Unmanned aerial vehicle battery replacing equipment
By designing drone battery swap equipment, using laser position sensors, battery charging chambers and forklift arm components, the automatic replacement and charging of drone batteries is achieved, which solves the problem of inconvenience in the battery life of the drone and manual battery swap, and realizes long-term, continuous and stable flight of drone.
Patent Information
- Application Number
- CN202421556096.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-07-03
- Publication Date
- 2025-05-16
- Estimated Expiration
- 2034-07-03
AI Technical Summary
The problem of drones' battery life during long flights and the inconvenience of manual battery replacement makes it difficult to achieve continuous and long-term independent work of drones.
A drone battery replacement device is designed, including a drone platform, laser position sensor, battery charging compartment, energy storage lithium battery and forklift arm assembly. Through the Z-axis lifting gear motor set, vertical transportation platform and battery locking mechanism, automatic replacement and charging of drone batteries are realized.
Automatic battery swap of drones is realized, manual intervention is avoided, and the drone is ensured for long-term, continuous and stable flight.
Smart Images

Figure CN222876303U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of unmanned aerial vehicle equipment, in particular to unmanned aerial vehicle battery replacement equipment. Background Art
[0002] Drones are now ubiquitous in society, but the endurance of drones and the inconvenience of manual battery replacement are still issues that need to be addressed. At this time, a device that can automatically replace the battery for drones without manual operation is needed, so as to achieve the purpose of allowing drones to work autonomously for a long time. Utility Model Content
[0003] The purpose of the utility model is to provide a battery replacement device for a drone to solve the problems raised in the above-mentioned background technology.
[0004] In order to achieve the above purpose, the utility model provides the following technical solutions:
[0005] A drone battery replacement device includes a drone platform and a drone. The drone platform is a square structure. A laser position sensor is arranged on the top of the drone platform. A battery charging compartment is arranged inside the drone platform. A storage lithium battery is arranged outside the battery charging compartment. A drone battery is placed in the battery charging compartment. A battery locking mechanism that cooperates with the drone battery is arranged inside the drone. The drone battery surface is provided with positive and negative electrodes of the drone battery. The bottom wall of the drone is provided with positive and negative electrodes of the drone that cooperate with the positive and negative electrodes of the drone battery. Battery locking grooves that cooperate with the battery locking mechanism are respectively arranged at both ends of the drone battery. Two groups of Y-axis pulley guides located outside the battery charging compartment are arranged inside the drone platform. A Y-axis pulley is arranged on the surface of the Y-axis pulley guide. A vertical transport platform is arranged on the surface of the Y-axis pulley. A Z-axis lifting gear motor group is arranged between the two groups of Y-axis pulleys. The Z-axis lifting gear motor group is connected to a forklift arm assembly. The forklift arm assembly includes a laser millimeter wave radar. The forklift arm assembly is connected to an X-axis electric linear guide, and the forklift arm assembly is connected to a Z-axis lifting rack group.
[0006] As a further solution of the utility model: the surface of the UAV platform is provided with an electric linear guide clamp, the surface of the UAV platform is provided with an electric linear guide wide clamp, and the electric linear guide clamp and the electric linear guide wide clamp are respectively connected to the laser position sensor.
[0007] As a further solution of the utility model: the Y-axis pulley is composed of a pulley and a turbine motor, and the output shaft of the turbine motor is connected to the pulley.
[0008] As a further solution of the utility model: the vertical transport platform includes a vertical transport ladder rack, a vertical transport ladder gear set is arranged on the surface of the vertical transport ladder rack, a vertical transport ladder gear motor is arranged on the surface of the vertical transport ladder gear set, the vertical transport ladder gear motor is connected to the vertical transport ladder loading platform, and a laser ranging radar is arranged on the surface of the vertical transport ladder loading platform.
[0009] As a further solution of the utility model: the Z-axis lifting gear motor group includes a Z-axis gear, the Z-axis gear is connected to a gear group motor, and the output shaft of the gear group motor is connected to the Z-axis gear.
[0010] Compared with the prior art, the beneficial effect of the utility model is that by setting the Z-axis lifting gear motor group, the vertical transport platform and the battery charging compartment to cooperate with each other, the position of the drone battery can be conveniently adjusted, and then the drone can be automatically replaced with a battery, thereby realizing long-term, continuous and stable flight of the drone. BRIEF DESCRIPTION OF THE DRAWINGS
[0011] Figure 1 This is a schematic diagram of the three-dimensional structure of the drone battery replacement equipment.
[0012] Figure 2 This is a schematic diagram of the structure of the energy storage lithium battery in the drone power replacement equipment.
[0013] Figure 3 This is a schematic diagram of the structure of the battery charging compartment in the drone battery replacement equipment.
[0014] Figure 4 This is a schematic diagram of the structure of the drone battery in the drone battery replacement equipment.
[0015] Figure 5 for Figure 2 Schematic diagram of the enlarged structure of A.
[0016] Figure 6 This is a schematic diagram of the structure of the battery locking mechanism in the drone battery replacement equipment.
[0017] Figure 7 This is a schematic diagram of the structure of the battery locking slot in the drone battery replacement equipment.
[0018] Figure 8 This is a schematic diagram of the structure of the electric linear guide fixture in the drone power exchange equipment.
[0019] Fig. 9 This is a schematic diagram of the structure of the laser millimeter-wave radar in the drone battery replacement equipment.
[0020] Fig.10 This is a schematic diagram of the structure of the laser ranging radar in the drone battery replacement equipment.
[0021] Fig.11 This is a schematic diagram of the structure of the positive and negative electrodes of the drone in the drone battery replacement equipment.
[0022] Fig.12 This is a schematic diagram of the structure of the positive and negative electrodes of the drone battery in the drone battery replacement equipment.
[0023] Among them: 11-UAV, 12-electric linear guide fixture, 13-electric linear guide wide fixture, 14-battery locking mechanism, 15-laser position sensor, 111-UAV positive and negative plates, 21-Y-axis pulley guide, 22-Y-axis pulley, 221-pulley, 222-turbine motor, 23-Z-axis lifting gear motor group, 231-Z-axis gear, 232-gear group motor, 24-forklift arm assembly, 241-laser millimeter wave radar, 25-X-axis electric linear guide, 26-Z-axis lifting rack group, 31-battery charging compartment, 32-UAV battery, 321-battery locking slot, 322-UAV battery positive and negative plates, 4-energy storage lithium battery, 5-vertical transport platform, 51-vertical transport ladder rack, 52-vertical transport ladder gear group, 53-vertical transport ladder gear motor, 54-vertical transport ladder loading platform, 55-laser ranging radar, 6-UAV platform. DETAILED DESCRIPTION
[0024] It should be noted that, in the absence of conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other.
[0025] In the description of the present invention, it should be noted that, unless otherwise clearly specified and limited, the terms "installation", "connection" and "connection" 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 a direct connection, or it can be an indirect connection through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood by specific circumstances.
[0026] The specific implementation of the present utility model is described in detail below in conjunction with specific embodiments.
[0027] like Figure 1-12As shown, it is a structural diagram of a UAV battery replacement device provided by an embodiment of the utility model, including a UAV platform 6 and a UAV 11, wherein the UAV platform 6 is a square structure, a laser position sensor 15 is arranged on the top of the UAV platform 6, a battery charging compartment 31 is arranged inside the UAV platform 6, a storage lithium battery 4 is arranged outside the battery charging compartment 31, a UAV battery 32 is placed in the battery charging compartment 31, a battery locking mechanism 14 which cooperates with the UAV battery 32 is arranged inside the UAV 11, a UAV battery positive and negative electrode sheets 322 are arranged on the surface of the UAV battery 32, and a UAV positive electrode sheet 322 which cooperates with the UAV battery positive and negative electrode sheets 322 is arranged on the bottom wall of the UAV 11 Negative electrode sheet 111, battery locking grooves 321 cooperating with the battery locking mechanism 14 are respectively arranged at both ends of the drone battery 32, two groups of Y-axis pulley guides 21 located outside the battery charging compartment 31 are arranged inside the drone platform 6, and a Y-axis pulley 22 is arranged on the surface of the Y-axis pulley guide 21, and a vertical transport platform 5 is arranged on the surface of the Y-axis pulley 22, and a Z-axis lifting gear motor group 23 is arranged between the two groups of Y-axis pulleys 22, and the Z-axis lifting gear motor group 23 is connected to a forklift arm assembly 24, and the forklift arm assembly 24 includes a laser millimeter wave radar 241, and the forklift arm assembly 24 is connected to an X-axis electric linear guide 25, and the forklift arm assembly 24 is connected to a Z-axis lifting rack group 26.
[0028] like Figure 1-12 As shown, as a preferred embodiment of the utility model, the surface of the UAV platform 6 is provided with an electric linear guide clamp 12, and the surface of the UAV platform 6 is provided with an electric linear guide wide clamp 13, and the electric linear guide clamp 12 and the electric linear guide wide clamp 13 are respectively connected to the laser position sensor 15.
[0029] like Figure 1-12 As shown, as a preferred embodiment of the present utility model, the Y-axis pulley 22 is composed of a pulley 221 and a turbine motor 222 , and the output shaft of the turbine motor 222 is connected to the pulley 221 .
[0030] like Figure 1-12 As shown, as a preferred embodiment of the utility model, the vertical transport platform 5 includes a vertical transport ladder rack 51, a vertical transport ladder gear set 52 is arranged on the surface of the vertical transport ladder rack 51, a vertical transport ladder gear motor 53 is arranged on the surface of the vertical transport ladder gear set 52, the vertical transport ladder gear motor 53 is connected to a vertical transport ladder loading platform 54, and a laser ranging radar 55 is arranged on the surface of the vertical transport ladder loading platform 54.
[0031] like Figure 1-12As shown, as a preferred embodiment of the utility model, the Z-axis lifting gear motor group 23 includes a Z-axis gear 231 , the Z-axis gear 231 is connected to a gear group motor 232 , and the output shaft of the gear group motor 232 is connected to the Z-axis gear 231 .
[0032] The working principle of the utility model is: when the battery of the drone 11 is almost exhausted and needs to be replaced, the drone 11 lands on the square drone platform 6, and the laser position sensor 15 works at this time. The laser position sensor 15 is an existing positioning instrument on the market that emits a laser beam and reflects it through an object to locate. When the drone 11 lands, the laser of the laser position sensor 15 irradiates the drone 11 to detect the real-time height of the drone 11. When it is detected that the drone 11 has completely landed, a signal is sent to the electric linear guide fixture 12 and the electric linear guide wide fixture 13, which slide synchronously toward the drone 11 through the slide rail, and fix the landing gear of the drone 11 through the fixture on the electric linear guide until the drone battery compartment is parallel to the battery loading port. The electric linear guide fixture 12 and the electric linear guide wide fixture 13 are fixed under the landing gear by screws and nuts, and are connected to the energy storage lithium battery 4 through wires.
[0033] After that, the vertical transport platform 5 starts working, and the vertical transport ladder gear motor 53 and the vertical transport ladder gear set 52 are connected through the bayonet to transmit power to the vertical transport ladder gear set 52, so that it can rise through the meshing connection of the vertical transport ladder rack 51 and the vertical transport ladder gear set 52 to drive the vertical transport ladder loading platform 54 to rise, until the laser ranging radar 55 detects that the distance between the vertical transport ladder loading platform 54 and the battery compartment of the drone 11 is zero, and is connected to the vertical transport ladder gear motor 53 through wires, and the vertical transport ladder gear motor 53 is connected to the energy storage lithium battery 4 through wires to provide it with power.
[0034] After that, the drone 11 rotates the two battery locking mechanisms 14 through internal system instructions. The battery locking mechanism 14 is composed of a motor and a locking slider. When the motor rotates, it drives the locking slider to rotate and rotate out or into the drone 11. The battery locking grooves 321 on both sides of the drone battery 32 achieve the effect of locking and unlocking the drone battery. After the battery locking mechanism 14 is unlocked, the battery can fall steadily on the vertical transport ladder loading platform 54 with gravity, and then the vertical transport ladder loading platform 54 carrying the battery descends to a fixed height.
[0035] When the vertical conveyor platform 54 carrying the battery descends to a fixed height, the three-axis forklift arm works. The three laser millimeter wave radars 241 on the forklift arm assembly 24 locate the precise position of the battery through millimeter waves. After the laser millimeter wave radar 241 determines the three-dimensional coordinates of the drone battery 32, the pulley motor 222 and the pulley 221 are connected by a bayonet connection to transmit power to the pulley 221, so that it can move forward and backward on the Y-axis pulley guide rail 21, thereby driving the overall movement. The pulley motor 222 is connected to the energy storage lithium battery 4 through wires to supply energy for it. The Z-axis lifting rack set 26 is fixed to the pulley 221 by bolts, and then the gear set motor 232 and the Z-axis gear 231 are connected by a bayonet connection with the Z-axis gear 231 and the Z-axis lifting rack set 26, and then the energy storage lithium battery 4 is connected to the gear set motor 232 by wires to supply energy for it, so that it can move up and down the Z-axis lifting rack set 26. Then, through the movement of the slider on the X-axis electric linear guide 25, the X-axis electric linear guide 25 is fixed to one side of the two gear group motors 232 by screws and nuts, and the X-axis electric linear guide 25 is connected to the energy storage lithium battery 4 through wires for power supply. Through the Y-axis movement of the Y-axis pulley guide 21 and the Y-axis pulley 22, the Z-axis movement of the Z-axis lifting gear motor group 23 and the Z-axis lifting rack group 26, and the X-axis movement of the X-axis electric linear guide 25, the forklift arm assembly 24 can achieve three-axis movement.
[0036] Then, the forklift arm assembly 24 moves through three axes, and through the precise three-dimensional spatial coordinates of the drone battery, the forklift arm assembly 24 can move accurately to the front of the drone battery and pick up the drone battery with the forklift arm through three-axis movement. After the laser millimeter wave radar 241 locates the empty battery charging compartment 31, it transports the drone battery to the empty battery charging compartment 31 through three-axis movement for energy replenishment and charging.
[0037] After the exhausted drone battery 32 is returned to the battery charging compartment 31 for charging, the laser millimeter wave radar 241 on the forklift arm assembly 24 begins to reposition to a three-dimensional coordinate system of a fully charged drone battery. Then, through the overall three-axis movement, the forklift arm assembly 24 forks the fully charged drone battery onto the vertical conveyor ladder loading platform 54, and ensures that the groove at the bottom of the drone battery corresponds to the groove on the vertical conveyor ladder loading platform 54 and moves it out to a position that does not affect the operation of the lifting platform. The groove at the bottom of the drone battery 32 corresponds to the groove on the vertical conveyor ladder loading platform 54, which ensures that the drone battery can be smoothly returned to the battery compartment of the drone. Through the meshing of the vertical conveyor ladder gear set 52 and the vertical conveyor ladder rack 51, the power provided by the vertical conveyor ladder gear motor 53 drives the vertical conveyor ladder loading platform 54 to rise, thereby driving the fully charged drone battery to move upward. When the laser ranging radar 55 measures that the distance to the bottom of the drone is 0, the vertical conveyor ladder loading platform 54 stops, which means that the fully charged drone battery has been loaded into the battery compartment of the drone. The drone electrode sheet 111 has a metal spring, so the drone electrode sheet 111 and the drone battery positive and negative plates 322 can ensure a good connection to power on the drone. The drone is back online and detects that the battery replacement is complete, and fixes the drone battery 32 through the battery locking mechanism 14. Then the electric linear guide fixture 12 and the electric linear guide wide fixture 13 move in the opposite direction, releasing the fixed drone 11, and the drone 11 takes off again. At this point, the drone 11 is fully powered.
[0038] The above describes in detail the preferred implementation of this patent, but this patent is not limited to the above implementation. Various changes can be made within the knowledge scope of ordinary technicians in this field without departing from the purpose of this patent.
Claims
1. A UAV battery replacement device, comprising a UAV platform and a UAV, characterized in that: The UAV platform is a square structure, a laser position sensor is arranged on the top of the UAV platform, a battery charging compartment is arranged inside the UAV platform, a storage lithium battery is arranged outside the battery charging compartment, a UAV battery is placed in the battery charging compartment, a battery locking mechanism that cooperates with the UAV battery is arranged inside the UAV, the UAV battery surface is provided with positive and negative electrodes of the UAV battery, the bottom wall of the UAV is provided with UAV positive and negative electrodes that cooperate with the positive and negative electrodes of the UAV battery, and battery locking grooves that cooperate with the battery locking mechanism are respectively arranged at both ends of the UAV battery, two groups of Y-axis pulley guides located outside the battery charging compartment are arranged inside the UAV platform, a Y-axis pulley is arranged on the surface of the Y-axis pulley guide, a vertical transport platform is arranged on the surface of the Y-axis pulley, a Z-axis lifting gear motor group is arranged between the two groups of Y-axis pulleys, and the Z-axis lifting gear motor group is connected to a forklift arm assembly, the forklift arm assembly includes a laser millimeter wave radar, the forklift arm assembly is connected to an X-axis electric linear guide, and the forklift arm assembly is connected to a Z-axis lifting rack group.
2. The UAV battery replacement device according to claim 1, characterized in that: The surface of the UAV platform is provided with an electric linear guide fixture, and the surface of the UAV platform is provided with an electric linear guide wide fixture, and the electric linear guide fixture and the electric linear guide wide fixture are respectively connected to the laser position sensor.
3. The UAV battery replacement device according to claim 1, characterized in that: The Y-axis pulley is composed of a pulley and a turbine motor, and the output shaft of the turbine motor is connected to the pulley.
4. The UAV battery replacement device according to claim 1, characterized in that: The vertical transport platform includes a vertical transport ladder rack, a vertical transport ladder gear set is arranged on the surface of the vertical transport ladder rack, a vertical transport ladder gear motor is arranged on the surface of the vertical transport ladder gear set, the vertical transport ladder gear motor is connected to the vertical transport ladder loading platform, and a laser ranging radar is arranged on the surface of the vertical transport ladder loading platform.
5. The UAV battery replacement device according to claim 1, characterized in that: The Z-axis lifting gear motor group includes a Z-axis gear, the Z-axis gear is connected to a gear group motor, and the output shaft of the gear group motor is connected to the Z-axis gear.