Temperature adjusting device of unmanned aerial vehicle nest
By installing a liftable landing platform and an air conditioning system inside the drone nest, and using axial flow fans and air ducts to directly regulate the drone battery temperature, the difficulties of charging and taking off drones at different temperatures are solved, and rapid adaptation of battery status is achieved.
Patent Information
- Application Number
- CN202520061269.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-01-10
- Publication Date
- 2026-01-06
- Estimated Expiration
- 2035-01-10
AI Technical Summary
Drones may experience difficulties charging or taking off due to unsuitable battery temperatures under varying external temperature conditions.
A liftable landing platform and air conditioning system are installed inside the drone nest. Axial fans and air ducts are used to blow hot and cold air directly onto the drone battery. Temperature sensors monitor the external temperature and control the air conditioning output mode.
It enables drone batteries to quickly adjust to a suitable state under different temperature conditions, ensuring smooth charging and takeoff.
Smart Images

Figure CN223764737U_ABST
Abstract
Description
Technical Field
[0001] This patent application relates to the field of hangar technology, and in particular to a temperature regulation device for an unmanned aerial vehicle (UAV) hangar. Background Technology
[0002] Mobile drone nests are becoming increasingly common, with drones landing in these nests to charge. When outdoor temperatures are high, the battery temperature is also high, requiring the drone battery to cool to room temperature before charging. Conversely, when outdoor temperatures are low, the drone battery temperature is also low, requiring it to self-heat to a certain temperature before takeoff. Therefore, we propose a temperature regulation device for drone nests. Utility Model Content
[0003] In view of the shortcomings of the prior art described above, the purpose of this patent application is to provide a temperature regulation device for unmanned aerial vehicle (UAV) nests to solve the problems of the prior art.
[0004] To achieve the above objectives, this utility model provides the following technical solution:
[0005] A temperature regulation device for a drone pod includes a pod body with a liftable landing platform inside. The landing platform is used to carry drones. An air conditioner is installed on the inner bottom wall of the pod body. The air outlet of the air conditioner is connected to an air duct. The top of the air duct is located directly below the landing platform. The lower end of the landing platform has a through hole that connects to the top of the air duct when the landing platform descends after carrying the drone. The air conditioner is used to regulate the temperature of the drone battery after it is activated.
[0006] Preferably, an axial flow fan is installed at the lower end of the landing platform, and the axial flow fan and the through hole are located on the same vertical line.
[0007] Preferably, the axial fan is fixed to the lower end of the landing platform by a fan bracket.
[0008] Preferably, the air duct includes an inclined section whose lower end is connected to the air outlet, and an integrally connected vertical section at the upper end of the inclined section that is located on the same vertical line as the axial fan.
[0009] Preferably, the cross-section of the air duct is rectangular.
[0010] Preferably, the air inlet of the air conditioner extends toward the side wall of the housing body and communicates with the outside of the housing body.
[0011] Preferably, a temperature sensor for monitoring the external temperature is installed on the outer wall of the nest body.
[0012] Compared with the prior art, the beneficial effects of this utility model are: the temperature regulation device for the drone nest proposed in this application, when the drone lands on the landing platform, the drone returns to center, the landing platform descends, the top of the air duct is in contact with the axial fan, the air conditioner blows cold air and hot air according to the outdoor temperature, and blows the air onto the drone battery through the axial fan, so that the drone battery cools down quickly and reaches a state where it can take off or be charged. Attached Figure Description
[0013] Figure 1 This is a three-dimensional structural diagram of the present invention;
[0014] Figure 2 This is a front view structural diagram of the hangar of this utility model;
[0015] Figure 3 This is a schematic diagram of the assembly structure of the landing platform and axial fan of this utility model;
[0016] Figure 4 This is a schematic diagram of the internal air conditioning and air duct installation structure of the machine nest body of this utility model.
[0017] The following are the reference numerals: 1. Air conditioner housing body; 2. Air landing platform; 21. Through hole; 3. Air conditioner; 31. Air outlet; 32. Air inlet; 4. Air duct; 5. Axial fan; 51. Fan bracket; 6. Temperature sensor. Detailed Implementation
[0018] The following specific examples illustrate the implementation of this patent application. Those skilled in the art can easily understand other advantages and effects of this patent application from the content disclosed in this specification. This patent application can also be implemented or applied through other different specific embodiments, and the details in this specification can also be modified or changed based on different viewpoints and applications without departing from the spirit of this patent application. It should be noted that, unless otherwise specified, the embodiments and features in the embodiments of this application can be combined with each other.
[0019] Please see Figure 1-4 This utility model provides a technical solution:
[0020] A temperature regulation device for a drone nest, such as Figure 1 and Figure 2 As shown, the device includes a nest body 1, and a liftable landing platform 2 is provided inside the nest body 1. The landing platform 2 is used to carry the drone. A through hole 21 is provided on the landing platform 2. An axial flow fan 5 is installed at the lower end of the landing platform 2 through a fan bracket 51, and the axial flow fan 5 and the through hole 21 are located on the same vertical line.
[0021] It should be noted that a lifting assembly is installed inside the main body 1 of the aircraft nest, and the landing platform 2 is installed at the lifting end of the lifting assembly. In this application, the lifting assembly is not a technical solution to solve the technical problem, and the lifting assembly is obvious to those skilled in the art, so it will not be described in detail here.
[0022] like Figure 2 and Figure 4 As shown, an air conditioner 3 is installed on the inner bottom wall of the drone housing 1. The air inlet 32 of the air conditioner 3 faces one side of the drone housing 1 and leads to the outside of the drone housing 1, communicating with the outside. The air outlet 31 of the air conditioner 3 is connected to the air duct 4. The top of the air duct 4 is located directly below the through hole 21. When the landing platform 2 carries the drone and descends to the lowest point, the air duct 4 is aligned with the axial fan 5. After the air conditioner 3 is turned on, it is used to regulate the temperature of the drone battery.
[0023] In some examples, such as Figure 4 As shown, the air duct 4 includes an inclined section and an integrated vertical section connected to the upper end of the inclined section. The lower end of the inclined section is connected to the air outlet 31 of the air conditioner 3. The vertical section and the through hole 21 are located on the same vertical line. Specifically, as shown... Figure 2 As shown, the cross-section of the air duct 4 is rectangular. It should be noted that the rectangular structure is only one form of the air duct 4; the cross-section of the air duct 4 can also be circular.
[0024] As a preferred embodiment of this case, see Figure 4 A temperature sensor 6 is installed on the outer wall of the nest body 1 to monitor the external temperature of the nest body 1. When the external temperature is high, the air conditioner 3 blows cold air, and vice versa.
[0025] After the drone lands on landing platform 2, the drone returns to center, landing platform 2 descends, the top of air duct 4 comes into contact with axial fan 5, and air conditioner 3 blows cold and hot air according to the outdoor temperature, and blows it to the drone battery through axial fan 5, so that the drone battery can be cooled down quickly and reach a state where it can take off or be charged.
[0026] The above embodiments are merely illustrative of the principles and effects of this patent application and are not intended to limit this patent application. Any person skilled in the art may modify or alter the above embodiments without departing from the spirit and scope of this patent application. Therefore, all equivalent modifications or alterations made by those skilled in the art without departing from the spirit and technical concept disclosed in this patent application shall still be covered by the claims of this patent application.
Claims
1. A temperature regulating device for a drone nest, comprising a nest body (1), a landing platform (2) is arranged in the nest body (1) and can be lifted, the landing platform (2) is used to carry a drone, characterized in that, The inner bottom wall of the nest body (1) is provided with an air conditioner (3), an air outlet (31) of the air conditioner (3) is communicated with an air duct (4), a top of the air duct (4) is located directly below the landing platform (2), a lower end of the landing platform (2) is provided with a through hole (21) which is communicated with the top of the air duct (4) when the landing platform (2) bears the unmanned aerial vehicle and descends, and the air conditioner (3) is used for temperature adjustment of the unmanned aerial vehicle battery after being started.
2. The temperature regulating apparatus of a drone nest according to claim 1, wherein, An axial flow fan (5) is mounted at the lower end of the landing platform (2), and the axial flow fan (5) is located on the same vertical line as the through hole (21).
3. The temperature regulating apparatus of a drone nest according to claim 2, wherein, The axial flow fan (5) is fixed to the lower end of the landing platform (2) through a fan support (51).
4. The temperature regulating apparatus of a drone nest according to claim 2, wherein, The air duct (4) comprises an inclined section which is communicated with the air outlet (31) at the lower end, and an integral vertical section which is communicated with the axial flow fan (5) at the upper end of the inclined section and is located on the same vertical line as the axial flow fan (5).
5. The temperature regulating apparatus of a drone nest according to claim 4, wherein, The cross section of the air duct (4) is in a rectangular structure.
6. The temperature regulating apparatus of a drone nest according to claim 1, wherein, The air inlet (32) of the air conditioner (3) extends to the side wall of the nest body (1) and is communicated with the outside of the nest body (1).
7. The temperature regulating apparatus of a drone nest according to claim 1, wherein, A temperature sensor (6) for monitoring the outside temperature is mounted on the outer side wall of the nest body (1).