Aviation warning device capable of preventing high-voltage line from shaking

Abstract

The invention relates to the technical field of high-voltage line anti-shaking warning, and discloses an aviation warning device capable of preventing high-voltage line shaking, which comprises two hemispherical shells, a clamping assembly, a mounting assembly, a butt joint mechanism and a light emitting assembly, and is characterized in that the clamping assembly comprises two connecting blocks, a supporting strip arc-shaped connecting frame and a clamp; a first electric push rod is installed in the middle of the bottom of the butt joint base, a bent rod is fixedly arranged at the output end of the first electric push rod, a sleeve is fixedly arranged at the bottom of the bent rod, and a second electric push rod is installed on one side of the sliding sleeve. An arc-shaped gasket at the bottom is extruded on a first supporting shaft at the upper end of the clamping assembly, and a first electric push rod and a second electric push rod are matched to stretch out and draw back, so that a limiting rod is clamped into a butt joint mechanism at the top of the clamping assembly, and then the unmanned aerial vehicle and the clamping assembly at the upper end of the anti-shaking warning device are rapidly disassembled and assembled.

Description

Technical Field

[0001] The present invention belongs to the technical field of high-voltage line safety protection, and particularly relates to an aviation warning device capable of preventing high-voltage lines from shaking. Background Art

[0002] High-voltage wires are conductors used to transmit high-voltage electrical energy. They are usually used for long-distance power transmission, can carry high voltages and currents, and transport a large amount of electrical energy generated by power stations to substations or other power-consuming areas. These wires have a high voltage level and play a key role in the power transmission system. High-voltage wires can be seen everywhere in life. Due to their high danger, special attention is required. As the demand for electrical energy in modern society gradually increases, high-voltage wires can be seen everywhere. To ensure the normal operation of ground facilities, the installation height of high-voltage wires is relatively high. The wind force at high altitudes is large and is closer to the flight height when an aircraft descends. Therefore, a warning device for preventing shaking needs to be installed on high-voltage wires.

[0003] In the prior art, ordinary high-voltage line anti-shaking warning devices have the following drawbacks: 1. Since the installation height of high-voltage wires is relatively high, manual installation is very difficult. Ordinary warning devices do not have the function of docking with drones and cannot be installed using drones, increasing the installation difficulty of warning devices on high-voltage wires. 2. At the same time, when a drone docks with a high-voltage line anti-shaking warning device and needs to be disassembled from the high-voltage line for replacement later, ordinary anti-shaking warning devices do not have a quick-docking structure, resulting in the drone being unable to quickly and conveniently dock with the device at high altitude, so that the drone cannot disassemble the warning device, causing the problem of inconvenient replacement of the device. 3. When existing anti-shaking warning devices droop and shake with each other, their own weight is fixed. For high-voltage wires with different diameters and capacities, if the weight is fixed, when installed on some high-capacity and large-diameter high-voltage wires for anti-shaking, the effect is poor, and the own weight cannot be adjusted. It is necessary to adjust during the production of the entire anti-shaking warning device, increasing the production cost.

[0004] Therefore, it is very necessary to invent an aviation warning device capable of preventing high-voltage lines from shaking to solve the above problems, which can realize the installation between the drone and the anti-shaking warning device and improve the anti-shaking performance of high-voltage lines. Summary of the Invention

[0005] In view of the above problems, the present invention provides an aviation warning device capable of preventing high-voltage lines from shaking to solve the problems raised in the above background art.

[0006] To achieve the above object, the present invention provides the following technical solution: An aviation warning device capable of preventing the shaking of high-voltage lines, comprising two hemispherical shells, a clamping assembly, a mounting assembly, a docking mechanism and a lighting assembly. The clamping assembly includes two connecting blocks, a support bar arc connecting frame and a clamp. Among them, the two connecting blocks are respectively installed at the outer wall edges of the two hemispherical shells and are distributed up and down. The support bar is fixedly installed at the top of one of the upper connecting blocks. The arc connecting frame is installed at the top of the support bar. One side of the bottom of the clamp is fixedly connected to the top of the arc connecting frame. A first support shaft is rotatably connected to the middle position inside the clamp. Anti-slip pads are fixedly provided on both sides of the inner wall of the clamp; The mounting assembly includes arc-shaped gaskets sleeved on the outer walls of both ends of the first support shaft. Second support shafts are fixedly provided at the tops of the two arc-shaped gaskets. A docking base is fixedly installed at the tops of the two second support shafts. A docking buckle is fixedly provided at the top of the docking base. A first electric push rod is installed at the middle position of the bottom of the docking base. A bent rod is fixedly provided at the output end of the first electric push rod. A sleeve is fixedly provided at the bottom of the bent rod. A sliding sleeve is slidably connected to the outer wall of one of the second support shafts. A second electric push rod is installed on one side of the sliding sleeve. A limiting rod is fixedly provided at the output end of the second electric push rod, and the outer wall of the limiting rod is inserted into the inner wall of the sleeve. A contact switch is installed at the bottom of the sleeve, and the contact switch is electrically connected to the second electric push rod; Preferably, the docking mechanism includes a connecting rod rotatably installed on the top of the clamp. A connecting shaft is fixedly installed at the middle position of the connecting rod. A clamping ring is sleeved on the outer wall of the connecting shaft. A limiting cylinder is installed at the top of the clamping ring.

[0007] Preferably, the outer wall of one end of the limiting rod passes through the inner wall of the sleeve and is inserted into the inner wall of the limiting cylinder. A first spring is fixedly provided on one side of the middle position of the connecting rod, and one end of the first spring is fixedly connected to one side of the clamping ring.

[0008] Preferably, an arc-shaped limiting chute is provided at the middle position of the bottom of the arc connecting frame. An arc-shaped slider is slidably connected to the inner wall of the arc-shaped limiting chute, and the top of the support bar is fixedly connected to the bottom of the arc-shaped slider. A plurality of card slots are equidistantly and fixedly provided at the outer wall edge of one of the hemispherical shells. A plurality of card strips are equidistantly and fixedly provided at the outer wall edge of the other hemispherical shell, and the outer walls of one ends of each card strip are respectively inserted into the inner walls of each card slot.

[0009] Preferably, mounting platforms are fixedly provided at the bottoms of the inner walls of the two hemispherical shells. A metal ball is wrapped between the two mounting platforms.

[0010] Preferably, the light-emitting component includes battery slots formed at the tops of the two mounting platforms. Lithium batteries are installed on the inner walls of the two battery slots, and two connecting wires are installed on the inner walls of the two mounting platforms.

[0011] Preferably, one end of each of two of the connecting wires is installed with a solar panel, and one end of each of the other two connecting wires is installed with a warning light. Adhesives are installed at the edges of the backs of the two solar panels, and the two solar panels and the two warning lights are electrically connected to the two lithium batteries through the connecting wires.

[0012] Preferably, arc-shaped grooves are formed on one side of each of the two mounting platforms, and the outer walls of the metal balls are respectively in contact with the inner walls of the two arc-shaped grooves.

[0013] Preferably, mounting grooves are formed on one side of the outer walls of the two hemispherical shells. Connecting holes are formed at the middle positions on one side of the outer walls of the two hemispherical shells and on one side of the inner walls of the two mounting grooves. One end of each of the four connecting wires passes through the inner walls of the four connecting holes and is connected to one side of the two solar panels and one side of the warning light.

[0014] Preferably, sealing washers are fixedly provided on the inner walls of two of the connecting holes, and the outer walls of one ends of the two warning lights are respectively in contact with the inner walls of the two sealing washers. A second spring is sleeved at the middle position of the outer wall of the first support shaft, and the two ends of the second spring are fixedly connected to the inner walls of both ends of the clip.

[0015] The technical effects and advantages of the present invention are as follows: 1. By designing the combined use of the clamping component and the mounting component, after docking the mounting component with the drone, the arc-shaped gasket at its bottom is pressed against the first support shaft at the upper end of the clamping component, and under the combined telescopic action of the first electric push rod and the second electric push rod, the limiting rod is inserted into the docking mechanism at the top of the clamping component, thereby realizing the quick disassembly and assembly of the drone and the clamping component at the upper end of the anti-vibration warning device, solving the problem in the prior art that it is difficult to disassemble and assemble the anti-vibration warning device on the high-voltage overhead line by the drone; 2. By designing the docking mechanism, by providing a limiting cylinder on the docking mechanism to dock and lock it with the limiting rod at the upper end of the mounting component, and the limiting cylinder connects the clamping ring and the side wall of the connecting rod through the first spring, so that when pulling, there is no movement interference between the clamping ring and the connecting rod, and at the same time, the docking mechanism always keeps the limiting cylinder perpendicular to the upward clamping ring state when not in use for a long time, facilitating the later docking of the drone with the mounting component at high altitude and improving the convenience of later disassembly and replacement of the anti-vibration warning device; 3. The present invention sets up mounting platforms inside the two hemispherical shells of the anti-shake warning device, and wraps metal balls in the arc-shaped grooves on the side walls of the mounting platforms. Later, according to the flux and diameter size of the working high-voltage wire, metal balls with the same volume but different material densities are replaced specifically to change the weight of the entire anti-shake warning device, facilitating the device to exhibit good anti-shake performance for various types of high-voltage wires, without specifically modifying and producing the entire device, and reducing the production and processing cost of the anti-shake warning device.

[0016] Other features and advantages of the present invention will be described in the subsequent specification, and part of them will be obvious from the specification or understood by implementing the present invention. The objectives and other advantages of the present invention can be achieved and obtained through the structures pointed out in the specification, claims, and drawings. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] In order to more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the following will briefly introduce the drawings required for use in the description of the embodiments or the prior art. Obviously, the drawings in the following description are some embodiments of the present invention. For those of ordinary skill in the art, other drawings can be obtained based on these drawings without creative efforts.

[0018] Figure 1 is a three-dimensional schematic diagram of the present invention; Figure 2 is a structural schematic diagram of the clamping assembly of the present invention; Figure 3 is a structural schematic diagram of the mounting assembly of the present invention; Figure 4 is a structural schematic diagram of the connection between the limiting rod and the bent rod, etc. of the present invention; Figure 5 is the appendix of the specification of the present invention Figure 1 is an enlarged structural schematic diagram at position A in the appendix of the specification of the present invention; Figure 6 is a structural schematic diagram of the connection between the snap ring and the limiting cylinder of the present invention; Figure 7 is a structural schematic diagram of the separated state of the two hemispherical shells of the present invention; Figure 8 is the appendix of the specification of the present invention Figure 7 is an enlarged structural schematic diagram at position B in the appendix of the specification of the present invention; Figure 9 is a structural schematic diagram inside the hemispherical shell of the present invention; Figure 10 is a structural schematic diagram of the light-emitting component of the present invention; Figure 11 is a structural schematic diagram of the outer wall of the hemispherical shell of the present invention; Figure 12It is a schematic structural diagram of the connection of the first support shaft, the clamp and the second spring in the present invention.

[0019] In the figure: 1, hemispherical shell; 2, clamping assembly; 201, connecting block; 202, support bar; 203, arc connecting frame; 204, clamp; 205, first support shaft; 206, anti-slip pad; 3, mounting assembly; 301, arc gasket; 302, second support shaft; 303, docking base; 304, docking buckle; 305, first electric push rod; 306, bent rod; 307, sleeve; 308, sliding sleeve; 309, second electric push rod; 310, limiting rod; 311, contact switch; 4, docking mechanism; 401, connecting rod; 402, connecting shaft; 403, snap ring; 404, limiting cylinder; 405, first spring; 5, arc limiting chute; 6, arc sliding block; 7, card slot; 8, card strip; 9, mounting table; 10, metal ball; 11, lighting assembly; 1101, battery slot; 1102, lithium battery; 1103, connecting wire; 1104, solar panel; 1105, warning light; 1106, back glue; 12, arc groove; 13, mounting groove; 14, connecting hole; 15, sealing washer; 16, second spring. Detailed implementation manners

[0020] To make the objectives, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are some, but not all, of the embodiments of the present invention. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present invention without creative efforts shall fall within the protection scope of the present invention.

[0021] The present invention provides an aviation warning device as shown in Figure 1-12 which can prevent the high-voltage line from shaking, including two hemispherical shells 1, a clamping assembly 2, a mounting assembly 3, a docking mechanism 4 and a lighting assembly 11, and is characterized in that: the clamping assembly 2 includes two connecting blocks 201, a support bar 202, an arc connecting frame 203 and a clamp 204. Among them, the two connecting blocks 201 are respectively installed at the outer wall edges of the two hemispherical shells 1 and are distributed vertically. The support bar 202 is fixedly installed at the top of one of the upper connecting blocks 201. The arc connecting frame 203 is installed at the top of the support bar 202. One side of the bottom of the clamp 204 is fixedly connected to the top of the arc connecting frame 203. The middle position inside the clamp 204 is rotatably connected to a first support shaft 205. Anti-slip pads 206 are fixedly provided on both sides of the inner wall of the clamp 204; The installation component 3 includes arc-shaped gaskets 301 sleeved on the outer walls of both ends of the first support shaft 205. Second support shafts 302 are fixedly arranged at the tops of the two arc-shaped gaskets 301. A docking base 303 is fixedly installed at the tops of the two second support shafts 302. A docking buckle 304 is fixedly arranged at the top of the docking base 303. A first electric push rod 305 is installed at the middle position of the bottom of the docking base 303. A bent rod 306 is fixedly arranged at the output end of the first electric push rod 305. A sleeve 307 is fixedly arranged at the bottom of the bent rod 306. A sliding sleeve 308 is slidably connected to the outer wall of one of the second support shafts 302. A second electric push rod 309 is installed on one side of the sliding sleeve 308. A limiting rod 310 is fixedly arranged at the output end of the second electric push rod 309, and the outer wall of the limiting rod 310 is inserted into the inner wall of the sleeve 307. A contact switch 311 is installed at the bottom of the sleeve 307, and the contact switch 311 is electrically connected to the second electric push rod 309. When the installation component 3 applies force through the first electric push rod 305, since its bottom is supported on the first support shaft 205 through the second support shaft 302 and the arc-shaped gasket 301, after applying force, the limiting rod 310 and the like apply upward force, and the clamping component 2 and the like are pulled to apply upward force and then squeeze on the arc-shaped gasket 301, so that it can maintain the original position to apply force and will not cause the situation of being unable to receive force; During use, the clamping component 2 is connected to the two hemispherical shells 1. When using a drone to install this anti-vibration warning device on a high-voltage line, the installation component 3 is docked and installed at the bottom of the drone through the docking buckle 304 at the top of its docking base 303, and rotated so that the docking buckle 304 is snapped into the docking groove of the drone. The opening shape of the docking groove of the drone can be referred to in the attached Figure 3It is only necessary to imitate the shape of the docking buckle 304 shown. After the drone is docked with the installation component 3, the two arc-shaped gaskets 301 at its bottom are placed on both sides of the first support shaft 205 inside the clamping 204 at the upper end of the clamping component 2. And an internal battery is arranged inside the docking base 303, which is electrically connected to the first electric push rod 305, and the internal battery functions for the second electric push rod 309 and the contact switch 311. Then, the first electric push rod 305 is controlled to expand and contract so that the bent rod 306 at its output end descends and drives the sleeve 307 at its bottom to descend until it touches the docking mechanism 4. Then, the contact switch 311 at the bottom of the sleeve 307 is touched and triggers the second electric push rod 309 to expand and contract, pushing the limiting rod 310 through the sleeve 307 and clamping it into the docking mechanism 4, fixing the installation component 3 on the clamping component 2 and then connecting it to the entire warning device. At the same time, the drone is docked with the anti-shake warning device. By controlling the drone to fly to the upper end of the high-voltage line, the first electric push rod 305 is controlled to start contracting, and then the docking mechanism 4 is pulled, pulling the clamping 204 on the clamping component 2 to expand and surround the high-voltage line. After wrapping the high-voltage line, the first electric push rod 305 is used to push the bent rod 306 to descend, so that the clamping 204 contracts and then clamps on the high-voltage line. Then, by starting the second electric push rod 309, the limiting rod 310 is withdrawn from the limiting cylinder 404 on the docking mechanism 4, and then the entire installation component 3 is detached from the fixation with the clamping component 2. The drone flies away with the installation component 3 to complete the installation of the anti-shake high-voltage line warning device by the drone, solving the problem in the prior art that it is difficult to disassemble and assemble the anti-shake warning device on the high-voltage line at high altitude by the drone; As Figure 4-6 shown, the docking mechanism 4 includes a connecting rod 401 rotatably installed on the top of the clamping 204. A connecting shaft 402 is fixedly installed at the middle position of the connecting rod 401. A snap ring 403 is sleeved on the outer wall of the connecting shaft 402. A limiting cylinder 404 is installed on the top of the snap ring 403. When the drone installs this high-voltage line anti-shake warning device, it is docked with the docking mechanism 4 at the top of the clamping component 2 through the installation component 3. During docking, the bent rod 306 drives the sleeve 307 to descend under the drive of the first electric push rod 305. At the same time, the limiting rod 310 connected to the sleeve 307 is fixed to the second electric push rod 309, and the second electric push rod 309 slides up and down through the sliding sleeve 308 on one of the second support shafts 302, and then the sleeve 307 is brought to abut against the outer wall of one side of the limiting cylinder 404, as shown in the attached Figure 6 figure. As shown, a buffer groove is opened on one side of the top of the limiting cylinder 404. The contact switch 311 of the sleeve 307 is snapped into it and contacts its inner wall to trigger the second electric push rod 309 to expand and contract and snap into the limiting cylinder 404. After the first electric push rod 305 pulls the bent rod 306 to rise, the connecting rod 401 is pulled and folded, and then the clamping 204 is driven to rotate and expand, opening the clamping 204 to facilitate clamping on the outside of the high-voltage line.

[0022] One end of the outer wall of the limiting rod 310 passes through the inner wall of the sleeve 307 and is inserted and connected with the inner wall of the limiting cylinder 404. On one side of the middle position of the connecting rod 401, a first spring 405 is fixedly arranged, and one end of the first spring 405 is fixedly connected with one side of the snap ring 403. During the period when the docking mechanism 4 is not in use, the snap ring 403 is connected to the limiting cylinder 404 at the top. Under the connection of the first spring 405, when the docking mechanism 4 is not in use, the limiting cylinder 404 is always in a state with the vertical snap ring 403 facing upwards, which is convenient for the installation component 3 to be docked with it during installation and for the limiting rod 310 to be inserted into the limiting cylinder 404 again when disassembling the device later, facilitating the quick docking with the drone when the warning device is disassembled from the high-voltage line and improving the convenience of using the device.

[0023] As Figure 2 and Figure 7-8 shown, an arc-shaped limiting chute 5 is opened at the middle position of the bottom of the arc-shaped connecting frame 203. An arc-shaped slider 6 is slidably connected to the inner wall of the arc-shaped limiting chute 5, and the top of the support bar 202 is fixedly connected to the bottom of the arc-shaped slider 6. A plurality of card slots 7 are equidistantly and fixedly arranged at the edge of the outer wall of one hemispherical shell 1, and a plurality of card strips 8 are equidistantly and fixedly arranged at the edge of the outer wall of the other hemispherical shell 1. One end of the outer wall of each card strip 8 is respectively inserted and connected with the inner wall of each card slot 7. After the high-voltage line anti-vibration warning device is clamped on the high-voltage line by the clamping component 2, when the wind blows and the high-voltage line shakes, the hemispherical shell 1 at the bottom, which slides through the support bar 202 and the arc-shaped slider 6 in the arc-shaped limiting chute 5 at the bottom of the arc-shaped connecting frame 203, also shakes accordingly. And the gravity ball formed by the two hemispherical shells 1 slides in the arc-shaped limiting chute 5 through the arc-shaped slider 6 and shakes relative to the clamping component 2, so that the shaking amplitude is different from that of the high-voltage line, more efficiently buffering the shaking amplitude of the high-voltage line and improving the anti-vibration effect of the device. And the hemispherical shell 1 is fixed by being clamped through the card slots 7 and the card strips 8 as shown in the attached Figure 8 shown. A depression is opened at one end of the card strip 8, and one side of its outer wall protrudes. When it is inserted into the card slot 7, they are mutually extruded so that the whole is aligned with the inner wall of the card slot 7. When the protruding end of the card strip 8 is separated from the inner wall of the card slot 7, the card strip 8 bounces off, and then the protruding part is limited on the other side of the card slot 7, and then they are mutually extruded to fix the two hemispherical shells 1.

[0024] At the bottom of the inner walls of both hemispherical shells 1, mounting platforms 9 are fixedly provided. A metal ball 10 is wrapped between the two mounting platforms 9. According to the flux model and diameter size of the high-voltage wire, metal balls with the same volume but different material densities are used and snapped between the two mounting platforms 9. Then, through the mutual clamping of the card slots 7 and the card strips 8 outside the hemispherical shell 1, it is fixed to the hemispherical shell 1. By adjusting the overall weight of the device, it can achieve an effective anti-vibration effect for high-voltage wires with different diameter sizes without modifying and producing the entire device, reducing the production cost of this anti-vibration warning device; As Figure 9-10 shown, the light-emitting component 11 includes battery slots 1101 opened at the tops of the two mounting platforms 9. Lithium batteries 1102 are installed on the inner walls of the two battery slots 1101. Two connecting wires 1103 are installed on the inner walls of the two mounting platforms 9. After the lithium batteries 1102 are installed in the battery slots 1101, they can be connected to the mounting platforms 9 through the connecting wires 1103. Then, after the connecting wires 1103 are respectively connected to the solar panels 1104 and the warning lights 1105, the two are electrically connected to the lithium batteries 1102.

[0025] One end of each of the two connecting wires 1103 is installed with a solar panel 1104, and one end of each of the other two connecting wires 1103 is installed with a warning light 1105. Adhesive tapes 1106 are installed at the edges of the backs of the two solar panels 1104. Both the two solar panels 1104 and the two warning lights 1105 are electrically connected to the two lithium batteries 1102 through the connecting wires 1103. When the light-emitting component 11 is in use, the solar panels 1104 are installed outside the hemispherical shell 1 to convert light energy into electrical energy and store it in the lithium batteries 1102. When the sun sets and after being illuminated, the solar panels 1104 trigger the lithium batteries 1102 to transfer current to the warning lights 1105, causing them to flash intermittently to achieve the purpose of high-altitude warning; As Figure 11 shown, arc-shaped grooves 12 are opened on one side of each of the two mounting platforms 9. The outer walls of the metal balls 10 are respectively in contact with the inner walls of the two arc-shaped grooves 12. When the metal ball 10 is clamped and wrapped by the two mounting platforms 9, the metal ball 10 is located inside the two arc-shaped grooves 12 and is in extrusion contact with their inner walls, so that when the hemispherical shell 1 shakes, the metal ball 10 inside it maintains the same shaking frequency as the hemispherical shell 1.

[0026] On one side of the outer walls of both hemispherical shells 1, mounting grooves 13 are provided. Connecting holes 14 are provided at the middle positions of one side of the outer walls of the two hemispherical shells 1 and on one side of the inner walls of the two mounting grooves 13. One ends of four connecting lines 1103 respectively pass through the inner walls of the four connecting holes 14 and are connected to one side of the two solar panels 1104 and one side of the warning lamp 1105. When the solar panel 1104 is installed outside the hemispherical shell 1, it is fixed in the mounting groove 13 by the adhesive 1106 on its back to prevent it from falling off when shaking. And the warning lamp 1105 passes through the connecting hole 14 so that its outer wall is squeezed and clamped by the sealing gasket 15, which is waterproof and not easy to fall off at the same time; As Figure 12 shown, sealing gaskets 15 are fixedly provided on the inner walls of two of the connecting holes 14, and the outer walls of one ends of the two warning lamps 1105 are respectively in contact with the inner walls of the two sealing gaskets 15. A second spring 16 is sleeved at the middle position of the outer wall of the first support shaft 205, and both ends of the second spring 16 are fixedly connected to the inner walls of both ends of the clip 204. When the clip 204 is unfolded and tightened for clamping, the second spring 16 is sleeved on the first support shaft 205 and connected to the clip 204. The elastic coefficient of the second spring 16 is relatively large, so that the clip 204 can be stably clamped on the high-voltage line and not easy to fall off under the elastic action of the second spring 16.

[0027] Although the present invention has been described in detail with reference to the foregoing embodiments, those of ordinary skill in the art should understand that: they can still modify the technical solutions recorded in the foregoing embodiments, or perform equivalent replacements on some of the technical features; and these modifications or replacements do not make the essence of the corresponding technical solutions deviate from the spirit and scope of the technical solutions of the embodiments of the present invention.

Claims

1. An aviation warning device capable of preventing high-voltage wires from shaking, comprising two hemispherical shells (1), a clamping assembly (2), a mounting assembly (3), a docking mechanism (4) and a light-emitting assembly (11), characterized in that: The clamping assembly (2) comprises two connecting blocks (201), a support bar (202), an arc-shaped connecting frame (203) and a clamp (204), wherein the two connecting blocks (201) are respectively mounted on the outer wall edges of the two hemispherical shells (1) and are arranged in an upper and lower arrangement, the support bar (202) is fixedly mounted on the top of one of the connecting blocks (201) located above, the arc-shaped connecting frame (203) is mounted on the top of the support bar (202), one side of the bottom of the clamp (204) is fixedly connected to the top of the arc-shaped connecting frame (203), a first supporting shaft (205) is rotatably connected to the middle position inside the clamp (204), and anti-slip pads (206) are fixedly provided on both sides of the inner wall of the clamp (204); The mounting assembly (3) comprises an arc-shaped gasket (301) sleeved on the outer walls of both ends of the first support shaft (205); the tops of the two arc-shaped gaskets (301) are fixedly provided with a second support shaft (302); the tops of the two second support shafts (302) are fixedly provided with a docking base (303); the tops of the docking bases (303) are fixedly provided with a docking buckle (304); the middle position of the bottom of the docking base (303) is installed with a first electric push rod (305); the output end of the first electric push rod (305) is fixedly provided with a bent rod (306) A sleeve (307) is fixedly provided at the bottom of the bent rod (306), a sliding sleeve (308) is slidably connected to the outer wall of one of the second support shafts (302), a second electric push rod (309) is installed on one side of the sliding sleeve (308), a limiting rod (310) is fixedly provided at the output end of the second electric push rod (309), and the outer wall of the limiting rod (310) is interlaced and connected with the inner wall of the sleeve (307), a contact switch (311) is installed at the bottom of the sleeve (307), and the contact switch (311) is electrically connected to the second electric push rod (309).

2. The aviation warning device capable of preventing high-voltage wire from shaking according to claim 1 is characterized in that: The docking mechanism (4) comprises a connecting rod (401) rotatably mounted on the top of the clamp (204), a connecting shaft (402) being fixedly mounted in the middle of the connecting rod (401), a clamping ring (403) being sleeved on the outer wall of the connecting shaft (402), and a limiting cylinder (404) being mounted on the top of the clamping ring (403).

3. The aviation warning device capable of preventing high-voltage line shaking according to claim 2 is characterized in that: The outer wall of one end of the limiting rod (310) passes through the inner wall of the sleeve (307) and is interlaced with the inner wall of the limiting cylinder (404); a first spring (405) is fixedly provided on one side of the middle position of the connecting rod (401), and one end of the first spring (405) is fixedly connected to one side of the clamping ring (403).

4. The aviation warning device capable of preventing high-voltage wire from shaking according to claim 1 is characterized in that: An arc-shaped limiting sliding groove (5) is provided in the middle of the bottom of the arc-shaped connecting frame (203); an arc-shaped sliding block (6) is slidably connected to the inner wall of the arc-shaped limiting sliding groove (5); and the top of the support bar (202) is fixedly connected to the bottom of the arc-shaped sliding block (6); a plurality of slots (7) are fixedly provided at equal distances on the edge of the outer wall of one of the hemispherical shells (1); and a plurality of clips (8) are fixedly provided at equal distances on the edge of the outer wall of the other hemispherical shell (1); and the outer wall of one end of each clip (8) is respectively interlaced and connected with the inner wall of each clip slot (7).

5. The aviation warning device capable of preventing high-voltage wire from shaking according to claim 1 is characterized in that: A mounting platform (9) is fixedly provided at the bottom of the inner wall of the two hemispherical shells (1), and a metal ball (10) is wrapped between the two mounting platforms (9).

6. The aviation warning device capable of preventing high-voltage wire from shaking according to claim 5, characterized in that: The light-emitting component (11) comprises a battery slot (1101) opened on the top of two mounting platforms (9), the inner walls of the two battery slots (1101) are both equipped with lithium batteries (1102), and the inner walls of the two mounting platforms (9) are both equipped with two connecting wires (1103).

7. The aviation warning device capable of preventing high-voltage wire from shaking according to claim 6 is characterized in that: Two of the connecting wires (1103) are each installed with a solar panel (1104) at one end, and the other two of the connecting wires (1103) are each installed with a warning light (1105) at one end. Adhesive tape (1106) is installed at the edges of the backs of the two solar panels (1104). The two solar panels (1104) and the two warning lights (1105) are electrically connected to the two lithium batteries (1102) via the connecting wires (1103).

8. The aviation warning device capable of preventing high-voltage wire from shaking according to claim 7 is characterized in that: One side of the two mounting platforms (9) is provided with an arc-shaped groove (12), and the outer wall of the metal ball (10) is in contact with the inner walls of the two arc-shaped grooves (12) respectively.

9. The aviation warning device capable of preventing high-voltage wire from shaking according to claim 8 is characterized in that: One side of the outer wall of the two hemispherical shells (1) is provided with a mounting groove (13), a connection hole (14) is provided at the middle position of one side of the outer wall of the two hemispherical shells (1) and one side of the inner wall of the two mounting grooves (13), and one end of four connecting wires (1103) passes through the inner wall of the four connecting holes (14) to connect to one side of the two solar panels (1104) and one side of the warning light (1105).

10. The aviation warning device capable of preventing high-voltage wire from shaking according to claim 9, characterized in that: The inner walls of the two connection holes (14) are fixedly provided with sealing gaskets (15), and the outer walls of one end of the two warning lights (1105) are respectively in contact with the inner walls of the two sealing gaskets (15), and a second spring (16) is sleeved at the middle position of the outer wall of the first support shaft (205), and the two ends of the second spring (16) are respectively fixedly connected to the inner walls of the two ends of the clamp (204).

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