Automatic battery changing device for unmanned aerial vehicle

By designing the automatic battery swap device of the drone and using alternating power exchange mechanisms and other components to realize automated battery swap and management, the existing drone's problems of low battery swap efficiency and poor portability are solved, and the battery swap efficiency and convenience are improved.

CN119568474AInactive Publication Date: 2025-03-07朱朗铭
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Patent Information

Application Number
CN202411851549.1
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2024-12-16
Publication Date
2025-03-07
Estimated Expiration
Not applicable · inactive patent

AI Technical Summary

Technical Problem

Existing drones require manual disassembly and install batteries when replacing batteries, which are inefficient and have safety risks. Large battery swap stations are large in size and are not portable, and cannot be efficiently managed and charged and back-up.

Method used

An automatic battery replacement device for drone is designed, including an alternating battery replacement mechanism, a battery compartment, a battery block, a lock box and a locking mechanism, a positioning mechanism and a mobile board arranged inside the battery swap box, and automatic battery replacement and management are realized through these components.

Benefits of technology

It realizes rapid and automated battery swap of the drone battery block, can manage and charge and backup the replaced battery block, improves battery swap efficiency and convenience, and the device is small in size and easy to carry.

✦ Generated by Eureka AI based on patent content.

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Abstract

The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle automatic battery replacing device which comprises a battery replacing box, and the automatic battery replacing device comprises an alternating type battery taking and replacing mechanism arranged in the battery replacing box; the battery bin is arranged in the unmanned aerial vehicle body, and a battery block is mounted in the battery bin; the battery replacing device comprises a battery bin, a battery block is arranged in the battery bin, the battery block is arranged in the battery bin, the lock box is arranged at the bottom of the battery block, the lock box is connected with the battery bin through a locking mechanism, and the alternating type battery taking and replacing mechanism is used in cooperation with the locking mechanism. According to the unmanned aerial vehicle, the battery block of the unmanned aerial vehicle body can be rapidly and automatically replaced, the replaced battery block can be managed and charged for standby application, and the whole device is small in size and convenient to carry when a user goes out.
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Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicles, and in particular to an automatic battery replacement device for unmanned aerial vehicles. Background Art

[0002] With the rapid development of science and technology, drone technology has been widely used in aerial photography, agricultural plant protection, geographic surveying and mapping, logistics and distribution and other fields. The widespread use of drones has greatly improved work efficiency and broadened the scope of operations. However, the endurance of drones has always been a key factor restricting their further development. Due to the limited battery power of drones, the single flight time is often short, which greatly limits the operating range and duration of drones.

[0003] Existing drones usually use manual methods or large-scale battery replacement stations to disassemble and replace batteries when replacing batteries, which has the following defects: 1. Manual removal and installation of batteries is not only time-consuming and labor-intensive, but also increases operational difficulty and safety risks, resulting in low battery replacement efficiency and a lack of real-time battery charging and backup battery management functions.

[0004] 2. Large battery swap stations are large in size and difficult to carry. In addition, they cannot efficiently replace batteries and charge the replaced batteries for backup. Summary of the invention

[0005] The present invention provides an automatic battery replacement device for a drone to solve the problem that the existing drones cannot automatically replace batteries and charge batteries for standby during battery replacement.

[0006] The technical solution of the present invention to solve the above technical problems is as follows: Provided is an automatic battery replacement device for a drone, comprising a battery replacement box, the automatic battery replacement device comprising: An alternating battery-taking and battery-swapping mechanism disposed inside the battery-swapping box; A battery compartment is disposed inside the drone body, wherein a battery block is installed inside the battery compartment; A lock box is arranged at the bottom of the battery block, the lock box is connected to the battery compartment through a locking mechanism, and the alternating battery replacement mechanism is used in conjunction with the locking mechanism; A box cover is arranged on the top of the battery-changing box, a positioning mechanism is arranged on the side wall of the box cover, and the drone body is connected to the box cover in a limited position through the positioning mechanism; and A movable plate is movably arranged inside the battery exchange box, and the movable plate drives the alternating battery exchange mechanism to move through a movable component.

[0007] The beneficial effects of the present invention are: The present invention designs a battery replacement device that can automatically replace the battery block of the drone body, which can realize the rapid and automatic battery replacement operation of the battery block of the drone body, manage the replaced battery block, and charge the replaced battery block for standby. The overall device is small in size and easy to carry outside, which is specifically embodied in the following aspects: In the process of battery replacement, traditional UAVs usually replace batteries manually or at large-scale battery replacement stations. Manual battery replacement has the problems of low efficiency, great difficulty in operation and certain safety hazards. Large-scale battery replacement stations are not easy to carry and cannot manage and charge the replaced batteries. The alternating battery replacement mechanism of the present invention can automatically remove and replace the battery blocks inside the battery compartment, and can realize alternating replacement of the removed battery blocks and the spare battery blocks, while managing and charging the replaced battery blocks. The locking mechanism can realize fast and stable locking and unlocking of the battery blocks and the battery compartment, and the positioning mechanism can realize the stability of the UAV body during battery replacement, realize automatic battery replacement operation of the battery blocks of the UAV body, manage and charge the replaced battery blocks, improve the battery replacement efficiency, and the whole device is easy to carry, which improves the convenience of battery replacement. BRIEF DESCRIPTION OF THE DRAWINGS

[0008] Figure 1 This is an overall structural view of an embodiment of the present invention; Figure 2 It is an overall left-side structural view of an embodiment of the present invention; Figure 3 In one embodiment of the present invention Figure 2 The three-dimensional cross-section view at AA in the middle; Figure 4 In one embodiment of the present invention Figure 3 A magnified structural view at center A; Figure 5 A structural view of a battery compartment, a battery block and a lock box in one embodiment of the present invention; Figure 6 A structural diagram of a mobile assembly in one embodiment of the present invention; Figure 7 A structural view of a positioning mechanism in one embodiment of the present invention; Figure 8 This is a disassembled structural view of an alternate power exchange mechanism in one embodiment of the present invention; Fig. 9 This is a disassembled structural view of a locking mechanism in one embodiment of the present invention; In the accompanying drawings, the components represented by the reference numerals are listed as follows: 1. Battery replacement box; 2. Alternating battery replacement mechanism; 3. Drone body; 4. Battery compartment; 5. Battery pack; 6. Lock box; 7. Locking mechanism; 8. Box cover; 9. Positioning mechanism; 10. Moving plate; 11. Moving assembly; Alternating battery replacement mechanism; 201, first electric push rod; 202, motor box; 203, drive motor; 204, unlocking cam; 205, positioning plate; 206, positioning hole; 207, positioning block; 208, charging seat; Locking mechanism; 701, through-hole; 702, driving block; 703, unlocking slot; 704, connecting seat; 705, pull rod; 706, pushing piece; 707, first spring; 708, pressure plate; 709, locking plate; 710, locking rod; 711, locking hole; 9 positioning mechanism; 901, T-shaped foot; 902, positioning cylinder; 903, movable slot; 904, second electric push rod; 905, positioning bar; 906, empty slot; Moving assembly; 111, slide rail; 112, slide block; 113, third electric push rod; Reinforcement block; 13. T-bar; 14. Reinforcement spring; 15. Guide plate; 16. Guide cylinder; 17. Guide rod; 18. Battery; 19. Threaded column; 20. Adjustment foot; 21. Heat dissipation port; 22. Protective frame. DETAILED DESCRIPTION

[0009] In order to make the purpose, technical scheme and advantages of the present invention clearer, the present invention is further described in detail below in conjunction with the accompanying drawings and embodiments. Examples of the embodiments are shown in the accompanying drawings, wherein the same or similar reference numerals throughout represent the same or similar elements or elements with the same or similar functions. The embodiments described below with reference to the accompanying drawings are exemplary and are only used to explain the present invention, and should not be construed as limiting the present invention. In addition, it should be understood that the specific embodiments described herein are only used to explain the present invention and are not intended to limit the present invention.

[0010] In the description of the present invention, it is necessary to understand that the terms "length", "width", "up", "down", "left", "right", "horizontal", "top", "bottom", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present invention 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 on the present invention.

[0011] In addition, the terms "first" and "second" are used for descriptive purposes only and should not be understood as indicating or implying relative importance or implicitly indicating the number of the indicated technical features. Therefore, the features defined as "first" and "second" may explicitly or implicitly include one or more of the features. In the description of the present invention, the meaning of "plurality" is two or more, unless otherwise clearly and specifically defined.

[0012] In the description of the present invention, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "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, an electrical connection, or mutual communication; it can be a direct connection, or an indirect connection through an intermediate medium, it can be the internal connection of two elements or the interaction relationship between two elements. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.

[0013] In the present invention, unless otherwise clearly specified and limited, a first feature being "above" or "below" a second feature may include that the first and second features are in direct contact, or may include that the first and second features are not in direct contact but are in contact through another feature between them. Moreover, a first feature being "above", "above" and "above" a second feature includes that the first feature is directly above and obliquely above the second feature, or simply indicates that the first feature is higher in level than the second feature. A first feature being "below", "below" and "below" a second feature includes that the first feature is directly below and obliquely below the second feature, or simply indicates that the first feature is lower in level than the second feature.

[0014] The disclosure below provides many different embodiments or examples for realizing different structures of the present invention. In order to simplify the disclosure of the present invention, the components and settings of specific examples are described below. Of course, they are merely examples, and the purpose is not to limit the present invention. In addition, the present invention may repeat reference numbers and / or reference letters in different examples, and such repetition is for the purpose of simplification and clarity, and does not itself indicate the relationship between the various embodiments and / or settings discussed. In addition, the present invention provides examples of various specific processes and materials, but those of ordinary skill in the art may be aware of the application of other processes and / or the use scenarios of other materials.

[0015] The present invention provides the following preferred embodiments: Example

[0016] refer to Figure 1 , Figure 2 , Figure 3 and Figure 4As shown, an automatic battery replacement device for a drone includes a battery replacement box 1, and the automatic battery replacement device includes: An alternating battery exchange mechanism 2 disposed inside the battery exchange box 1; A battery compartment 4 is disposed inside the drone body 3, and a battery block 5 is installed inside the battery compartment 4; A lock box 6 is arranged at the bottom of the battery block 5, the lock box 6 is connected to the battery compartment 4 through a locking mechanism 7, and the alternating battery exchange mechanism 2 is used in conjunction with the locking mechanism 7; A box cover 8 is arranged on the top of the battery exchange box 1, and a positioning mechanism 9 is arranged on the side wall of the box cover 8. The drone body 3 is connected to the box cover 8 by the positioning mechanism 9 and the positioning mechanism 9; and A movable plate 10 is movably arranged inside the battery exchange box 1, and the movable plate 10 drives the alternating battery exchange mechanism 2 to move through the movable component 11.

[0017] By providing a battery replacement box 1, an alternating battery replacement mechanism 2, a battery compartment 4, a battery block 5, a lock box 6, a locking mechanism 7, a box cover 8, a positioning mechanism 9, a movable plate 10 and a movable component 11, an automated battery replacement operation for the drone body 3 is realized, the battery block 5 inside the battery compartment 4 can be automatically taken out and replaced, the replaced battery block 5 can be managed and charged for standby use, and the whole is easy to carry, thereby improving the battery replacement efficiency and convenience of replacing the battery block 5 for the drone body 3.

[0018] When using the drone's automatic battery replacement device, follow these steps: Positioning of the drone body 3: The positioning mechanism 9 is used to realize the limit connection between the drone body 3 and the box cover 8, so that the drone body 3 can stably perform the battery replacement operation; Alternating battery removal and replacement: The battery block 5 inside the battery compartment 4 can be automatically taken out by the alternating battery removal and replacement mechanism 2. The alternating battery removal and replacement mechanism 2 cooperates with the locking mechanism 7 to unlock the locking mechanism 7, so that the battery block 5 and the lock box 6 are taken out from the battery compartment 4. The spare battery block 5 is taken out while the battery block 5 inside the battery compartment 4 is taken out. At the same time, the movable plate 10 is moved by the movable component 11. The movable plate 10 drives the alternating battery removal and replacement mechanism 2 to move, so that the spare battery block 5 is located below the drone body 3 for installation. At the same time, the taken out battery block 5 is placed in the battery replacement box 1 for management and charging standby.

[0019] In this embodiment, the automatic battery replacement device for the drone can automatically complete the battery removal and replacement operations of the battery pack 5, and can manage and charge the replaced battery pack 5 for standby, thereby improving the efficiency and safety of replacing the battery pack 5 of the drone body 3. Example

[0020] refer to Figure 7 and Figure 8 As shown, the alternating power exchange mechanism 2 includes: Two sets of first electric push rods 201 installed on the top of the moving plate 10; A motor box 202 is installed at the output end of the first electric push rod 201, and a driving motor 203 is installed inside the motor box 202; An unlocking cam 204 fixedly connected to the output end of the driving motor 203; A positioning plate 205 is fixedly connected to the top of the motor box 202, and positioning holes 206 are formed at both ends of the positioning plate 205; Two positioning blocks 207 are provided at the bottom of the lock box 6, and the positioning holes 206 are adapted to the positioning blocks 207; and Two charging seats 208 are arranged on the side wall of the box cover 8, and the charging seats 208 are adapted to the battery pack 5.

[0021] By setting the first electric push rod 201, the motor box 202, the drive motor 203, the unlocking cam 204, the positioning plate 205, the positioning hole 206, the positioning block 207 and the charging seat 208, the two first electric push rods 201 respectively drive the positioning plate 205 to contact the lock box 6 inside the battery compartment 4 and the lock box 6 inside the charging seat 208, so that the positioning plate 205 and the lock box 6 are limitedly connected, and the unlocking cam 204 can be driven by the drive motor 203 to unlock the two lock boxes 6 respectively, so that the two lock boxes 6 are unlocked with the battery compartment 4 and the charging seat 208 respectively. The two battery blocks 5 are then taken out respectively, and the moving assembly 11 drives the moving plate 10 to move, so that the spare battery block 5 is located below the drone body 3, and the used battery block 5 is located below another set of charging seats 208. The first electric push rod 201 is started to transport the battery blocks 5 to the inside of the battery compartment 4 and the charging seat 208 respectively, and then the reverse drive of the driving motor 203 is used to realize the unlocking operation of the lock box 6, so that the lock box 6 is connected with the battery compartment 4 and the charging seat 208 to achieve the limit connection, and the battery block 5 is taken out and replaced. The implementation method is as follows: Positioning unlocking: After the drone body 3 is limitedly locked between the positioning mechanism 9 and the box cover 8, the two first electric push rods 201 respectively drive the positioning plate 205 to contact the lock box 6 inside the battery compartment 4 and the lock box 6 inside the charging seat 208, so that a limited connection is achieved between the positioning plate 205 and the lock box 6. The driving motor 203 can drive the unlocking cam 204 to unlock the two lock boxes 6 respectively, so that the two lock boxes 6 are unlocked from the battery compartment 4 and the charging seat 208 respectively.

[0022] Alternating battery removal and replacement: When the two battery blocks 5 are unlocked, the first electric push rod 201 takes the battery block 5 out from the battery compartment 4 and the charging seat 208, and drives the movement of the moving plate 10 through the moving component 11, so that the spare battery block 5 is located below the drone body 3, and the used battery block 5 is located below another group of charging seats 208. By starting the first electric push rod 201 to transport, the battery blocks 5 are transported to the battery compartment 4 and the charging seat 208 respectively, and then the reverse drive of the driving motor 203 is used to realize the unlocking operation of the lock box 6, so that the lock box 6 is limitedly connected with the battery compartment 4 and the charging seat 208, and the battery removal and replacement operation of the battery block 5 is completed.

[0023] In this embodiment, through the cooperation of the first electric push rod 201, the positioning plate 205, the drive motor 203 and the unlocking block, the unlocking operation between the lock box 6 and the battery compartment 4 and the charging seat 208 is realized, and the battery block 5 can be taken out and replaced at the same time, realizing the automatic battery replacement of the battery block 5, and managing and charging the battery block 5 after the replacement. Example

[0024] refer to Figure 8 and Fig. 9 As shown, the locking mechanism 7 includes: A through hole 701 formed on the side wall of the lock box 6; A driving block 702 movably disposed inside the lock box 6, the driving block 702 is arranged in an elliptical cam shape, and an unlocking groove 703 is provided on the side wall of the driving block 702, and the unlocking groove 703 is adapted to the unlocking cam 204; Two connecting seats 704 are respectively fixedly connected to the two side walls of the lock box 6, and a pull rod 705 is movably provided in the middle of the two connecting seats 704; A push piece 706 fixedly connected to the side wall of the pull rod 705, and two push pieces 706 are respectively located on both sides of the driving block 702; Two pressure plates 708 are fixedly connected to the side wall of the pull rod 705, and a first spring 707 is arranged between the pressure plate 708 and the connecting seat 704; A lock plate 709 fixedly connected to one end of the pull rod 705, two lock rods 710 fixedly connected to the side wall of the lock plate 709, and the lock rods 710 are movably connected to the lock box 6; and The locking holes 711 are respectively formed on the inner wall of the battery compartment 4 and the charging base 208 , and the locking rod 710 is matched with the locking holes 711 .

[0025] By setting the through opening 701, the driving block 702, the unlocking groove 703, the connecting seat 704, the pull rod 705, the pushing piece 706, the pressure plate 708, the first spring 707, the locking plate 709, the locking rod 710 and the locking hole 711, the lock box 6 is locked and limited with the battery compartment 4 and the charging seat 208 through the adaptation of the locking rod 710 and the locking hole 711, and the driving block 702 is rotated to push the pushing piece 706, and the pushing piece 706 drives the pull rod 705 to move. In this process, the pull rod 705 drives the locking plate 709 to move so that the locking rod 710 is separated from the locking hole 711, thereby realizing the unlocking operation of the lock box 6 with the battery compartment 4 and the charging seat 208. The unlocking cam 204 is adapted to the unlocking groove 703 so that the unlocking cam 204 can drive the rotation of the driving block 702, thereby realizing the locking and unlocking of the unlocking box 6. The implementation method is as follows: Battery block 5 locking: When the battery block 5 is placed in the lock box 6 or the battery compartment 4, the lock rod 710 at one end of the lock plate 709 will automatically align with the lock hole 711 on the side wall of the lock box 6 or the battery compartment 4. Since the first spring 707 is provided between the two pressure plates 708 on the side wall of the pull rod 705 and the connecting seat 704, the first spring 707 is in a supporting state to provide a supporting force for the pull rod 705. Under the action of the first spring 707, the lock rod 710 will be firmly supported into the lock hole 711 to achieve battery locking; Unlocking the battery block 5: First, the positioning plate 205 is unlocked from the lock box 6, and the positioning hole 206 and the positioning block 207 are adapted to realize a limited connection between the positioning plate 205 and the lock box 6. The through-hole 701 on the side wall of the lock box 6 allows the unlocking cam 204 to enter the interior of the lock box 6 and contact the unlocking groove 703 on the side wall of the driving block 702. When the battery needs to be unlocked, the driving motor 203 is started to drive the unlocking cam 204 to rotate. The rotation of the unlocking cam 204 will push the driving block 702 (elliptical cam shape) to rotate in the lock box 6. The rotation of the driving block 702 will squeeze the movement of the push sheet 706, so that the push sheet 706 drives the pull rod 705 to move. In this process, the movement of the pull rod 705 causes the pressure plate 708 to squeeze the first spring 707 to contract, so that the lock plate 709 follows the movement of the pull rod 705. In this process, the lock rod 710 disengages from the lock hole 711.

[0026] In this embodiment, the driving block 702 pushes the pushing plate 706, so that the pull rod 705 can move in the middle of the connecting seat 704, realize the separation of the locking rod 710 and the locking hole 711, and realize the unlocking operation of the lock box 6. The cooperation between the locking rod 710 and the locking hole 711 enables the lock box 6 to be locked with the battery compartment 4 or the charging seat 208. Example

[0027] refer to Figure 5 and Figure 7 As shown, the positioning mechanism 9 includes: Four T-shaped feet 901 provided at the feet of the drone body 3; Four positioning cylinders 902 are arranged on the side wall of the box cover 8, and the T-shaped feet 901 are adapted to the positioning cylinders 902; A movable groove 903 is provided on the side wall of the positioning tube 902; A second electric push rod 904 is mounted on the side wall of the box cover 8, and the output end of the second electric push rod 904 is fixedly connected to two positioning bars 905; and Two empty slots 906 are formed on the side wall of the positioning strip 905 , and the side wall of the positioning strip 905 is in contact with the T-shaped foot 901 .

[0028] By setting the T-shaped foot 901, the positioning tube 902, the movable groove 903, the second electric push rod 904, the positioning bar 905 and the empty groove 906, the second electric push rod 904 pushes the positioning bar 905 to move, so that the empty groove 906 and the movable groove 903 move. When the drone body 3 is parked on the box cover 8, the T-shaped foot 901 enters the interior of the positioning tube 902, and the positioning bar 905 moves and contacts with the T-shaped foot 901 to limit the T-shaped foot 901, so that the drone body 3 can achieve stable battery replacement operation. The implementation method is as follows: Positioning and parking of the drone body 3: When the drone body 3 is parked on the box cover 8, the T-shaped foot 901 enters the interior of the positioning tube 902 to achieve positioning and parking of the drone body 3; Limiting the drone body 3: First, the empty groove 906 on the side wall of the positioning groove is located on one side of the positioning tube 902. During this process, the T-shaped foot 901 can enter the interior of the positioning tube 902. Then the second electric push rod 904 pushes the positioning bar 905 to move, so that the positioning bar 905 contacts the T-shaped foot 901. At this time, the T-shaped foot 901 is limited to achieve the limitation of the drone body 3.

[0029] In this embodiment, the positioning bar 905 limits the T-shaped foot 901 to achieve limit locking of the drone body 3, so that the drone body 3 can be parked in a limited position, allowing the drone body 3 to perform stable battery replacement operations. Example

[0030] refer to Figure 6 As shown, the mobile component 11 includes: Two slide rails 111 installed inside the battery exchange box 1, two sliders 112 movably arranged inside the slide rails 111, and the sliders 112 are fixedly connected to the movable plate 10; and The third electric push rod 113 is installed inside the battery-changing box 1 , and the output end of the third electric push rod 113 is fixedly connected to the movable plate 10 .

[0031] By providing the slide rail 111, the slider 112 and the third electric push rod 113, the movable plate 10 can be moved by the conveyance of the third electric push rod 113, and the movement of the movable plate 10 can be guided and limited by the provision of the slider 112 and the slide rail 111. The implementation method is as follows: After the two battery blocks 5 are taken out, they are pulled into the battery exchange box 1 following the first electric push rod 201. At this time, the third electric push rod 113 pushes or pulls the movable plate 10 to move. During this process, the slider 112 moves inside the slide rail 111 to support and guide the movement of the movable plate 10.

[0032] In this embodiment, the slide rail 111 , the slider 112 and the third electric push rod 113 cooperate to achieve stable driving movement of the moving plate 10 , so that the moving plate 10 can drive the battery block 5 to move alternately. Example

[0033] refer to Fig. 9 As shown, a reinforcement block 12 is fixedly connected to the interior of the lock box 6, a T-bar 13 is fixedly connected to the side wall of the lock plate 709, the T-bar 13 is movably connected to the reinforcement block 12, a reinforcement spring 14 is sleeved on the side wall of the T-bar 13, and both ends of the reinforcement spring 14 are in contact with the lock plate 709 and the reinforcement block 12 respectively.

[0034] By providing the reinforcement block 12, the T-shaped rod 13 and the reinforcement spring 14, when in use, the reinforcement spring 14 can be provided to reinforce and support the lock plate 709, thereby improving the stability of the lock rod 710 inside the lock hole 711. The implementation method is as follows: When the locking rod 710 enters the locking hole 711, the locking plate 709 is supported by the reinforcement spring 14, so that the locking rod 710 is stably placed inside the locking hole 711. When unlocking, the locking plate 709 squeezes the reinforcement spring 14. During this process, the T-bar 13 moves in the middle of the reinforcement block 12 to guide and protect the reinforcement spring 14.

[0035] In this embodiment, by providing the reinforcing spring 14 , the lock plate 709 can be reinforced and stabilized, so that the lock rod 710 is stably located inside the lock hole 711 . Example

[0036] refer to Figure 8 As shown, the output end of the first electric push rod 201 is fixedly connected to a guide plate 15, two guide cylinders 16 are fixedly connected to the side wall of the guide plate 15, and a plurality of guide rods 17 are fixedly connected to the side wall of the movable plate 10, and the guide rods 17 are movably connected to the guide cylinders 16.

[0037] By providing the guide plate 15, the guide cylinder 16 and the guide rod 17, the movement of the guide cylinder 16 and the guide rod 17 guides and reinforces the output of the first electric push rod 201, and the implementation method is as follows: During use, when the first electric push rod 201 pushes and pulls the motor box 202 to move, the guide plate 15 drives the guide cylinder 16 to move, and the movement of the guide cylinder 16 and the guide rod 17 guides and reinforces the movement of the first electric push rod 201 .

[0038] In this embodiment, the movement of the first electric push rod 201 is guided and reinforced by the cooperation of the guide plate 15 , the guide cylinder 16 and the guide rod 17 . Example

[0039] refer to Figure 6 As shown, two groups of batteries 18 are installed inside the battery swap box 1. The batteries 18 are electrically connected to the charging seat 208, and the batteries 18 provide power for the internal electrical equipment of the battery swap box 1.

[0040] By providing the storage battery 18, the storage battery 18 can provide power to the power equipment inside the battery swap box 1, and can charge the battery block 5 inside the charging seat 208. The implementation method is as follows: When the battery exchange box 1 performs a battery exchange operation, the battery 18 provides power to the internal power equipment. When the charging seat 208 charges the battery block 5, the battery 18 provides power to the charging seat 208.

[0041] In this embodiment, through the operation of the battery 18, the battery replacement box 1 can operate outdoors without power supply. Example

[0042] refer to Figure 2 As shown, four threaded columns 19 are fixedly connected to the bottom surface of the battery swap box 1 , and the four threaded columns 19 are distributed at the corners of the battery swap box 1 . Adjustment feet 20 are threadedly connected to the side walls of the threaded columns 19 .

[0043] By setting the threaded column 19 and the adjusting foot 20, the power exchange box 1 is supported and horizontally adjusted by the threaded column 19 and the adjusting foot 20, and the implementation method is as follows: When in use, the battery swap box 1 can be adjusted horizontally by rotating the four adjustment feet 20 and the threaded movement of the threaded column 19 respectively, so that the battery swap box 1 can be placed horizontally on the placement surface.

[0044] In this embodiment, through the cooperation of the threaded column 19 and the adjustment foot 20, the battery swap box 1 can be supported and adjusted, so that the battery swap box 1 can be placed stably and horizontally on the placement surface. Example

[0045] refer to Figure 1 As shown, heat dissipation openings 21 are provided on both side walls of the battery exchange box 1 , and a protective frame 22 is provided inside the heat dissipation openings 21 .

[0046] By providing the heat dissipation port 21 and the protection frame 22, the air inside and outside the power exchange box 1 can be circulated through the heat dissipation port 21, and the power equipment inside the power exchange box 1 is cooled. The implementation method is as follows: When the battery swap box 1 is in operation, the heat inside the battery swap box 1 is dissipated through the heat dissipation port 21 , and the heat dissipation port 21 is protected by the protective frame 22 .

[0047] In this embodiment, the heat dissipation and protection of the power exchange box 1 are achieved through the cooperation of the heat dissipation port 21 and the protection frame 22.

[0048] It should be noted that the present invention is an automatic battery replacement device for unmanned aerial vehicles. When in use, when the unmanned aerial vehicle body 3 is parked on the box cover 8, the T-shaped foot 901 enters the interior of the positioning tube 902, and the positioning bar 905 moves and contacts with the T-shaped foot 901 to limit the T-shaped foot 901, so that the unmanned aerial vehicle body 3 can achieve stable battery replacement operation. The two first electric push rods 201 respectively drive the positioning plate 205 to contact the lock box 6 inside the battery compartment 4 and the lock box 6 inside the charging seat 208. The positioning hole 206 is adapted to the positioning block 207, so that the positioning plate 205 and the lock box 6 are limitedly connected. The through-hole 701 on the side wall of the lock box 6 allows the unlocking cam 204 to enter the lock box 6 and contact the unlocking groove 703 on the side wall of the driving block 702. When it is necessary to unlock the battery, the driving motor 203 is started to drive the unlocking cam 204 to rotate, and the rotation of the unlocking cam 204 will push the driving block 702 (elliptical cam setting) When rotating in the lock box 6, the rotation of the drive block 702 will squeeze the movement of the push piece 706, so that the push piece 706 drives the pull rod 705 to move. In this process, the movement of the pull rod 705 causes the pressure plate 708 to squeeze the first spring 707 to contract, so that the lock plate 709 moves with the pull rod 705. In this process, the lock rod 710 disengages from the lock hole 711, and then the two groups of first electric push rods 201 pull the battery block 5 into the battery exchange box 1, and the third electric push rod 113 pushes or pulls the movable plate 10 to move, so that the spare battery block 5 is located below the drone body 3, and the used battery block 5 is located below another group of charging seats 208. By starting the transportation of the first electric push rod 201, the battery block 5 is respectively transported to the battery compartment 4 and the charging seat 208, and then the reverse driving of the drive motor 203 is realized to realize the unlocking operation of the lock box 6, so that the lock box 6 is limitedly connected with the battery compartment 4 and the charging seat 208, and the battery removal and replacement operation of the battery block 5 is completed.

[0049] The beneficial effects of the present invention are specifically embodied in that the above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. An automatic battery replacement device for a drone, comprising a battery replacement box (1), characterized in that: The automatic battery replacement device comprises: An alternating battery exchange mechanism (2) disposed inside the battery exchange box (1); A battery compartment (4) disposed inside the drone body (3), wherein a battery block (5) is installed inside the battery compartment (4); A lock box (6) is arranged at the bottom of the battery block (5), the lock box (6) is connected to the battery compartment (4) via a locking mechanism (7), and the alternating battery replacement mechanism (2) is used in conjunction with the locking mechanism (7); A box cover (8) is arranged on the top of the battery exchange box (1), a positioning mechanism (9) is arranged on the side wall of the box cover (8), and the drone body (3) is connected to the box cover (8) in a limited position through the positioning mechanism (9); and A movable plate (10) is movably arranged inside the battery exchange box (1), and the movable plate (10) drives the alternating battery exchange mechanism (2) to move via a movable component (11).

2. The automatic battery replacement device for drone according to claim 1, characterized in that: The alternating power supply mechanism (2) comprises: Two sets of first electric push rods (201) installed on the top of the moving plate (10); A motor box (202) installed at the output end of the first electric push rod (201), wherein a driving motor (203) is installed inside the motor box (202); An unlocking cam (204) fixedly connected to the output end of the driving motor (203); A positioning plate (205) fixedly connected to the top of the motor box (202), with positioning holes (206) being provided at both ends of the positioning plate (205); Two positioning blocks (207) are arranged at the bottom of the lock box (6), and the positioning holes (206) are adapted to the positioning blocks (207); and Two charging seats (208) are arranged on the side wall of the box cover (8), and the charging seats (208) are compatible with the battery block (5).

3. The automatic battery replacement device for unmanned aerial vehicles according to claim 2, characterized in that: The locking mechanism (7) comprises: A through opening (701) formed on the side wall of the lock box (6); a driving block (702) movably arranged inside the lock box (6), the driving block (702) being arranged in an elliptical cam shape, an unlocking groove (703) being provided on a side wall of the driving block (702), the unlocking groove (703) being adapted to the unlocking cam (204); Two connecting seats (704) respectively fixedly connected to the two side walls of the lock box (6), and a pull rod (705) is movably provided in the middle of the two connecting seats (704); A push piece (706) fixedly connected to the side wall of the pull rod (705), wherein the two push pieces (706) are respectively located on both sides of the driving block (702); Two pressure plates (707) are fixedly connected to the side walls of the pull rod (705), and a first spring (708) is provided between the pressure plates (707) and the connecting seat (704); A lock plate (709) fixedly connected to one end of the pull rod (705), two lock rods (710) fixedly connected to the side wall of the lock plate (709), and the lock rods (710) are movably connected to the lock box (6); and Lock holes (711) are respectively provided on the inner walls of the battery compartment (4) and the charging seat (208), and the lock rod (710) is adapted to fit the lock holes (711).

4. The automatic battery replacement device for drone according to claim 1, characterized in that: The positioning mechanism (9) comprises: Four T-shaped feet (901) arranged at the feet of the drone body (3); Four positioning cylinders (902) are arranged on the side wall of the box cover (8), and the T-shaped feet (901) are adapted to the positioning cylinders (902); A movable groove (903) formed on the side wall of the positioning cylinder (902); a second electric push rod (904) mounted on the side wall of the box cover (8), the output end of the second electric push rod (904) being fixedly connected to two positioning bars (905); and Two empty grooves (906) are formed on the side wall of the positioning strip (905), and the side wall of the positioning strip (905) is in contact with the T-shaped foot (901).

5. The automatic battery replacement device for drone according to claim 1, characterized in that: The moving component (11) comprises: Two slide rails (111) installed inside the battery exchange box, two sliders (112) movably arranged inside the slide rails (111), the sliders (112) being fixedly connected to the movable plate (10); and A third electric push rod (113) is installed inside the battery exchange box (1), and an output end of the third electric push rod (113) is fixedly connected to the movable plate (10).

6. The automatic battery replacement device for drone according to claim 3, characterized in that: A reinforcing block (12) is fixedly connected to the interior of the lock box (6), a T-shaped rod (13) is fixedly connected to the side wall of the lock plate (709), the T-shaped rod (13) is movably connected to the reinforcing block (12), a reinforcing spring (14) is sleeved on the side wall of the T-shaped rod (13), and two ends of the reinforcing spring (14) are respectively in contact with the lock plate (709) and the reinforcing block (12).

7. The automatic battery replacement device for drone according to claim 2, characterized in that: The output end of the first electric push rod (201) is fixedly connected to a guide plate (15), the side wall of the guide plate (15) is fixedly connected to two guide cylinders (16), the side wall of the movable plate (10) is fixedly connected to a plurality of guide rods (17), and the guide rods (17) are movably connected to the guide cylinders (16).

8. The automatic battery replacement device for drone according to claim 2, characterized in that: Two groups of storage batteries (18) are installed inside the battery exchange box (1); the storage batteries (18) are electrically connected to the charging seat (208); and the storage batteries (18) provide power for the internal electrical equipment of the battery exchange box (1).

9. The automatic battery replacement device for drone according to claim 1, characterized in that: Four threaded columns (19) are fixedly connected to the bottom surface of the battery exchange box (1), the four threaded columns (19) are distributed at the corners of the battery exchange box (1), and adjustment feet (20) are threadedly connected to the side walls of the threaded columns (19).

10. The automatic battery replacement device for drone according to claim 1, characterized in that: Both side walls of the battery exchange box (1) are provided with heat dissipation openings (21), and a protective frame (22) is provided inside the heat dissipation openings (21).