Battery box structure of logistics carrying unmanned aerial vehicle

Abstract

The utility model discloses a battery box structure of a logistics carrying unmanned aerial vehicle, and relates to the technical field of logistics carrying unmanned aerial vehicles, the battery box structure comprises a box body and a connecting assembly, a cover body is arranged above the box body, the connecting assembly is arranged at the bottom of the cover body, the connecting assembly comprises a fixed frame, a damper, a compression spring, a clamping plate, a rotating plate and a clamping groove, a fixing frame is fixed to the bottom of the cover body, a damper is arranged in the middle of the fixing frame, a compression spring is connected to the outer side of one end of the damper in a sleeving mode, and a clamping plate is connected to the end of the compression spring. According to the battery box structure of the logistics carrying unmanned aerial vehicle, through the arrangement of the connecting assembly, when a battery in the box body needs to be replaced, a rotating plate is conveniently buckled out and rotated to be vertical through an avoiding groove, and at the moment, a clamping plate can be pulled through the rotating plate, so that the clamping plate horizontally moves and is separated from a clamping groove in the box body; and then the rotating plate is lifted upwards, so that the clamping plate can be quickly moved out of the clamping groove, and the cover body can be disassembled.

Description

TECHNICAL FIELD

[0001] The utility model relates to the technical field of logistics carrying unmanned plane, concretely is a battery box structure of logistics carrying unmanned plane. BACKGROUND

[0002] Logistics carrying unmanned plane refers to the unmanned plane that is specially used for logistics transportation, is mainly used for realizing the circulation of entity goods from supply place to receiving place, and can stably fly in complex environment, complete the delivery task of goods, and needs to use the battery endurance when flying.

[0003] The existing unmanned plane battery box is mostly fixed or semi-fixed, when replacing the battery, needs to use screwdriver or other tools to open the shell cover, causes the problem of long overall time consumption when manually operating.

[0004] Therefore, in view of the above, the existing structure and the lack are researched and improved, and a battery box structure of logistics carrying unmanned plane is provided. UTILITY MODEL CONTENT

[0005] The utility model aims at providing a battery box structure of logistics carrying unmanned plane to solve the problems in the above background technology.

[0006] In order to achieve the above object, the utility model provides the following technical scheme: a battery box structure of logistics carrying unmanned plane, including box and connecting assembly, the top of box is provided with cover, the connecting assembly is arranged in the bottom of cover, the connecting assembly includes fixed frame, damper, compression spring, clamping plate, rotating plate and clamping groove, the bottom of cover is fixed with fixed frame, and the middle part of fixed frame is arranged with damper, one end of damper is sleeved with compression spring outside, and the end of compression spring is connected with clamping plate, the upper portion of clamping plate is rotatably connected with rotating plate, and the top of box is provided with clamping groove at both ends.

[0007] Further, the clamping plate is J-shaped, and the clamping plate is fixedly connected with the damper.

[0008] Further, the rotating plate is embedded with the cover, and the top arc of the rotating plate is matched with the top arc of the cover.

[0009] Further, the top of the box is provided with positioning hole at four ends, and the positioning hole is slidably connected with positioning column inside.

[0010] Further, the clamping plate is slidably connected with the fixed frame, and the positioning column is fixedly connected with the fixed frame.

[0011] Further, the top of the cover is symmetrically provided with an avoiding slot at both ends, and the middle of the cover is provided with a heat dissipation assembly.

[0012] Further, the heat dissipation assembly comprises a heat dissipation plate, a heat pipe and a heat conduction plate, the bottom of the heat dissipation plate is fixed with the heat pipe, and the bottom of the heat pipe is connected with the heat conduction plate.

[0013] Further, the heat pipe is rectangular, and the heat pipe is equidistantly distributed about the bottom of the heat dissipation plate.

[0014] The utility model provides a kind of battery box structure of logistics carrying unmanned plane, with following beneficial effects:

[0015] 1, the utility model is provided with, when needing to replace the battery inside box, the rotating plate is conveniently buckled out and rotated to vertical by avoiding slot, at this time, the rotating plate can pull the clamping plate, so that it is horizontally moved and separated from the clamping groove on the box, then the clamping plate is removed from the clamping groove by lifting the rotating plate, to disassemble the cover, to replace the battery inside box, and when installing, the cover is covered on the unmanned plane body, and the positioning hole and positioning column can avoid the horizontal movement of the box and the cover, then the compression spring will push the clamping plate, so that it is clamped with the box by clamping groove, to be positioned in vertical direction, so it is not necessary to lend other tools in the process of disassembly and assembly, to improve the convenience when using.

[0016] 2, the utility model is provided with heat dissipation assembly, after installing cover, the upper part of battery can be compressed by heat conduction plate, to reduce the shaking of battery, and the heat of battery is also conducted to heat conduction plate, and then conducted to heat dissipation plate by heat pipe, so that when unmanned plane is flying, the heat dissipation plate can be used to cool battery by convection heat exchange, to improve the heat dissipation performance of battery. ACCURACY

[0017] Figure 1 It is the whole three-dimensional structure schematic diagram of the utility model a kind of battery box structure of logistics carrying unmanned plane;

[0018] Figure 2 It is the cover bottom structure schematic diagram of the utility model a kind of battery box structure of logistics carrying unmanned plane;

[0019] Figure 3 It is the connection assembly partial structure schematic diagram of the utility model a kind of battery box structure of logistics carrying unmanned plane.

[0020] In the diagram: 1. Box body; 2. Cover body; 3. Connecting assembly; 301. Fixing frame; 302. Damper; 303. Compression spring; 304. Card plate; 305. Rotating plate; 306. Card slot; 4. Positioning hole; 5. Positioning post; 6. Clearance groove; 7. Heat dissipation assembly; 701. Heat dissipation plate; 702. Heat pipe; 703. Heat conduction plate. Detailed Implementation

[0021] The embodiments of this utility model will be described in further detail below with reference to the accompanying drawings and examples. The following examples are for illustrative purposes only and should not be construed as limiting the scope of this utility model.

[0022] like Figures 1 to 3 As shown, a battery box structure for a logistics transport drone includes a box body 1 and a connecting assembly 3. A cover 2 is provided on the top of the box body 1, and the connecting assembly 3 is located at the bottom of the cover 2. The connecting assembly 3 includes a fixing frame 301, a damper 302, a compression spring 303, a locking plate 304, a rotating plate 305, and a slot 306. The fixing frame 301 is fixed to the bottom of the cover 2, and the damper 302 is placed in the middle of the fixing frame 301. A compression spring 303 is sleeved on the outer side of one end of the damper 302, and the end of the compression spring 303 is connected to the locking plate 304. When the drone is flying, the damper 302 can reduce the vibration of the compression spring 303, thereby improving the stability during installation. The locking plate 304 is J-shaped and is fixedly connected to the damper 302. The compression spring 303 pushes the locking plate 304, causing it to engage with the box body 1 through the slot 306, thus positioning it in the vertical direction. A rotating plate 305 is rotatably connected to the upper part of 304. The top of the box 1 has slots 306 at both ends. By rotating the plate 305, the card plate 304 is pulled to move horizontally and separate from the slots 306 on the box 1. Then, by lifting the rotating plate 305, the card plate 304 can be quickly removed from the slots 306 to disassemble the cover 2, so as to facilitate the replacement of the battery inside the box 1. The rotating plate 305 fits into the cover 2, and the top curvature of the rotating plate 305 matches the top curvature of the cover 2, so that the top of the rotating plate 305 is flush with the top of the cover 2, reducing wind resistance during flight. The top of the box 1 has positioning holes 4 at four ends, and positioning posts 5 are slidably connected inside the positioning holes 4. The card plate 304 is slidably connected to the fixing frame 301, and the positioning posts 5 are fixedly connected to the fixing frame 301. After the cover 2 is placed on the drone body, the positioning holes 4 and positioning posts 5 can prevent the box 1 and the cover 2 from moving horizontally.

[0023] like Figure 1 and Figure 2As shown, the top two ends of the cover body 2 are symmetrically provided with avoiding grooves 6, and the middle part of the cover body 2 is provided with a heat dissipation assembly 7, which is convenient to buckle out the rotating plate 305 and rotate to vertical, the heat dissipation assembly 7 comprises a heat dissipation plate 701, a heat pipe 702 and a heat conduction plate 703, the bottom of the heat dissipation plate 701 is fixedly provided with the heat pipe 702, and the bottom of the heat pipe 702 is connected with the heat conduction plate 703, after the cover body 2 is installed, the heat conduction plate 703 can be used to press the upper part of the battery, which is beneficial to reduce the shaking of the battery, the heat pipe 702 is rectangular, and the heat pipe 702 is equidistantly distributed about the bottom of the heat dissipation plate 701, the heat of the battery is conducted to the heat conduction plate 703 and then conducted to the heat dissipation plate 701 through the heat pipe 702, so that when the unmanned aerial vehicle is flying, the battery can be cooled by the convection heat exchange of the heat dissipation plate 701.

[0024] In summary, the battery box structure of the logistics carrying unmanned aerial vehicle is used, first according to Figure 1 、 Figure 2 and Figure 3 The structure shown in the process of replacing the battery, the rotating plate 305 is buckled out through the avoiding groove 6 and rotated to vertical, and then the rotating plate 305 is pinched and pulled, so that the clamping plate 304 can be controlled to move horizontally and be separated from the clamping groove 306 on the box body 1, and then the rotating plate 305 is lifted to quickly remove the clamping plate 304 from the clamping groove 306 to disassemble the cover body 2, then after replacing the battery, the cover body 2 is covered on the unmanned aerial vehicle, at this time, the positioning hole 4 and the positioning column 5 can avoid the horizontal movement of the box body 1 and the cover body 2, then the compression spring 303 pushes the clamping plate 304 to make it pass through the clamping groove 306 and be clamped with the box body 1, so that the vertical direction can be positioned, then the rotating plate 305 is actuated to make the top of the rotating plate 305 flush with the top of the cover body 2, so as to reduce the wind resistance during flight, and after the cover body 2 is installed, the heat conduction plate 703 can be used to press the upper part of the battery, finally, when the unmanned aerial vehicle is flying, the damper 302 can reduce the vibration of the compression spring 303, and the heat of the battery is conducted to the heat conduction plate 703 and then conducted to the heat dissipation plate 701 through the heat pipe 702, so that when the unmanned aerial vehicle is flying, the battery can be cooled by the convection heat exchange of the heat dissipation plate 701.

[0025] The embodiments of the present application are given for the purpose of illustration and description, and are not exhaustive or limit the present application to the disclosed form. Many modifications and variations will be apparent to those of ordinary skill in the art. The embodiments are chosen and described in order to better illustrate the principles and practical application of the present application, and to enable those of ordinary skill in the art to understand the present application in order to design various embodiments with various modifications for specific purposes.

Claims

1. A battery box structure of a logistics carrying drone, comprising a box body (1) and a connecting assembly (3), characterized in that, The upper portion of the box (1) is provided with a cover (2), the connecting assembly (3) is arranged at the bottom of the cover (2), the connecting assembly (3) comprises a fixed frame (301), a damper (302), a compression spring (303), a clamping plate (304), a rotating plate (305) and a clamping groove (306), the bottom of the cover (2) is fixedly provided with the fixed frame (301), the middle portion of the fixed frame (301) is arranged with the damper (302), one end of the damper (302) is sleeved with the compression spring (303) outside, the end of the compression spring (303) is connected with the clamping plate (304), the upper portion of the clamping plate (304) is rotatably connected with the rotating plate (305), and the top of the box (1) is provided with the clamping groove (306) at both ends.

2. The battery case structure of claim 1, wherein, The clamping plate (304) is J-shaped, and the clamping plate (304) is fixedly connected with the damper (302).

3. The battery box structure of claim 1, wherein, The rotating plate (305) is embedded with the cover (2), and the top curvature of the rotating plate (305) matches the top curvature of the cover (2).

4. The battery case structure of claim 1, wherein, The top of the box (1) is provided with a positioning hole (4) at four ends, and the positioning hole (4) is slidably connected with a positioning column (5) inside.

5. The battery box structure of claim 4, wherein, The clamping plate (304) is slidably connected with the fixed frame (301), and the positioning column (5) is fixedly connected with the fixed frame (301).

6. The battery case structure of claim 1, wherein, The top of the cover (2) is symmetrically provided with an avoiding groove (6) at both ends, and the middle portion of the cover (2) is provided with a heat dissipation assembly (7).

7. The battery box structure of claim 6, wherein, The heat dissipation assembly (7) comprises a heat dissipation plate (701), a heat pipe (702) and a heat conduction plate (703), the bottom of the heat dissipation plate (701) is fixedly provided with the heat pipe (702), and the bottom of the heat pipe (702) is connected with the heat conduction plate (703).

8. The battery case structure of claim 7, wherein, The heat pipe (702) is rectangular, and the heat pipe (702) is equidistantly distributed about the bottom of the heat dissipation plate (701).

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