Electromagnetic connection unmanned aerial vehicle bypass cable access device

Abstract

The invention discloses an electromagnetically-connected unmanned aerial vehicle bypass cable access device, and belongs to the technical field of bypass cable connection, the device comprises an auxiliary plate, the left end of the auxiliary plate is detachably connected with a first connection assembly used for butt joint with a cable, and the right end of the auxiliary plate is detachably connected with a second connection assembly used for butt joint with a main wire; the first connecting assembly and the second connecting assembly are electrically connected through a wire. A lower electromagnetic assembly is arranged on the upper surface of the auxiliary plate, a middle assembly used for being in butt joint with an unmanned aerial vehicle base is arranged above the auxiliary plate, and an upper electromagnetic assembly corresponding to the lower electromagnetic assembly is arranged at the lower end of the middle assembly. The device is simpler and more convenient to use, simple to operate, labor-saving and easy, and the working efficiency is further improved.

Description

Technical Field

[0001] The invention belongs to the technical field of bypass cable connection, and in particular relates to an electromagnetically connected unmanned aerial vehicle bypass cable access device. Background Art

[0002] ‌Bypass cable refers to a temporary power supply system formed by temporarily laying a flexible high-voltage power cable during the transformation or maintenance of the power grid to ensure that users can continue to use electricity during the transformation or maintenance of the power grid. ‌ This cable operation method uses quick connection and bypass switch operation to direct the power supply to the temporary bypass power supply cable line, thereby ensuring uninterrupted power supply to users. When the original power grid transformation or maintenance is completed, the bypass cable is removed and normal power supply is restored. In the prior art, it is time-consuming and labor-intensive to connect the bypass cable to the main circuit, and the work efficiency is low. Publication number: CN118315875B, discloses an electromagnetically connected bypass cable intelligent access device and method for drones, including a first connection component, a second connection component, and a lifting component and a power-taking component connected to the second connection component; the first connection component includes a plurality of suspension ropes for connecting to the drone, a connection plate connected to the plurality of suspension ropes, a first electromagnetic connector arranged on the connection plate, and a bell-mouth structure arranged on the connection plate; the first electromagnetic connector is located in the bell-mouth structure; the second connection component includes a second electromagnetic connector; when the drone mounts the lifting component and the power-taking component on the main line, the electromagnetic connector can be quickly separated, and when the lifting component and the power-taking component need to be removed from the main line, the drone can quickly dock the second electromagnetic connector with the first electromagnetic connector through the bell-mouth structure, and the docking accuracy can be ensured, thereby improving the operation efficiency and hoisting stability. The above patent discloses a method of electromagnetically cooperating with drones to connect the bypass cable to the main line, which improves the installation efficiency as a whole compared to the prior art, but the above patent is not simple in use and is still laborious and time-consuming. Summary of the invention

[0003] The purpose of the present invention is to overcome the deficiencies of the prior art and to provide an electromagnetically connected drone bypass cable access device, which solves the problems in the above-mentioned background technology.

[0004] The object of the present invention is achieved as follows: an electromagnetically connected drone bypass cable access device, comprising an auxiliary plate, the left end of the auxiliary plate is detachably connected with a first connection component for docking a cable, and the right end of the auxiliary plate is detachably connected with a second connection component for docking a main wire; the first connection component and the second connection component are electrically connected through a wire; the upper surface of the auxiliary plate is provided with a lower electromagnetic component, and the upper part of the auxiliary plate is provided with an intermediate component for docking a drone base, and the lower end of the intermediate component is provided with an upper electromagnetic component corresponding to the lower electromagnetic component. When in use, the first connection component is electrically connected to one end of the bypass cable through the first connection component, and then the base bracket of the drone is connected to the intermediate component, and the intermediate component can realize electromagnetic quick connection through the upper electromagnetic component and the lower electromagnetic component, and the drone takes off to pull the intermediate component to take off, and then pull the auxiliary plate, the first connection component and the second connection component to take off synchronously, and after the drone is controlled to arrive near the main wire, the second connection component is hooked with the main wire, that is, the connection between the bypass cable and the main wire is completed, and at this time, the upper electromagnetic component and the lower electromagnetic component are separated by the remote control to separate the drone from the auxiliary plate. The invention has a simpler use process, is easy to operate, saves effort and is more relaxed, thus further improving work efficiency.

[0005] Furthermore, the first connection assembly includes a connection plate, the lower surface of which is provided with a first slide groove and a second slide groove, and the first slide groove and the second slide groove are arranged parallel to each other, and a left clamping plate and a right clamping plate are arranged below the connection plate, and the left clamping plate and the right clamping plate are connected by a spring. When in use, in a default state, due to the effect of the spring restoring force, the left clamping plate and the right clamping plate are in a close clamping state, the end of the cable is placed between the left clamping plate and the right clamping plate, the left clamping plate and the right clamping plate are separated outwardly along the first slide groove and the second slide groove, and due to the effect of the spring, the cable is clamped and fixed between the left clamping plate and the right clamping plate. The first slide groove and the second slide groove are arranged to limit the moving trajectory of the left clamping plate and the right clamping plate, thereby enhancing the stability of the cable fixing.

[0006] Furthermore, the upper ends of the left clamping plate and the right clamping plate are fixedly connected with a first sliding protrusion and a second sliding protrusion, and the first sliding protrusion is slidably connected in the first sliding groove, and the second sliding protrusion is slidably connected in the second sliding groove; the outer end of the left clamping plate is fixedly connected with a left clamping head, and the outer end of the right clamping plate is fixedly connected with a right clamping head, and the left clamping head and the right clamping head are both arc-shaped. By providing the arc-shaped left clamping head and the right clamping head, the contact area between the left clamping plate and the right clamping plate and the bypass cable is increased, thereby increasing the friction force and enhancing the connection stability.

[0007] Further, the lower electromagnetic component includes a front groove and a rear groove provided on the upper surface of the auxiliary plate, and the front groove is arranged corresponding to the rear groove, the inner bottom surface of the front groove is provided with a front guide groove, and the inner bottom surface of the rear groove is provided with a rear guide groove, the front guide groove is slidably connected with a lower front magnetic block, the rear guide groove is slidably connected with a lower rear magnetic block, the lower front magnetic block is connected with a front drive component for driving the lower front magnetic block to move, and the lower rear magnetic block is connected with a rear drive component for driving the lower rear magnetic block to move. The front drive component includes a front cavity provided on the left inner wall of the front groove, an electric control component is provided inside the front cavity, the electric control component is connected with a remote control, a front electric push rod electrically connected to the electric control component is fixedly provided inside the front cavity, and the outer end of the telescopic rod of the front electric push rod is connected to the side wall of the lower front magnetic block. The rear drive assembly includes a rear cavity opened on the inner wall of the rear groove seat, a rear electric push rod is fixedly arranged inside the rear cavity, the outer end of the telescopic rod of the rear electric push rod is connected to the side wall of the lower rear magnetic block, and the rear electric push rod is electrically connected to the electric control assembly. When in use, after the bypass cable is fixed between the left clamping plate and the right clamping plate, and the auxiliary plate is fixedly connected to the base bracket of the drone, a signal is sent to the electric control assembly through the remote control, and the electric control assembly controls the telescopic rods of the front electric push rod and the rear electric push rod to extend synchronously, and the lower front magnetic block and the lower rear magnetic block are pushed out of the front cavity and the rear cavity along the front guide groove and the rear guide groove, respectively, and are pushed into the inside of the front groove and the rear groove. After the upper electromagnetic assembly is brought close to the lower front magnetic block and the lower rear magnetic block, the intermediate assembly is quickly connected to the auxiliary plate under the attraction of the magnetic force.

[0008] Furthermore, the intermediate component includes a support plate, the surface of the support plate is provided with a first through hole and a second through hole, the first through hole and the second through hole are used for the base bracket below the drone to pass through, the left end of the support plate is fixedly connected with a first vertical plate extending downward, the right end of the support plate is fixedly connected with a second vertical plate extending downward, the surface of the first vertical plate is provided with a threaded hole, and the surface of the second vertical plate is threadedly connected with a screw. When in use, the base bracket of the drone is extended to the bottom of the support plate through the first through hole and the second through hole, and then the screw is rotated so that the inner end of the screw passes through the drone base bracket and is connected to the threaded hole of the first vertical plate, so as to realize the quick connection between the drone and the support plate.

[0009] Furthermore, the upper electromagnetic assembly includes an upper rear magnetic block fixedly arranged at the lower end of the first vertical plate, and an upper front magnetic block fixedly arranged at the lower end of the second vertical plate. The second connection assembly includes a connecting strip arranged at the right end of the auxiliary plate, and the connecting strip is connected with a tube hook portion, and the tube hook portion is used to hang the main electric wire. When in use, after the tube hook portion is connected to the main electric wire by the drone, the operator controls the telescopic rods of the front electric push rod and the rear electric push rod to shorten through the remote control, thereby driving the lower front magnetic block and the lower rear magnetic block to be retracted into the front cavity and the rear cavity. At this time, the upper front magnetic block and the upper rear magnetic block cannot enter the front cavity and the rear cavity, so that the drone can be quickly detached.

[0010] The beneficial effects of the present invention are as follows: the first connecting component is electrically connected to one end of the bypass cable, and then the base bracket of the drone is connected to the intermediate component. The intermediate component can realize electromagnetic quick connection through the upper electromagnetic component and the lower electromagnetic component. The drone takes off to pull the intermediate component to take off, and then pull the auxiliary board, the first connecting component and the second connecting component to take off synchronously. After the drone is controlled to reach the vicinity of the main wire, the second connecting component is connected to the main wire to complete the connection between the bypass cable and the main wire. At this time, the upper electromagnetic component is separated from the lower electromagnetic component by the remote control to separate the drone from the auxiliary board. The present invention is more convenient to use, simple to operate, labor-saving and easy, and further improves the work efficiency.

[0011] In the default state, due to the effect of the spring restoring force, the left clamp and the right clamp are in a close clamping state. The end of the cable is placed between the left clamp and the right clamp, and the left clamp and the right clamp are separated outward along the first slide groove and the second slide groove. Due to the effect of the spring, the cable is clamped and fixed between the left clamp and the right clamp. The first slide groove and the second slide groove are used to limit the movement trajectory of the left clamp and the right clamp, thereby enhancing the stability of the cable fixation. By setting the arc-shaped left clamp and the right clamp, the contact area between the left clamp and the right clamp and the bypass cable is increased, thereby increasing the friction force and enhancing the connection stability.

[0012] After the bypass cable is fixed between the left clamping plate and the right clamping plate, and the auxiliary plate is fixedly connected to the base bracket of the drone, a signal is sent to the electronic control component through the remote control, and the electronic control component controls the telescopic rods of the front electric push rod and the rear electric push rod to extend synchronously, and the lower front magnetic block and the lower rear magnetic block are pushed out from the front cavity and the rear cavity along the front guide groove and the rear guide groove respectively, and are pushed into the inside of the front groove and the rear groove. After the upper electromagnetic component is brought close to the lower front magnetic block and the lower rear magnetic block, the middle component is quickly connected to the auxiliary plate under the attraction of the magnetic force. The base bracket of the drone is extended to the bottom of the support plate through the first through hole and the second through hole, and then the screw is rotated so that the inner end of the screw passes through the base bracket of the drone and is connected to the threaded hole of the first vertical plate to achieve a quick connection between the drone and the support plate. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 It is a schematic diagram of the main structure of the present invention; Figure 2 It is a schematic diagram of the top view of the structure of the present invention; Figure 3 It is a left-side structural schematic diagram of the present invention; Figure 4 It is a top view of the three-dimensional structure of the present invention; Figure 5 It is a schematic diagram of the three-dimensional structure of the present invention when viewed from above; Figure 6 The present invention Figure 5 Middle A: Enlarged view; Figure 7 It is a perspective structural schematic diagram of the present invention; Figure 8 It is a schematic diagram of the use state of the present invention.

[0014] In the figure: 1, auxiliary plate 2, connecting plate 3, first slide groove 4, second slide groove 5, left clamping plate 6, right clamping plate 7, spring 8, left clamping head 9, right clamping head 10, front groove 11, rear groove 12, front guide groove 13, rear guide groove 14, lower front magnetic block 15, lower rear magnetic block 16, front cavity 17, rear cavity 18, front electric push rod 19, rear electric push rod 20, support plate 21, first through hole 22, second through hole 23, first vertical plate 24, second vertical plate 25, screw 26, upper rear magnetic block 27, upper front magnetic block 28, barrel hook part 29, drone 30, bypass cable. DETAILED DESCRIPTION

[0015] The present invention will be further described in detail below in conjunction with the accompanying drawings. It should be pointed out that all directional words such as up, down, front, back, left, and right appearing in the present invention do not limit the present invention, but are only for clearer description and explanation of the present invention. Example 1

[0016] like Figure 1-8As shown, the present embodiment discloses an electromagnetically connected UAV bypass cable access device, which includes an auxiliary plate 1, the left end of the auxiliary plate 1 is detachably connected with a first connection component for docking a cable, and the right end of the auxiliary plate 1 is detachably connected with a second connection component for docking a main wire; the first connection component and the second connection component are electrically connected via a wire; a lower electromagnetic component is arranged on the upper surface of the auxiliary plate 1, and an intermediate component for docking a UAV 29 base is arranged above the auxiliary plate 1, and an upper electromagnetic component corresponding to the lower electromagnetic component is arranged at the lower end of the intermediate component. When in use, the first connecting component is electrically connected to one end of the bypass cable 30, and then the base bracket of the drone 29 is connected to the intermediate component. The intermediate component can be electromagnetically quickly connected through the upper electromagnetic component and the lower electromagnetic component. The drone 29 takes off to pull the intermediate component to take off, and then pull the auxiliary board 1, the first connecting component and the second connecting component to take off synchronously. After the drone 29 is controlled to reach the vicinity of the main wire, the second connecting component is connected to the main wire, that is, the connection between the bypass cable 30 and the main wire is completed. At this time, the upper electromagnetic component and the lower electromagnetic component are separated by the remote control to separate the drone 29 from the auxiliary board 1. The invention is more convenient to use, simple to operate, labor-saving and easy, and further improves the working efficiency. Example 2

[0017] like Figure 1-8 As shown, the present embodiment discloses an electromagnetically connected UAV bypass cable access device, which includes an auxiliary plate 1, the left end of the auxiliary plate 1 is detachably connected with a first connection component for docking a cable, and the right end of the auxiliary plate 1 is detachably connected with a second connection component for docking a main wire; the first connection component and the second connection component are electrically connected via a wire; a lower electromagnetic component is arranged on the upper surface of the auxiliary plate 1, and an intermediate component for docking a UAV 29 base is arranged above the auxiliary plate 1, and an upper electromagnetic component corresponding to the lower electromagnetic component is arranged at the lower end of the intermediate component. When in use, the first connecting component is electrically connected to one end of the bypass cable 30, and then the base bracket of the drone 29 is connected to the intermediate component. The intermediate component can be electromagnetically quickly connected through the upper electromagnetic component and the lower electromagnetic component. The drone 29 takes off to pull the intermediate component to take off, and then pull the auxiliary board 1, the first connecting component and the second connecting component to take off synchronously. After the drone 29 is controlled to reach the vicinity of the main wire, the second connecting component is connected to the main wire, that is, the connection between the bypass cable 30 and the main wire is completed. At this time, the upper electromagnetic component and the lower electromagnetic component are separated by the remote control to separate the drone 29 from the auxiliary board 1. The invention is more convenient to use, simple to operate, labor-saving and easy, and further improves the working efficiency.

[0018] For better effect, the first connection assembly includes a connection plate 2, the lower surface of the connection plate 2 is provided with a first slide groove 3 and a second slide groove 4, and the first slide groove 3 and the second slide groove 4 are arranged parallel to each other, and a left clamping plate 5 and a right clamping plate 6 are arranged below the connection plate 2, and the left clamping plate 5 and the right clamping plate 6 are connected by a spring 7. When in use, in the default state, due to the effect of the restoring force of the spring 7, the left clamping plate 5 and the right clamping plate 6 are close to the clamping state, the end of the cable is placed between the left clamping plate 5 and the right clamping plate 6, the left clamping plate 5 and the right clamping plate 6 are separated outward along the first slide groove 3 and the second slide groove 4, and due to the effect of the spring 7, the cable is clamped and fixed between the left clamping plate 5 and the right clamping plate 6. The first slide groove 3 and the second slide groove 4 are arranged to limit the moving track of the left clamping plate 5 and the right clamping plate 6, thereby enhancing the stability of the cable fixing.

[0019] For better effect, the upper ends of the left clamping plate 5 and the right clamping plate 6 are fixedly connected with the first sliding protrusion and the second sliding protrusion, and the first sliding protrusion is slidably connected in the first sliding groove 3, and the second sliding protrusion is slidably connected in the second sliding groove 4; the outer end of the left clamping plate 5 is fixedly connected with the left clamping head 8, and the outer end of the right clamping plate 6 is fixedly connected with the right clamping head 9, and the left clamping head 8 and the right clamping head 9 are both arc-shaped. By providing the arc-shaped left clamping head 8 and right clamping head 9, the contact area between the left clamping plate 5 and the right clamping plate 6 and the bypass cable 30 is increased, thereby increasing the friction force and enhancing the connection stability.

[0020] For better effect, the lower electromagnetic assembly includes a front groove 10 and a rear groove 11 opened on the upper surface of the auxiliary plate 1, and the front groove 10 is arranged corresponding to the rear groove 11, the inner bottom surface of the front groove 10 is provided with a front guide groove 12, and the inner bottom surface of the rear groove 11 is provided with a rear guide groove 13, the front guide groove 12 is slidably connected with a lower front magnetic block 14, the rear guide groove 13 is slidably connected with a lower rear magnetic block 15, the lower front magnetic block 14 is connected with a front drive assembly for driving the lower front magnetic block 14 to move, and the lower rear magnetic block 15 is connected with a rear drive assembly for driving the lower rear magnetic block 15 to move. The front drive assembly includes a front cavity 16 opened on the left inner wall of the front groove 10, an electric control assembly is arranged inside the front cavity 16, and the electric control assembly is connected with a remote control, and a front electric push rod 18 electrically connected to the electric control assembly is fixedly arranged inside the front cavity 16, and the outer end of the telescopic rod of the front electric push rod 18 is connected to the side wall of the lower front magnetic block 14. The rear drive assembly includes a rear cavity 17 opened on the inner wall of the rear groove 11, and a rear electric push rod 19 is fixedly arranged inside the rear cavity 17. The outer end of the telescopic rod of the rear electric push rod 19 is connected to the side wall of the lower rear magnetic block 15, and the rear electric push rod 19 is electrically connected to the electric control assembly. When in use, after the bypass cable 30 is fixed between the left clamping plate 5 and the right clamping plate 6, the auxiliary plate 1 is fixedly connected to the base bracket of the drone 29, and a signal is sent to the electric control assembly through the remote controller, the electric control assembly controls the telescopic rods of the front electric push rod 18 and the rear electric push rod 19 to extend synchronously, and the lower front magnetic block 14 and the lower rear magnetic block 15 are pushed out of the front cavity 16 and the rear cavity 17 along the front guide groove 12 and the rear guide groove 13, respectively, and are pushed into the interior of the front groove 10 and the rear groove 11. After the upper electromagnetic assembly is close to the lower front magnetic block 14 and the lower rear magnetic block 15, the intermediate assembly is quickly connected to the auxiliary plate 1 under the attraction of the magnetic force. Example 3

[0021] like Figure 1-8As shown, the present embodiment discloses an electromagnetically connected UAV bypass cable access device, which includes an auxiliary plate 1, the left end of the auxiliary plate 1 is detachably connected with a first connection component for docking a cable, and the right end of the auxiliary plate 1 is detachably connected with a second connection component for docking a main wire; the first connection component and the second connection component are electrically connected via a wire; a lower electromagnetic component is arranged on the upper surface of the auxiliary plate 1, and an intermediate component for docking a UAV 29 base is arranged above the auxiliary plate 1, and an upper electromagnetic component corresponding to the lower electromagnetic component is arranged at the lower end of the intermediate component. When in use, the first connecting component is electrically connected to one end of the bypass cable 30, and then the base bracket of the drone 29 is connected to the intermediate component. The intermediate component can be electromagnetically quickly connected through the upper electromagnetic component and the lower electromagnetic component. The drone 29 takes off to pull the intermediate component to take off, and then pull the auxiliary board 1, the first connecting component and the second connecting component to take off synchronously. After the drone 29 is controlled to reach the vicinity of the main wire, the second connecting component is connected to the main wire, that is, the connection between the bypass cable 30 and the main wire is completed. At this time, the upper electromagnetic component and the lower electromagnetic component are separated by the remote control to separate the drone 29 from the auxiliary board 1. The invention is more convenient to use, simple to operate, labor-saving and easy, and further improves the working efficiency.

[0022] For better effect, the first connection assembly includes a connection plate 2, the lower surface of the connection plate 2 is provided with a first slide groove 3 and a second slide groove 4, and the first slide groove 3 and the second slide groove 4 are arranged parallel to each other, and a left clamping plate 5 and a right clamping plate 6 are arranged below the connection plate 2, and the left clamping plate 5 and the right clamping plate 6 are connected by a spring 7. When in use, in the default state, due to the effect of the restoring force of the spring 7, the left clamping plate 5 and the right clamping plate 6 are close to the clamping state, the end of the cable is placed between the left clamping plate 5 and the right clamping plate 6, the left clamping plate 5 and the right clamping plate 6 are separated outward along the first slide groove 3 and the second slide groove 4, and due to the effect of the spring 7, the cable is clamped and fixed between the left clamping plate 5 and the right clamping plate 6. The first slide groove 3 and the second slide groove 4 are arranged to limit the moving track of the left clamping plate 5 and the right clamping plate 6, thereby enhancing the stability of the cable fixing.

[0023] For better effect, the upper ends of the left clamping plate 5 and the right clamping plate 6 are fixedly connected with the first sliding protrusion and the second sliding protrusion, and the first sliding protrusion is slidably connected in the first sliding groove 3, and the second sliding protrusion is slidably connected in the second sliding groove 4; the outer end of the left clamping plate 5 is fixedly connected with the left clamping head 8, and the outer end of the right clamping plate 6 is fixedly connected with the right clamping head 9, and the left clamping head 8 and the right clamping head 9 are both arc-shaped. By providing the arc-shaped left clamping head 8 and right clamping head 9, the contact area between the left clamping plate 5 and the right clamping plate 6 and the bypass cable 30 is increased, thereby increasing the friction force and enhancing the connection stability.

[0024] For better effect, the lower electromagnetic assembly includes a front groove 10 and a rear groove 11 opened on the upper surface of the auxiliary plate 1, and the front groove 10 is arranged corresponding to the rear groove 11, the inner bottom surface of the front groove 10 is provided with a front guide groove 12, and the inner bottom surface of the rear groove 11 is provided with a rear guide groove 13, the front guide groove 12 is slidably connected with a lower front magnetic block 14, the rear guide groove 13 is slidably connected with a lower rear magnetic block 15, the lower front magnetic block 14 is connected with a front drive assembly for driving the lower front magnetic block 14 to move, and the lower rear magnetic block 15 is connected with a rear drive assembly for driving the lower rear magnetic block 15 to move. The front drive assembly includes a front cavity 16 opened on the left inner wall of the front groove 10, an electric control assembly is arranged inside the front cavity 16, and the electric control assembly is connected with a remote control, and a front electric push rod 18 electrically connected to the electric control assembly is fixedly arranged inside the front cavity 16, and the outer end of the telescopic rod of the front electric push rod 18 is connected to the side wall of the lower front magnetic block 14. The rear drive assembly includes a rear cavity 17 opened on the inner wall of the rear groove 11, and a rear electric push rod 19 is fixedly arranged inside the rear cavity 17. The outer end of the telescopic rod of the rear electric push rod 19 is connected to the side wall of the lower rear magnetic block 15, and the rear electric push rod 19 is electrically connected to the electric control assembly. When in use, after the bypass cable 30 is fixed between the left clamping plate 5 and the right clamping plate 6, the auxiliary plate 1 is fixedly connected to the base bracket of the drone 29, and a signal is sent to the electric control assembly through the remote controller, the electric control assembly controls the telescopic rods of the front electric push rod 18 and the rear electric push rod 19 to extend synchronously, and the lower front magnetic block 14 and the lower rear magnetic block 15 are pushed out of the front cavity 16 and the rear cavity 17 along the front guide groove 12 and the rear guide groove 13, respectively, and are pushed into the interior of the front groove 10 and the rear groove 11. After the upper electromagnetic assembly is close to the lower front magnetic block 14 and the lower rear magnetic block 15, the intermediate assembly is quickly connected to the auxiliary plate 1 under the attraction of the magnetic force.

[0025] For better effect, the intermediate component includes a support plate 20, the surface of which is provided with a first through hole 21 and a second through hole 22, the first through hole 21 and the second through hole 22 being used for the base bracket below the drone 29 to pass through, the left end of the support plate 20 being fixedly connected with a first vertical plate 23 extending downward, the right end of the support plate 20 being fixedly connected with a second vertical plate 24 extending downward, the surface of the first vertical plate 23 being provided with a threaded hole, and the surface of the second vertical plate 24 being threadedly connected with a screw 25. When in use, the base bracket of the drone 29 is extended to the bottom of the support plate 20 through the first through hole 21 and the second through hole 22, and then the screw 25 is rotated so that the inner end of the screw 25 passes through the base bracket of the drone 29 and is connected to the threaded hole of the first vertical plate 23, so as to realize the quick connection between the drone 29 and the support plate 20.

[0026] For better effect, the upper electromagnetic assembly includes an upper rear magnetic block 26 fixedly arranged at the lower end of the first vertical plate 23, and an upper front magnetic block 27 fixedly arranged at the lower end of the second vertical plate 24. The second connecting assembly includes a connecting strip arranged at the right end of the auxiliary plate 1, and the connecting strip is connected with a tube hook portion 28, and the tube hook portion 28 is used to hang the main wire. When in use, after the tube hook portion 28 is connected to the main wire by the drone 29, the operator controls the telescopic rods of the front electric push rod 18 and the rear electric push rod 19 to shorten through the remote control, thereby driving the lower front magnetic block 14 and the lower rear magnetic block 15 to be retracted into the front cavity 16 and the rear cavity 17. At this time, the upper front magnetic block 27 and the upper rear magnetic block 26 cannot enter the front cavity 16 and the rear cavity 17, so that the drone 29 can be quickly detached.

[0027] The above are only preferred specific implementation modes of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can make equivalent replacements or changes according to the technical solutions and concepts of the present invention within the technical scope disclosed by the present invention, which should be covered by the protection scope of the present invention.

Claims

1. An electromagnetically connected UAV bypass cable access device, comprising an auxiliary board, characterized in that: The left end of the auxiliary plate is detachably connected to a first connecting component for docking the cable, and the right end of the auxiliary plate is detachably connected to a second connecting component for docking the main wire; a lower electromagnetic component is arranged on the upper surface of the auxiliary plate, and an intermediate component for docking the drone base is arranged above the auxiliary plate, and an upper electromagnetic component corresponding to the lower electromagnetic component is arranged at the lower end of the intermediate component.

2. The electromagnetically connected drone bypass cable access device according to claim 1, characterized in that: The first connecting component includes a connecting plate, a first slide groove and a second slide groove are opened on the lower surface of the connecting plate, and the first slide groove and the second slide groove are arranged parallel to each other, a left clamping plate and a right clamping plate are arranged below the connecting plate, and the left clamping plate and the right clamping plate are connected by a spring.

3. The electromagnetically connected drone bypass cable access device according to claim 2, characterized in that: The upper ends of the left clamping plate and the right clamping plate are fixedly connected with a first sliding protrusion and a second sliding protrusion, and the first sliding protrusion is slidably connected in the first sliding groove, and the second sliding protrusion is slidably connected in the second sliding groove; the outer end of the left clamping plate is fixedly connected with a left clamping head, and the outer end of the right clamping plate is fixedly connected with a right clamping head, and the left clamping head and the right clamping head are both arc-shaped.

4. The electromagnetically connected drone bypass cable access device according to claim 1, characterized in that: The lower electromagnetic component includes a front groove and a rear groove opened on the upper surface of the auxiliary plate, and the front groove is arranged corresponding to the rear groove, the inner bottom surface of the front groove is provided with a front guide groove, and the inner bottom surface of the rear groove is provided with a rear guide groove, the front guide groove is slidably connected to the lower front magnetic block, the rear guide groove is slidably connected to the lower rear magnetic block, the lower front magnetic block is connected to a front driving component for driving the lower front magnetic block to move, and the lower rear magnetic block is connected to a rear driving component for driving the lower rear magnetic block to move.

5. The electromagnetically connected drone bypass cable access device according to claim 4, characterized in that: The front drive assembly includes a front cavity opened on the left inner wall of the front groove, an electric control assembly is arranged inside the front cavity, the electric control assembly is connected to a remote control, a front electric push rod electrically connected to the electric control assembly is fixedly arranged inside the front cavity, and the outer end of the telescopic rod of the front electric push rod is connected to the side wall of the lower front magnetic block.

6. The electromagnetically connected drone bypass cable access device according to claim 5, characterized in that: The rear drive assembly includes a rear cavity opened on the inner wall of the rear groove seat, a rear electric push rod is fixedly arranged inside the rear cavity, the outer end of the telescopic rod of the rear electric push rod is connected to the side wall of the lower rear magnetic block, and the rear electric push rod is electrically connected to the electric control assembly.

7. The electromagnetically connected drone bypass cable access device according to claim 1, characterized in that: The intermediate component includes a support plate, a first through hole and a second through hole are opened on the plate surface of the support plate, the first through hole and the second through hole are used for the base bracket under the drone to pass through, the left end of the support plate is fixedly connected to a first vertical plate extending downward, the right end of the support plate is fixedly connected to a second vertical plate extending downward, the plate surface of the first vertical plate is opened with a threaded hole, and the plate surface of the second vertical plate is threadedly connected with a screw.

8. The electromagnetically connected drone bypass cable access device according to claim 7, characterized in that: The upper electromagnetic assembly includes an upper rear magnetic block fixedly arranged at the lower end of the first vertical plate, and an upper front magnetic block fixedly arranged at the lower end of the second vertical plate.

9. The electromagnetically connected drone bypass cable access device according to claim 1, characterized in that: The second connecting assembly includes a connecting strip arranged at the right end of the auxiliary plate, the connecting strip is connected with a barrel hook portion, and the barrel hook portion is used to hang the main electric wire.

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