Unmanned aerial vehicle battery module
By introducing a cooling fan, a BMS balanced battery information acquisition port and an elastic connecting piece into the drone battery module, combined with the aluminum alloy shell and soft silicone bonding, the stability problems of traditional battery modules under vibration and temperature changes are solved, and the performance and life of the battery module are improved.
Patent Information
- Application Number
- CN202422073227.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-08-26
- Publication Date
- 2025-07-18
- Estimated Expiration
- 2034-08-26
AI Technical Summary
Traditional UAV battery modules are prone to problems such as connecting plate damage and solder joints falling off under high-frequency vibration and temperature changes, which affect stability and service life.
The design of the battery case is equipped with a cooling fan, a BMS balanced battery information acquisition port, a battery elastic connection sheet and a soft silicone bonding design. Combined with the aluminum alloy case, the stability of the battery module is enhanced through active heat dissipation, elastic connection and bonding and shock absorption.
It improves the stability and life of the battery module, reduces the overall weight of the drone, enhances the load capacity, and prevents the connection piece from breaking and the solder joints from falling off.
Smart Images

Figure CN223124062U_ABST
Abstract
Description
Technical Field
[0001] The utility model belongs to the technical field of UAV battery modules, and more specifically, particularly relates to a UAV battery module. Background Art
[0002] The UAV battery module is a battery component specifically designed for UAVs. It plays a key role in improving the endurance, flight performance, and safety of UAVs and is an indispensable part of the development of modern UAV technology.
[0003] With the development of UAV technology, the performance requirements for battery modules are getting higher and higher. During the flight of UAVs, due to high-frequency vibration and temperature changes, traditional battery modules are prone to problems such as damage to connecting pieces and solder joint detachment, seriously affecting the stability and service life of the battery module.
[0004] Therefore, in view of this, research and improvement are carried out on the existing structure and deficiencies to provide a UAV battery module, with the expectation of achieving a more practical value. Summary of the Utility Model
[0005] In order to solve the above technical problems, the utility model provides a UAV battery module, which is achieved by the following specific technical means:
[0006] The UAV battery module includes a battery housing and a battery module. The battery module is installed inside the battery housing. A plurality of cooling fans are installed on one side of the battery housing. A BMS balanced battery information collection port is provided on the side of the battery housing away from the cooling fans. The battery module includes a plurality of battery bodies, battery brackets, and battery elastic connection pieces. A pair of battery brackets are installed on the upper and lower end faces of the plurality of battery bodies. A plurality of battery elastic connection pieces are installed on the upper end face of the battery bracket located above. A pair of elastic mechanisms one are installed on one side of the upper end face of the battery elastic connection piece. Three groups of elastic mechanisms two are installed on the other side of the upper end face of the battery elastic connection piece. The battery bodies, battery brackets, battery elastic connection pieces, and the battery housing are bonded together by soft silicone.
[0007] Further, a pair of high-current plugs are installed on one side of the battery housing near the BMS balanced battery information collection port.
[0008] Further, a control switch is installed on one side of the battery housing below the BMS balanced battery information collection port.
[0009] Further, a pair of voltage and temperature meters are installed on one side of the battery housing near the control switch.
[0010] Further, a pair of handles are installed on the upper end face of the battery housing.
[0011] Furthermore, the material of the battery housing is aluminum alloy.
[0012] Furthermore, a pair of heat dissipation grooves are provided on both sides of the battery housing.
[0013] Compared with the prior art, the utility model has the following beneficial effects:
[0014] By the combined use of the BMS balanced battery information acquisition port and the battery module, the battery module adopts an external battery protection system. The charger current enters the battery module after passing through the battery protection system. The battery protection system collects the information of the battery module through the BMS balanced battery information acquisition port, thereby reducing the overall weight and improving the load capacity of the drone.
[0015] By the use of a heat dissipation fan, a heat dissipation fan is installed inside the battery housing, and the temperature of the battery body is reduced by active heat dissipation, improving the performance and service life of the battery body.
[0016] By the combined use of the battery elastic connecting piece, the elastic mechanism one and the elastic mechanism two, the design of the battery elastic connecting piece has a structure with tensile elasticity, so as to be able to adapt to the thermal expansion and contraction of the battery, prevent the battery elastic connecting piece from breaking and the solder joints from falling off. At the same time, the battery body, the battery bracket, the battery elastic connecting piece and the battery housing are bonded by soft silicone, which can carry out shock absorption and reinforcement, and further reduce the influence of vibration on the battery module. BRIEF DESCRIPTION OF THE DRAWINGS
[0017] Figure 1 is a front perspective schematic diagram of the utility model.
[0018] Figure 2 is a rear perspective schematic diagram of the utility model.
[0019] Figure 3 is a top cross-sectional schematic diagram of the utility model.
[0020] Figure 4 is a side cross-sectional schematic diagram of the utility model.
[0021] Figure 5 is a three-dimensional schematic diagram of the battery elastic connecting piece in the utility model.
[0022] In the figure, the corresponding relationship between the component names and the drawing reference numerals is as follows:
[0023] 1. Battery housing; 2. Battery module; 3. Heat dissipation fan; 4. BMS balanced battery information acquisition port; 5. Battery body; 6. Battery bracket; 7. Battery elastic connecting piece; 701. Elastic mechanism one; 702. Elastic mechanism two; 8. High-current plug; 9. Control switch; 10. Voltage and temperature meter; 11. Handle; 12. Heat dissipation groove. Detailed implementation manners
[0024] The following further describes in detail the implementation manners of the present utility model in conjunction with the accompanying drawings and embodiments. The following embodiments are used to illustrate the present utility model, but cannot be used to limit the scope of the present utility model.
[0025] In the description of the present utility model, unless otherwise specified, the meaning of "a plurality of" is two or more; the orientation or positional relationship indicated by the terms "upper", "lower", "left", "right", "inner", "outer", "front end", "rear end", "head", "tail", etc. is based on the orientation or positional relationship shown in the accompanying drawings, and is only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation of the present utility model. In addition, the terms "first", "second", "third", etc. are only used for descriptive purposes and cannot be understood as indicating or implying relative importance.
[0026] In the description of the present utility model, it should be noted that unless otherwise clearly specified and defined, the terms "connected" and "connected" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be directly connected or indirectly connected through an intermediate medium. For those of ordinary skill in the art, the specific meanings of the above terms in the present utility model can be understood according to specific situations.
[0027] Embodiment:
[0028] As shown in the attached Figure 1 to the attached Figure 5 figure:
[0029] The present utility model provides a drone battery module, which includes a battery housing 1 and a battery module 2. The battery module 2 is installed inside the battery housing 1. A plurality of cooling fans 3 are installed on one side of the battery housing 1, and the cooling fans 3 are installed inside the battery housing 1. By active heat dissipation, the temperature of the battery body 5 is reduced, improving the performance and lifespan of the battery body 5. On the side of the battery housing 1 away from the cooling fans 3, there is a BMS balanced battery information acquisition port 4. The battery module 2 includes a plurality of battery bodies 5, battery brackets 6, and battery elastic connection sheets 7. A pair of battery brackets 6 are installed on the upper and lower end faces of the plurality of battery bodies 5. A plurality of battery elastic connection sheets 7 are installed on the upper end face of the battery bracket 6 located above. On one side of the upper end face of the battery elastic connection sheet 7, a pair of elastic mechanisms 701 are installed, and on the other side of the upper end face of the battery elastic connection sheet 7, three groups of elastic mechanisms 702 are installed. Through the combined use of the battery elastic connection sheet 7, the elastic mechanism 701, and the elastic mechanism 702, the design of the battery elastic connection sheet 7 has a structure with tensile elasticity, thus being able to adapt to the thermal expansion and contraction of the battery, preventing the battery elastic connection sheet 7 from breaking and the solder joints from falling off. The battery body 5, the battery bracket 6, the battery elastic connection sheet 7, and the battery housing 1 are bonded together by soft silicone. The soft silicone can provide shock absorption and reinforcement, thereby reducing the impact of vibration on the battery module 2.
[0030] Among them, on one side of the battery housing 1 near the BMS balanced battery information acquisition port 4, a pair of high-current plugs 8 are installed. Through the high-current plugs 8, the battery body 5 can be charged.
[0031] Among them, on one side of the battery housing 1 below the BMS balanced battery information acquisition port 4, a control switch 9 is installed. Through the control switch 9, the turning on and off of the cooling fans 3 can be controlled.
[0032] Among them, on one side of the battery housing 1 near the control switch 9, a pair of voltage and temperature meters 10 are installed. Through the voltage and temperature meters 10, the voltage and temperature of the battery module 2 can be displayed.
[0033] Among them, on the upper end face of the battery housing 1, a pair of handles 11 are installed. Through the handles 11, it is convenient to carry the battery housing 1.
[0034] Among them, the material of the battery housing 1 is aluminum alloy. Aluminum alloy has a relatively low density and high strength, with a lighter weight than many other structural materials such as steel. Aluminum alloy has good corrosion resistance, and its surface can be further enhanced in corrosion resistance through anodic oxidation or other surface treatment technologies, enabling it to maintain stable performance in harsh environments (or other materials with relatively high specific strength, engineering plastics, composite materials).
[0035] Among them, a pair of heat dissipation grooves 12 are provided on both sides of the battery housing 1. Quick self-locking limit buckles (which are prior arts and will not be elaborated here) are respectively installed at the edges on both sides of the heat dissipation grooves 12. The cooling fan 3 blows the external cold air onto the surface of the battery body 5 for heat dissipation, and the hot air inside the battery housing 1 is discharged through the heat dissipation grooves 12.
[0036] The working principle of this embodiment:
[0037] Through the combined use of the BMS balanced battery information acquisition port 4 and the battery module 2, the battery module 2 adopts an external battery protection system. The charger current enters the battery module 2 after passing through the battery protection system. The battery protection system collects the information of the battery module 2 through the BMS balanced battery information acquisition port 4, thereby reducing the overall weight and improving the load capacity of the drone. Through the use of the cooling fan 3, the cooling fan 3 is installed inside the battery housing 1, and the temperature of the battery body 5 is reduced by active heat dissipation, improving the performance and lifespan of the battery body 5. Through the combined use of the battery elastic connecting piece 7, the elastic mechanism one 701, and the elastic mechanism two 702, the design of the battery elastic connecting piece 7 has a structure with tensile elasticity, so as to be able to adapt to the thermal expansion and contraction of the battery, prevent the battery elastic connecting piece 7 from breaking and the solder joints from falling off. At the same time, the battery body 5, the battery bracket 6, the battery elastic connecting piece 7, and the battery housing 1 are bonded together by soft silicone, which can perform shock absorption and reinforcement, and thus can reduce the impact of vibration on the battery module 2.
[0038] The embodiments of the present utility model are given for the purposes of illustration and description, and are not exhaustive or limit the present utility model to the disclosed form. Many modifications and variations are obvious to those of ordinary skill in the art. The embodiments are selected and described to better illustrate the principles and practical applications of the present utility model, and enable those of ordinary skill in the art to understand the present utility model and thus design various embodiments with various modifications suitable for specific purposes.
Claims
1. Drone battery module, including a battery housing (1) and a battery module (2), characterized in that: A battery module (2) is installed inside the battery housing (1). A number of cooling fans (3) are installed on one side of the battery housing (1). A BMS equalization battery information collection port (4) is provided on the side of the battery housing (1) away from the cooling fans (3). The battery module (2) includes a number of battery bodies (5), battery brackets (6), and battery elastic connection pieces (7). A pair of battery brackets (6) are installed on the upper and lower end faces of the number of battery bodies (5). A number of battery elastic connection pieces (7) are installed on the upper end face of the battery bracket (6) located above. A pair of elastic mechanisms one (701) are installed on one side of the upper end face of the battery elastic connection piece (7). Three groups of elastic mechanisms two (702) are installed on the other side of the upper end face of the battery elastic connection piece (7). The battery body (5), battery bracket (6), battery elastic connection piece (7), and battery housing (1) are bonded together by soft silicone.
2. The drone battery module according to claim 1, wherein: A pair of high-current plugs (8) are installed at a position on one side of the battery housing (1) close to the BMS equalization battery information collection port (4).
3. The drone battery module according to claim 1, wherein: A control switch (9) is installed on one side of the battery housing (1) below the BMS equalization battery information collection port (4).
4. The drone battery module according to claim 3, wherein: A pair of voltage and temperature gauges (10) are installed at a position on one side of the battery housing (1) close to the control switch (9).
5. The drone battery module according to claim 1, characterized in that: A pair of handles (11) are installed on the upper end face of the battery housing (1).
6. The drone battery module according to claim 1, wherein: The material of the battery housing (1) is aluminum alloy.
7. The drone battery module according to claim 1, wherein: A pair of heat dissipation grooves (12) are provided on both sides of the battery housing (1).