Battery compartment integrated structure and six-rotor unmanned aerial vehicle integrated frame

Abstract

The application provides a battery compartment integrated structure and a six-rotor unmanned aerial vehicle integrated frame, and belongs to the technical field of unmanned aerial vehicles. The battery compartment integrated structure comprises a frame, and a battery compartment body is installed on the frame. By installing the battery compartment body on the frame, U-shaped tracks are installed on the side walls at both ends of the battery compartment body, the battery body is inserted into the battery compartment body, sliders are installed on the side walls at both ends of the battery body, the two sliders are connected with the two U-shaped tracks respectively, a graphene heat conduction layer is installed on the top and the bottom of the battery compartment body, the graphene heat conduction layer is in contact with the battery body to absorb the heat generated by the battery body, the first and second heat dissipation holes are communicated with the bottom of the battery compartment body, thereby realizing heat dissipation inside the battery compartment body, and in addition, battery contact points in contact with the battery body interface are installed on the inner wall of the battery compartment body, so that the integrated structure inside the battery compartment body is realized, and the effects of quick disassembly and good heat dissipation inside the battery compartment body are achieved.

Description

Technical Field

[0001] This application relates to the field of unmanned aerial vehicles (UAVs), and more specifically, to a battery compartment integrated structure and an integrated frame for a six-rotor UAV. Background Technology

[0002] Unmanned aerial vehicles (UAVs) are devices operated using radio remote control equipment and onboard program control devices, or operated autonomously by an onboard computer, either completely or intermittently. Hexacopter UAVs are widely used in fields such as power, forestry, and surveying. Hexacopter UAVs have a battery compartment inside, and the batteries are installed in the battery compartment. However, the existing battery compartment is not convenient to install and remove. At the same time, the battery generates heat when it is powered during the operation of the UAV, and the existing battery compartment has low heat dissipation efficiency. To address these issues, we propose an integrated battery compartment structure and an integrated frame for hexacopter UAVs. Utility Model Content

[0003] To overcome the above shortcomings, this application provides an integrated battery compartment structure and an integrated frame for a six-rotor drone, aiming to improve the problem of poor battery heat dissipation in existing drone battery compartment structures.

[0004] In a first aspect, embodiments of this application provide a battery compartment integrated structure, including a frame body, a battery compartment body mounted on the frame body, a battery body inserted into the battery compartment body, a heat dissipation channel formed between the battery body and the battery compartment body, and a heat dissipation hole group formed between the top of the frame body and the top of the battery compartment body, the heat dissipation hole group communicating with the heat dissipation channel.

[0005] In one specific implementation, U-shaped tracks are fixedly installed on both ends of the battery compartment, and sliders are fixedly installed on both ends of the battery body. The two sliders are respectively slidably disposed within the two U-shaped tracks.

[0006] In one specific implementation, graphene thermal conductive layers are fixedly installed on the top and bottom of the battery compartment, and the top and bottom of the battery body are respectively in sliding contact with the two graphene thermal conductive layers.

[0007] In one specific implementation, each of the two U-shaped tracks has several through holes.

[0008] In one specific implementation, the heat dissipation hole group includes a plurality of first heat dissipation holes and a plurality of second heat dissipation holes. The plurality of first heat dissipation holes are disposed with the graphene thermal conductive layer below, and the plurality of second heat dissipation holes are disposed in communication with the bottom of the heat dissipation channel.

[0009] In one specific implementation, a groove is provided on the top of the battery body, and an insert block is slidably provided in the groove. The bottom of the insert block is connected to the bottom of the groove by the same spring, and the insert block is inserted into the battery compartment.

[0010] In one specific implementation, a through-hole is provided on one side wall of the groove, a connecting block is fixedly installed on one side wall of the insert block, the connecting block is disposed through the through-hole, an insertion port is provided on the top of the battery compartment, and one end of the insert block is inserted into the insertion port.

[0011] In one specific implementation, the top of the plug is sloped, and the slope faces the direction of the socket.

[0012] In one specific implementation, battery contact points are provided on the inner wall of the battery compartment, and the battery body interface is in contact with the battery contact points.

[0013] Secondly, this application also provides an integrated frame for a six-rotor unmanned aerial vehicle, including... The aforementioned integrated battery compartment structure.

[0014] The beneficial effects of this application are as follows: By installing a battery compartment on a frame, U-shaped rails are installed on the side walls at both ends of the battery compartment, the battery body is inserted into the battery compartment, and sliders are installed on the side walls at both ends of the battery body. The two sliders are connected to the two U-shaped rails respectively. Graphene thermal conductive layers are installed on the top and bottom of the battery compartment, and the graphene thermal conductive layers are in contact with the battery body to absorb the heat generated by the battery body. At the same time, the bottom of the battery compartment is connected to the first heat dissipation hole and the second heat dissipation hole, thereby realizing heat dissipation inside the battery compartment. In addition, battery contact points that contact the interface of the battery body are installed on the inner wall of the battery compartment, thereby realizing the integrated structure inside the battery compartment, achieving the effects of quick disassembly and good heat dissipation inside the battery compartment. Attached Figure Description

[0015] To more clearly illustrate the technical solutions of the embodiments of this application, the drawings used in the embodiments will be briefly introduced below. It should be understood that the following drawings only show some embodiments of this application and should not be regarded as a limitation of the scope. For those skilled in the art, other related drawings can be obtained from these drawings without creative effort.

[0016] Figure 1 This is a schematic diagram of the main structure of the battery compartment integrated structure and the integrated frame of the hexacopter UAV provided in the embodiments of this application; Figure 2 A schematic diagram of the integrated battery compartment structure and the heat dissipation hole group structure of the integrated frame of the hexacopter UAV provided for the embodiments of this application; Figure 3 A side cross-sectional view of the battery compartment integrated structure and the integrated frame of the hexacopter UAV provided for the embodiments of this application; Figure 4 A schematic diagram of the battery compartment integrated structure and the battery body disassembly structure of the integrated frame of the hexacopter UAV provided in the embodiments of this application; Figure 5 A schematic diagram of the internal structure of the battery compartment of the integrated battery compartment structure and the integrated frame of the hexacopter UAV provided for the embodiments of this application; Figure 6 for Figure 3 A magnified view of a portion of point A in the middle.

[0017] In the diagram: 10-Frame body; 110-Groove; 120-Insertion block; 130-Spring; 140-Through opening; 150-Connecting block; 20-Battery compartment; 210-U-shaped track; 220-Graphene thermal conductive layer; 230-Through hole; 240-Insertion; 30-Battery body; 310-Slider; 40-Heat dissipation channel; 50-Heat dissipation hole group; 510-First heat dissipation hole; 520-Second heat dissipation hole. Detailed Implementation

[0018] The technical solutions in the embodiments of this application will now be described with reference to the accompanying drawings.

[0019] Please see Figure 1-6 This application provides a battery compartment integrated structure, including a frame body 10, a battery compartment 20 mounted on the frame body 10, a battery body 30 inserted inside the battery compartment 20, a heat dissipation channel 40 formed between the battery body 30 and the battery compartment 20, and a heat dissipation hole group 50 opened between the top of the frame body 10 and the top of the battery compartment 20. The heat dissipation hole group 50 is connected to the heat dissipation channel 40. Specifically, the heat dissipation channel 40 is connected to the external environment through the heat dissipation hole group 50, so that during the movement of the drone, the inside of the battery compartment 20 exchanges heat with the outside through the heat dissipation hole group 50 to achieve the purpose of heat dissipation of the battery compartment 20.

[0020] See Figure 3-5U-shaped tracks 210 are fixedly installed on both end sidewalls of the battery compartment 20, and sliders 310 are fixedly installed on both end sidewalls of the battery body 30. The two sliders 310 are slidably positioned within the two U-shaped tracks 210. During installation, the U-shaped tracks 210 limit the sliders 310, thereby limiting the battery body 30 and allowing it to be inserted into the battery compartment 20. Simultaneously, there is space between the battery body 30 and the sidewalls of the battery compartment 20. Furthermore, graphene thermal conductive layers 220 are fixedly installed on the top and bottom of the battery compartment 20. The top and bottom of the battery body 30 are in sliding contact with the two graphene thermal conductive layers 220. Specifically, the graphene thermal conductive layers 220 have excellent thermal conductivity and can absorb electrical current. The battery body 30 generates heat during operation. In addition, several through holes 230 are opened on each of the two U-shaped tracks 210. The through holes 230 on the U-shaped tracks 210 allow the upper and lower spaces of the battery compartment 20 to be connected. It should be noted that the heat dissipation hole group 50 includes several first heat dissipation holes 510 and several second heat dissipation holes 520. Several first heat dissipation holes 510 are set with the lower graphene thermal conductive layer 220, and several second heat dissipation holes 520 are connected with the bottom of the heat dissipation channel 40. During the high-altitude movement of the drone, the heat absorbed by the graphene thermal conductive layer 220 can be exchanged with the outside air through the first heat dissipation holes 510, while the inside of the battery compartment 20 is connected to the external environment through the second heat dissipation holes 520 to achieve the purpose of heat dissipation inside the battery compartment 20.

[0021] See Figure 3 and 6The battery body 30 has a groove 110 on its top, and an insert 120 is slidably disposed within the groove 110. A spring 130 connects the bottom of the insert 120 to the bottom of the groove 110. The insert 120 is inserted into the battery compartment 20. Specifically, the insert 120 is inserted into the battery compartment 20 to fix the battery body 30 within the battery compartment 20. Further, a through-hole 140 is formed on one side wall of the groove 110, and a connecting block 150 is fixedly installed on one side wall of the insert 120, passing through the through-hole 140. An insertion port 240 is formed on the top of the battery compartment 20, and one end of the insert 120 is inserted into the insertion port 240. In practice, pressing down on the connecting block 150 causes the connecting block 150 to move the insert 120 downwards, causing one end of the insert 120 to exit from the insertion port 240, thus securing the battery body 30. Furthermore, the insert 120... The top of the battery compartment 20 is sloping, and the sloping surface faces the direction of the insertion port 240. When the battery body 30 is inserted into the battery compartment 20, the sloping surface of the insertion block 120 is squeezed by the front end of the battery compartment 20, causing the insertion block 120 to slide into the groove 110. At the same time, the insertion block 120 compresses the spring 130. When the insertion block 120 moves to correspond with the insertion port 240, the spring 130 drives the insertion block 120 to reset, so that the insertion block 120 is inserted into the insertion port 240, thereby fixing the battery body 30 and facilitating quick installation and removal of the battery body 30. Battery contact points are provided on the inner wall of the battery compartment 20. The interface of the battery body 30 is in contact with the battery contact points. After the battery body 30 is fixed, the interface at the end of the battery body 30 is connected to the battery contact points to connect the power. The battery contact points at the end of the battery compartment 20 are connected to the existing control system of the UAV. The specific connection structure and principle are existing technologies.

[0022] An integrated frame for a hexacopter unmanned aerial vehicle, including The aforementioned integrated battery compartment structure.

[0023] When using this integrated battery compartment structure and the integrated frame of a hexacopter drone: The battery body 30 is installed and inserted into the battery compartment 20. The slider 310 is inserted into the corresponding U-shaped track 210, thus inserting the battery body 30 into the battery compartment 20. This ensures that the end interface of the battery body 30 contacts the battery contact point at the end of the battery compartment 20. At this time, the insert block 120 is inserted into the insertion port 240 at the top of the battery compartment 20 to fix the battery body 30 inside the battery compartment 20. Simultaneously, the graphene thermal conductive layer 220 is in contact with the battery body 30. When removing the battery body 30, pressing down on the connecting block 150 releases the fixation of the battery body 30, allowing it to be pulled out easily, facilitating the installation and removal of the battery body 30.

[0024] It should be noted that the specific model and specifications of the battery compartment 20 and the battery body 30 need to be selected and determined according to the actual specifications of the device. The specific selection and calculation method adopts the existing technology in this field, so it will not be described in detail.

[0025] The power supply and principle of the battery compartment 20 and the battery body 30 are clear to those skilled in the art and will not be described in detail here.

[0026] The above description is merely an embodiment of this application and is not intended to limit the scope of protection of this application. Various modifications and variations can be made to this application by those skilled in the art. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this application should be included within the scope of protection of this application. It should be noted that similar reference numerals and letters in the following figures indicate similar items; therefore, once an item is defined in one figure, it does not need to be further defined and explained in subsequent figures.

Claims

1. A battery compartment integrated structure, characterized in that, The device includes a frame body (10), on which a battery compartment (20) is mounted. A battery body (30) is inserted into the battery compartment (20). A heat dissipation channel (40) is formed between the battery body (30) and the battery compartment (20). A heat dissipation hole group (50) is opened between the top of the frame body (10) and the battery compartment (20). The heat dissipation hole group (50) is connected to the heat dissipation channel (40).

2. The battery compartment integrated structure according to claim 1, characterized in that, U-shaped tracks (210) are fixedly installed on both ends of the battery compartment (20), and sliders (310) are fixedly installed on both ends of the battery body (30). The two sliders (310) are respectively slidably disposed in the two U-shaped tracks (210).

3. The battery compartment integrated structure according to claim 1, characterized in that, The top and bottom of the battery compartment (20) are fixedly installed with graphene thermal conductive layers (220), and the top and bottom of the battery body (30) are respectively in sliding contact with the two graphene thermal conductive layers (220).

4. The battery compartment integrated structure according to claim 2, characterized in that, Each of the two U-shaped tracks (210) has several through holes (230).

5. The battery compartment integrated structure according to claim 3, characterized in that, The heat dissipation hole group (50) includes a plurality of first heat dissipation holes (510) and a plurality of second heat dissipation holes (520). The plurality of first heat dissipation holes (510) are disposed with the graphene thermal conductive layer (220) below, and the plurality of second heat dissipation holes (520) are disposed in communication with the bottom of the heat dissipation channel (40).

6. The battery compartment integrated structure according to claim 1, characterized in that, The top of the battery body (30) is provided with a groove (110), and a plug (120) is slidably provided in the groove (110). The bottom of the plug (120) is connected to the bottom of the groove (110) by the same spring (130), and the plug (120) is inserted into the battery compartment (20).

7. The battery compartment integrated structure according to claim 6, characterized in that, A through-hole (140) is provided on one side wall of the groove (110), and a connecting block (150) is fixedly installed on one side wall of the insert (120). The connecting block (150) passes through the through-hole (140), and an insertion port (240) is provided on the top of the battery compartment (20). One end of the insert (120) is inserted into the insertion port (240).

8. The battery compartment integrated structure according to claim 7, characterized in that, The top of the plug (120) is inclined, and the inclined surface is oriented toward the direction of the socket (240).

9. The battery compartment integrated structure according to claim 1, characterized in that, The battery compartment (20) has battery contact points on its inner wall, and the interface of the battery body (30) is in contact with the battery contact points.

10. An integrated frame for a six-rotor unmanned aerial vehicle (UAV), characterized in that, include The battery compartment integrated structure according to any one of claims 1-9.

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