Unmanned aerial vehicle battery dismounting device
By designing the slot and power module of the drone battery disassembly device, the problem of easy damage to the connector during the drone battery is solved, and stable power supply and safety improvement are achieved.
Patent Information
- Application Number
- CN202422200141.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-09-09
- Publication Date
- 2025-07-08
- Estimated Expiration
- 2034-09-09
AI Technical Summary
When disassembling the battery, the manual operation strength of the drone is not easy to master, which can easily damage the banana head connection cable, and the battery is not firmly fixed may cause it to fly during rolling action.
A drone battery disassembly device is designed, including two card slots, a sliding module and a power module. The power module drives the card slot to slide to achieve stable separation between the drone and the battery, and the reset module is used to maintain the connection state to avoid battery fall off caused by vibration or accidental touch.
It realizes uniform stress separation between the drone battery and the drone, avoids joint damage, and maintains a stable power supply during takeoff, flight and landing, improving the safety and reliability of the drone.
Smart Images

Figure CN223072775U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of unmanned aerial vehicles, and particularly relates to a battery disassembly device for an unmanned aerial vehicle. Background Art
[0002] An unmanned aerial vehicle, abbreviated as "UAV", is an unpiloted aircraft controlled by a radio remote control device and a self - contained program control device, or is completely or intermittently autonomously operated by an on - vehicle computer. During the flight of the UAV, in order to ensure that the battery will not be thrown off due to insecure fixation when performing some rolling actions, fragmented fixing parts are required to strengthen the fixation of the battery. Therefore, when disassembling the battery of the UAV, it is very inconvenient.
[0003] Generally, the battery is disassembled by manually inserting and separating the banana plugs of the battery. However, it is difficult to master the force of manual operation, and it is easy to damage the connecting wire of the banana plug. Summary of the Invention
[0004] In order to solve the above problems, the utility model proposes a battery disassembly device for an unmanned aerial vehicle.
[0005] The utility model proposes a battery disassembly device for an unmanned aerial vehicle, which includes two card slots, a sliding module and a power module;
[0006] The two card slots are respectively detachably connected to the unmanned aerial vehicle and the battery, and the two card slots are arranged through the sliding module, and at least one card slot can slide along the sliding module;
[0007] The power module is connected to the card slot that can slide along the sliding module, and is used to drive the corresponding card slot to slide along the sliding module until the unmanned aerial vehicle is separated from the battery.
[0008] Preferably, the two card slots are respectively: a first card slot detachably connected to the unmanned aerial vehicle and a second card slot detachably connected to the battery;
[0009] The second card slot can slide along the sliding module;
[0010] Correspondingly, the power module is connected to the second card slot, and is used to drive the second card slot to slide along the sliding module until the unmanned aerial vehicle is separated from the battery.
[0011] Preferably, the first card slot is fixedly connected to the sliding module;
[0012] The power module is respectively hinged to the first card slot and the second card slot, and is used to change the angle between the power module and the second card slot under the action of an external force, so as to drive the second card slot to slide along the sliding module until the unmanned aerial vehicle is separated from the battery.
[0013] Preferably, the UAV battery disassembly device further includes a reset module;
[0014] The reset module is arranged between the power module and the first card slot, and is used to restore the angle between the power module and the second card slot to the initial state after the external force is removed.
[0015] The power module includes a holding unit and a connecting unit;
[0016] One end of the holding unit is hinged to the first card slot, and the other end is a free end for bearing the external force;
[0017] Both ends of the connecting unit are respectively hinged to the holding unit and the second card slot, and are used to drive the angle between the connecting unit and the second card slot to change under the drive of the holding unit, so as to drive the second card slot to slide along the sliding module until the UAV is separated from the battery.
[0018] Preferably, the reset module includes a fixing unit and an elastic clamping unit;
[0019] The fixing unit is used to hinge the power module and the first card slot;
[0020] The elastic clamping unit is sleeved on the fixing unit, and one end of the elastic clamping unit abuts against the power module, and the other end abuts against the first card slot.
[0021] Preferably, the fixing unit is a pin shaft for hinging the power module and the first card slot;
[0022] The elastic clamping unit is a torsion spring, the torsion spring is sleeved on the fixing unit, and one torsion arm of the torsion spring abuts against the power module, and the other torsion arm abuts against the first card slot.
[0023] Preferably, the detachable connection is a snap connection.
[0024] Compared with the prior art, the utility model has the following beneficial effects:
[0025] (1) By using the power module to drive the separation of the card slots respectively connecting the UAV and the battery, the setting of the card slots makes the overall force of the UAV and the battery more uniform, and by applying a preset pulling force to the power module, the UAV and the battery can be smoothly separated while not easily damaging the connector;
[0026] (2) Through the cooperation of the reset module and the power module, the battery and the drone are kept connected in the natural state, and only disconnect when an external force is applied. As a result, the device of the present utility model can maintain a stable power supply during the take-off, flight and landing of the drone, effectively avoiding problems such as battery detachment or poor contact caused by vibration or accidental touch, thereby improving the safety and reliability of the drone. BRIEF DESCRIPTION OF THE DRAWINGS
[0027] Figure 1 is a front structural schematic diagram of the present utility model;
[0028] Figure 2 is a reverse structural schematic diagram of the present utility model;
[0029] Figure 3 is a side structural schematic diagram of the present utility model;
[0030] In the figure, 1 is the free end; 2 is the end opposite to the free end; 3 is the side of the holding unit; 4 is the second card slot; 5 is the first card slot; 6 is the first pin shaft; 7 is the sliding module; 8 is the connecting unit; 9 is the second pin shaft; 10 is the first perforated protrusion; 11 is the second perforated protrusion; 12 is the third perforated protrusion; 13 is the fourth perforated protrusion; 14 is the torsion spring; 15 is the first hanging ring; 16 is the second hanging ring. DETAILED DESCRIPTION OF THE EMBODIMENTS
[0031] In the following description, specific details such as specific system structures and technologies are presented for the purpose of illustration rather than limitation, in order to thoroughly understand the embodiments of the present utility model. However, those skilled in the art should clearly understand that the present utility model can also be implemented in other embodiments without these specific details. In other cases, detailed descriptions of well-known systems, devices, circuits, and methods are omitted to avoid unnecessary details from interfering with the description of the present utility model.
[0032] The present utility model provides a drone battery disassembly device, including two card slots, a sliding module 7, and a power module;
[0033] The two card slots are respectively detachably connected to the drone and the battery, and the two card slots are passed through the sliding module 7, and at least one card slot can slide along the sliding module 7; preferably, the detachable connection is a snap connection.
[0034] The power module is connected to the card slot that can slide along the sliding module 7, and is used to drive the corresponding card slot to slide along the sliding module 7 until the drone is separated from the battery.
[0035] The utility model drives the separation of the card slots respectively connected to the drone and the battery by using the power module. The setting of the card slots enables the overall force on the drone and the battery to be more uniform, and by applying a preset pulling force to the power module, the drone and the battery can be smoothly separated while not easily damaging the connectors.
[0036] The following are several embodiments of the utility model:
[0037] Embodiment 1
[0038] The two card slots are respectively: the first card slot 5 detachably connected to the drone and the second card slot 4 detachably connected to the battery;
[0039] The second card slot 4 can slide along the sliding module 7;
[0040] Correspondingly, the power module is connected to the second card slot 4 and is used to drive the second card slot 4 to slide along the sliding module 7 until the drone is separated from the battery.
[0041] In this embodiment, the power module is used to drive the second card slot 4 detachably connected to the battery to slide. Compared with driving the card slot connected to the drone to slide, this embodiment is more convenient and easier to operate.
[0042] Embodiment 2
[0043] On the basis of Embodiment 1, the first card slot 5 is fixedly connected to the sliding module 7;
[0044] The power module is respectively hinged to the first card slot 5 and the second card slot 4 and is used to change the angle between the power module and the second card slot 4 under the action of an external force, thereby driving the second card slot 4 to slide along the sliding module 7 until the drone is separated from the battery.
[0045] The external force can be a human force or a force applied by a machine, and the force applied by the machine can be adjusted according to actual needs.
[0046] In this embodiment, the power module can be a first rod-shaped object and a second rod-shaped object hinged at the ends, and the other ends of the two rod-shaped objects are respectively hinged to the first card slot 5 and the second card slot 4; when an external force is applied, the angles between the two rod-shaped objects and the corresponding card slots change, thereby driving the second card slot 4 to move along the sliding module 7;
[0047] In other embodiments, the power module can also be an elastic member, and the two ends of the elastic member are respectively hinged to the first card slot 5 and the second card slot 4; when subjected to an external force, it deforms, thereby driving the second card slot 4 to move along the sliding module 7.
[0048] Embodiment 3
[0049] On the basis of Embodiment 2, the drone battery disassembly device further includes a reset module;
[0050] The reset module is disposed between the power module and the first card slot 5 and is configured to restore the angle between the power module and the second card slot 4 to the initial state after the external force is removed.
[0051] In this embodiment, the reset module can be an elastic component such as a spring or rubber.
[0052] Embodiment 4
[0053] Based on Embodiment 2 or Embodiment 3, the power module includes a holding unit and a connecting unit 8;
[0054] One end of the holding unit is hinged to the first card slot 5, and the other end is a free end 1 for bearing an external force;
[0055] Both ends of the connecting unit 8 are respectively hinged to a preset position in the middle of the holding unit and the second card slot 4, and are configured to drive the angle between the connecting unit 8 and the second card slot 4 to change under the drive of the holding unit, so as to drive the second card slot 4 to slide along the sliding module 7 until the drone is separated from the battery.
[0056] As Figure 1 shown, the holding unit in this embodiment is a pair of components similar in shape to "<>", as Figure 2 shown, a first hanging ring 15 is provided at the connection between the first card slot 5 and the holding unit. The first pin shaft 6 sequentially passes through the holding unit and the first hanging ring 15 to hinge one end of the holding unit to the first card slot 5; both ends of the connecting unit 8 are respectively hinged to the holding unit and the second card slot 4 through a second pin shaft 9. Correspondingly, a second hanging ring 16 is provided at the connection between the second card slot 4 and the connecting unit 8. The second pin shaft 9 sequentially passes through the second hanging ring 16 and the connecting unit 8 to hinge one end of the connecting unit 8 to the first card slot 5.
[0057] Embodiment 5
[0058] Based on Embodiment 3, the reset module includes a fixing unit and an elastic clamping unit;
[0059] The fixing unit is used for hinging the power module to the first card slot 5;
[0060] The elastic clamping unit is sleeved on the fixing unit, and one end of the elastic clamping unit abuts against the power module and the other end abuts against the first card slot 5.
[0061] Through the cooperation of the reset module and the power module, the battery and the drone are kept connected in the natural state and only disconnect when an external force is applied. Furthermore, the device of the present utility model can maintain a stable power supply during the take-off, flight and landing of the drone, effectively avoiding problems such as battery detachment or poor contact caused by vibration or accidental touch, thereby improving the safety and reliability of the drone.
[0062] Example 6
[0063] Based on Example 5, the fixing unit is the first pin shaft 6, which is used to hinge the power module and the first card slot 5;
[0064] The elastic clamping unit is a torsion spring 14. The torsion spring 14 is sleeved on the fixing unit, and one torsion arm of the torsion spring 14 abuts against the power module, and the other torsion arm abuts against the first card slot 5.
[0065] As Figure 1 shown, it can be seen from the side 3 of the holding unit that the end of the holding unit connected to the two card slots has a certain thickness; and as Figure 3 shown, at the end of the holding unit connected to the first card slot 5, corresponding first hole-bearing protrusions 10 and second hole-bearing protrusions 11 are provided; the first pin shaft 6 sequentially passes through the first hole-bearing protrusion 10 of the holding unit, the hanging ring on the first card slot 5, and the second hole-bearing protrusion 11; and a torsion spring 14 is sleeved on the first pin shaft 6; the first torsion arm of the torsion spring 14 abuts against the holding unit; the second torsion arm abuts against the first card slot 5; the torsion spring 14 and the first pin shaft 6 cooperate with each other to enable the holding unit to recover the angle with the first card slot 5 when not under force.
[0066] Similarly, at the end of the holding unit connected to the second card slot 4, third hole-bearing protrusions 12 and fourth hole-bearing protrusions 13 are provided; the second pin shaft 9 sequentially passes through the third hole-bearing protrusion, the connecting unit 8, and the fourth hole-bearing protrusion to hinge the connecting unit 8 and the second card slot 4.
[0067] To facilitate the understanding of the structure of this embodiment, looking from the side 3 of the holding unit, the connection manner between the holding unit and the first card slot 5 and the second card slot 4 can be analogized to the connection manner between the dial and the watchband of a watch. The end 2 opposite to the free end of the holding unit is regarded as the dial, and the two card slots are respectively regarded as the watchbands on both sides. The difference is that a torsion spring 14 is also provided on the first pin shaft 6 analogous to the watchband of the first card slot 5.
[0068] Taking Example 6 as an example, the usage method of the present utility model is as follows:
[0069] Drive the angle change of the free end 1 of the holding unit. Since the holding unit is hinged to the connecting unit 8, driven by the free end 1 of the holding unit, the connecting unit 8, the end of the holding unit hinged to the first card slot rotates successively, thereby driving the second card slot 4 to slide along the sliding module 7, and the battery is separated from the drone; when the external force is removed, under the action of the torsion spring 14, the angle between the holding unit and the first card slot 5 returns to the initial state, and successively drives the free end 1 of the holding unit, the connecting unit 8, and the second card slot 4 to return to their original positions.
[0070] The design of the reset module of the present utility model enables users to easily relock the battery onto the drone when needed, providing a solid energy guarantee for the long-term and high-performance operation of the drone. Further, the connection method of the cooperation between the reset module and the power module also simplifies the process of battery replacement and maintenance, improves the overall operation convenience, enabling drone users to focus more on task execution without excessive concern about the stability of battery connection.
[0071] The above are only several embodiments of the present application and do not impose any form of limitation on the present application. Although the present application is disclosed above with preferred embodiments, it is not intended to limit the present application. Any person skilled in the art, without departing from the scope of the technical solution of the present application, makes some changes or modifications using the technical content disclosed above, which are all equivalent to equivalent embodiments and fall within the scope of the technical solution.
Claims
1. An unmanned aerial vehicle battery disassembly device, characterized in that, It includes two card slots, a sliding module and a power module; The two card slots are respectively detachably connected to the drone and the battery, and the two card slots are disposed through the sliding module, and at least one card slot can slide along the sliding module; The power module is connected to the card slot that can slide along the sliding module, and is configured to drive the corresponding card slot to slide along the sliding module until the drone is separated from the battery.
2. The drone battery disassembly device according to claim 1, wherein The two card slots are respectively: a first card slot detachably connected to the drone and a second card slot detachably connected to the battery; The second card slot can slide along the sliding module; Correspondingly, the power module is connected to the second card slot, and is configured to drive the second card slot to slide along the sliding module until the drone is separated from the battery.
3. The drone battery disassembly device according to claim 2, wherein, The first card slot is fixedly connected to the sliding module; The power module is respectively hinged to the first card slot and the second card slot, and is configured to change the angle between the power module and the second card slot under the action of an external force, so as to drive the second card slot to slide along the sliding module until the drone is separated from the battery.
4. The drone battery disassembly device according to claim 3, wherein, It further includes a reset module; The reset module is disposed between the power module and the first card slot, and is configured to restore the angle between the power module and the second card slot to the initial state after the external force is removed.
5. The drone battery disassembly device according to claim 3 or 4, characterized in that, The power module includes a holding unit and a connecting unit; One end of the holding unit is hinged to the first card slot, and the other end is a free end for bearing an external force; Both ends of the connecting unit are respectively hinged to the holding unit and the second card slot, and are configured to change the angle between the connecting unit and the second card slot under the drive of the holding unit, so as to drive the second card slot to slide along the sliding module until the drone is separated from the battery.
6. The drone battery disassembly device according to claim 4, wherein, The reset module includes a fixing unit and an elastic clamping unit; The fixing unit is configured to hinge the power module and the first card slot; The elastic clamping unit is sleeved on the fixing unit, and one end of the elastic clamping unit abuts against the power module, and the other end abuts against the first card slot.
7. The drone battery disassembly device according to claim 6, wherein, The fixing unit is a pin shaft for hinging the power module and the first card slot; The elastic clamping unit is a torsion spring, the torsion spring is sleeved on the fixing unit, and one torsion arm of the torsion spring abuts against the power module, and the other torsion arm abuts against the first card slot.
8. The drone battery disassembly device according to any one of claims 1-4, characterized in that, The detachable connection is a snap connection.