Quick-release replacement structure for unmanned aerial vehicle battery

CN224857162UActive Publication Date: 2026-10-16SUZHOU MINTAI AVIATION TECHNOLOGY CO LTD
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Patent Information

Application Number
CN202620082009.X
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2026-01-22
Publication Date
2026-10-16
Estimated Expiration
2036-01-22

AI Technical Summary

Technical Problem

[0004]为解决上述背景技术中提出的问题,本实用新型的目的在于提供一种无人机电池用快拆更换结构,具备了快速拆卸电池的优点,解决了无人机更换电池时存在诸多不便,需手动拧动螺丝,依赖工具且步骤复杂,非专业人员易操作失误的问题

Benefits of technology

1、本实用新型通过设置弹出组件、安装槽、定位组件、凹槽、防滑板、倒角、插接板、容纳槽、挤出块和第一弹簧,解决了无人机更换电池时存在诸多不便,需手动拧动螺丝,依赖工具且步骤复杂,非专业人员易操作失误的问题,达到了快速拆卸电池的效果。

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Abstract

The utility model discloses a kind of quick detach replacement structure for unmanned aerial vehicle battery, it is related to unmanned aerial vehicle technical field, including body, battery compartment and battery plate, the battery compartment is opened in the rear side of body, the battery plate is inserted and connected in the inner chamber of battery compartment;The rear side of the battery plate is fixedly connected with connecting plate, the rear side of the body is equipped with the connecting groove of using cooperation with connecting plate, the connecting plate is inserted and connected in the inner chamber of connecting groove, the left side and the right side of the connecting groove are equipped with the insertion slot The inner chamber of the connecting plate is equipped with mounting groove, the inner chamber of the mounting groove is provided with positioning assembly.The utility model is provided with pop-up assembly, mounting groove, positioning assembly, groove, non-slip plate, chamfer, insertion plate, containing groove, extrusion block and first spring, solve the problem that there are many inconveniences when unmanned aerial vehicle replaces battery, need to manually screw, rely on tool and step complex, non-professional personnel easy to operate mistake, reach the effect of quick disassembly battery.
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Description

Technical Field

[0001] This utility model relates to the field of drone technology, specifically a quick-release replacement structure for drone batteries. Background Technology

[0002] This drone can be widely used in various fields such as agricultural plant protection, power line inspection, geographic surveying, emergency rescue, and film and television aerial photography. Its application scenarios cover complex environments such as farmland, power transmission line corridors, remote mountainous areas, disaster sites, and film and television shooting locations. In agricultural scenarios, it can carry pesticides, seeds, and other materials to achieve precise application of pesticides and sowing operations on large areas of farmland, while also completing pest and disease monitoring and growth assessment. In the power sector, it can replace manual labor for all-weather inspection of high-voltage power transmission lines, promptly detecting potential hazards such as line damage and foreign object attachments. In emergency rescue, it can quickly fly to disaster areas to perform tasks such as searching for trapped personnel, transmitting on-site images, and delivering emergency supplies, significantly improving operational efficiency and safety.

[0003] However, the above-mentioned device still has the following problems during implementation: Existing technologies make replacing drone batteries inconvenient, requiring manual screw tightening, relying on tools, and involving complex procedures. Non-professionals are prone to operational errors. Therefore, a quick-release replacement structure for drone batteries is proposed to solve the above problems. Utility Model Content

[0004] To address the problems mentioned in the background art, the purpose of this utility model is to provide a quick-release replacement structure for drone batteries, which has the advantage of quick battery removal and solves the problems of inconvenience when replacing drone batteries, such as the need to manually tighten screws, reliance on tools, complicated steps, and easy operation errors by non-professionals.

[0005] To achieve the above objectives, this utility model provides the following technical solution: a quick-release replacement structure for a drone battery, comprising a body, a battery compartment, and a battery plate, wherein the battery compartment is located on the rear side of the body, and the battery plate is inserted into the inner cavity of the battery compartment; A connecting plate is fixedly connected to the rear side of the battery panel, and a connecting groove for use with the connecting plate is opened on the rear side of the body. The connecting plate is inserted into the inner cavity of the connecting groove, and insertion slots are opened on the left and right sides of the connecting groove. Two pop-up components are located on the left and right sides of the internal cavity of the machine. The connecting plate has an inner cavity with a mounting groove, and the inner cavity of the mounting groove is provided with a positioning component.

[0006] As a preferred embodiment of this utility model, the top and bottom of the connecting plate are provided with grooves, and the inner cavity of the groove is fixedly connected to an anti-slip plate, and the number of anti-slip plates is multiple.

[0007] As a preferred embodiment of this utility model, the left and right sides of the inner cavity of the connecting groove are chamfered, and the inner cavity of the insertion groove is movably connected to an insertion plate.

[0008] As a preferred embodiment of the present invention, the ejector assembly includes two receiving slots, which are formed in the inner cavity of the machine body. An extrusion block is movably connected to the inner cavity of the receiving slot. A first spring is fixedly connected to the front side of the extrusion block, and the rear side of the extrusion block passes through the receiving slot and contacts the connecting plate.

[0009] In a preferred embodiment of this invention, the positioning component includes two movable blocks, which are movably connected to the inner cavity of the mounting groove. A second spring is fixedly connected to one side of each of the two movable blocks, and a mating hole is provided on the top of each movable block.

[0010] As a preferred embodiment of this utility model, extrusion holes are provided on both the front and rear sides of the mating hole, and an extrusion rod is movably connected to the inner cavity of the extrusion hole.

[0011] In a preferred embodiment of this invention, a mating plate is movably connected to the inner cavity of the mating hole, the side of the pressing rod near the mating plate is fixedly connected to the mating plate, and a pressing block is fixedly connected to the top of the mating plate. The top of the pressing block penetrates the mounting groove and extends into the inner cavity of the connecting groove.

[0012] Compared with the prior art, the beneficial effects of this utility model are as follows: 1. This utility model solves the many inconveniences of replacing drone batteries by setting up a pop-out component, mounting slot, positioning component, groove, anti-slip plate, chamfer, plug-in plate, receiving slot, extrusion block and first spring. It solves the problems of manual screwing, tool dependence and complicated steps, and easy operation errors by non-professionals, and achieves the effect of quick battery removal.

[0013] 2. By setting up a pop-out component, after the plug-in plate is disengaged from the plug-in slot, the second spring drives the extrusion block to move. The extrusion block can drive the connecting plate and the battery plate to move, which makes it convenient to remove the battery plate.

[0014] 3. This utility model, by setting up a chamfer, a plug-in plate, a positioning component, a pressing hole, a pressing rod, a mating plate, and a pressing block, allows the plug-in plate to automatically move and move the movable block when the battery panel is inserted into the battery compartment, as the bevel on the plug-in plate engages with the chamfer. After the battery panel is fully inserted, the plug-in plate will automatically insert into the plug-in slot due to the elastic force of the second spring. Pressing the pressing block moves the mating plate, and the movement of the mating plate moves the pressing rod within the pressing hole, thus simultaneously moving both movable blocks. Attached Figure Description

[0015] Figure 1This is a schematic diagram of the structure of this utility model; Figure 2 A three-dimensional disassembled diagram of the body and battery panel; Figure 3 This is a three-dimensional sectional view of the machine body; Figure 4 This is a three-dimensional schematic diagram of the positioning component.

[0016] In the diagram: 1. Body; 2. Battery compartment; 3. Battery plate; 4. Connecting plate; 5. Connecting slot; 6. Insertion slot; 7. Pop-out assembly; 8. Mounting slot; 9. Positioning assembly; 10. Groove; 11. Anti-slip plate; 12. Chamfer; 13. Insertion plate; 71. Receiving slot; 72. Extrusion block; 73. First spring; 91. Movable block; 92. Second spring; 93. Mating hole; 14. Extrusion hole; 15. Extrusion rod; 16. Mating plate; 17. Pressing block. Detailed Implementation

[0017] To make the above-mentioned objectives, features and advantages of this utility model more apparent and understandable, the specific embodiments of this utility model will be described in detail below with reference to the accompanying drawings.

[0018] Many specific details are set forth in the following description in order to provide a full understanding of the present invention. However, the present invention may also be implemented in other ways different from those described herein. Those skilled in the art can make similar extensions without departing from the spirit of the present invention. Therefore, the present invention is not limited to the specific embodiments disclosed below.

[0019] Secondly, the term "an embodiment" or "embodiment" as used herein refers to a specific feature, structure, or characteristic that may be included in at least one implementation of the present invention. The phrase "in one embodiment" appearing in different places in this specification does not necessarily refer to the same embodiment, nor is it a single or selective embodiment that excludes other embodiments.

[0020] Secondly, this utility model is described in detail with reference to the schematic diagrams. When describing the embodiments of this utility model, for ease of explanation, the cross-sectional views illustrating the device structure may be partially enlarged, not adhering to the usual scale. Furthermore, the schematic diagrams are merely examples and should not limit the scope of protection of this utility model. In addition, actual manufacturing should include the three-dimensional spatial dimensions of length, width, and depth.

[0021] Example 1: Refer to Figure 1-4 This is the first embodiment of the present utility model, which provides a quick-release replacement structure for a drone battery, including a body 1, a battery compartment 2 and a battery plate 3. The battery compartment 2 is located on the rear side of the body 1, and the battery plate 3 is inserted into the inner cavity of the battery compartment 2. A connecting plate 4 is fixedly connected to the rear side of the battery plate 3. A connecting groove 5 that works with the connecting plate 4 is provided on the rear side of the body 1. The connecting plate 4 is inserted into the inner cavity of the connecting groove 5. Insertion grooves 6 are provided on the left and right sides of the connecting groove 5. Two pop-out components 7 are located on the left and right sides of the inner cavity of the body 1; The inner cavity of the connecting plate 4 is provided with a mounting groove 8, and the inner cavity of the mounting groove 8 is provided with a positioning component 9; The top and bottom of the connecting plate 4 are provided with grooves 10, and the inner cavity of the grooves 10 is fixedly connected to the anti-slip plate 11, and there are multiple anti-slip plates 11.

[0022] Specifically, when the body 1 is in use, the pop-out component 7 can easily pop out the battery, and the positioning component 9 can fix the position of the connecting plate 4.

[0023] Furthermore, by pinching the anti-slip plates 11 at the top and bottom of the connecting plate 4 with your fingers, you can pull the connecting plate 4 and the battery plate 3 to detach from the battery compartment 2.

[0024] Example 2: The second embodiment of this utility model provides a quick-release replacement structure for a drone battery. The pop-out component 7 includes two receiving slots 71. The receiving slots 71 are opened in the inner cavity of the body 1. An extrusion block 72 is movably connected to the inner cavity of the receiving slot 71. A first spring 73 is fixedly connected to the front side of the extrusion block 72. The rear side of the extrusion block 72 passes through the receiving slot 71 and contacts the connecting plate 4.

[0025] Specifically, by setting the pop-out component 7, after the plug-in plate 13 is disengaged from the plug-in slot 6, the second spring 92 drives the extrusion block 72 to move. The extrusion block 72 can drive the connecting plate 4 and the battery plate 3 to move, which makes it easier to remove the battery plate 3.

[0026] Furthermore, the first spring 73 will then undergo elastic deformation, causing the extrusion block 72 to move. The movement of the extrusion block 72 will cause the battery plate 3 and the connecting plate 4 to move. When the connecting plate 4 moves to the appropriate position, the anti-slip plates 11 at the top and bottom of the connecting plate 4 can be pinched with fingers to pull the connecting plate 4 and the battery plate 3 away from the battery compartment 2.

[0027] Example 3: The third embodiment of this utility model provides a quick-release replacement structure for a drone battery. Chamfers 12 are provided on both the left and right sides of the inner cavity of the connecting groove 5. A plug-in plate 13 is movably connected to the inner cavity of the plug-in groove 6. The positioning component 9 includes two movable blocks 91, which are movably connected to the inner cavity of the mounting groove 8. A second spring 92 is fixedly connected to the opposite side of each of the two movable blocks 91. A mating hole 93 is provided at the top of the movable block 91. A pressing hole 14 is provided on both the front and rear sides of the mating hole 93. A pressing rod 15 is movably connected to the inner cavity of the pressing hole 14. A mating plate 16 is movably connected to the inner cavity of the mating hole 93. The side of the pressing rod 15 closest to the mating plate 16 is fixedly connected to the mating plate 16. A pressing block 17 is fixedly connected to the top of the mating plate 16. The top of the pressing block 17 penetrates the mounting groove 8 and extends into the inner cavity of the connecting groove 5.

[0028] Specifically, by setting up a chamfer 12, a plug-in plate 13, a positioning component 9, a pressing hole 14, a pressing rod 15, a mating plate 16, and a pressing block 17, when the battery panel 3 is inserted into the battery compartment 2, the inclined surface on the plug-in plate 13 will engage with the chamfer 12, thus driving the plug-in plate 13 to move automatically and causing the movable block 91 to move. After the battery panel 3 is fully inserted, the plug-in plate 13 will automatically insert into the plug-in slot 6 due to the elastic force of the second spring 92. Pressing the pressing block 17 will drive the mating plate 16 to move, and the movement of the mating plate 16 will drive the pressing rod 15 to move within the pressing hole 14, thus simultaneously driving the two movable blocks 91 to move.

[0029] Furthermore, when the battery panel 3 needs to be replaced, pressing the pressing block 17 causes the mating plate 16 to descend in the mounting groove 8. The movement of the mating plate 16 will cause the extrusion rod 15 to extrude the inner wall in the extrusion hole 14. At this time, the two movable blocks 91 can be moved to extrude the second spring 92. After the movable block 91 causes the plug plate 13 to disengage from the plug groove 6.

[0030] Working principle: When the battery panel 3 needs to be replaced, press the pressing block 17 to drive the mating plate 16 to descend in the mounting groove 8. The movement of the mating plate 16 will drive the extrusion rod 15 to extrude the inner wall in the extrusion hole 14. At this time, the two movable blocks 91 can be moved to extrude the second spring 92. After the movable block 91 drives the plug plate 13 to disengage from the plug groove 6. Subsequently, the first spring 73 will undergo elastic deformation, causing the extrusion block 72 to move. The movement of the extrusion block 72 will cause the battery plate 3 and the connecting plate 4 to move. When the connecting plate 4 moves to the appropriate position, pinch the anti-slip plate 11 at the top and bottom of the connecting plate 4 with your fingers to pull and cause the connecting plate 4 and the battery plate 3 to detach from the battery compartment 2.

[0031] In summary, the quick battery removal effect is achieved through the cooperation of the pop-out component 7, mounting slot 8, positioning component 9, groove 10, anti-slip plate 11, chamfer 12, plug plate 13, receiving slot 71, extrusion block 72 and first spring 73.

[0032] The springs used in this application can be additionally fitted with protective measures that are common knowledge in the field of this technology under different usage environments, including but not limited to the following methods, such as protective covers for equipment protection, dustproof nets for equipment dust protection, and sealing components or waterproof coatings for equipment waterproofing, which are commonly used by those skilled in the art.

[0033] It should be noted that the (spring) is a device or equipment existing in the prior art, or a device or equipment that can be implemented by the prior art. The power supply, connection method, usage method, power source, fixing method, installation method, control method, etc. of the device, as well as the materials of each accessory and the selection of various parameters are all common knowledge in the art, and therefore will not be described in detail in this application document. It is important to note that the constructions and arrangements of this application shown in several different exemplary embodiments are merely illustrative. Although only a few embodiments are described in detail in this disclosure, those who consult this disclosure will readily understand that many modifications are possible (e.g., changes in the size, dimensions, structure, shape and proportion of various elements, as well as parameter values ​​(e.g., temperature, pressure, etc.), mounting arrangements, use of materials, color, orientation, etc.) without substantially departing from the novel teachings and advantages of the subject matter described in this application). For example, an element shown as integrally formed may be composed of multiple parts or elements, the position of elements may be inverted or otherwise altered, and the nature or number or position of discrete elements may be changed or altered. Therefore, all such modifications are intended to be included within the scope of this utility model. The order or sequence of any process or method steps may be changed or reordered according to alternative embodiments. In the claims, any "device plus function" clause is intended to cover the structure described herein that performs the function, and not only structural equivalents but also equivalent structures. Without departing from the scope of this invention, other substitutions, modifications, alterations, and omissions may be made in the design, operation, and arrangement of the exemplary embodiments. Therefore, this invention is not limited to the specific embodiments, but extends to various modifications that still fall within the scope of the appended claims.

[0034] Furthermore, in order to provide a concise description of exemplary embodiments, not all features of actual embodiments (i.e., those features that are not relevant to the best mode of carrying out the present invention as currently considered, or those features that are not relevant to implementing the present invention) may be omitted.

[0035] It should be understood that numerous specific implementation decisions can be made during the development of any practical implementation, such as in any engineering or design project. Such development efforts may be complex and time-consuming, but for those skilled in the art who benefit from this disclosure, the development effort will be a routine work of design, manufacturing, and production without requiring much experimentation.

[0036] It should be noted that the above embodiments are only used to illustrate the technical solution of this utility model and are not intended to limit it. Although this utility model has been described in detail with reference to preferred embodiments, those skilled in the art should understand that modifications or equivalent substitutions can be made to the technical solution of this utility model without departing from the spirit and scope of the technical solution of this utility model, and all such modifications or substitutions should be covered within the scope of the claims of this utility model.

Claims

1. A quick-release battery replacement structure for a drone, comprising a body (1), a battery compartment (2), and a battery plate (3), characterized in that: The battery compartment (2) is located on the rear side of the body (1), and the battery panel (3) is inserted into the inner cavity of the battery compartment (2). A connecting plate (4) is fixedly connected to the rear side of the battery panel (3). A connecting groove (5) is provided on the rear side of the body (1) to cooperate with the connecting plate (4). The connecting plate (4) is inserted into the inner cavity of the connecting groove (5). Insertion grooves (6) are provided on the left and right sides of the connecting groove (5). Two pop-out components (7) are located on the left and right sides of the inner cavity of the body (1); The inner cavity of the connecting plate (4) is provided with an installation groove (8), and the inner cavity of the installation groove (8) is provided with a positioning component (9).

2. The quick-release replacement structure for a drone battery according to claim 1, characterized in that: The top and bottom of the connecting plate (4) are provided with grooves (10), and the inner cavity of the groove (10) is fixedly connected with anti-slip plate (11), and there are multiple anti-slip plates (11).

3. The quick-release replacement structure for a drone battery according to claim 1, characterized in that: The left and right sides of the inner cavity of the connecting groove (5) are chamfered (12), and the inner cavity of the plug groove (6) is movably connected to the plug plate (13).

4. The quick-release replacement structure for a drone battery according to claim 1, characterized in that: The pop-out assembly (7) includes two receiving slots (71), which are opened in the inner cavity of the body (1). An extrusion block (72) is movably connected to the inner cavity of the receiving slot (71). A first spring (73) is fixedly connected to the front side of the extrusion block (72). The rear side of the extrusion block (72) passes through the receiving slot (71) and contacts the connecting plate (4).

5. The quick-release replacement structure for a drone battery according to claim 1, characterized in that: The positioning component (9) includes two movable blocks (91), which are movably connected to the inner cavity of the mounting groove (8). A second spring (92) is fixedly connected to one side of each of the two movable blocks (91), and a mating hole (93) is provided on the top of each movable block (91).

6. The quick-release replacement structure for a drone battery according to claim 5, characterized in that: The front and rear sides of the mating hole (93) are provided with extrusion holes (14), and the inner cavity of the extrusion hole (14) is movably connected to an extrusion rod (15).

7. The quick-release replacement structure for a drone battery according to claim 6, characterized in that: The inner cavity of the mating hole (93) is movably connected to the mating plate (16), the side of the pressing rod (15) near the mating plate (16) is fixedly connected to the mating plate (16), and the top of the mating plate (16) is fixedly connected to the pressing block (17). The top of the pressing block (17) passes through the mounting groove (8) and extends into the inner cavity of the connecting groove (5).