A multi-station drone charging and testing integrated device

Abstract

This utility model relates to a multi-station drone charging and testing integrated device, belonging to the field of drone technology. It includes a device body with a heat dissipation assembly and a placement assembly. The heat dissipation assembly includes an air pump fixedly connected to the outer wall of the device body, with an output pipe fixedly connected to the air pump's outlet. A cooling pipe is provided on the inner wall of the device body, with one end of the output pipe fixedly connected to one end of the cooling pipe. The placement assembly includes an electric push rod fixedly connected to the bottom inner wall of the device body, with a spring fixedly connected to the top of the electric push rod. By incorporating the heat dissipation assembly, the drone can be cooled, thus preventing excessive heat generation during charging and avoiding potential internal short circuits, fires, or even explosions. Furthermore, reducing heat on the drone extends its battery life, thereby lowering operating costs.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, and specifically to a multi-station UAV charging and testing integrated device. Background Technology

[0002] In recent years, with the widespread application of drones in logistics delivery, power line inspection, agricultural plant protection and other fields, multi-station drone charging and testing integrated devices have become a key infrastructure for drone operation and management because they can achieve efficient charging and comprehensive testing of drone swarms.

[0003] According to the public announcement (CN222682717U), a drone charging device is disclosed. This technology discloses "a housing, multiple placement slots on the housing, a box slot on the housing, a box body disposed in the box slot, the shape of the placement slots being adapted to the drone, a control circuit being provided in the box body, multiple connecting lines corresponding to the number of placement slots being provided in the housing, the ends of the multiple connecting lines being respectively located in the multiple placement slots, the ends of the connecting lines being provided with USB Type-C interfaces that cooperate with the drone, and the connecting lines being electrically connected to the control circuit, etc., which has the technical effect of accommodating multiple drones for charging at the same time and improving charging efficiency."

[0004] However, although the aforementioned comparative documents show that multiple placement slots can accommodate multiple drones for charging simultaneously, thus improving charging efficiency, in actual use, the lithium battery and charging module generate a large amount of heat during drone charging. Under high temperatures, the electrolyte in the lithium battery decomposes rapidly, which can easily cause internal short circuits, leading to battery fires or even explosions, seriously threatening personnel and property safety. At the same time, temperature has a significant impact on the lifespan of drone batteries. Drone batteries working in high-temperature environments for a long time experience rapid performance degradation, which not only shortens battery lifespan but also significantly increases battery replacement and equipment maintenance costs during drone operation. Furthermore, the aforementioned patent documents require staff to manually place the drones into the placement slots, which affects efficiency during placement.

[0005] To address the aforementioned issues, this application proposes a multi-station drone charging and testing integrated device. Utility Model Content

[0006] This utility model addresses the technical problems existing in the prior art by providing a multi-station drone charging and testing integrated device.

[0007] The technical solution of this utility model to solve the above-mentioned technical problems is as follows: A multi-station UAV charging and testing integrated device includes a device body, a heat dissipation component and a placement component on the device body; the heat dissipation component includes an air pump fixedly connected to the outer wall of the device body, the air outlet of the air pump is fixedly connected to an output pipe, a cooling pipe is provided on the inner wall of the device body, one end of the output pipe is fixedly connected to one end of the cooling pipe, the placement component includes an electric push rod fixedly connected to the inner bottom wall of the device body, a spring is fixedly connected to the top of the electric push rod, a placement plate is fixedly connected to the top of the spring, a telescopic rod is fixedly connected to the inner bottom wall of the device body, the top of the telescopic rod is fixedly connected to the bottom of the placement plate, a sealing component is provided on the cooling pipe, and a controller is provided on the outer wall of the device body.

[0008] The sealing assembly includes a circular pipe fixedly connected to the outer wall of the cooling pipe, a guide member provided on the inner wall of the circular pipe, a connecting rod fixedly connected to the bottom of the placement plate, and a spreading rod fixedly connected to the bottom of the connecting rod. By setting the sealing assembly, the heat dissipation gas flows out from the corresponding position, thereby avoiding ineffective heat dissipation energy consumption. When heat dissipation is required, it is only turned on in the area that needs heat dissipation, reducing the power consumption and energy loss of the air pump, while reducing thermal interference between adjacent workstations and avoiding temperature crosstalk, thereby preventing the overall temperature from rising.

[0009] A magnetic plate is provided on the top of the placement plate, and a through hole is provided on the magnetic plate. By setting the magnetic plate, the drone is fixed, thereby preventing the drone from swaying when exposed to wind.

[0010] The device body has an indicator light on its top, and a protective cover is detachably connected to the top. The indicator light and protective cover allow for monitoring of the drone's charging status.

[0011] A bearing is fixedly connected to the outer wall of the connecting rod, and a fan blade is fixedly connected to the outer shaft of the bearing. By setting the bearing and the fan blade, the gas is diffused, thereby avoiding the gas from concentrating and thus avoiding affecting the heat dissipation efficiency.

[0012] A telescopic frame is fixedly connected to the bottom of the placement plate. The outer wall of the bottom of the telescopic frame fits against the outer wall of the placement plate. By setting the telescopic frame, the spring is protected, thereby avoiding the spring from being affected by external factors.

[0013] A support plate is fixedly connected to the inner bottom wall of the device body, and a soft pad is fixedly connected to the top of the support plate. The top of the soft pad is in contact with the outer wall of the cooling pipe. By setting the support plate and the soft pad, the cooling pipe is further supported, thereby preventing shaking when there is gas flowing inside the cooling pipe.

[0014] The beneficial effects of this utility model are:

[0015] By incorporating heat dissipation components, the drone can be cooled down, thus preventing excessive heat generation during charging and avoiding potential internal short circuits, fires, or even explosions. Reducing heat on the drone also extends battery life, thereby lowering operating costs.

[0016] By setting up sealing components, the heat dissipation gas flows out from the corresponding location, thereby avoiding ineffective heat dissipation energy consumption. When heat dissipation is needed, it is only turned on in the area that needs heat dissipation, reducing the power consumption and energy loss of the air pump, while reducing thermal interference between adjacent workstations and avoiding temperature crosstalk, thus preventing the overall temperature from rising. Attached Figure Description

[0017] Figure 1 This is a schematic diagram illustrating the overall structure of this utility model;

[0018] Figure 2 This utility model is a schematic diagram showing the structure of the protective plate and its related parts;

[0019] Figure 3 This utility model is a schematic diagram illustrating the structure of an electric linear actuator and its related parts;

[0020] Figure 4 This utility model is a schematic diagram illustrating the structure of a circular tube and its related parts.

[0021] The attached diagram lists the components represented by each number as follows:

[0022] 1. Device body;

[0023] 2. Heat dissipation components; 201. Air pump; 202. Output pipe; 203. Cooling pipe;

[0024] 3. Placement components; 301. Electric actuator; 302. Spring; 303. Placement plate; 304. Telescopic rod;

[0025] 4. Sealing assembly; 401. Round tube; 402. Guide component; 403. Connecting rod; 404. Spreading rod;

[0026] 5. Controller; 6. Magnetic plate; 7. Signal light; 8. Protective plate; 9. Bearing; 10. Fan blade; 11. Telescopic frame; 12. Support plate; 13. Soft pad. Detailed Implementation

[0027] The technical solutions of the embodiments of this application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this application, and not all embodiments. Based on the embodiments of this application, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of this application.

[0028] In the description of this application, 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 indicated technical features. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of the stated features. In the description of this application, "multiple" means two or more, unless otherwise explicitly specified.

[0029] In the description of this application, the term "for example" is used to mean "used as an example, illustration, or description." Any embodiment described as "for example" in this application is not necessarily to be construed as being more preferred or advantageous than other embodiments. The following description is provided to enable any person skilled in the art to implement and use the present invention. Details are set forth in the following description for purposes of explanation. It should be understood that those skilled in the art will recognize that the present invention can be implemented without using these specific details. In other instances, well-known structures and processes will not be described in detail to avoid obscuring the description of the present invention with unnecessary detail. Therefore, the present invention is not intended to be limited to the embodiments shown, but is consistent with the broadest scope of the principles and features disclosed in this application.

[0030] Reference Figure 1-4A multi-station drone charging and testing integrated device includes a device body 1, a heat dissipation component 2 for heat dissipation, and a placement component 3 for convenient drone placement. The heat dissipation component 2 includes an air pump 201 fixedly connected to the outer wall of the device body 1, with an output pipe 202 fixedly connected to the air outlet of the air pump 201. The air pump 201 can blow air into the output pipe 202. A cooling pipe 203 is provided on the inner wall of the device body 1, and the output pipe 202 delivers gas into the cooling pipe 203, thereby achieving heat dissipation for the drone. One end of the output pipe 202 is fixedly connected to one end of the cooling pipe 203. The placement component 3 includes an electric push rod 301 fixedly connected to the inner bottom wall of the device body 1. The electric push rod 301 can extend and retract. A spring 302 is fixedly connected to the top of the electric push rod 301. The electric push rod 301 can drive the spring 302 to extend and retract. A placement plate 303 is fixedly connected to the top of the spring 302. The spring 302 is used to realize the extension and retraction of the placement plate 303. The placement plate 303 is used to place the drone. A telescopic rod 304 is fixedly connected to the inner bottom wall of the device body 1. The telescopic rod 304 is used to limit the placement plate 303 and prevent the telescopic rod 304 from shaking. The top of the telescopic rod 304 is fixedly connected to the bottom of the placement plate 303. A sealing component 4 is provided on the cooling pipe 203. The sealing component 4 is used to realize the release of gas at the top. A controller 5 is provided on the outer wall of the device body 1. The controller 5 is used to control multiple components.

[0031] Reference Figure 4 The sealing component 4 includes a circular tube 401 fixedly connected to the outer wall of the cooling pipe 203. The circular tube 401 facilitates the outflow of gas inside the cooling pipe 203. A guide 402 is provided on the inner wall of the circular tube 401. The guide 402 is made of rubber. A connecting rod 403 is fixedly connected to the bottom of the placement plate 303. A spreading rod 404 is fixedly connected to the bottom of the connecting rod 403. The connecting rod 403 is used to fix the connecting rod 403. The number of spreading rods 404 is the same as the number of petals of the guide 402.

[0032] Reference Figure 2 and Figure 3 A magnetic plate 6 is provided on the top of the placement plate 303. The magnetic plate 6 is used to fix the drone and prevent the drone from shaking when it is exposed to wind. The magnetic plate 6 has through holes that are connected to the through holes on the placement plate 303 to facilitate the outflow of gas.

[0033] Reference Figure 2 and Figure 3 The top of the device body 1 is equipped with a signal light 7, which allows staff to easily observe the charging status of the drone. A protective plate 8 is detachably connected to the top of the device body 1 to protect the signal light 7.

[0034] Reference Figure 4 A bearing 9 is fixedly connected to the outer wall of the connecting rod 403. The bearing 9 is located at the top of the connecting rod 403. A fan blade 10 is fixedly connected to the outer shaft of the bearing 9. The rotation of the fan blade 10 can diffuse the gas, thereby increasing the heat dissipation efficiency.

[0035] Reference Figure 3 The bottom of the placement plate 303 is fixedly connected to a telescopic frame 11. The telescopic frame 11 has two sections, which are slidably connected. The bottom outer wall of the telescopic frame 11 fits against the outer wall of the placement plate 303. The telescopic frame 11 is used to protect the spring 302.

[0036] Reference Figure 3 A support plate 12 is fixedly connected to the inner bottom wall of the device body 1. The support plate 12 is used to support the cooling pipe 203. A soft pad 13 is fixedly connected to the top of the support plate 12. The soft pad 13 is used to protect the cooling pipe 203. The top of the soft pad 13 is in contact with the outer wall of the cooling pipe 203. The cooperation of the support plate 12 and the soft pad 13 can further support the cooling pipe 203.

[0037] Working principle:

[0038] This multi-station drone charging and testing integrated device allows the drone to be placed on the placement plate 303 when charging or testing is required. After the drone is placed, the testing or charging cable is connected to the drone. After the drone is placed, the placement plate 303 can be moved down by the electric push rod 301. When the placement plate 303 moves down, it will drive the connecting rod 403 and the spreading rod 404 to move. After the spreading rod 404 moves, it will open the guide member 402. After the guide member 402 is opened, the operator can use the air pump 201 to ventilate the cooling pipe 203 and the output pipe 202 to dissipate heat from the drone and avoid heat accumulation and damage.

[0039] Although preferred embodiments of the present invention have been described, those skilled in the art, upon learning the basic inventive concept, can make other changes and modifications to these embodiments. Therefore, the appended claims are intended to be interpreted as including the preferred embodiments as well as all changes and modifications falling within the scope of the present invention.

[0040] Obviously, those skilled in the art can make various modifications and variations to this utility model without departing from its spirit and scope. Therefore, if these modifications and variations fall within the scope of the claims of this utility model and their equivalents, this utility model also intends to include these modifications and variations.

Claims

1. A multi-station UAV charging and testing integrated device, comprising a device body (1), characterized in that, The device body (1) is provided with a heat dissipation component (2) and a placement component (3). The heat dissipation component (2) includes an air pump (201) fixedly connected to the outer wall of the device body (1), the air outlet of the air pump (201) is fixedly connected to an output pipe (202), a cooling pipe (203) is provided on the inner wall of the device body (1), one end of the output pipe (202) is fixedly connected to one end of the cooling pipe (203), the placement component (3) includes an electric push rod (301) fixedly connected to the inner bottom wall of the device body (1), a spring (302) is fixedly connected to the top of the electric push rod (301), a placement plate (303) is fixedly connected to the top of the spring (302), a telescopic rod (304) is fixedly connected to the inner bottom wall of the device body (1), the top of the telescopic rod (304) is fixedly connected to the bottom of the placement plate (303), a sealing component (4) is provided on the cooling pipe (203), and a controller (5) is provided on the outer wall of the device body (1).

2. The multi-station UAV charging and testing integrated device according to claim 1, characterized in that, The sealing assembly (4) includes a cooling pipe (203) with a circular pipe (401) fixedly connected to its outer wall. The inner wall of the circular pipe (401) is provided with a guide (402). The bottom of the placement plate (303) is fixedly connected with a connecting rod (403), and the bottom of the connecting rod (403) is fixedly connected with a spreading rod (404).

3. The multi-station UAV charging and testing integrated device according to claim 1, characterized in that, A magnetic plate (6) is provided on the top of the placement plate (303), and a through hole is provided on the magnetic plate (6).

4. The multi-station UAV charging and testing integrated device according to claim 1, characterized in that, The device body (1) is provided with a signal light (7) on the top, and a protective plate (8) is detachably connected to the top of the device body (1).

5. The multi-station UAV charging and testing integrated device according to claim 2, characterized in that, The outer wall of the connecting rod (403) is fixedly connected to a bearing (9), and a fan blade (10) is fixedly connected to the outer shaft of the bearing (9).

6. The multi-station UAV charging and testing integrated device according to claim 1, characterized in that, The bottom of the placement plate (303) is fixedly connected to a telescopic frame (11), and the bottom outer wall of the telescopic frame (11) is in contact with the outer wall of the placement plate (303).

7. The multi-station UAV charging and testing integrated device according to claim 1, characterized in that, A support plate (12) is fixedly connected to the inner bottom wall of the device body (1), and a soft pad (13) is fixedly connected to the top of the support plate (12). The top of the soft pad (13) is in contact with the outer wall of the cooling pipe (203).

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