TWI879221B - Drone automatic battery replacement system - Google Patents

Abstract

The present invention provides a drone automatic battery replacement system, which includes: a base, on which at least one side frame is disposed, and a battery replacement port is formed on one side frame; a horizontal clamp, which is disposed on the base, and includes a base body, a first clamping group, a second clamping group, a third clamping group, and a fourth clamping group, and the base body is provided with a driving motor and at least two sets of plates, and the base body forms a accommodating space between the two sets of plates, and the first clamping group, the second clamping group, and the third clamping group are provided with a driving motor and at least two sets of plates, and the base body forms a accommodating space between the two sets of plates, and the first clamping group, the second clamping group, and the third clamping group are provided with a driving motor and at least two sets of plates, and the first clamping group, the second clamping group, and the third clamping group are provided with a driving motor and at least two sets of plates, and the first clamping group, the second clamping group, and the third clamping group are provided with a driving motor and a driving motor. and a fourth clamping assembly is arranged in the accommodation space; a displacement carrier, which is arranged on the base, and a displacement platform is arranged on one side of the displacement carrier relative to the horizontal clamp, and the displacement platform is provided with a first displacement clamping member and a second displacement clamping member; at least one fixed clamping member, which is arranged on the side frame, and the fixed clamping member is provided with a fixed clamping member; and at least one battery exchange seat, which is arranged on the side frame, and the battery exchange seat is provided with at least one bottom battery exchange connection port.

Description

Drone automatic battery replacement system

The present invention relates to an automatic battery replacement system, in particular to an automatic battery replacement system for drones that can be automatically set up and automatically replace batteries and can be lightweight.

Due to the maturity of flight control technology, consumer drones and commercial drones have developed rapidly, prompting multi-wing drones to develop in a diversified direction, such as aerial photography, reconnaissance, scientific research, geological surveys, air pollution detection, meteorological observation and remote sensing.

In addition, with the development of unmanned automated control, more and more automated equipment that matches drones has begun to be developed and produced. Among them, the automated drone battery replacement system is one of them. Compared with traditional manual battery replacement, automated battery replacement can save time and manpower. However, in the process of automated battery replacement, how to automatically and accurately and effectively fix the drone to make the battery replacement process fast and make the system lightweight as a whole is a topic to be developed.

Therefore, in order to effectively solve the above-mentioned problems, the main purpose of the present invention is to provide a drone automatic battery replacement system that can be automatically set up and automatically replace batteries and can be lightweight.

To achieve the above-mentioned purpose, the present invention provides a drone automatic battery replacement system, which includes: a base, on which at least one side frame is disposed, and a battery replacement port is formed on one side frame; a horizontal clamp, which is disposed on the base, and the horizontal clamp includes a base body and a first clamping group, a second clamping group, a third clamping group, and a fourth clamping group, and the base body is provided with a driving motor and at least two sets of plates, and the base body forms a accommodating space between the two sets of plates, and the first clamping group, the second clamping group, and the third clamping group are provided with a driving motor and at least two sets of plates, and the base body forms a accommodating space between the two sets of plates, and the first clamping group, the second clamping group, and the fourth clamping group are provided with a driving motor and at least two sets of plates, and the first clamping group, the second clamping group, and the third ... a third clamping group. The third clamping group and the fourth clamping group are arranged in the accommodation space; a displacement carrier, which is arranged on the base, and a displacement platform is arranged on one side of the displacement carrier relative to the horizontal clamp, and the displacement platform is provided with a first displacement clamping member and a second displacement clamping member; at least one fixed clamping member, which is arranged on the side frame, and the fixed clamping member is provided with a fixed clamping member; and at least one battery exchange seat, which is arranged on the side frame, and the battery exchange seat is provided with at least one bottom battery exchange connection port.

According to an embodiment of the automatic battery replacement system for a drone of the present invention, the driving motor is provided with a driving rod and a displacement member is connected to the driving rod. The displacement member is pivotally provided with a first connecting member and a second connecting member. The first connecting member is pivotally provided with a first connecting rod, and the second connecting member is pivotally provided with a second connecting rod. The first clamping assembly has a first main clamping member and a first auxiliary clamping member. The first main clamping member is connected to the first auxiliary clamping member. The first linking member is pivoted with each other, the second clamping assembly has a second main clamping member and a second sub-clamping member, the second main clamping member is pivoted with the second linking member, the third clamping assembly has a third main clamping member and a third sub-clamping member, the third main clamping member is pivoted with the first connecting rod, and the fourth clamping assembly has a fourth main clamping member and a fourth sub-clamping member, the fourth main clamping member is pivoted with the second connecting rod, and The displacement member is formed by a displacement hinge, the first linking member and the second linking member pivoting with each other, and a displacement hole is formed on the assembly plate for the displacement hinge to pass through, and the first linking member is formed by a first linking hinge and the first main clamping member pivoting with each other, and a first linking hole is formed on the assembly plate for the first linking hinge to pass through, and the second linking member is formed by a second linking hinge and the second main clamping member pivoting with each other , and a second connecting hole is formed on the set plate for the second connecting hinge to pass through, and the first connecting rod is mutually pivoted by a third connecting hinge and the third main clamp, and a third connecting hole is formed on the set plate for the third connecting hinge to pass through, and the second connecting rod is mutually pivoted by a fourth connecting hinge and the fourth main clamp, and a fourth connecting hole is formed on the set plate for the fourth connecting hinge to pass through.

According to an embodiment of the automatic battery replacement system for a drone of the present invention, the first clamping assembly further includes a first pulling member, the first pulling member is mutually pivoted by at least one first pulling hinge, the first main clamping member and the first auxiliary clamping member, and a first pulling hole is formed on the assembly plate for the first pulling hinge to pass through, and the second clamping assembly further includes a second pulling member, the second pulling member is mutually pivoted by at least one second pulling hinge, the second main clamping member and the second auxiliary clamping member, and a second pulling hole is formed on the assembly plate for The second pull hinge passes through, and the third clamping assembly further includes a third pull hinge, the third pull hinge is mutually pivoted by at least one third pull hinge, the third main clamping assembly and the third auxiliary clamping assembly, and a third pull hole is formed on the assembly plate for the third pull hinge to pass through, and the fourth clamping assembly further includes a fourth pull hinge, the fourth pull hinge is mutually pivoted by at least one fourth pull hinge, the fourth main clamping assembly and the fourth auxiliary clamping assembly, and a fourth pull hole is formed on the assembly plate for the fourth pull hinge to pass through.

According to an embodiment of the automatic battery replacement system for a drone of the present invention, the first main clamp is formed by a first main clamp pivotally connected to the panel assembly, the second main clamp is formed by a second main clamp pivotally connected to the panel assembly, the third main clamp is formed by a third main clamp pivotally connected to the panel assembly, and the fourth main clamp is formed by a fourth main clamp pivotally connected to the panel assembly. A first limit rod and a second limit rod are further provided on the set of plates. The first limit rod and the second limit rod are mutually assembled with the two sets of plates. The first limit rod is formed with two first rod embedding grooves for the first main clamp and the third main clamp to pass through respectively, and the second limit rod is formed with two second rod embedding grooves for the second main clamp and the fourth main clamp to pass through respectively.

According to an embodiment of the automatic battery replacement system for drones of the present invention, the displacement platform is further provided with at least one displacement plate assembly pivotally connected to the first displacement clamping member and the second displacement clamping member, and the displacement plate assembly is further provided with at least one release pin, and the first displacement clamping member is assembled with a first displacement clamping driving member, and the second displacement clamping member is assembled with a second displacement clamping driving member.

According to an embodiment of the automatic battery replacement system for drones of the present invention, the fixed clamp is further provided with at least one fixed plate assembly, at least one clamp connection port and at least one clamp plug, and the fixed plate assembly is pivotally connected to the fixed clamp, and the fixed clamp is assembled with a fixed clamp drive, and the bottom of the battery replacement base is further provided with at least one battery replacement plug, and the top is further provided with at least one top battery replacement connection port.

According to one embodiment of the drone automatic battery replacement system of the present invention, a drone is provided with a drone vehicle through the battery replacement port and is assembled with the horizontal clamp by a quick release device, wherein the quick release device includes a frame and a docking assembly, the frame has a first frame assembly, a second frame assembly and a power supply battery, and the first frame assembly forms a first inner assembly channel, and the second frame assembly forms a second inner assembly channel, and the power supply battery passes through the first inner assembly channel and the second inner assembly channel and is fixed on the frame, and the first frame assembly has at least one first group slot, and the second frame assembly has at least one second group slot and at least one latch, and a battery power supply module is provided on the second frame assembly to electrically connect the power supply battery, and the battery The battery power supply module is provided with at least one guide member, at least one first electrical transmission member and at least one second electrical transmission member, and at least one guide hole is formed on the side of the electrical docking module, and the guide member is mutually assembled with the guide hole, and the first electrical transmission member is mutually electrically connected with the electrical docking module, and the second electrical transmission member is mutually electrically connected with the power supply battery, and the docking assembly has a first set of plates, a second set of plates and an electrical docking module, the first set of plates passes through the first set of slots, and the front side of the first set of plates is formed with at least one rib and at least one positioning hole, the rib passes through the second set of slots, and the latch member passes through the positioning hole, and the electrical docking module is electrically connected to the battery power supply module.

According to an embodiment of the automatic battery replacement system for drones of the present invention, at least one set of holes is formed on the second frame and a block is provided, and the latch is provided in the block, and the latch has a socket and a positioning column.

According to an embodiment of the automatic battery replacement system for drones of the present invention, the first set of plates and the second set of plates are assembled with each other by at least one connecting column, and the second set of plates is assembled with the drone by the connecting column, and the drone is electrically connected to the electrical docking module, and at least one card slot is formed on the side of the second set of plates.

According to an embodiment of the automatic battery replacement system for drones of the present invention, the drone has four legs, and the first clamping group, the second clamping group, the third clamping group, and the fourth clamping group are clamped on one of the legs respectively, and the drone is mounted on the drone by the legs, and the drone is formed with four top bearings, each of which has a top group groove formed thereon and carries one of the legs respectively.

1: Drone automatic battery replacement system

2: Base

21: Side frame

211: Change the power port

3: Horizontal clamp

31: Seat

311: Driving motor

3111:Drive rod

3112: Displacement parts

31121: Displacement hinge

3113: First linkage

31131: First linkage armature

3114: Second linkage

31141: Second linkage armature

3115: First connecting rod

31151: Third linkage arm

3116: Second connecting rod

31161: Fourth linkage arm

312: Assembly board

3121: Displacement hole

3122: First linkage hole

3123: Second linkage hole

3124: The third linkage hole

3125: Fourth linkage hole

3126: First traction hole

3127: Second traction hole

3128: The third traction hole

3129: The fourth traction hole

313: Storage space

314: First limit rod

3141: First rod groove

315: Second limit rod

3151: Second rod slot

32: First clamp group

321: First main clamp

3211: First main clamping hinge

322: First pair of clamps

3221: First clamping hinge

323: First traction piece

3231: First traction hinge

33: Second clamp group

331: Second main clamp

3311: Second main clamp hinge

332: Second pair of clamps

3321: Second clamping hinge

333: Second traction member

3331: Second traction hinge

34: The third clamp group

341: The third main clamp

3411: Third main clamping hinge

342: The third pair of clips

3421: The third clamping hinge

343: The third traction member

3431: The third traction hinge

35: The fourth clamp group

351: The fourth main clamp

3511: Fourth main hinge

352: The fourth clip

3521: The fourth clamping hinge

353: The fourth traction element

3531: The fourth traction hinge

36: First side panel

37: Second side panel

4: Displacement mount

41: Displacement platform

411: First displacement clamp

412: Second displacement clamp

413: Displacement plate set

414: Release pin

415: First displacement clamping drive member

416: Second displacement clamping drive member

5:Fixed clamp

51:Fixed clamp

52:Fixed plate assembly

53: Clip connection port

54: Clamp latch

55:Fixed clamping drive parts

6: Change the power socket

61: Bottom battery replacement port

62: Replace the power plug

63: Top battery replacement port

7: Drones

71: Legs

8: Quick release device

81:Frame

811: The first group

8111: The first set of slots

8112: First inner group channel

8113: Bottom electrical transmission component

8114: Bottom guide hole

812: The second set

8121: The second set of slots

8122: Second inner channel

8123: Latch

81231: Socket

81232: Positioning column

8124: Group hole

8125: Guide piece

8126: Block

813: Power supply battery

814:Battery power module

8141: First electrical transmission element

8142: Second electrical transmission element

82: Docking assembly

821: The first set of plates

8211: Connecting column

8212: ribs

8213: Positioning hole

822: The second set of plates

8221:Card slot

823: Electrical docking module

8231: Guide hole

9: Autonomous vehicles

91: Top bearing

911: Top group slot

Figure 1 is a three-dimensional schematic diagram of the automatic battery replacement system for drones of the present invention.

Figure 2 is a three-dimensional schematic diagram of the horizontal clamp of the present invention.

Figure 3A is a partial schematic diagram of the horizontal clamp of the present invention.

Figure 3B is the second partial schematic diagram of the horizontal clamp of the present invention.

Figure 4 is a three-dimensional schematic diagram of the displacement platform of the present invention.

Figure 5 is a three-dimensional schematic diagram of the fixed clamp of the present invention.

Figure 6 is a three-dimensional schematic diagram of the battery replacement socket of the present invention.

Figure 7 is a schematic diagram of the assembly of the drone quick-release device of the present invention.

Figure 8 is a schematic diagram of the three-dimensional assembly of the quick-release device of the present invention.

Figure 9 is a three-dimensional exploded schematic diagram of the quick-release device of the present invention.

Figure 10 is a side view of the quick release device of the present invention.

Figure 11 is a schematic diagram of the implementation of the drone and the unmanned vehicle of the present invention entering the drone automatic battery replacement system.

Figure 12 is a schematic diagram of the implementation of the horizontal clamp of the present invention.

Figure 13 is a schematic diagram of the implementation of the drone and drone combined horizontal clamp of the present invention.

Figure 14 is a schematic diagram of the implementation of the displacement platform of the present invention moving to the horizontal fixture.

Figure 15 is a partial schematic diagram of the quick-release device of the present invention.

Figure 16 is a schematic diagram of the implementation of the quick-release device combined with the displacement platform of the present invention.

Figure 17 is a schematic diagram of the implementation of the displacement platform of the present invention moving to the fixed clamp.

Figure 18 is a schematic diagram of the implementation of the displacement platform combined with the fixed clamp of the present invention.

Figure 19 is a schematic diagram of the implementation of the displacement platform of the present invention being separated from the fixed clamp.

Figure 20 is a schematic diagram of the implementation of the displacement platform of the present invention moving to the power exchange seat.

The above-mentioned purpose of the present invention and its structural and functional characteristics will be explained according to the preferred embodiments of the attached drawings.

In the following, various applicable examples are listed and detailed descriptions are given with reference to the accompanying drawings regarding the structure and technical contents of the drone automatic battery replacement system of the present invention; however, the present invention is certainly not limited to the listed embodiments, drawings or detailed description contents.

Furthermore, those familiar with this technology should also understand that the listed embodiments and attached drawings are only for reference and explanation purposes, and are not used to limit the present invention; inventions that can be easily implemented based on these records and modified or changed to complete are also considered to be within the scope of the spirit and purpose of the present invention, and of course, these inventions are also included in the scope of the patent application of the present invention.

Furthermore, the directional terms mentioned in the following embodiments, such as "up", "down", "left", "right", "front", "back", etc., are only reference to the directions of the attached diagrams. Therefore, the directional terms used are for explanation and are not used to limit the present invention; furthermore, in the following embodiments, the same or similar components will use the same or similar component numbers.

First, please refer to FIG. 1, which is a three-dimensional assembly schematic diagram of the drone automatic battery-changing system of the present invention. It can be clearly seen from the figure that the drone automatic battery-changing system 1 includes a base 2, a horizontal clamp 3, a displacement carrier 4, at least one fixed clamp 5, and at least one battery-changing seat 6, wherein the displacement carrier 4, the fixed clamp 5, and the battery-changing seat 6 are all electrically connected to a central control module (not shown in the figure) so that the central control module automatically controls the movement of each component, and wherein at least one side frame 21 is provided on the base 2, and the side frames 21 are mainly provided on the four sides of the base 2, and the top of the side frame 21 The top frame is assembled together, and in this embodiment, a single side frame 21 is used as an implementation method, and a power exchange port 211 is formed on the side frame 21, and the power exchange port 211 is connected to the outside and inside of the base 2, and the horizontal clamp 3 is arranged on the base 2 and adjacent to the power exchange port 211, and the displacement carrier 4 is arranged on the base 2, and the displacement carrier 4 is a carrier that can be moved three-dimensionally on the base 2, and the displacement carrier 4 is arranged on one side of the horizontal clamp 3. A displacement platform 41 is arranged, and the fixed clamp 5 is arranged on the side frame 21, and the power exchange seat 6 is arranged on the side frame 21.

Please refer to Figure 2, Figure 3A and Figure 3B, which are three-dimensional schematic diagrams and partial schematic diagrams 1 and 2 of the horizontal clamp of the present invention, wherein Figure 3A is a schematic diagram with two sets of plates 312, and Figure 3B is a schematic diagram with the upper set of plates 312 removed, wherein the horizontal clamp 3 includes a base 31, a first clamping group 32, a second clamping group 33, a third clamping group 34 and a fourth clamping group 35, and the horizontal clamp 3 is provided with a first side plate 36 and a second side plate 37 on both sides.

A driving motor 311 is disposed on one side of the base 31 and two sets of plates 312 are disposed on the other side of the base 31 and are aligned with each other at an upper and lower interval. A receiving space 313 is defined on one side of the base 31 by the two sets of plates 312. The driving motor 311 has a driving rod 3111. The driving rod 3111 passes through the base 31 and extends toward the receiving space 313. A displacement member 3112 is assembled at the other end of the driving rod 3111. A first linking member 3113 and a second linking member 3114 are pivotally connected to the displacement member 3112 on the other side of the driving rod 3111. The first linking member 3113 is pivotally connected to the displacement member 3112 on the other side of the driving rod 3111. The other end of the displacement member 3112 is provided with a first connecting hinge 31131, and the first connecting member 3113 is pivoted with a first connecting rod 3115 by the first connecting hinge 31131, and the other end of the first connecting rod 3115 is provided with a third connecting hinge 31151 relative to the first connecting hinge 31131, and the other end of the second connecting member 3114 is provided with a second connecting hinge 31141 relative to the displacement member 3112, and the second connecting member 3114 is pivoted with a second connecting rod 3116 by the second connecting hinge 31141, and the other end of the second connecting rod 3116 is provided with a fourth connecting hinge 31161 relative to the second connecting hinge 31141.

In addition, the two sets of plates 312 are respectively formed with a displacement hole 3121, a first linkage hole 3122, a second linkage hole 3123, a third linkage hole 3124, and a fourth linkage hole 3125, which are vertically connected to each other. In addition, the two sets of plates 312 are further formed with a first pull hole 3126, a second pull hole 3127, a third pull hole 3128, and a fourth pull hole 3129, which are vertically connected to each other. The displacement hinge 31121 passes through the displacement hole 3121, the first linkage hinge 31131 passes through the first linkage hole 3122, and the second linkage hinge 31141 passes through the first linkage hole 3122. The second linkage hole 3123 and the third linkage hinge 31151 pass through the third linkage hole 3124, and the fourth linkage hinge 31161 passes through the fourth linkage hole 3125. A first limit rod 314 and a second limit rod 315 are provided on one side of the seat body 31 opposite to the accommodating space 313. The first limit rod 314 and the second limit rod 315 are provided between two sets of plates 312 and the sets of plates 312 are respectively provided on the upper and lower parts. Two first rod embedding grooves 3141 are formed on the first limit rod 314, and two second rod embedding grooves 3151 are formed on the second limit rod 315.

The first clamping assembly 32 is disposed in the accommodating space 313, and the first clamping assembly 32 includes a first main clamping member 321, a first auxiliary clamping member 322, and a first pulling member 323. One end of the first main clamping member 321 is pivoted with the first linking member 31131 and passes through the first rod slot 3141 on one side. A first main clamping hinge 3211 is provided to be pivoted with the set of plates 312, and a first sub-clamping hinge 3221 is provided to be pivoted with the set of plates 312. In addition, the first pulling member 323 is composed of at least one first pulling hinge 3231 pivoted with the first main clamping member 321 and the first sub-clamping member 322, and the first pulling hinge 3231 passes through the first pulling hole 3126.

The second clamping assembly 33 is disposed in the accommodating space 313, and the second clamping assembly 33 includes a second main clamping member 331, a second auxiliary clamping member 332, and a second pulling member 333. One end of the second main clamping member 331 is pivoted with the second linking member 31141 and the second linking member 3114 through the second rod slot 3151 on the one side. A second main clamping hinge 3311 is provided to be pivoted with the set of plates 312, and a second sub-clamping hinge 3321 is provided to be pivoted with the set of plates 312, and the second pulling member 333 is composed of at least one second pulling hinge 3331 pivoted with the second main clamping member 331 and the second sub-clamping member 332, and the second pulling hinge 3331 passes through the second pulling hole 3127.

The third clamping assembly 34 is disposed in the accommodation space 313, and the second clamping assembly 33 includes a third main clamping member 341, a third auxiliary clamping member 342, and a third pulling member 343. One end of the third main clamping member 341 is pivoted with the first connecting rod 3115 by the third linking pivot 31151 and passes through the first rod slot 3141 on the other side. A third main clamping hinge 3411 is provided to be pivoted with the set of plates 312, and a third sub-clamping hinge 3421 is provided to be pivoted with the set of plates 312. In addition, the third pulling member 343 is composed of at least one third pulling hinge 3431 pivoted with the third main clamping member 341 and the third sub-clamping member 342, and the third pulling hinge 3431 passes through the third pulling hole 3128.

The fourth clamping assembly 35 is disposed in the accommodation space 313, and the fourth clamping assembly 35 includes a fourth main clamping member 351, a fourth auxiliary clamping member 352, and a fourth pulling member 353. One end of the fourth main clamping member 351 is mutually pivoted with the second connecting rod 3116 by the fourth linking pivot 31161 and passes through the second rod slot 3151 on the other side. A fourth main clamping hinge 3511 is provided to be pivoted with the set of plates 312, and a fourth sub-clamping hinge 3521 is provided to be pivoted with the set of plates 312. In addition, the fourth pulling member 353 is composed of at least one fourth pulling hinge 3531 pivoted with the fourth main clamping member 351 and the fourth sub-clamping member 352, and the fourth pulling hinge 3531 passes through the fourth pulling hole 3129.

Please refer to Figure 4, which is a three-dimensional schematic diagram of the displacement platform of the present invention, wherein the displacement platform 41 is provided with a first displacement clamping member 411 and a second displacement clamping member 412, and the displacement platform 41 is further provided with at least one displacement plate set 413 pivotally connecting the first displacement clamping member 411 and the second displacement clamping member 412, and the displacement plate set 413 is further provided with at least one release pin 414, and the release pin 414 can be a release pin 414 with an inclined surface, and the first displacement clamping member 411 is assembled with a first displacement clamping driving member 415, and the second displacement clamping member 412 is assembled with a second displacement clamping driving member 416.

Please refer to Figure 5, which is a three-dimensional schematic diagram of the fixed clamp of the present invention, wherein the fixed clamp 5 is provided with a fixed clamping member 51, and the fixed clamp 5 is further provided with at least one fixed plate assembly 52, at least one clamp connection port 53, and at least one clamp latch 54, and the fixed plate assembly 52 is pivotally connected to the fixed clamping member 51, and the fixed clamping member 51 is assembled with a fixed clamping driving member 55.

Please refer to Figure 6, which is a three-dimensional schematic diagram of the battery exchange seat of the present invention, wherein the battery exchange seat 6 is provided with at least one bottom battery exchange connection port 61, and the bottom of the battery exchange seat 6 is further provided with at least one battery exchange plug 62, and the top is further provided with at least one top battery exchange connection port 63.

Please refer to Figures 7 to 10, which are schematic diagrams of the assembly of the drone assembly quick-release device of the present invention, schematic diagrams of the three-dimensional assembly of the quick-release device, schematic diagrams of the three-dimensional decomposition, and side views, wherein the drone automatic battery replacement system 1 is mainly used to replace power for a drone 7, and the drone 7 is first assembled with a quick-release device 8, wherein the quick-release device 8 mainly includes a frame 81 and a docking assembly 82, wherein the frame 81 includes a first frame assembly 811 and a second frame assembly 812 and a power supply battery 813 and a battery power supply module 24, wherein the first frame assembly 811 and the second frame assembly 812 are respectively fixed by two plates, and the top of the first frame assembly 811 is formed with at least one first assembly The first set of grooves 8111 is provided with a first inner channel 8112 formed below the first set of grooves 8111, and the two plates are respectively provided with the first set of grooves 8111 and the first inner channel 8112, and the first set of grooves 8111 of the two plates are connected to each other and arranged in parallel, and the first inner channel 8112 of the two plates are connected to each other and arranged in parallel, and the bottom of the first frame 811 is further provided with a bottom electrical transmission member 8113 electrically connected to the power supply battery 813 and formed with two bottom guide holes 814, and the second frame 812 is formed with at least one second set of grooves 221, and a second inner channel 8122 is formed below the second set of grooves 221, and the two plates are respectively provided with the second set of grooves 22 1 and the second inner group channel 8122, and the second group of grooves 221 of the two plates are connected and arranged in parallel, and the second inner group of channels 8122 of the two plates are connected and arranged in parallel, and the power supply battery 813 is fixed on the frame 81 through the first inner group channel 8112 and the second inner group channel 8122, and the second frame 812 is further provided with at least one latch 8123 and at least one group of holes 8124, at least one guide 8125 and a group block 8126, wherein the latch 8123 is arranged in the group block 8126, and the latch 8123 has a plug hole 81231 and a positioning column 81232, and the two plates are respectively formed with the group of holes 8124, and the two plates are The holes 8124 of the two plates are connected and arranged in parallel, and the latch 8123 is arranged between the holes 8124 of the two plates, and the guide 8125 is arranged on one side of the second frame 812 opposite to the first frame 811 and extends toward the first frame 811. In addition, the battery power module 814 is arranged on one side of the second frame 812 opposite to the first frame 811, and the battery power module 814 is arranged on one side of the first frame 811 with at least one first electrical transmission component 8141, and on the other side with at least one second electrical transmission component 8142, the second electrical transmission component 8142 passes through the two plates and is electrically connected to the power supply battery 813 (not shown in the figure).

The docking assembly 82 includes a first set of plates 821, a second set of plates 822, and an electrical docking module 823, wherein the first set of plates 821 is assembled with a plurality of connecting columns 8211 to the lower side of the second set of plates 822, and the second set of plates 822 is formed with at least one slot 8221 on the side, and the first set of plates 821 passes through the first set of slots 8111, and the front side of the first set of plates 821 is formed with at least one rib 8212 and at least one positioning hole 8213, and the rib 8212 passes through the second set of slots 8111. The electrical connection module 823 is provided between the first set of plates 821 and the second set of plates 822, and the electrical connection module 823 is electrically connected to the first electrical transmission member 8141 of the battery power module 814, and the electrical connection module 823 is formed with at least one guide hole 8231 on one side of the battery power module 814, and the guide member 8125 is mutually assembled with the guide hole 8231.

When the docking assembly 82 of the quick release device 8 and the frame 81 are to be separated from each other, the release pin 414 of the displacement platform 41 can be inserted into the assembly hole 8124 and drive the latch member 8123 to move upward. The release pin 414 can be a release pin 414 with an inclined surface. To further explain, when the latch member 8123 is in a downward locking state, the positioning column 81232 falls into the positioning hole 821. 3, the first set of plates 821 is fixed, at this time, the docking assembly 82 and the frame 81 are in a locked state, and the hole surface of the set of holes 8124 and the hole 81231 form a height difference. When unlocking, the release pin 414 with an inclined surface is inserted into the set of holes 8124 and the hole 81231, and the inclined surface of the release pin 414 passes through the hole 81231 to push the release pin 414 upward, so that the positioning column 81232 leaves. The positioning hole 8213 is unlocked, so that the docking assembly 82 and the frame 81 are in a released state, and the latch member 8123 is lifted up and disengaged from the positioning hole 8213, so that the first set of plates 821 can slide on the frame 81, and the docking assembly 82 can be pulled out from the frame 81, so that the rib 8212 is disengaged from the second set of grooves 221, and the battery is separated from the electrical docking module 823. The power supply module 814 is connected to the first plate 821 until it is separated from the first groove 8111. Thus, the docking assembly 82 can be quickly disassembled from the frame 81, which can solve the problem of removing multiple sets of fixing structures such as screws or wrenches for disassembly. The docking assembly 82 and the frame 81 can be quickly disassembled from each other in an automated manner, thereby achieving the effect of automated setting and lightweight.

On the contrary, if the docking assembly 82 of the quick release device 8 and the frame 81 are to be locked together, the docking assembly 82 and the frame 81 can be assembled together, wherein the first set of plates 821 pass through the first set of grooves 8111, and the first set of plates 821 are continuously moved toward the second frame 812, so that the guide member 8125 is inserted into the guide hole 8231, and the docking assembly 82 can be The relative positions of the docking assembly 82 and the frame 81 are corrected by the guide member 8125 and the guide hole 8231, so that the electrical docking module 823 can be stably assembled with the battery power module 814 and electrically connected to the first electrical transmission member 8141. The rib 8212 of the first set of plates 821 will be inserted into the second set of grooves 221, and the release pin 414 is also inserted into the set hole 8124. The first plate 821 is fixed to the frame 81 by the insertion hole 81231. At this time, the docking assembly 82 and the frame 81 can be assembled with each other. Then, when the release pin 414 is separated from the hole 8124 and the insertion hole 81231, the latch member 8123 of the second frame 812 is released and inserted into the positioning hole 8213 by the positioning column 81232, so that the first plate 821 can be fixed to the frame 81 by the passage of the latch member 8123. 1, thereby, the docking assembly 82 can be quickly and stably locked on the frame 81, and the electrical docking module 823 can be stably assembled with the battery power module 814, which can relatively solve the need for multiple sets of fixing structures such as screws or wrenches for fixing, and the docking assembly 82 and the frame 81 can be automatically limited and fixed to each other, thereby achieving the effect of automatic setting and lightweight.

The drone 7 is assembled on the quick release device by assembling the second set of plates 822 and the drone 7 with the connecting column 8211, and the drone 7 is electrically connected to the electrical docking module 823. When the drone 7 moves toward the frame 81, the drone 7 passes the first set of plates 821 through the first set of slots 8111, and continues to move the first set of plates 821 toward the second frame 812, so that the guide member 8125 is inserted into the guide hole 8111. 231, and the docking assembly 82 can use the guide member 8125 and the guide hole 8231 to correct the relative position of the docking assembly 82 and the frame 81, so that the electrical docking module 823 can be stably assembled with the battery power module 814 and electrically connected to the first electrical transmission member 8141. In addition, the rib 8212 of the first set of plates 821 will be inserted into the second set of grooves 221, and the release pin 414 is also inserted into the set hole 8124 and the insertion hole 81231. At this time, The docking assembly 82 and the frame 81 can be assembled with each other, and then when the release pin 414 is separated from the set hole 8124 and the plug hole 81231, the latch member 8123 of the second frame 812 is released and inserted into the positioning hole 8213 by the positioning column 81232, so that the first set of plates 821 can be fixed on the frame 81 through the passage of the latch member 8123, thereby, the drone 7 and the docking assembly 82 can be quickly and stably locked on the frame 81, and the electric The electrical docking module 823 can be stably assembled with the battery supply module 814, and the power of the power supply battery 813 can be transmitted from the battery supply module 814 to the electrical docking module 823, and the electrical docking module 823 then transmits the power to the drone 7 for use. Thus, the drone 7 can be automatically electrically connected to the power supply battery 813 through the quick-release device 8, and can automatically separate the power supply battery 813, thereby achieving the effect of automatic installation and lightweight.

Please refer to the above-mentioned attached figures and Figures 11 to 13, which are schematic diagrams of the implementation of the drone and the drone entering the drone automatic battery replacement system, the schematic diagram of the implementation of the horizontal clamp, and the schematic diagram of the implementation of the drone and the drone combined horizontal clamp, wherein the drone 7 has four legs 71, and the drone 7 is landed on the drone 9 by the legs 71, and the drone 9 is formed with four top bearings 91, each of which is formed with a top group groove 911 and carries one of the support members 91. The four legs 71 of the drone 7 can land on each top support 91 respectively when the drone 7 lands on the drone 9, and the top support 91 guides the legs 71 to slide in and park at the correct position through the inclined surface of the top assembly slot 911. After the drone 7 is parked on the drone 9, the drone 9 can drive toward the power exchange port 211 of the side frame 21, and the drone 9 will first adhere to the first side panel 36 and the second side panel 37 to accurately park the drone 7 on the horizontal fixture 3.

The drone 7 is parked in front of the horizontal clamp 3, and the horizontal clamp 3 will first unfold the first clamp group 32, the second clamp group 33, the third clamp group 34, and the fourth clamp group 35. First, the drive motor 311 is started and drives the displacement member 3112 to move toward the base 31, so that the drive rod 3111 protrudes out of the drive motor 311 in a large area. At this time, the displacement arm 31121 moves toward the base 31 in the displacement hole 3121 and moves relatively to the position of one end of the displacement hole 3121 relative to the base 31, and the displacement member 3112 is pulled by the displacement arm 31121. The first linking member 3113 and the second linking member 3114 are respectively displaced according to the hole tracks of the first linking hole 3122 and the second linking hole 3123, and the first linking member 31131 pulls the first connecting rod 3115 and the first main clamp 321, and the second linking member 31141 pulls the second connecting rod 3116 and the second main clamp 331, and the third linking member 2151 pulls the third main clamp 341, and the fourth linking member 2161 pulls the fourth main clamp 351.

When the first main clamp 321, the second main clamp 331, the third main clamp 341, and the fourth main clamp 351 are pulled, the first main clamp 321, the second main clamp 331, the third main clamp 341, and the fourth main clamp 351 will rotate toward the inside of the accommodation space 313 with the first main clamp pivot 3211, the second main clamp pivot 3311, the third main clamp pivot 3411, and the fourth main clamp pivot 3511 as the axis, and the first main clamp 321, the second main clamp 331, the third main clamp 341, and the fourth main clamp 351 will rotate respectively when the first main clamp 321, the second main clamp 331, the third main clamp 341, and the fourth main clamp 351 rotate. The first pull member 323, the second pull member 333, the third pull member 343, and the fourth pull member 353 are displaced according to the hole tracks of the first pull hole 3126, the second pull hole 3127, the third pull hole 3128, and the fourth pull hole 3129, and push the first sub-clamp 322, the second sub-clamp 332, the third sub-clamp 342, and the fourth sub-clamp 352, respectively, so that the first sub-clamp 322, the second sub-clamp 332, the third sub-clamp 342, and the fourth sub-clamp 352 are displaced according to the hole tracks of the first pull hole 3126, the second pull hole 3127, the third pull hole 3128, and the fourth pull hole 3129, respectively. The first sub-clamping hinge 3221, the second sub-clamping hinge 3321, the third sub-clamping hinge 3421, and the fourth sub-clamping hinge 3521 are respectively rotated in the direction of the accommodating space 313 with the first sub-clamping hinge 3221, the second sub-clamping hinge 3321, the third sub-clamping hinge 3421, and the fourth sub-clamping hinge 3521 as the axis, so that the first clamping group 32, the second clamping group 33, the third clamping group 34, and the fourth clamping group 35 are in an unfolded state, and this state is the setting state of the horizontal clamp 3 when it is not in use. In this way, the first clamping group 32, the second clamping group 33, the third clamping group 34, and the fourth clamping group 35 can be driven by a single driving motor 311 to unfold or clamp, thereby achieving the effect of reducing the setting cost, and the first main clamping member 321 and the The second main clamp 331, the third main clamp 341, the fourth main clamp 351, the first sub-clamp 322, the second sub-clamp 332, the third sub-clamp 342, and the fourth sub-clamp 352 can be unfolded at a large angle (greater than 90 degrees and less than 180 degrees) and accommodated in the accommodating space 313 through the above-mentioned structural design when unfolded. When clamped, they can be clamped at a large angle, so that the clamping range is large, and the occurrence of the situation where the object cannot be clamped is reduced. In addition, each component is actuated inwardly, so that the clamp will not protrude outward when clamping again, reducing the external space required for actuation, thereby achieving the effect of being used in equipment with small space.

On the contrary, after the drone 7 is parked on the horizontal clamp 3, the horizontal clamp 3 will clamp the first clamp group 32, the second clamp group 33, the third clamp group 34 and the fourth clamp group 35. First, the driving motor 311 is started and pushes the displacement member 3112 to move toward the base 31, so that the driving rod 3111 protrudes into the accommodating space 313 in a large area. At this time, the displacement arm 31121 moves in the displacement hole 3121 toward the base 31 and moves relatively to the other end of the displacement hole 3121 relative to the base 31, and the displacement member 3112 is pushed by the displacement arm 31121. The first linking member 3113 and the second linking member 3114 are driven, and the first linking hinge 31131 and the second linking hinge 31141 are displaced according to the hole tracks of the first linking hole 3122 and the second linking hole 3123 respectively, and the first linking hinge 31131 drives the first connecting rod 3115 and the first main clamp 321, and the second linking hinge 31141 drives the second connecting rod 3116 and the second main clamp 331, and the third linking hinge drives the third main clamp 341, and the fourth linking hinge drives the fourth main clamp 351.

When the first main clamp 321, the second main clamp 331, the third main clamp 341, and the fourth main clamp 351 are pushed, the first main clamp 321, the second main clamp 331, the third main clamp 341, and the fourth main clamp 351 will rotate outward of the accommodation space 313 with the first main clamp pivot 3211, the second main clamp pivot 3311, the third main clamp pivot 3411, and the fourth main clamp pivot 3511 as the axis, and the first main clamp 321 and the second main clamp When the first main clamp 331 and the third main clamp 341 and the fourth main clamp 351 rotate, they will drive the first lead 323 and the second lead 333 and the third lead 343 and the fourth lead 353 respectively, and the first lead 323 and the second lead 333 and the third lead 343 and the fourth lead 353 will move according to the hole tracks of the first lead hole 3126 and the second lead hole 3127 and the third lead hole 3128 and the fourth lead hole 3129 respectively, and push the first lead hole 3126 and the second lead hole 3127 and the third lead hole 3128 and the fourth lead hole 3129 respectively. The first sub-clamp 322, the second sub-clamp 332, the third sub-clamp 342, and the fourth sub-clamp 352 are respectively rotated outward of the accommodation space 313 with the first sub-clamp hinge 3221, the second sub-clamp hinge 3321, the third sub-clamp hinge 3421, and the fourth sub-clamp hinge 3521 as the axis, so that the first clamping group 32, the second clamping group 33, the third clamping group 34, and the fourth clamping group 3 5 is in a clamped state, and this state is the setting state of the horizontal clamp 3 for clamping, and the first clamp 32, the second clamp 33, the third clamp 34, and the fourth clamp 35 clamp the legs 71 of the drone 7, so that the drone 7 can be stably parked on the horizontal clamp 3. In this way, the first clamp 32, the second clamp 33, the third clamp 34, and the fourth clamp 35 can be driven by a single drive motor 311 to expand or clamp, thereby achieving the effect of reducing the installation cost.

Please refer to the aforementioned attached figures and Figures 14 to 16, which are schematic diagrams of the implementation of the displacement platform of the present invention moving to the horizontal fixture, partial schematic diagrams of the quick release device, and schematic diagrams of the implementation of the quick release device combined with the displacement platform 41. After the drone 7 is parked on the horizontal fixture 3, the displacement carrier 4 moves to the position of the drone 7 and moves the displacement platform 41 to the side of the drone 7. Then, the displacement platform 41 is driven by the first displacement clamping driving member 415 to clamp the first displacement clamping member 411 to clamp the slot 8221 of the second set of plates 822, and by the second displacement clamping driving member 416 to drive the second displacement clamping member 412 to clamp the first frame 811 and the second frame 812, and at the same time, the release The pin 414 is inserted into the set of holes 8124 and the insertion hole 81231, and the inclined surface of the release pin 414 pushes the release pin 414 upward through the insertion hole 81231, so that the positioning column 81232 leaves the positioning hole 8213 to complete the unlocking, so that the docking assembly 82 and the frame 81 are in a released state, and the latch member 8123 is lifted up and separated from the positioning hole 8213. After the first displacement clamping member 411 clamps the second set of plates 822 and the second displacement clamping member 412 clamps the first frame group 811 and the second frame group 812, the first clamping group 32, the second clamping group 33, the third clamping group 34 and the fourth clamping group 35 of the horizontal clamp 3 are unfolded and release the support leg 71 of the drone 7.

Please refer to the aforementioned attached figures and Figures 17, 18 and 19, which are schematic diagrams of the implementation of the displacement platform of the present invention moving to the fixed clamp, the implementation of the displacement platform combined with the fixed clamp, and the implementation of the displacement platform detaching from the fixed clamp, wherein the displacement carrier 4 drives the displacement platform 41 clamping the drone 7 and the quick release device 8 to move to the fixed clamp 5, and the clamp pin 54 is inserted into the bottom guide hole 8114 and guides the quick release device 8 and the drone 7 to move to the correct position, and the clamp connection port 53 is electrically connected to the The bottom electrical transmission component 8113 is then driven by the fixed clamping driver 55 to drive the fixed clamping component 51 to clamp the slot 8221 of the second set of plates 822, and the first displacement clamping driver 415 drives the first displacement clamping component 411 to release the slot 8221 of the second set of plates 822. At the same time, the docking assembly 82 and the frame 81 are in a released state, so when the displacement carrier 4 moves backward, the drone 7 stays on the fixed clamping component 5, and the displacement platform 41 clamps the frame 81 and the power supply battery 813 to separate from the drone 7.

Furthermore, the fixed clamping member 51 clamps the second set of plates 822. If the second displacement clamping driving member 416 simultaneously drives the second displacement clamping member 412 to release the first frame group 811 and the second frame group 812, and the displacement carrier 4 moves backward, the release pin 414 disengages from the set of holes and the plug hole 81231, and the latch member 8123 of the second frame group 812 is released and is locked by the positioning column 8123. 2 is inserted into the positioning hole 8213 so that the first set of plates 821 can be fixed on the frame 81 through the passage of the latch 8123. Therefore, when the displacement carrier 4 moves backward, the drone 7, the frame 81 and the power supply battery 813 stay on the fixed clamp 5, and the power supply battery 813 can be electrically connected to the bottom electrical transmission component 8113 through the clamp connection port 53 for charging.

Please refer to the above-mentioned attached figure and Figure 20, which is a schematic diagram of the implementation of the displacement platform of the present invention moving to the power exchange seat, wherein, if the displacement platform 41 clamps the frame 81 and the power supply battery 813 away from the drone 7, the displacement carrier 4 can be moved to the power exchange seat 6, and the power exchange plug 62 is inserted into the bottom guide hole 8114 and guides the frame 81 to move to the correct position, and the bottom power exchange connection port 61 is electrically connected to the bottom electrical transmission component 8113, so that the power supply battery 813 can be electrically connected to the bottom electrical transmission component 8113 through the bottom power exchange connection port 61 for charging, and the power supply battery 813 can also be electrically connected to the first electrical transmission component 8141 through the top power exchange connection port 63 for fast charging, and The second displacement clamping driving member 416 simultaneously drives the second displacement clamping member 412 to release the first frame group 811 and the second frame group 812, and the displacement carrier 4 can bring the displacement platform 41 to the battery exchange seat 6 where the power supply battery 813 is fully charged, and the first frame group 811 and the second frame group 812 are clamped by the second displacement clamping member 412, and then the frame 81 of the fully charged power supply battery 813 is taken out from the battery exchange seat 6 and assembled with other drones 7 and docking assemblies 82, and then the above description can be reversed to make the drone 7 parked on the unmanned vehicle 9, and then the unmanned vehicle 9 drives away from the drone automatic battery exchange system 1, thereby achieving the effect of automatic setting, automatic battery replacement and lightweight.

The present invention has been described in detail above. However, what is described above is only a preferred embodiment of the present invention and should not limit the scope of implementation of the present invention. That is, all equivalent changes and modifications made according to the application scope of the present invention should still fall within the scope of patent coverage of the present invention.

1: Drone automatic battery replacement system

2: Base

21: Side frame

211: Change the power port

3: Horizontal clamp

4: Displacement mount

41: Displacement platform

5:Fixed clamp

6: Change the power socket

Claims (10)

A drone automatic battery replacement system includes: a base, on which at least one side frame is disposed, and a battery replacement port is formed on one side frame; a horizontal clamp is disposed on the base, and the horizontal clamp includes a base body and a first clamping group, a second clamping group, a third clamping group, and a fourth clamping group, and the base body is provided with a driving motor and at least two sets of plates, and the base body forms a accommodating space between the two sets of plates, and the first clamping group, the second clamping group, the third clamping group, and the fourth clamping group are provided with a driving motor and at least two sets of plates, and the base body forms a accommodating space between the two sets of plates, and the first clamping group, the second clamping group, the third clamping group, and the fourth clamping group are provided with a driving motor and at least two sets of plates, and the first clamping group, the second clamping group, the third clamping group, and the fourth clamping group are provided with a driving motor and a driving motor. The assembly is arranged in the accommodation space; a displacement carrier, which is arranged on the base, and a displacement platform is arranged on one side of the displacement carrier relative to the horizontal clamp, and the displacement platform is provided with a first displacement clamp and a second displacement clamp; at least one fixed clamp, which is arranged on the side frame, and the fixed clamp is provided with a fixed clamp; and at least one battery exchange seat, which is arranged on the side frame, and the battery exchange seat is provided with at least one bottom battery exchange connection port. As described in claim 1, the automatic battery replacement system for a drone, wherein the driving motor is provided with a driving rod and a displacement member is connected to the driving rod, the displacement member is pivotally provided with a first connecting member and a second connecting member, the first connecting member is also pivotally provided with a first connecting rod, and the second connecting member is also pivotally provided with a second connecting rod, and the first clamping assembly has a first main clamping member and a first auxiliary clamping member, the first main clamping member is connected to the The first linking member is pivoted with each other, the second clamping assembly has a second main clamping member and a second sub-clamping member, the second main clamping member is pivoted with the second linking member, the third clamping assembly has a third main clamping member and a third sub-clamping member, the third main clamping member is pivoted with the first connecting rod, and the fourth clamping assembly has a fourth main clamping member and a fourth sub-clamping member, the fourth main clamping member is pivoted with the second connecting rod, and The displacement member is formed by a displacement hinge, the first linking member and the second linking member pivoting with each other, and a displacement hole is formed on the assembly plate for the displacement hinge to pass through, and the first linking member is formed by a first linking hinge and the first main clamping member pivoting with each other, and a first linking hole is formed on the assembly plate for the first linking hinge to pass through, and the second linking member is formed by a second linking hinge and the second main clamping member pivoting with each other , and a second connecting hole is formed on the set plate for the second connecting hinge to pass through, and the first connecting rod is mutually pivoted by a third connecting hinge and the third main clamp, and a third connecting hole is formed on the set plate for the third connecting hinge to pass through, and the second connecting rod is mutually pivoted by a fourth connecting hinge and the fourth main clamp, and a fourth connecting hole is formed on the set plate for the fourth connecting hinge to pass through. As described in claim 2, the first clamping assembly further includes a first pull member, the first pull member is mutually pivoted by at least one first pull hinge, the first main clamping member and the first auxiliary clamping member, and a first pull hole is formed on the assembly plate for the first pull hinge to pass through, and the second clamping assembly further includes a second pull member, the second pull member is mutually pivoted by at least one second pull hinge, the second main clamping member and the second auxiliary clamping member, and a second pull hole is formed on the assembly plate for the second pull hinge to pass through. The second pull hinge passes through, and the third clamping assembly further includes a third pull hinge, the third pull hinge is mutually pivoted by at least one third pull hinge, the third main clamping assembly and the third auxiliary clamping assembly, and a third pull hole is formed on the assembly plate for the third pull hinge to pass through, and the fourth clamping assembly further includes a fourth pull hinge, the fourth pull hinge is mutually pivoted by at least one fourth pull hinge, the fourth main clamping assembly and the fourth auxiliary clamping assembly, and a fourth pull hole is formed on the assembly plate for the fourth pull hinge to pass through. The automatic battery replacement system for a drone as described in claim 3, wherein the first main clamp is formed by a first main clamp pivotally connected to the panel, the second main clamp is formed by a second main clamp pivotally connected to the panel, the third main clamp is formed by a third main clamp pivotally connected to the panel, and the fourth main clamp is formed by a fourth main clamp pivotally connected to the panel. A first limit rod and a second limit rod are further provided on the assembly plate. The first limit rod and the second limit rod are assembled with the two assembly plates. The first limit rod is formed with two first rod embedding grooves for the first main clamp and the third main clamp to pass through respectively, and the second limit rod is formed with two second rod embedding grooves for the second main clamp and the fourth main clamp to pass through respectively. As described in claim 1, the automatic battery replacement system for unmanned aerial vehicles, wherein the displacement platform is further provided with at least one displacement plate assembly pivotally connected to the first displacement clamping member and the second displacement clamping member, and the displacement plate assembly is further provided with at least one release pin, and the first displacement clamping member is assembled with a first displacement clamping driving member, and the second displacement clamping member is assembled with a second displacement clamping driving member. As described in claim 1, the automatic battery replacement system for unmanned aerial vehicles, wherein the fixed clamp is further provided with at least one fixed plate assembly, at least one clamp connection port and at least one clamp plug, and the fixed plate assembly is pivotally connected to the fixed clamp, and the fixed clamp is assembled with a fixed clamp drive, and the bottom of the battery replacement base is further provided with at least one battery replacement plug, and the top is further provided with at least one top battery replacement connection port. The automatic battery replacement system for drones as described in claim 1 is for a drone to carry a drone through the battery replacement port and to be assembled with the horizontal clamp by a quick release device, wherein the quick release device includes a frame and a docking assembly, the frame has a first frame assembly, a second frame assembly and a power supply battery, and the first frame assembly forms a first inner group channel, and the second frame assembly forms a second inner group channel, and the power supply battery passes through the first inner group channel and the second inner group channel and is fixed on the frame, and the first frame assembly has at least one first group slot, and the second frame assembly has at least one second group slot and at least one latch, and a battery power supply module is provided on the second frame assembly to be electrically connected to the power supply battery, and the battery power supply module is provided to ... The battery power supply module is provided with at least one guide member, at least one first electrical transmission member and at least one second electrical transmission member, and at least one guide hole is formed on the side of the electrical docking module, and the guide member is mutually assembled with the guide hole, and the first electrical transmission member is mutually electrically connected with the electrical docking module, and the second electrical transmission member is mutually electrically connected with the power supply battery, and the docking assembly has a first set of plates, a second set of plates and an electrical docking module, the first set of plates passes through the first set of slots, and the front side of the first set of plates is formed with at least one rib and at least one positioning hole, the rib passes through the second set of slots, and the latch member passes through the positioning hole, and the electrical docking module is electrically connected to the battery power supply module. As described in claim 7, the automatic battery replacement system for drones, wherein the second frame is formed with at least one set of holes and a block is provided, and the latch is provided in the block, and the latch has a socket and a positioning column. As described in claim 7, the first set of plates and the second set of plates are assembled with each other by at least one connecting column, and the second set of plates is assembled with the drone by the connecting column, and the drone is electrically connected to the electrical docking module, and at least one card slot is formed on the side of the second set of plates. As described in claim 7, the drone has four legs, and the first clamping group, the second clamping group, the third clamping group, and the fourth clamping group are clamped on one of the legs, respectively, and the drone is mounted on the drone by the legs, and the drone is formed with four top bearings, each of which has a top group groove and carries one of the legs.

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