Flight awning battery pack convenient to disassemble and assemble

By setting up adjustable counterweights on the flying skylight battery pack, the problem of the traditional battery pack affecting the gravity balance of the drone is solved, and the gravity balance of the battery pack and the working state of the drone are achieved during flight are achieved.

CN222562852UActive Publication Date: 2025-03-04SHENZHEN TIM TECH CO LTD
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Patent Information

Application Number
CN202420990963.X
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-05-09
Publication Date
2025-03-04
Estimated Expiration
2034-05-09

AI Technical Summary

Technical Problem

The traditional flying skylight battery pack affects the gravity balance of the drone during disassembly and assembly, resulting in unstable working state during flight.

Method used

A flying skylight battery pack is designed to be easily disassembled and assembled. By setting up multiple sets of counterweight blocks on the battery pack, using structures such as columns, fixed plates and screws to adjust the center of gravity of the battery pack.

Benefits of technology

By adjusting the position of the counterweight, the gravity balance of the battery pack can be achieved, thereby ensuring the stable working state of the drone during flight.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model relates to the technical field of flying sky screen batteries, in particular to a flying sky screen battery pack convenient to disassemble and assemble, which comprises a bottom plate, four upright posts are fixedly connected onto the bottom plate, a fixing plate is fixedly connected between every two adjacent upright posts, a battery mechanism is arranged on the bottom plate, and the battery mechanism is connected with the battery mechanism. A group of baffles are fixedly connected between every two adjacent stand columns, a battery main body is arranged on the bottom plate, a plurality of fixing plates surround the battery main body, adjusting mechanisms are arranged on the stand columns, each adjusting mechanism comprises balancing weights, and one balancing weight is slidably connected between one fixing plate and one group of baffles which are close to each other. A screw rod is rotationally connected between every two adjacent stand columns, and the screw rods are in threaded connection with the interior of the balancing weight; a plurality of groups of balancing weights can be arranged on the battery pack, so that the gravity center of the whole device can be conveniently adjusted, the gravity balance of the device is ensured, and the working state of the device during flight is further ensured.
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Description

Technical Field

[0001] The utility model relates to a flying canopy battery pack, in particular to a flying canopy battery pack which is convenient to assemble and disassemble, and belongs to the technical field of flying canopy batteries. Background Art

[0002] The skylight, also known as "bright curtain", "strip curtain", "light strip screen" and "grille screen", is an LED display screen composed of many LED light strips. It is light, thin, transparent and has significant energy-saving effects. In order to further broaden the application scope of the skylight, flying skylights that are used in conjunction with drones have now appeared. The drones provide a stable bearing platform for the suspended screen; and in order to ensure the stability of the entire working process, the battery pack that is equipped on it is particularly important.

[0003] Traditional flying canopy battery packs are mostly plug-in or snap-on, which are convenient for assembly and disassembly. However, since the flying canopy battery pack is assembled on the drone, the drone's own gravity balance is very important, which will affect the actual working state of the flight. In this way, when the battery pack is inspected and replaced, the quality of batteries with different capacities or different battery materials will deviate, thereby affecting the center of gravity of the entire fuselage and ultimately affecting the working state during flight. Utility Model Content

[0004] The purpose of the utility model is to provide a flying canopy battery pack that is easy to disassemble and assemble in order to solve the above-mentioned problem. Multiple sets of counterweights can be set on the battery pack to facilitate the adjustment of the center of gravity of the entire device according to actual conditions to ensure the gravity balance of the device, and then ensure the working state of the device during flight.

[0005] The utility model achieves the above-mentioned purpose through the following technical scheme: a flying skylight battery pack that is easy to disassemble and assemble, including a base plate, a placement mechanism is provided on the base plate, the placement mechanism includes columns, four columns are fixedly connected to the base plate, a fixing plate is fixedly connected between two adjacent columns, a battery mechanism is provided on the base plate, the battery mechanism includes baffles, a group of baffles are fixedly connected between two adjacent columns, a battery body is provided on the base plate, a plurality of fixing plates surround the battery body, an adjustment mechanism is provided on the column, the adjustment mechanism includes a counterweight, a counterweight is slidably connected between a fixing plate and a group of baffles that are close to each other, a screw is rotatably connected between two adjacent columns, and the screw is threadedly connected to the inside of the counterweight.

[0006] Preferably, two side wing plates are provided on the bottom plate, and the side wing plates are trapezoidal in shape.

[0007] Preferably, the four columns are respectively arranged at the four corners of the top surface of the base plate, and the columns are L-shaped.

[0008] Preferably, the plurality of fixing plates are divided into two groups, wherein the fixing plates in one group are longer than those in the other group, and the fixing plates with the longer length are provided with heat dissipation holes.

[0009] Preferably, each group of baffles is provided with a plurality of baffles, and the plurality of baffles are linearly distributed with equal intervals.

[0010] Preferably, two partitions are provided on the bottom plate, the partitions are surrounded by a plurality of fixing plates, and the partitions are rectangular in shape.

[0011] Preferably, one end of the screw rod extends to the outside of the column and is connected to a rotating block, and the counterweight block is rectangular.

[0012] Preferably, a sliding block is fixedly connected to the counterweight block, and the sliding block is slidably connected to the inside of the fixed plate.

[0013] Preferably, a covering mechanism is provided on the column, and the covering mechanism comprises a covering body. The four columns are commonly provided with a covering body, and a buckle block is fixedly connected to the covering body.

[0014] Preferably, four clamping blocks are fixedly connected to the cover body, and a clamping groove is provided on the column.

[0015] The beneficial effects of the utility model are as follows: when in use, a single battery body can be first inserted into the inner cavity surrounded by multiple fixing plates and multiple columns, so as to facilitate the installation of the battery pack; and during use, the user can manually drive the screw to rotate according to actual conditions, and as the screw rotates, the corresponding counterweight block will be driven to move back and forth between the baffle plate and the fixing plate, and by adjusting the positions of multiple counterweight blocks, it is convenient to continuously adjust the center of gravity of the entire device, and finally achieve gravity balance, so that by arranging multiple counterweight blocks on the battery pack, it is convenient to adjust the center of gravity of the entire device according to actual conditions, so as to ensure the gravity balance of the device, and then ensure the working state of the device during flight. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0017] Figure 2 It is a structural schematic diagram of the capping mechanism of the utility model;

[0018] Figure 3 It is a schematic diagram of the connection structure of the bottom plate, side wing plates, placement mechanism, battery mechanism and adjustment mechanism of the utility model;

[0019] Figure 4 for Figure 1 A schematic diagram of the enlarged structure of part A shown;

[0020] Figure 5 for Figure 3 The enlarged structural diagram of part B is shown.

[0021] In the figure: 1. bottom plate; 2. side wing plate; 3. placement mechanism; 301. column; 302. fixing plate; 303. heat dissipation hole; 4. battery mechanism; 401. baffle; 402. partition; 403. battery body; 5. adjustment mechanism; 501. rotating block; 502. screw; 503. counterweight block; 504. slider; 6. capping mechanism; 601. capping body; 602. buckle block; 603. clamping block; 604. clamping slot. DETAILED DESCRIPTION

[0022] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0023] See also Figure 1-5 As shown, a flying canopy battery pack that is easy to disassemble and assemble comprises a base plate 1, a placement mechanism 3 is provided on the base plate 1, the placement mechanism 3 comprises columns 301, four columns 301 are fixedly connected to the base plate 1, a fixing plate 302 is fixedly connected between two adjacent columns 301, a battery mechanism 4 is provided on the base plate 1, the battery mechanism 4 comprises a baffle 401, a group of baffles 401 are fixedly connected between two adjacent columns 301, a battery body 403 is provided on the base plate 1, a plurality of the fixing plates 302 surround the battery body 403, an adjustment mechanism 5 is provided on the column 301, the adjustment mechanism 5 comprises a counterweight 503, a counterweight 503 is slidably connected between a fixing plate 302 and a group of baffles 401 that are close to each other, a screw 502 is rotatably connected between two adjacent columns 301, and the screw 502 is threadedly connected to the inside of the counterweight 503.

[0024] As a technical optimization solution of the utility model, two side wing plates 2 are provided on the bottom plate 1, and the side wing plates 2 are trapezoidal in shape. The side wing plates 2 further facilitate the assembly of the entire battery pack.

[0025] As a technical optimization scheme of the utility model, the four columns 301 are respectively arranged at the four corners of the top surface of the base plate 1, and the columns 301 are L-shaped, in order to facilitate the fixed connection of the fixing plate 302; the multiple fixing plates 302 are divided into two groups, and the length of one group of fixing plates 302 is longer than that of the other group, in order to facilitate the installation of multiple battery bodies 403, and the longer fixing plates 302 are provided with heat dissipation holes 303, in order to facilitate the dissipation of heat generated by the battery body 403 when working.

[0026] As a technical optimization solution of the utility model, each group of baffles 401 is provided with a plurality of pieces, and the plurality of baffles 401 are linearly distributed with equal intervals, in order to facilitate better limiting and guiding the counterweight block 503; two partitions 402 are provided on the bottom plate 1, and the partitions 402 are surrounded by a plurality of fixed plates 302, and the partitions 402 are rectangular, in order to facilitate the separation of the placement space of the battery body 403.

[0027] As a technical optimization solution of the utility model, one end of the screw rod 502 extends to the outside of the column 301 and is connected to a rotating block 501, in order to facilitate manual operation of the screw rod 502; the counterweight block 503 is rectangular, and in order to facilitate adjustment of the counterweight block 503, a slider 504 is fixedly connected to the counterweight block 503, and the slider 504 is slidably connected to the inside of the fixed plate 302, in order to further play a role of limiting and guiding the counterweight block 503.

[0028] As a technical optimization solution of the utility model, a covering mechanism 6 is provided on the column 301, and the covering mechanism 6 includes a covering body 601. The four columns 301 are jointly provided with a covering body 601, and a buckle block 602 is fixedly connected to the covering body 601. Four clamping blocks 603 are fixedly connected to the covering body 601. A clamping slot 604 is provided on the column 301. When in use, the clamping block 603 can be buckled into the inside of the clamping slot 604 to facilitate the installation and closure of the covering body 601, and the buckle block 602 can be used to facilitate the disassembly of the covering body 601.

[0029] When the utility model is used, first, the whole device is installed on the corresponding parts of the flying canopy and the UAV through the bottom plate 1 and the side wing plate 2; the user can first open the cover body 601 through the buckle block 602, and then insert the single battery body 403 into the inner cavity surrounded by the multiple fixing plates 302 and the multiple columns 301, so as to facilitate the installation of the battery pack; and during use, the user can manually hold the corresponding rotating block 501 and rotate it according to the actual situation, and the rotating block 501 rotates to drive the screw rod 502 to rotate together, and as the screw rod 502 rotates, the rotating block 501 rotates to drive the screw rod 502 to rotate together, and the screw rod 502 rotates to drive the screw rod 502 to rotate together. The rotation of 02 will drive the corresponding counterweight block 503 to move back and forth between the baffle plate 401 and the fixed plate 302. By adjusting the positions of multiple counterweight blocks 503, it is convenient to continuously adjust the center of gravity of the entire device to ultimately achieve gravity balance. By arranging multiple counterweight blocks 503 on the battery pack, it is convenient to adjust the center of gravity of the entire device according to actual conditions to ensure the gravity balance of the device, thereby ensuring the working state of the device during flight; in addition, through the heat dissipation holes 303, it is convenient to dissipate the heat generated by the battery pack when it is working.

[0030] It is obvious to those skilled in the art that the present invention is not limited to the details of the exemplary embodiments described above, and that the present invention can be implemented in other specific forms without departing from the spirit or essential features of the present invention. Therefore, the embodiments should be regarded as exemplary and non-restrictive from any point of view, and the scope of the present invention is defined by the appended claims rather than the above description, and it is intended that all changes falling within the meaning and scope of the equivalent elements of the claims be included in the present invention. Any reference numeral in a claim should not be regarded as limiting the claim to which it relates.

[0031] In addition, it should be understood that although the present specification is described according to implementation modes, not every implementation mode contains only one independent technical solution. This description of the specification is only for the sake of clarity. Those skilled in the art should regard the specification as a whole. The technical solutions in each embodiment may also be appropriately combined to form other implementation modes that can be understood by those skilled in the art.

Claims

1. A flying canopy battery pack that is easy to disassemble and assemble, comprising a bottom plate (1), characterized in that: The bottom plate (1) is provided with a placement mechanism (3), the placement mechanism (3) comprising a column (301), four columns (301) are fixedly connected to the bottom plate (1), a fixing plate (302) is fixedly connected between two adjacent columns (301), a battery mechanism (4) is provided on the bottom plate (1), the battery mechanism (4) comprises a baffle (401), a group of baffles (401) are fixedly connected between two adjacent columns (301), and a battery mechanism (4) is provided on the bottom plate (1). The battery body (403) is provided with a plurality of fixing plates (302) surrounding the battery body (403); an adjusting mechanism (5) is provided on the column (301); the adjusting mechanism (5) comprises a counterweight (503); a counterweight (503) is slidably connected between each of the fixing plates (302) and a group of baffles (401) adjacent to each other; a screw rod (502) is rotatably connected between each of two adjacent columns (301); the screw rod (502) is threadedly connected to the inside of the counterweight (503).

2. The flying canopy battery pack that is easy to disassemble and assemble according to claim 1, characterized in that: Two side wing plates (2) are arranged on the bottom plate (1), and the side wing plates (2) are in a trapezoidal shape.

3. The flying canopy battery pack that is easy to disassemble and assemble according to claim 1 is characterized in that: The four upright posts (301) are respectively arranged at the four corners of the top surface of the bottom plate (1), and the upright posts (301) are L-shaped.

4. The flying canopy battery pack that is easy to disassemble and assemble according to claim 3 is characterized by: The plurality of fixing plates (302) are divided into two groups, wherein the fixing plates (302) in one group are longer than those in the other group, and the fixing plates (302) with the longer length are provided with heat dissipation holes (303).

5. The flying canopy battery pack that is easy to disassemble and assemble according to claim 1, characterized in that: Each group of baffles (401) is provided with a plurality of baffles, and the plurality of baffles (401) are linearly distributed at equal intervals.

6. The flying canopy battery pack that is easy to disassemble and assemble according to claim 5, characterized in that: Two partitions (402) are provided on the bottom plate (1), the partitions (402) are surrounded by a plurality of fixed plates (302), and the partitions (402) are rectangular in shape.

7. The flying canopy battery pack that is easy to disassemble and assemble according to claim 1, characterized in that: One end of the screw rod (502) extends to the outside of the column (301) and is connected to the rotating block (501), and the counterweight block (503) is rectangular.

8. The flying canopy battery pack that is easy to disassemble and assemble according to claim 1, characterized in that: The counterweight block (503) is fixedly connected with a slider (504), and the slider (504) is slidably connected to the inside of the fixed plate (302).

9. The flying canopy battery pack that is easy to disassemble and assemble according to claim 1, characterized in that: The pillar (301) is provided with a sealing mechanism (6), and the sealing mechanism (6) comprises a sealing body (601). The four pillars (301) are provided with a sealing body (601) in common, and a buckle block (602) is fixedly connected to the sealing body (601).

10. The flying canopy battery pack that is easy to disassemble and assemble according to claim 9, characterized in that: Four clamping blocks (603) are fixedly connected to the cover body (601), and a clamping slot (604) is provided on the column (301).