlet are arranged on the hangar main body and are spaced apart along a first direction, the air inlet and the air outlet both communicate the containing cavity and an external environment, the air inlet is located on a windward side and the air outlet is located on a leeward side when the vehicle is running. In this way, the air inlet and the air outlet cooperate to ventilate the containing cavity, so as to reduce the temperature of the UAV arranged in the containing cavity, thereby improving the service life of the UAV.

[0010] In some embodiments, the air inlet and the air outlet are disposed on two sides of the hangar body in the first direction.

[0011] In some embodiments, the ventilation assembly further comprises an air guide channel disposed in the accommodation cavity and communicating the air inlet and the landing platform position of the UAV.

[0012] In some embodiments, the ventilation assembly further comprises a filter screen disposed on the air inlet close to the air guide channel.

[0013] In some embodiments, the air inlet comprises at least a first air inlet and a second air inlet disposed on the hangar body, the first air inlet and the second air inlet are symmetrically disposed about a central axis of the hangar body in the first direction.

[0014] In some embodiments, the ventilation assembly further comprises an air guide channel, the air guide channel comprises at least a first air guide channel and a second air guide channel;

[0015] the first air guide channel is disposed in the accommodation cavity and communicates the first air inlet and the landing platform position of the UAV;

[0016] the second air guide channel is disposed in the accommodation cavity and communicates the second air inlet and the landing platform position of the UAV;

[0017] the first air guide channel and the second air guide channel are symmetrically disposed about a central axis of the hangar body in the first direction.

[0018] In some embodiments, in the first direction, the first air inlet and the second air inlet are disposed on the front side of the hangar body, and the air outlet is disposed on the rear side of the hangar body.

[0019] In some embodiments, the hangar body comprises a first surface and a second surface disposed opposite in the first direction, the hangar body comprises a third surface and a fourth surface disposed opposite in a second direction, a first transition surface is disposed between the first surface and the third surface, and a second transition surface is disposed between the second surface and the fourth surface, wherein the first direction and the second direction are perpendicular.

[0020] the first air inlet is formed in the first transition surface, the second air inlet is formed in the second transition surface, and the air outlet is formed in the fourth surface.

[0021] In some embodiments, the ventilation assembly further comprises a water baffle and a drainage structure, the drainage structure and the water baffle are both connected to the hangar body and located in the accommodation cavity, the water baffle is adapted to guide liquid passing through the air inlet or the air outlet into the drainage structure, and the drainage structure is adapted to guide the liquid out of the accommodation cavity.

[0022] In some embodiments, the drainage structure is inclined downward along a direction close to the air inlet or the air outlet, and an inclination angle β of the drainage structure with respect to a horizontal plane is greater than or equal to 3 degrees.

[0023] In some embodiments, the ventilation assembly further comprises a fan module, the fan module is arranged in the accommodation cavity and located between the air outlet and a parking platform of the UAV, the fan module is used to rotate to generate an air flow to reduce the temperature of the accommodation cavity, and a direction of the air flow generated by the rotation of the fan module is toward the air outlet.

[0024] In some embodiments, the fan module is located between the air outlet and the parking platform of the UAV.

[0025] In some embodiments, the ventilation assembly further comprises an air conditioner air inlet, the air conditioner air inlet is arranged on a bottom surface of the hangar body, and the air conditioner air inlet is adapted to communicate the accommodation cavity and an air conditioning system of the vehicle.

[0026] In some embodiments, the ventilation assembly further comprises an air conditioner air outlet, the air conditioner air outlet is arranged on the bottom surface of the hangar body, and the air outlet is adapted to cooperate with the air conditioner air inlet to communicate the accommodation cavity and the air conditioning system of the vehicle.

[0027] The present application provides a temperature control method for controlling the UAV hangar of any one of the above embodiments, the temperature control method comprising:

[0028] According to the mode of the UAV and according to the temperature of the accommodation cavity and / or a battery state parameter of the UAV, the working state of the ventilation assembly is controlled.

[0029] In some embodiments, if the UAV is in a first mode, the working state of the ventilation assembly is controlled according to the temperature of the accommodation cavity and / or the battery state parameter of the UAV, comprising:

[0030] In the case that the temperature of the accommodation cavity is in a first temperature range, the ventilation assembly is controlled to work in a first working mode.

[0031] In some embodiments, the battery state parameter comprises a battery capacity of the UAV.

[0032] The method of controlling the operating state of the ventilation assembly based on the temperature of the accommodating cavity and / or the battery status parameters of the drone includes:

[0033] When the accommodating cavity is in the second temperature range and the battery power of the drone is greater than the first parameter threshold, the ventilation component is controlled to operate in the second working mode.

[0034] When the accommodating cavity is in the second temperature range and the battery power of the drone is less than or equal to the first parameter threshold, the ventilation component is controlled to operate in a first operating mode, wherein the maximum temperature of the second temperature range is less than the minimum temperature of the first temperature range, and the fan speed in the second operating mode is less than the fan speed in the first operating mode.

[0035] In some embodiments, the battery status parameters include the drone's battery charge and battery temperature;

[0036] The step of controlling the operating state of the ventilation component based on the temperature of the accommodating cavity and the battery status parameters of the drone includes:

[0037] While the containment cavity is in a third temperature range, the battery charge and battery temperature of the drone are monitored, wherein the maximum temperature value in the third temperature range is less than the minimum temperature value in the second temperature range;

[0038] The operating status of the ventilation component is controlled based on the battery level and temperature of the drone.

[0039] In some embodiments, controlling the operating state of the ventilation component based on the battery level and battery temperature of the drone includes:

[0040] When the battery power of the drone is less than the second parameter threshold and the battery temperature of the drone is greater than the first temperature threshold, the ventilation component is controlled to operate in a first working mode, wherein the second parameter threshold is less than the first parameter threshold.

[0041] When the battery power of the drone is less than the second parameter threshold, and the battery temperature of the drone is less than or equal to the first temperature threshold and greater than or equal to the second temperature threshold, the ventilation component is controlled to operate in a second working mode, wherein the fan speed in the second working mode is less than the fan speed in the first working mode.

[0042] When the battery power of the drone is less than the second parameter threshold and the battery temperature of the drone is less than the second temperature threshold, the ventilation component is controlled to operate in a third working mode, wherein the fan speed in the third working mode is less than the fan speed in the second working mode.

[0043] In some embodiments, controlling the operating state of the ventilation component based on the battery level and battery temperature of the drone includes:

[0044] When the battery power of the drone is greater than or equal to the second parameter threshold and less than or equal to the first parameter threshold, and the battery temperature of the drone is greater than the first temperature threshold, the ventilation component is controlled to operate in the first working mode.

[0045] When the battery power of the drone is greater than or equal to the second parameter threshold and less than or equal to the first parameter threshold, and the battery temperature of the drone is less than or equal to the first temperature threshold and greater than or equal to the second temperature threshold, the ventilation component is controlled to operate in a third working mode, wherein the fan speed in the third working mode is less than the fan speed in the first working mode.

[0046] When the drone's battery charge is greater than or equal to the second parameter threshold and less than or equal to the first parameter threshold, and the drone's battery temperature is less than the second temperature threshold, the ventilation component is controlled to stop working.

[0047] In some embodiments, controlling the operating state of the ventilation component based on the battery level and battery temperature of the drone includes:

[0048] When the battery power of the drone is greater than the first parameter threshold and the battery temperature of the drone is greater than the first temperature threshold, the ventilation component is controlled to operate in the second working mode.

[0049] When the battery power of the drone is greater than the first parameter threshold, and the battery temperature of the drone is less than or equal to the first temperature threshold and greater than or equal to the second temperature threshold, the ventilation component is controlled to operate in a third working mode, wherein the fan speed in the third working mode is less than the fan speed in the second working mode.

[0050] When the drone's battery charge is greater than the first parameter threshold and the drone's battery temperature is less than the second temperature threshold, the ventilation component is controlled to stop working.

[0051] In some embodiments, controlling the operating state of the ventilation assembly based on the temperature of the accommodating cavity and the battery state parameters of the drone includes:

[0052] When the accommodating cavity is in the fourth temperature range, the ventilation assembly is controlled to stop operating.

[0053] In some embodiments, the control method further includes:

[0054] When the drone is in the second mode and the drone is in the receiving cavity, if the battery temperature of the drone is greater than the first temperature threshold, the ventilation component is controlled to operate in the first working mode; otherwise, the ventilation component is controlled to stop working.

[0055] This application provides an electronic device including a processor and a memory, wherein the processor is configured to execute a computer program stored in the memory to perform the temperature control method described in any of the above embodiments.

[0056] This application provides a readable storage medium storing a computer program that, when executed by one or more processors, implements the temperature control method described in any of the above embodiments.

[0057] This application provides a vehicle that includes a drone hangar as described in any of the above embodiments, an electronic device as described in the above embodiments, or a storage medium as described in the above embodiments. Attached Figure Description

[0058] To more clearly illustrate the technical solutions of the embodiments of this application, the drawings used in the description of the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this application. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0059] Figure 1 This is a structural diagram of a drone hangar provided according to some embodiments;

[0060] Figure 2 This is a structural diagram of a ventilation assembly provided according to some embodiments;

[0061] Figure 3 This is another structural diagram of a drone hangar provided according to some embodiments;

[0062] Figure 4 This is a structural diagram of a vehicle provided according to some embodiments;

[0063] Figure 5 This is yet another structural diagram of a drone hangar provided according to some embodiments;

[0064] Figure 6 This is another structural diagram of a drone hangar provided according to some embodiments;

[0065] Figure 7 This is a partial structural diagram of a drone hangar provided according to some embodiments;

[0066] Figure 8 This is a partial structural diagram of a drone hangar provided according to some embodiments;

[0067] Figure 9 This is a flowchart of a temperature control method provided according to some embodiments;

[0068] Figure 10 This is another flowchart of a temperature control method provided according to some embodiments;

[0069] Figure 11 This is yet another flowchart of a temperature control method provided according to some embodiments;

[0070] Figure 12 This is another flowchart of a temperature control method provided according to some embodiments;

[0071] Figure 13 This is another flowchart of a temperature control method provided according to some embodiments.

[0072] Figure label:

[0073] Unmanned Aerial Vehicle (UAV) hangar 200, hangar main body 1, first surface 11, second surface 12, third surface 13, fourth surface 14, first transition surface 15, second transition surface 16, receiving cavity 17, ventilation assembly 2, air inlet 21, first air inlet 211, second air inlet 212, air outlet 22, air guide duct 23, first air guide duct 231, second air guide duct 232, filter screen 24, drainage space 241, fan module 25, air conditioning air inlet 26, air conditioning air outlet 27, water baffle 28, drainage structure 29, inclined plate 291, baffle 292, dustproof net 293, door 3, vehicle 300, UAV 400. Detailed Implementation

[0074] The technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of the present invention.

[0075] In the description of this invention, it should be understood that the terms "upper," "lower," "left," "right," "front," "rear," "inner," and "outer," etc., indicate the orientation or positional relationship based on the orientation or relative positional relationship shown in the accompanying drawings. They are used only for the convenience of describing the invention 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 the invention. Unless otherwise specified, the above-described orientation can be flexibly set in practical applications, provided that the relative positional relationship shown in the accompanying drawings is satisfied.

[0076] The terms "first" and "second" are used for descriptive purposes only and should not be construed as indicating or implying relative importance or implicitly specifying the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of this invention, unless otherwise stated, "a plurality of" means two or more.

[0077] In the description of this invention, it should be noted that, unless otherwise explicitly specified and limited, the terms "installation," "connection," "linking," and "communication" 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 direct connection or an indirect connection through an intermediate medium, or a communication between the internal components of two elements. Those skilled in the art can understand the specific meaning of the above terms in this invention according to the specific circumstances.

[0078] In embodiments of the invention, the terms "comprising," "including," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, article, or apparatus that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such a process, article, or apparatus. Without further limitation, an element defined by the phrase "comprising one..." does not exclude the presence of other identical elements in the process, article, or apparatus that includes that element.

[0079] In embodiments of the present invention, the terms "exemplary" or "for example" are used to indicate that something is an example, illustration, or description. Any embodiment or design described as "exemplary" or "for example" in embodiments of the present invention should not be construed as being more preferred or advantageous than other embodiments or designs. Rather, the use of the terms "exemplary" or "for example" is intended to present the relevant concepts in a specific manner.

[0080] Please see Figures 1 to 4The present invention provides a drone hangar 200 for use with a vehicle 300. The drone hangar 200 includes a hangar body 1 and a ventilation component 2. The hangar body 1 includes a receiving cavity 17 for accommodating a drone 400. The ventilation component 2 includes an air inlet 21 and an air outlet 22. The air inlet 21 and the air outlet 22 are both located on the hangar body 1 and are spaced apart along a first direction. The air inlet 21 and the air outlet 22 are both connected to the receiving cavity 17 and the external environment. When the vehicle 300 is in motion, the air inlet 21 is located on the windward side and the air outlet 22 is located on the leeward side.

[0081] In the drone hangar 200 and vehicle 300 of this application embodiment, the drone hangar 200 is used for the vehicle 300. The drone hangar 200 includes a hangar body 1 and a ventilation assembly 2. The hangar body 1 includes a receiving cavity 17 for accommodating drones 400. The ventilation assembly 2 includes an air inlet 21 and an air outlet 22. The air inlet 21 and the air outlet 22 are both located in the hangar body 1 and spaced apart along a first direction. The air inlet 21 and the air outlet 22 are both connected to the receiving cavity 17 and the external environment. When the vehicle 300 is moving, the air inlet 21 is located on the windward side, and the air outlet 22 is located on the leeward side. In this way, the air inlet 21 and the air outlet 22 work together to ventilate the receiving cavity 17, thereby reducing the temperature of the drone 400 located in the receiving cavity 17 and improving the service life of the drone 400.

[0082] In some embodiments, the air inlet 21 and the air outlet 22 are located on both sides of the hangar body 1 along a first direction. In this way, the air inlet 21 and the air outlet 22 can be located on both sides along the length of the vehicle 300. When the vehicle 300 is traveling normally in a straight line, the airflow can enter through the air inlet 21, pass through the receiving cavity 17 and exit through the air outlet 22, thereby regulating the temperature of the receiving cavity 17.

[0083] Understandably, with the advancement of people's living standards and technological conditions, the requirements for vehicle 300 are no longer limited to its basic function of carrying passengers. Greater demands are placed on it for social needs such as route exploration, photography, entertainment, and social media vlogging, as well as professional fields such as surveying, disaster monitoring, traffic patrol, forest fire prevention, border patrol, and natural disaster monitoring and assessment. The drone hangar 200 of this embodiment, in conjunction with the drone 400, can realize these functions, thus improving the practicality of vehicle 300 in this embodiment.

[0084] The drone 400 is stored in the drone 400 compartment of the vehicle 300. Due to its high mobility, exposure to direct sunlight in summer often causes the temperature inside the compartment to exceed the charging and normal operating temperatures of the drone 400's lithium battery. Therefore, the drone hangar 200 of this embodiment is equipped with a ventilation component 2, which helps dissipate heat from the drone 400 and improves its service life.

[0085] Please see Figure 4 This application provides a vehicle 300, which includes a drone hangar 200 according to an embodiment of this application, or an electronic device according to an embodiment of this application, or a storage medium according to an embodiment of this application.

[0086] Specifically, vehicle 300 can load drone 400 into drone hangar 200, enabling the integration of drone 400 and vehicle 300 functions and providing various possibilities for their application scenarios. For example, drone 400 can survey the surrounding terrain of vehicle 300, find roads, or perform self-driving aerial photography for entertainment. In this embodiment, drone hangar 200 can be set at any location on vehicle 300; for example, it can be set on top of vehicle 300 or in the trunk of vehicle 300 to meet different needs.

[0087] For example, the drone 400 is placed inside the drone hangar 200, which is mounted on the roof of a vehicle. Since summer temperatures typically reach above 38 degrees Celsius, the drone hangar 200, exposed to direct sunlight, experiences even higher temperatures, exceeding the normal operating temperature of the drone 400. To ensure the safety and normal operation of the drone 400, the drone hangar 200 in this embodiment of the application includes a ventilation component 2. The ventilation component 2 includes an air inlet 21 and an air outlet 22, both located on opposite sides of the hangar body 1 along a first direction. Both the air inlet 21 and the air outlet 22 connect the receiving cavity 17 to the external environment. When the vehicle 300 is in motion, the air inlet 21 is on the windward side, and the air outlet 22 is on the leeward side. Thus, during normal vehicle operation, airflow can ventilate and cool the drone 400 inside the drone hangar 200.

[0088] In this way, the drone 400 can be parked in the drone hangar 200, providing it with a sheltered place. Specifically, the drone 400 in the drone hangar 200 is protected from wind, rain, sun and impacts, is dustproof and waterproof, extending the service life of the drone 400, and providing energy supply for the drone 400, facilitating the movement of the drone platform and enabling multiple uses.

[0089] Furthermore, the vehicle 300 in this application embodiment can be a pure electric vehicle 300, a hybrid electric vehicle 300, a plug-in hybrid electric vehicle 300, a range-extended electric vehicle 300, a gasoline vehicle, etc. The vehicle 300 can also be a sedan, a truck, a bus, a lorry, a trailer, etc. This application does not specifically limit the type of vehicle 300.

[0090] In some embodiments, the ventilation assembly 2 further includes an air duct 23, which is disposed in the receiving cavity 17 and connects the air inlet 21 and the landing platform position of the drone 400.

[0091] In this way, the air duct 23 can work with the air inlet 21 to guide the airflow to the landing platform where the drone 400 is located, so that the drone 400 can be cooled down quickly.

[0092] Please see Figures 5 to 8 In some embodiments, the ventilation assembly 2 further includes a filter 24, which is disposed on the side of the air inlet 21 near the air duct 23.

[0093] Thus, as the vehicle 300 moves, the airflow passes sequentially through the air inlet 21, filter 24, air duct 23, landing platform, and air outlet 22. This continuous airflow within the containment cavity 17 removes heat from the surface of the drone 400, thereby reducing problems with the drone 400 and extending its service life.

[0094] Specifically, the filter 24 can keep sand, dust, impurities and insects in the external environment out of the housing cavity 17, thereby improving the cleanliness of the housing cavity 17, preventing the drone 400 from being scratched, and ensuring the normal use of the drone 400.

[0095] In some embodiments, the air inlet 21 includes at least a first air inlet 211 and a second air inlet 212 disposed on the hangar body 1, and the first air inlet 211 and the second air inlet 212 are symmetrically arranged about the central axis of the hangar body 1 in a first direction.

[0096] Specifically, the first direction can be the direction of travel of the vehicle 300. As the vehicle 300 moves forward, the airflow can enter the receiving cavity 17 from the first air inlet 211 and the second air inlet 212 respectively, and blow air to cool the drone 400.

[0097] In some embodiments, the ventilation assembly 2 further includes an air guide 23, which includes at least a first air guide 231 and a second air guide 232.

[0098] The first air duct 231 is located in the receiving cavity 17 and connects the first air inlet 211 and the landing platform of the UAV 400;

[0099] The second air duct 232 is located in the receiving cavity 17 and connects the second air inlet 212 and the landing platform of the UAV 400;

[0100] The first air duct 231 and the second air duct 232 are symmetrically arranged about the central axis of the hangar body 1 in the first direction.

[0101] In some embodiments, in a first direction, a first air inlet 211 and a second air inlet 212 are located on the front side of the hangar body 1, and an air outlet 22 is located on the rear side of the hangar body 1.

[0102] Thus, during the movement of the vehicle 300, the first air duct 231 and the second air duct 232 can respectively work with the first air inlet 211 and the second air inlet 212 to cool the drone 400. After passing through the drone platform, the airflow returns to the environment through the air outlet 22 on the rear side of the hangar body 1. In this way, regardless of the driving state of the vehicle 300, the airflow can always cool the drone 400 through the first air inlet 211 and the second air inlet 212.

[0103] In some embodiments, the hangar body 1 includes a first surface 11 and a second surface 12 disposed opposite to each other along a first direction, and a third surface 13 and a fourth surface 14 disposed opposite to each other along a second direction. A first transition surface 15 is provided between the first surface 11 and the third surface 13, and a second transition surface 16 is provided between the second surface 12 and the fourth surface 14, wherein the first direction and the second direction are perpendicular.

[0104] The first air inlet 211 is formed on the first transition surface 15, the second air inlet 212 is formed on the second transition surface 16, and the air outlet 22 is formed on the fourth surface 14.

[0105] Thus, when the vehicle 300 makes a left or right turn, or when there is wind in the environment where the vehicle 300 is located at an angle to the direction of travel of the vehicle 300, the first air inlet 211 and the second air inlet, together with the first air guide duct 231 and the second air guide duct 232, can guide airflow from different directions toward the drone 400.

[0106] For example, the hangar body 1 can be rectangular and positioned on top of the vehicle 300. The first surface 11 can be the front of the vehicle 300, the second surface 12 can be the back of the vehicle 300, and the third surface 13 and the fourth surface 14 can be the two sides of the vehicle 300, respectively. In this way, the first transition surface 15 and the second transition surface 16 are two curved surfaces. The first air inlet 211 and the second air inlet 212, respectively located on the first transition surface 15 and the second transition surface 16, can have a large frontal area, receiving airflow from multiple directions. Simultaneously, this avoids the aesthetic problems caused by placing the first air inlet 211 and the second air inlet 212 on the first surface 11, as well as the noise problem caused by direct airflow during vehicle 300 operation.

[0107] In this application embodiment, the positions of the air inlet 21 and the air outlet 22 are not limited to meet different needs. For example, the two air inlets 21 can be respectively provided on the first transition surface 15 and the second transition surface 16; or the two air inlets 21 can be respectively provided on the third surface 13 and the fourth surface 14; or the air inlet 21 can be provided on the first surface 11.

[0108] In one example, an air inlet 21 may be provided on the first transition surface 15 or the second transition surface 16. In addition, multiple air outlets 22 may be provided on the second surface 12, which is not limited here. Of course, in other embodiments, the air inlet 21 may also be provided on the first surface 11 or the third surface 13 and the fourth surface 14, which is not limited here.

[0109] In some embodiments, the ventilation assembly 2 further includes a baffle plate 28 and a drainage structure 29. Both the drainage structure 29 and the baffle plate 28 are connected to the hangar body 1 and located in the receiving cavity 17. The baffle plate 28 is adapted to guide liquid passing through the air inlet 21 or the air outlet 22 into the drainage structure 29, and the drainage structure 29 is adapted to discharge the liquid out of the receiving cavity 17.

[0110] In this way, rainwater and sand and other impurities in the external environment are blocked from the receiving cavity 17 by the baffle plate 28 and the drainage structure 29, ensuring the cleanliness of the receiving cavity 17.

[0111] In some embodiments, the drainage structure 29 is inclined downward along the direction close to the air inlet 21 or the air outlet 22, and the inclination angle β between the drainage structure 29 and the horizontal plane is ≥3°. For example, the inclination angle β between the drainage structure 29 and the horizontal plane can be 3°, 4°, 5°, 6°, 7°, 8°, 9°, 10°, etc.

[0112] In this way, the drainage structure 29 can discharge rainwater into the environment, preventing the dampness inside the containment cavity 17 from affecting the normal use of the drone 400.

[0113] Specifically, the drainage structure 29 includes an inclined plate 291 and a baffle 292. The inclined plate 291 is connected to the hangar body 1 by clips and screws, and is located at the air inlet 21 and air outlet 22 of the receiving cavity 17. The baffle 292 can be set at the end of the inclined plate 291 away from the hangar body 1. Filters 24 can be installed at the air inlet 21 and air outlet 22, and the filters 24 and the drainage structure 29 can form a drainage space 241. The inclined plate 291 is inclined downward along the direction close to the air inlet 21 or air outlet 22, and the inclination angle β of the drainage structure 29 with the horizontal plane is ≥3°. In this way, the filters 24 can provide initial waterproofing, preventing rainwater and other impurities from entering the drainage space 241. Rainwater and other impurities entering the drainage space 241 can also be blocked by the baffle 292 and flow towards the inclined plate 291, which can guide the rainwater to the external environment.

[0114] Furthermore, the ventilation assembly 2 may also include a dustproof net 293, which is installed on the hangar body 1 and extends towards the baffle 292. The baffle 292 and the dustproof net 293 can separate a drainage space 241. The drainage space 241 can be a sub-space of the receiving cavity 17. In addition, the distance between the end of the baffle 292 away from the inclined plate 291 and the inclined plate 291 is greater than the distance between the end of the water baffle 28 near the inclined plate 291 and the inclined plate 291. That is, the bottom surface of the water baffle 28 needs to be higher than the lowest point of the dustproof net 293 to prevent water from splashing directly onto the dustproof net 293 during rain or car washing, thereby entering the drone 400 hangar.

[0115] Furthermore, in this embodiment, the specific form of the filter 24 is not limited to meet different needs. In one example, the filter 24 can be a ventilation grille, which can be a combination of multiple "Z"-shaped grilles to form a louver-like structure.

[0116] Furthermore, the dustproof net 293, filter screen 24, water baffle 28, and drainage structure 29 can be connected by, but not limited to, ultrasonic welding, hot melting, etc. The sealing foam is bonded to the dustproof net 293 mounting frame using adhesive backing or coating. The dustproof net 293 is connected to the hangar main body 1 using clips, screws, or other fastening methods.

[0117] In this embodiment, the grille is designed with a self-draining structure 29, and the angle α between the grille and the horizontal plane is ≥3° to prevent water accumulation or water droplets from flowing back into the component. Simultaneously, the filter screen 24 is sealed to the hangar body 1 using sealing foam or expanding foam. Water droplets and dust enter the drainage space 241 through the filter screen 24 and are discharged through the inclined plate 291.

[0118] In some embodiments, the ventilation assembly 2 further includes a fan module 25, which is disposed in the receiving cavity 17 and located between the air outlet 22 and the landing platform of the drone 400. The fan module 25 is used to rotate to generate airflow to reduce the temperature of the receiving cavity 17. The airflow generated by the rotation of the fan module 25 is directed toward the air outlet 22.

[0119] In some embodiments, the fan module 25 is located between the air outlet 22 and the landing platform of the drone 400.

[0120] In this way, the fan module 25 can actively rotate to generate airflow to cool the drone 400, thus cooling the drone 400 even when the vehicle 300 is not moving.

[0121] Specifically, when the vehicle 300 stops, the fan in the fan module 25 near the air outlet 22 can be turned on to blow air into the housing 17, causing airflow and driving the heat around the drone 400 to be discharged to the outside through the first air inlet 211 and the second air inlet 212 through the first air guide duct 231 and the second air guide duct 232 respectively, so that the temperature of the housing 17, especially around the drone 400, can be reduced to ensure the normal operation of the drone 400.

[0122] In this embodiment, the hangar body 1 has an air inlet 21 on each side of the first surface 11 and an air outlet 22 on the second surface 12. The drone hangar 200 is aligned with the front-rear direction of the vehicle 300 and is mounted on the roof. An opening in the middle of the top of the drone hangar 200 allows the drone 400 to enter and exit. The drone 400 has a door 3 on its top that can be opened and closed. Normally, the drone 400 is stored inside the drone hangar 200 with the door 3 closed. If the temperature sensor detects that the temperature of the receiving cavity 17 is high, exceeding the charging or normal operating temperature of the drone 400, the fan in the fan module 25 starts, and the fan speed varies according to the specific temperature value for ventilation and heat dissipation.

[0123] In this embodiment, the fan module 25 blows air from the outlet 22 into the drone hangar 200, passing the drone 400 and its surroundings. The air then passes through the first air duct 231 and the second air duct 232, and through the first air inlet 211 and the second air inlet 212, carrying heat out of the housing cavity 17 and ensuring the drone 400 remains at its normal operating temperature. Of course, the fan blowing direction in this embodiment does not mean that air can only blow inwards from the housing cavity 17; it can also blow outwards from the housing cavity 17.

[0124] Furthermore, in this embodiment, the specific location of the fan module 25 and the number of fans in the fan module 25 are not limited, in order to meet different needs. In one example, the fan module 25 may include four fans.

[0125] In this embodiment, for aesthetic and active fan cooling purposes, the first air inlet 211 and the second air inlet 212 are arranged on the left and right front sides of the hangar body 1. In other embodiments, the first air inlet 211 and the second air inlet 212 can be located on the third surface 13 and the fourth surface 14, which saves the cost of two ventilation ducts.

[0126] In some embodiments, the ventilation assembly 2 further includes an air conditioning inlet 26, which is located on the bottom surface of the hangar body 1 and is adapted to connect the air conditioning system of the receiving cavity 17 and the vehicle 300.

[0127] In this way, the air conditioning inlet 26 can cooperate with the air inlet 21 or the air outlet 22 to achieve airflow, thereby cooling the housing 17.

[0128] In some embodiments, the ventilation assembly 2 further includes an air conditioning outlet 27, which is located on the bottom surface of the hangar body 1, and the air inlet 26 is adapted to connect the air conditioning system of the receiving cavity 17 and the vehicle 300 in conjunction with the air conditioning inlet 26.

[0129] Specifically, the housing 17 is connected to the air conditioning system of the vehicle 300, allowing air conditioning air to be introduced into the housing 17 for cooling. In this embodiment, to avoid excessive energy consumption due to air conditioning air being directly exhausted outside the vehicle through the air inlet 21 or air outlet 22 of the housing 17, closable covers can be installed at the air inlet 21 and air outlet 22 to seal them off. The housing 17 is equivalent to the interior space of the vehicle 300. An air conditioning air inlet 26 and an air conditioning air outlet 27 are opened at the bottom of the hangar body 1. The drone 400 is located between the air conditioning air inlet 26 and the air conditioning air outlet 27. Thus, the air conditioning air enters the housing 17 through the air conditioning air inlet 26 at the bottom of the housing 17, passes around the drone 400 in the drone hangar 200, and then is drawn back into the vehicle through the air outlet 22 at the bottom of the drone hangar 200. This method is more energy-efficient when the temperature is low.

[0130] Furthermore, the air conditioning inlet 26 and the air conditioning outlet 27 can be spaced apart along the first direction, with the air conditioning inlet 26 positioned near the air inlet 21 and the air conditioning outlet 27 positioned near the air outlet 22. In this way, during the movement of the vehicle 300, the airflow entering the receiving cavity 17 from the air conditioning inlet 26 will flow through the drone 400 and exit from the air outlet 22.

[0131] Please see Figure 9 This application provides a temperature control method for controlling the unmanned aerial vehicle hangar 200 of any of the above embodiments; or the vehicle 300 of the above embodiments. The temperature control method includes:

[0132] S1, based on the mode of the drone 400, and based on the temperature of the receiving cavity 17 and / or the battery status parameters of the drone 400, control the operating state of the ventilation component 2.

[0133] Specifically, a controller can be set up to implement the temperature control method of this application embodiment. The controller can be the vehicle controller of the vehicle 300, or it can be an independent control module located in the drone hangar 200. In the temperature control method of this application embodiment, the controller can acquire the mode of the drone 400, the temperature of the housing 17, and the battery status parameters of the drone 400 to control the working state of the ventilation component 2. In this way, the state of the drone 400 can be comprehensively judged based on the three parameters of the drone 400 mode, the temperature of the housing 17, and the battery status parameters of the drone 400, thereby achieving reasonable control of the drone 400 and ensuring that the drone 400 is always in the optimal state.

[0134] It is understood that the controller can also control the operating state of the ventilation component 2 based on the temperature of the housing 17 or the battery status parameters of the drone 400. That is, in one embodiment, the controller can control the operating state of the ventilation component 2 based on the mode of the drone 400 and the battery status parameters of the drone 400; in another embodiment, the controller can control the operating state of the ventilation component 2 based on the mode of the drone 400 and the temperature of the housing 17.

[0135] It should be noted that, in the embodiments of this application, the working state includes the speed of the fan module 25, the air conditioning power, and other states.

[0136] In this application embodiment, the mode of the drone 400, the temperature range of the receiving cavity 17, the battery power of the drone 400, the working mode of the ventilation component 2, and the battery temperature threshold of the drone 400 are not limited, so as to meet different needs.

[0137] In one implementation, the first mode of the drone 400 can be a charging mode, and the second mode of the drone 400 can be a smart mode or a standby mode.

[0138] The first temperature range of the receiving cavity 17 can be a temperature greater than 35°C, the second temperature range of the receiving cavity 17 can be a temperature greater than 25°C and less than or equal to 35°C, the third temperature range of the receiving cavity 17 can be a temperature greater than or equal to 15°C and less than or equal to 25°C, and the fourth temperature range of the receiving cavity 17 can be a temperature less than 15°C.

[0139] The first parameter threshold can be 70% battery capacity for the drone 400, and the second parameter threshold can be 50% battery capacity for the drone 400.

[0140] The ventilation component 2 operates in the first working mode, which can start the fan module 25 to operate at 100% speed; the ventilation component 2 operates in the second working mode, which can start the fan module 25 to operate at 60% speed; the ventilation component 2 operates in the third working mode, which can start the fan module 25 to operate at 30% speed.

[0141] The first temperature threshold of the drone 400 battery can be 45°C, and the second temperature threshold of the drone 400 battery can be 30°C.

[0142] Please see Figure 10 In some embodiments, if the drone 400 is in a first mode, the operating state of the ventilation assembly 2 is controlled based on the temperature of the receiving cavity 17 and / or the battery state parameters of the drone 400, including:

[0143] S11, when the receiving cavity 17 is in the first temperature range, control the ventilation assembly 2 to operate in the first operating mode.

[0144] Specifically, the first mode can be the charging mode of the drone 400. At this time, the drone 400 has a charging requirement. The charging of the drone 400's battery has higher requirements for temperature. Therefore, the embodiments of this application adjust the working state according to the mode in which the drone 400 is located in order to improve the efficiency of temperature control.

[0145] For example, when the temperature of the receiving cavity 17 is >35°C, the control fan module 25 starts the fan to operate at 100% speed.

[0146] In some embodiments, the battery status parameter includes the battery charge of the drone 400;

[0147] The operating state of the ventilation assembly 2 is controlled based on the temperature of the accommodating cavity 17 and / or the battery status parameters of the drone 400, including:

[0148] S12, when the receiving cavity 17 is in the second temperature range and the battery power of the drone 400 is greater than the first parameter threshold, control the ventilation component 2 to work in the second working mode.

[0149] S13, when the accommodating cavity 17 is in the second temperature range and the battery power of the drone 400 is less than or equal to the first parameter threshold, the ventilation component 2 is controlled to operate in the first working mode, wherein the maximum temperature of the second temperature range is less than the minimum temperature of the first temperature range, and the fan speed in the second working mode is less than the fan speed in the first working mode.

[0150] Specifically, the battery status parameters include the battery charge level of the drone 400. In this implementation, the controller can perform temperature control based on the battery charge level of the drone 400. Additionally, a temperature sensor can be installed in the housing 17, connected to the controller, thereby ensuring that the controller monitors the temperature of the housing.

[0151] For example, in step S12, when the temperature of the receiving cavity 17 is greater than 25°C and less than or equal to 35°C, and the battery power of the drone 400 is greater than 70%, the fan module 25 is controlled to start the fan at 60% speed.

[0152] In step S13, when the temperature of the accommodating cavity 17 is greater than 25°C and less than or equal to 35°C, and the battery power of the drone 400 is less than or equal to 70%, the fan module 25 is controlled to start the fan at 100% speed.

[0153] In some embodiments, battery status parameters include the battery charge and battery temperature of the drone 400;

[0154] The operating status of the ventilation assembly 2 is controlled based on the temperature of the accommodating cavity 17 and the battery status parameters of the UAV 400, including:

[0155] S14, in the third temperature range of the receiving cavity 17, monitor the battery power and battery temperature of the drone 400, wherein the maximum temperature of the third temperature range is less than the minimum temperature of the second temperature range.

[0156] S15 controls the operating status of the ventilation component 2 based on the battery level and temperature of the drone 400.

[0157] For example, in step S14, when the temperature of the receiving cavity 17 is greater than or equal to 15°C and less than or equal to 25°C, the battery power and battery temperature of the drone 400 are monitored, and then the working state of the ventilation component 2 is controlled according to the battery power and battery temperature of the drone 400.

[0158] Please see Figure 11 In some embodiments, the operating state of the ventilation assembly 2 is controlled based on the battery level and battery temperature of the drone 400, including:

[0159] S151, when the battery power of the drone 400 is less than the second parameter threshold and the battery temperature of the drone 400 is greater than the first temperature threshold, the ventilation component 2 is controlled to work in the first working mode, wherein the second parameter threshold is less than the first parameter threshold.

[0160] S152, when the battery power of the drone 400 is less than the second parameter threshold, and the battery temperature of the drone 400 is less than or equal to the first temperature threshold and greater than or equal to the second temperature threshold, the ventilation component 2 is controlled to work in the second working mode, wherein the fan speed in the second working mode is less than the fan speed in the first working mode.

[0161] S153, when the battery power of the drone 400 is less than the second parameter threshold and the battery temperature of the drone 400 is less than the second temperature threshold, the ventilation component 2 is controlled to operate in a third working mode, wherein the fan speed in the third working mode is less than the speed in the second working mode.

[0162] For example, when the receiving cavity 17 is in the third temperature range, the battery level of the drone 400 can be detected. In step S151, when the battery level of the drone 400 is less than 50% and the battery temperature of the drone 400 is greater than the first temperature threshold, the ventilation component 2 is controlled to operate in the first operating mode, that is, the fan module 25 starts the fan to operate at 100% speed.

[0163] In step S152, when the battery power of the drone 400 is less than 50% and the battery temperature of the drone 400 is less than or equal to 45°C and greater than or equal to 30°C, the ventilation component 2 is controlled to work in the second working mode, that is, the fan module 25 starts the fan to work at 60% speed.

[0164] In step S153, when the battery power of the drone 400 is less than 50% and the battery temperature of the drone 400 is less than 30°C, the ventilation component 2 is controlled to work in the third working mode, that is, the fan module 25 starts the fan to work at 30% speed.

[0165] Please see Figure 12 In some embodiments, the operating state of the ventilation assembly 2 is controlled based on the battery level and battery temperature of the drone 400, including:

[0166] S154, when the battery power of the drone 400 is greater than or equal to the second parameter threshold and less than or equal to the first parameter threshold, and the battery temperature of the drone 400 is greater than the first temperature threshold, the ventilation component 2 is controlled to work in the first working mode.

[0167] S155, when the battery power of the drone 400 is greater than or equal to the second parameter threshold and less than or equal to the first parameter threshold, and the battery temperature of the drone 400 is less than or equal to the first temperature threshold and greater than or equal to the second temperature threshold, the ventilation component 2 is controlled to work in a third working mode, wherein the fan speed in the third working mode is less than the fan speed in the first working mode.

[0168] S156, when the battery power of the drone 400 is greater than or equal to the second parameter threshold and less than or equal to the first parameter threshold, and the battery temperature of the drone 400 is less than the second temperature threshold, the ventilation component 2 is controlled to stop working.

[0169] For example, when the receiving cavity 17 is in the third temperature range, the battery level of the drone 400 can be detected. In step S154, when the battery level of the drone 400 is greater than or equal to 50% and less than or equal to 70%, and the battery temperature of the drone 400 is greater than 45°C, the ventilation component 2 is controlled to operate in the first operating mode, that is, the fan module 25 starts the fan to operate at 100% speed.

[0170] In step S155, when the battery charge of the drone 400 is greater than or equal to 50% and less than or equal to 70%, and the battery temperature of the drone 400 is less than or equal to 45°C and greater than or equal to 30°C, the ventilation component 2 is controlled to work in the third working mode, that is, the fan module 25 starts the fan to work at 30% speed.

[0171] In step S156, when the battery charge of the drone 400 is greater than or equal to 50% and less than or equal to 70%, and the battery temperature of the drone 400 is less than 30°C, the ventilation component 2 is controlled to stop working.

[0172] Please see Figure 13 In some embodiments, the operating state of the ventilation assembly 2 is controlled based on the battery level and battery temperature of the drone 400, including:

[0173] S157, when the battery power of the drone 400 is greater than the first parameter threshold and the battery temperature of the drone 400 is greater than the first temperature threshold, control the ventilation component 2 to work in the second working mode.

[0174] S158, when the battery power of the drone 400 is greater than the first parameter threshold, and the battery temperature of the drone 400 is less than or equal to the first temperature threshold and greater than or equal to the second temperature threshold, the ventilation component 2 is controlled to work in a third working mode, wherein the fan speed in the third working mode is less than the fan speed in the second working mode.

[0175] S159, when the battery power of the drone 400 is greater than the first parameter threshold and the battery temperature of the drone 400 is less than the second temperature threshold, control the ventilation component 2 to stop working.

[0176] For example, when the receiving cavity 17 is in the third temperature range, the battery level of the drone 400 can be detected. In step S157, when the battery level of the drone 400 is greater than 70% and the battery temperature of the drone 400 is greater than 45°C, the ventilation component 2 is controlled to operate in the second operating mode, that is, the fan module 25 starts the fan to operate at 60% speed.

[0177] In step S158, when the battery charge of the drone 400 is greater than 70% and the battery temperature of the drone 400 is less than or equal to 45°C and greater than or equal to 30°C, the ventilation component 2 is controlled to work in the third working mode, that is, the fan module 25 starts the fan to work at 30% speed.

[0178] In step S159, when the battery power of the drone 400 is greater than 70% and the battery temperature of the drone 400 is less than 30°C, the ventilation component 2 is controlled to stop working.

[0179] In some embodiments, controlling the operating state of the ventilation assembly 2 based on the temperature of the receiving cavity 17 and the battery state parameters of the drone 400 includes:

[0180] S16, when the receiving cavity 17 is in the fourth temperature range, control the ventilation assembly 2 to stop working.

[0181] For example, in step S16, when the temperature of the receiving cavity 17 is less than 15°C, the ventilation assembly 2 is controlled to stop working.

[0182] Please see Figure 9 In some embodiments, the control method further includes:

[0183] S2, when the drone 400 is in the second mode and the drone 400 is in the receiving cavity 17, if the battery temperature of the drone 400 is greater than the first temperature threshold, control the ventilation component 2 to work in the first working mode; otherwise, control the ventilation component 2 to stop working.

[0184] For example, in step S2, the second mode of the drone 400 can be either smart mode or standby mode, meaning that the drone 400 has no charging requirement. At this time, if the battery temperature of the drone 400 is greater than 45°C, the ventilation component 2 is controlled to operate in the first working mode, that is, the fan module 25 starts the fan at 100% speed; otherwise, the ventilation component 2 is controlled to stop working.

[0185] In one implementation, when the drone 400 is in a non-charging cooling state, the fan module 25 uses negative feedback to regulate speed and heat dissipation. When the temperature of the housing 17 exceeds a threshold, the fan is activated at 50% speed, with the temperature sensor periodically monitoring. When the temperature of the housing 17 does not drop to the threshold, the fan speed increases by 10% until it reaches its maximum speed. If the detected temperature is below the threshold, the fan periodically slows down until it reaches a minimum speed of 15%, maintains this speed for 5 minutes, and then shuts off.

[0186] This application provides an electronic device including a processor and a memory, wherein the processor is configured to execute a computer program stored in the memory to perform the temperature control method described in any of the above embodiments. The electronic device of this application embodiment can be installed on the vehicle 300 of this application embodiment.

[0187] Furthermore, embodiments of this application provide a readable storage medium storing a computer program, which, when executed by one or more processors, implements the temperature control method of any of the above embodiments.

[0188] For example, a temperature control method in which a computer program can be executed by a processor to perform the following steps:

[0189] S1, based on the mode of the drone 400, and based on the temperature of the receiving cavity 17 and / or the battery status parameters of the drone 400, control the operating state of the ventilation component 2.

[0190] In the description of this specification, specific features, structures, materials, or characteristics may be combined in any suitable manner in one or more embodiments or examples.

[0191] The above are merely specific embodiments of the present invention, but the scope of protection of the present invention is not limited thereto. Any variations or substitutions that can be easily conceived by those skilled in the art within the technical scope disclosed in the present invention should be included within the scope of protection of the present invention. Therefore, the scope of protection of the present invention should be determined by the scope of the claims.

Claims

1. An unmanned aerial vehicle hangar (200) for a vehicle (300), characterized in that, The utility model relates to a kind of unmanned aerial vehicle hangar, including: Hangar body (1), the hangar body (1) includes containing cavity (17), the containing cavity (17) is used to contain unmanned aerial vehicle (400), Ventilation assembly (2), including air inlet (21) and air outlet (22), the air inlet (21) and the air outlet (22) are located in the hangar body (1) and are spaced apart along the first direction, the air inlet (21) and the air outlet (22) are communicated containing cavity (17) and external environment, the air inlet (21) is located at windward side when the vehicle (300) travels, and the air outlet (22) is located at leeward side.

2. The drone hangar (200) according to claim 1, characterized in that The air inlet (21) and the air outlet (22) are located on both sides of the hangar body (1) along the first direction.

3. The drone hangar (200) according to claim 1, characterized in that, The ventilation assembly (2) further includes air duct (23), and the air duct (23) is arranged in the containing cavity (17) and is communicated with the air inlet (21) and the parking platform position of the unmanned aerial vehicle (400).

4. The drone hangar (200) according to claim 3, characterized in that The ventilation assembly (2) further includes filter screen (24), and the filter screen (24) is arranged on one side of the air inlet (21) close to the air duct (23).

5. The drone hangar (200) according to claim 1, characterized in that, The air inlet (21) at least includes first air inlet (211) and second air inlet (212) arranged on the hangar body (1), and the first air inlet (211) and the second air inlet (212) are symmetrically arranged about the central axis of the hangar body (1) in the first direction.

6. The drone hangar (200) according to claim 5, characterized in that The ventilation assembly (2) further includes air duct (23), and the air duct (23) at least includes first air duct (231) and second air duct (232); The first air duct (231) is arranged in the containing cavity (17) and is communicated with the first air inlet (211) and the parking platform position of the unmanned aerial vehicle (400). The second air duct (232) is arranged in the containing cavity (17) and is communicated with the second air inlet (212) and the parking platform position of the unmanned aerial vehicle (400). The first air duct (231) and the second air duct (232) are symmetrically arranged about the central axis of the hangar body (1) in the first direction.

7. The drone hangar (200) according to claim 6, characterized in that In the first direction, the first air inlet (211) and the second air inlet (212) are arranged on the front side of the hangar body (1), and the air outlet (22) is arranged on the rear side of the hangar body (1).

8. The drone hangar (200) according to claim 7, characterized in that The hangar body (1) includes first surface (11) and second surface (12) arranged oppositely along the first direction, and the hangar body (1) includes third surface (13) and fourth surface (14) arranged oppositely along the second direction, and the first surface (11) and the third surface (13) are provided with first transition surface (15), and the second surface (12) and the fourth surface (14) are provided with second transition surface (16), wherein the first direction and the second direction are perpendicular. The first air inlet (211) is formed on the first transition surface (15), the second air inlet (212) is formed on the second transition surface (16), and the air outlet (22) is formed on the fourth surface (14).

9. The drone hangar (200) according to claim 1, characterized in that, The ventilation assembly (2) further comprises a water baffle (28) and a drainage structure (29), the drainage structure (29) and the water baffle (28) are both connected to the hangar body (1) and located in the containing cavity (17), the water baffle (28) is adapted to guide liquid passing through the air inlet (21) or the air outlet (22) into the drainage structure (29), and the drainage structure (29) is adapted to guide the liquid out of the containing cavity (17).

10. The drone hangar (200) according to claim 9, characterized in that The drainage structure is inclined downward along a direction close to the air inlet (21) or the air outlet (22), and the inclination angle β of the drainage structure with respect to the horizontal plane is greater than or equal to 3°.

11. The drone hangar (200) according to claim 1, characterized in that The ventilation assembly (2) further comprises a fan module (25), the fan module (25) is arranged in the containing cavity (17), the fan module (25) is used to rotate to generate an air flow to reduce the temperature of the containing cavity (17), and the air flow generated by the rotation of the fan module (25) is directed towards the air outlet (22).

12. The drone hangar (200) according to claim 11, characterized in that The fan module (25) is located between the air outlet (22) and the parking platform of the unmanned aerial vehicle (400).

13. The drone hangar (200) of claim 1, wherein, The ventilation assembly (2) further comprises an air conditioner air inlet (26), the air conditioner air inlet (26) is arranged on the bottom surface of the hangar body (1), and the air conditioner air inlet (26) is adapted to communicate the containing cavity (17) and the air conditioning system of the vehicle (300).

14. The drone hangar (200) according to claim 13, characterized in that The ventilation assembly (2) further comprises an air conditioner air outlet (27), the air conditioner air outlet (27) is arranged on the bottom surface of the hangar body (1), and the air inlet (26) is adapted to cooperate with the air conditioner air inlet (26) to communicate the containing cavity (17) and the air conditioning system of the vehicle (300).

15. A temperature control method for controlling the drone hangar (200) according to any one of claims 1-14, characterized in that, The temperature control method comprises: According to the mode of the unmanned aerial vehicle (400) and according to the temperature of the containing cavity (17) and / or the battery state parameter of the unmanned aerial vehicle (400), the working state of the ventilation assembly (2) is controlled.

16. The temperature control method of claim 15, wherein, If the unmanned aerial vehicle (400) is in a first mode, the working state of the ventilation assembly (2) is controlled according to the temperature of the containing cavity (17) and / or the battery state parameter of the unmanned aerial vehicle (400), which comprises: When the containing cavity (17) is in a first temperature range, the ventilation assembly (2) is controlled to work in a first working mode.

17. The temperature control method of claim 16, wherein, The battery state parameter comprises the battery capacity of the unmanned aerial vehicle (400); The working state of the ventilation assembly (2) is controlled according to the temperature of the containing cavity (17) and / or the battery state parameter of the unmanned aerial vehicle (400), which comprises: When the containing cavity (17) is in a second temperature range and the battery capacity of the unmanned aerial vehicle (400) is greater than a first parameter threshold, the ventilation assembly (2) is controlled to work in a second working mode; When the accommodation cavity (17) is in a second temperature range and the battery power of the UAV (400) is less than or equal to the first parameter threshold, the ventilation assembly (2) is controlled to work in a first working mode, wherein the maximum temperature of the second temperature range is less than the minimum value of the first temperature range, and the heat dissipation efficiency of the second working mode is less than that of the first working mode.

18. The temperature control method of claim 17, wherein, The battery state parameter includes the battery power and the battery temperature of the UAV (400); The control of the working state of the ventilation assembly (2) according to the temperature of the accommodation cavity (17) and the battery state parameter of the UAV (400) includes: When the accommodation cavity (17) is in a third temperature range, the battery power and the battery temperature of the UAV (400) are monitored, wherein the maximum temperature of the third temperature range is less than the minimum value of the second temperature range; The control of the working state of the ventilation assembly (2) according to the battery power and the battery temperature of the UAV (400) includes:

19. The temperature control method of claim 18, wherein, When the battery power of the UAV (400) is less than a second parameter threshold and the battery temperature of the UAV (400) is greater than a first temperature threshold, the ventilation assembly (2) is controlled to work in a first working mode, wherein the second parameter threshold is less than the first parameter threshold; When the battery power of the UAV (400) is less than a second parameter threshold and the battery temperature of the UAV (400) is less than or equal to the first temperature threshold and greater than or equal to a second temperature threshold, the ventilation assembly (2) is controlled to work in a second working mode, wherein the heat dissipation efficiency of the second working mode is less than that of the first working mode; When the battery power of the UAV (400) is less than a second parameter threshold and the battery temperature of the UAV (400) is less than the second temperature threshold, the ventilation assembly (2) is controlled to work in a third working mode, wherein the heat dissipation efficiency of the third working mode is less than that of the second working mode. The control of the working state of the ventilation assembly (2) according to the battery power and the battery temperature of the UAV (400) includes:

20. The temperature control method of claim 18, wherein, When the battery power of the UAV (400) is greater than or equal to a second parameter threshold and less than or equal to the first parameter threshold and the battery temperature of the UAV (400) is greater than a first temperature threshold, the ventilation assembly (2) is controlled to work in a first working mode; When the battery power of the UAV (400) is greater than or equal to a second parameter threshold and less than or equal to the first parameter threshold and the battery temperature of the UAV (400) is less than or equal to the first temperature threshold and greater than or equal to a second temperature threshold, the ventilation assembly (2) is controlled to work in a third working mode, wherein the heat dissipation efficiency of the third working mode is less than that of the first working mode; ​ when the battery level of the UAV (400) is greater than or equal to the second parameter threshold and less than or equal to the first parameter threshold, and the battery temperature of the UAV (400) is less than the second temperature threshold, the ventilation assembly (2) is controlled to stop working.

21. The temperature control method of claim 18, wherein, The control of the working state of the ventilation assembly (2) according to the battery level and the battery temperature of the UAV (400) comprises: when the battery level of the UAV (400) is greater than the first parameter threshold, and the battery temperature of the UAV (400) is greater than the first temperature threshold, the ventilation assembly (2) is controlled to work in a second working mode; when the battery level of the UAV (400) is greater than the first parameter threshold, and the battery temperature of the UAV (400) is less than or equal to the first temperature threshold and greater than or equal to a second temperature threshold, the ventilation assembly (2) is controlled to work in a third working mode, wherein the heat dissipation efficiency of the third working mode is less than that of the second working mode; when the battery level of the UAV (400) is greater than the first parameter threshold, and the battery temperature of the UAV (400) is less than the second temperature threshold, the ventilation assembly (2) is controlled to stop working.

22. The temperature control method of claim 15, wherein, The control of the working state of the ventilation assembly (2) according to the temperature of the accommodation cavity (17) and the battery state parameter of the UAV (400) comprises: when the accommodation cavity (17) is in a fourth temperature range, the ventilation assembly (2) is controlled to stop working.

23. The temperature control method of claim 15, wherein, The control method further comprises: when the UAV (400) is in the second mode, and the UAV (400) is in the accommodation cavity (17), if the battery temperature of the UAV (400) is greater than the first temperature threshold, the ventilation assembly (2) is controlled to work in a first working mode; otherwise, the ventilation assembly (2) is controlled to stop working.

24. An electronic device, comprising: A computer device comprising a processor and a memory, wherein the processor is configured to execute a computer program stored in the memory to perform the temperature control method of any one of claims 15-23.

25. A readable storage medium storing a computer program, characterized in that, The computer program is configured to, when executed by one or more processors, perform the temperature control method of any one of claims 15-23.

26. A vehicle (300) characterized by The computer program is configured to, when executed by one or more processors, perform the temperature control method of any one of claims 15-23. The computer program is configured to, when executed by one or more processors, perform the temperature control method of any one of claims 15-23. The computer program is configured to, when executed by one or more processors, perform the temperature control method of any one of claims 15-23. The computer program is configured to, when executed by one or more processors, perform the temperature control method of any one of claims 15-23.

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