CN210761311U - Unmanned aerial vehicle for eliminating risks of high-altitude power line in electrified mode - Google Patents
Unmanned aerial vehicle for eliminating risks of high-altitude power line in electrified mode Download PDFInfo
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- CN210761311U CN210761311U CN201921707246.7U CN201921707246U CN210761311U CN 210761311 U CN210761311 U CN 210761311U CN 201921707246 U CN201921707246 U CN 201921707246U CN 210761311 U CN210761311 U CN 210761311U
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Abstract
The utility model provides an unmanned aerial vehicle of danger is arranged with electricity to eminence power line, which comprises a bod, the equal first fixed plate of fixedly connected with in the left and right sides at both ends around the organism, rotor device of the equal fixedly connected with in upper end of first fixed plate, the equal U-shaped frame of fixedly connected with in lower extreme left part and the right part of organism, and the flexible engine of lower wall fixedly connected with of left side U-shaped frame, the output fixedly connected with telescopic link of flexible engine, the first connecting plate of upper end fixedly connected with of telescopic link, the front end middle part fixed mounting of first connecting plate has the second connecting plate, the anterior fixedly connected with motor in upper end of second connecting plate, the lower extreme front portion of second connecting plate is provided with sways extrusion device, the lower extreme fixedly connected with second fixed plate of first connecting plate, the front. The utility model discloses an unmanned aerial vehicle of danger is arranged with electricity to eminence power line keeps away from the crushing plate unmanned aerial vehicle organism and the nearly contact of high-voltage line cross, ensures unmanned aerial vehicle's safe in utilization.
Description
Technical Field
The utility model belongs to the technical field of the unmanned air vehicle technique and specifically relates to an electrified danger elimination unmanned aerial vehicle of eminence power line.
Background
Unmanned aircraft, also called "drones" for short, are unmanned aircraft that are operated by means of radio remote control devices and self-contained program control devices, or are operated autonomously, either completely or intermittently, by an onboard computer, unmanned aircraft often being more suited to tasks that are too "fool, dirty or dangerous" than manned aircraft; with the development of informatization, the laying of high-voltage power lines across the country is visible everywhere, however, in rainy and snowy weather, many overhead high-voltage power lines are easy to freeze, the weight of the frozen high-voltage power lines obviously increases, and serious influence is caused to power transmission, so that ice needs to be broken, and people usually adopt an unmanned aerial vehicle to break ice due to the limitation of severe environment.
The existing high-altitude power line electrified danger elimination unmanned aerial vehicle is used, the technical requirement of the unmanned aerial vehicle on an operator for ice breaking is high, the operation is complex, ice blocks on a high-voltage line cannot be effectively broken when ice breaking is carried out, the deicing efficiency is reduced, the labor intensity of workers is improved, meanwhile, the unmanned aerial vehicle needs to enter a distance to contact a high-voltage wire in the deicing process, the unmanned aerial vehicle and the high-voltage wire are easy to collide, so that the unmanned aerial vehicle crashes, potential safety hazards are caused for the unmanned aerial vehicle, and the cost of deicing danger elimination is improved.
Disclosure of Invention
The utility model aims to solve the technical problem that an electrified dangerous unmanned aerial vehicle of arranging of eminence power line is provided, can solve deicing speed slow, the deicing effect is not obvious, unmanned aerial vehicle has the problem of potential safety hazard.
In order to solve the technical problem, the utility model discloses the technical scheme who adopts is: an unmanned aerial vehicle for eliminating danger of a high-altitude power line with electricity comprises a machine body, wherein the left side and the right side of the front end and the rear end of the machine body are both fixedly connected with a first fixing plate, the upper end of the first fixing plate is both fixedly connected with a rotor wing device, the left part and the right part of the lower end of the machine body are both fixedly connected with a U-shaped frame, and the lower wall of the left U-shaped frame is fixedly connected with a telescopic power machine, the output end of the telescopic power machine is fixedly connected with a telescopic rod, the upper end of the telescopic rod is fixedly connected with a first connecting plate, the middle part of the front end of the first connecting plate is fixedly provided with a second connecting plate, the front part of the upper end of the second connecting plate is fixedly connected with a motor, the front part of the lower end of the second connecting plate is provided with a swinging extrusion device, the lower end of the first connecting plate is fixedly connected with a second fixing plate, the lower part of the front end of the second fixing plate is connected with a beating crushing device, and the.
The main structure of rotor device has a fixed cylinder and a first rotating rod, the first rotating rod is inserted and connected at the upper end of the fixed cylinder, the outer surface upper part of the first rotating rod is fixedly connected with a rotor, and the fixed cylinder is fixedly connected with the rotor device and a first fixed plate at the front part of the upper end of the first fixed plate.
The main structure of the swinging extrusion device is provided with a second rotating rod and a U-shaped block, the U-shaped block is fixedly connected at the lower end of the second rotating rod, the middle parts of the front and rear inner walls of the U-shaped block are movably connected with a third connecting plate through a rotating shaft, the lower end of the third connecting plate is fixedly connected with an extrusion disc, and the upper end of the second rotating rod penetrates through the second connecting plate and is fixedly connected with the output end of a motor to swing the extrusion device and the motor to be connected together.
The main structure of the rapping crushing device is provided with a third rotating rod and a crushing plate, the crushing plate is fixedly arranged on the front portion of the outer surface of the third rotating rod, a balance plate is fixedly connected to the upper portions of the left end and the right end of the crushing plate, a fourth connecting plate is fixedly connected to the left portion and the right portion of the upper ends of the two groups of balance plates, and the third rotating rod is inserted and connected to the lower portion of the front end of a second fixing plate to be rapped and movably connected with the second fixing plate.
The right part of the first connecting plate is connected with a limiting rod in an inserting mode, and the lower end of the limiting rod is fixedly connected to the lower wall of the right U-shaped frame.
The lower part of the swinging extrusion device is positioned in the middle of the beating and crushing device.
The utility model provides a pair of electrified dangerous unmanned aerial vehicle of arranging of eminence power line, beneficial effect is as follows:
1. the fourth connecting plate on both sides is extruded when rotating through the disc to drive the balance plate and be in the horizontal hunting state, the third bull stick is in the horizontal hunting state simultaneously, thereby drive the breaker and be in when horizontal hunting to strike the ice-cube on the high-tension line, and then can effectually break the ice-cube and drop from the electric wire, operation process is simple, has reduced staff's intensity of labour, has improved deicing efficiency, the effectual transport safety of protecting the high-tension line.
2. The swing extrusion device is driven to swing and the breaking device is beaten to move downwards when the first connecting plate moves downwards, so that the unmanned aerial vehicle body is kept away from the breaking plate, the unmanned aerial vehicle is prevented from being in close contact with a high-voltage line in the ice breaking process, the use safety of the unmanned aerial vehicle is effectively guaranteed, the potential safety hazard is reduced, and the cost of deicing and danger elimination is reduced.
Drawings
The invention will be further explained with reference to the following figures and examples:
fig. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a schematic view of the overall structure of the rotor device of the present invention;
FIG. 3 is a schematic view of the overall structure of the swing extrusion device of the present invention;
fig. 4 is a schematic view of the overall structure of the rapping and breaking device of the present invention.
In the figure: 1. a body; 2. a first fixing plate; 3. a rotor device; 4. a U-shaped frame; 5. a telescopic power machine; 6. a telescopic rod; 7. a first connecting plate; 8. a second connecting plate; 9. a motor; 10. a rocking extrusion device; 11. a second fixing plate; 12. beating the crushing device; 13. a limiting rod; 31. a fixed cylinder; 32. a first rotating lever; 33. a rotor; 101. a second rotating rod; 102. a U-shaped block; 103. a third connecting plate; 104. extruding the disc; 121. a third rotating rod; 122. a breaker plate; 123. a balance plate; 124. and a fourth connecting plate.
Detailed Description
As shown in fig. 1-4, an unmanned aerial vehicle with high power line live danger elimination function comprises a machine body 1, wherein a first fixing plate 2 is fixedly connected to each of the left and right sides of the front end and the rear end of the machine body 1, a rotor device 3 is fixedly connected to each of the upper ends of the first fixing plates 2, a U-shaped frame 4 is fixedly connected to each of the left portion and the right portion of the lower end of the machine body 1, a telescopic power machine 5 is fixedly connected to the lower wall of the U-shaped frame 4 on the left side, the telescopic power machine 5 drives the telescopic rod 6 to extend and retract, a telescopic rod 6 is fixedly connected to the output end of the telescopic power machine 5, a first connecting plate 7 is fixedly connected to the upper end of the telescopic rod 6, a second connecting plate 8 is fixedly installed in the middle of the front end of the first connecting plate 7, a motor 9 is fixedly connected to the front portion of the upper end, a lower portion of the front end of the second fixing plate 11 is connected with a rapping crusher device 12, and the rapping crusher device 12 is located below the rocking pressing device 10.
Rotor device 3's primary structure has solid fixed cylinder 31 and first bull stick 32, and first bull stick 32 alternates to be connected in the upper end of solid fixed cylinder 31, and thereby the surface upper portion fixedly connected with rotor 33 of first bull stick 32 drives rotor 33 through first bull stick 32 and rotates and make unmanned aerial vehicle take off, and solid fixed cylinder 31 fixed connection is with rotor device 3 and 2 fixed connection of first fixed plate 2 in the upper end front portion of first fixed plate 2.
The main structure of the swing extrusion device 10 is provided with a second rotating rod 101 and a U-shaped block 102, the U-shaped block 102 is fixedly connected to the lower end of the second rotating rod 101, the middle parts of the front and rear inner walls of the U-shaped block 102 are movably connected with a third connecting plate 103 through rotating shafts, the lower end of the third connecting plate 103 is fixedly connected with an extrusion disc 104, a fourth connecting plate 124 is extruded through the extrusion disc 104, and the upper end of the second rotating rod 101 penetrates through the second connecting plate 8 and is fixedly connected to the output end of a motor 9 to movably connect the swing extrusion device 10 and the motor 9 together.
The main structure of the rapping breaking device 12 is provided with a third rotating rod 121 and a crushing plate 122, the crushing plate 122 is used for rapping ice cubes on a broken high-voltage electric wire, the crushing plate 122 is fixedly arranged at the front part of the outer surface of the third rotating rod 121, a balance plate 123 is fixedly connected to the upper parts of the left end and the right end of the crushing plate 122, a fourth connecting plate 124 is fixedly connected to the left part and the right part of the upper ends of the two groups of balance plates 123, and the third rotating rod 121 is inserted and connected to the lower part of the front end of the second fixing plate 11 to movably connect the rapping breaking device 12 and the second fixing plate 11.
The right part of the first connecting plate 7 is connected with a limiting rod 13 in an inserting mode, the lower end of the limiting rod 13 is fixedly connected to the lower wall of the right U-shaped frame 4, and the limiting rod 13 plays a limiting role in limiting the first connecting plate 7.
The lower portion of the rocking pressing device 10 is located at a middle position of the rapping crushing device 12, so that the rapping crushing device 12 is pressed by the rocking pressing device 10.
The working process of the utility model is as follows:
the second rotating rod 101 is driven to rotate by the motor 9, so that the third connecting plate 103 is driven to rotate when the U-shaped block 102 is driven to rotate, the fourth connecting plates 124 at two sides are extruded when the extrusion disc 104 is driven to rotate, the balance plate 123 is driven to be in a left-right swinging state, meanwhile, the third rotating rod 121 is in a left-right rotating state, so that the crushing plate 122 is driven to knock ice blocks on the high-voltage wire left and right when swinging left and right, the ice blocks can be effectively crushed and fall off the wire, the operation process is simple, the labor intensity of workers is reduced, the deicing efficiency is improved, the conveying safety of the high-voltage wire is effectively protected, the telescopic rod 6 is driven to stretch by the telescopic power machine 5, the first connecting plate 7 is driven to move downwards, the swinging extrusion device 10 and the knocking crushing device 12 are driven to move downwards, and the crushing plate 122 is far away, avoid unmanned aerial vehicle and high-voltage line to cross nearly contact at the in-process that opens ice, effectual ensured unmanned aerial vehicle's safety in utilization, reduced the potential safety hazard, reduced the cost that the deicing was arranged danger.
The above embodiments are merely preferred technical solutions of the present invention, and should not be considered as limitations of the present invention, and the features in the embodiments and the examples in the present application may be arbitrarily combined with each other without conflict. The protection scope of the present invention shall be defined by the claims and the technical solutions described in the claims, including the technical features of the equivalent alternatives as the protection scope. Namely, equivalent alterations and modifications within the scope of the invention are also within the scope of the invention.
Claims (6)
1. The utility model provides an unmanned aerial vehicle of danger is arranged with electricity to eminence power line, includes organism (1), its characterized in that: the left side and the right side of the front end and the rear end of the machine body (1) are fixedly connected with a first fixing plate (2), the upper end of the first fixing plate (2) is fixedly connected with a rotor wing device (3), the left part and the right part of the lower end of the machine body (1) are fixedly connected with a U-shaped frame (4), the lower wall of the left U-shaped frame (4) is fixedly connected with a telescopic power machine (5), the output end of the telescopic power machine (5) is fixedly connected with a telescopic rod (6), the upper end of the telescopic rod (6) is fixedly connected with a first connecting plate (7), the middle part of the front end of the first connecting plate (7) is fixedly provided with a second connecting plate (8), the front part of the upper end of the second connecting plate (8) is fixedly connected with a motor (9), the front part of the lower end of the second connecting plate (8) is provided with, the lower part of the front end of the second fixing plate (11) is connected with a beating and crushing device (12), and the beating and crushing device (12) is positioned below the swinging and extruding device (10).
2. The unmanned aerial vehicle with high power line danger elimination of claim 1, wherein: the main structure of rotor device (3) has a fixed cylinder (31) and a first rotating rod (32), first rotating rod (32) is inserted and connected at the upper end of fixed cylinder (31), the outer surface upper portion fixedly connected with rotor (33) of first rotating rod (32), and fixed cylinder (31) fixed connection is with rotor device (3) and first fixed plate (2) fixed connection at the upper end front portion of first fixed plate (2).
3. The unmanned aerial vehicle with high power line danger elimination of claim 1, wherein: the main structure of the swing extrusion device (10) is provided with a second rotating rod (101) and a U-shaped block (102), the U-shaped block (102) is fixedly connected to the lower end of the second rotating rod (101), the middle parts of the front inner wall and the rear inner wall of the U-shaped block (102) are movably connected with a third connecting plate (103) through a rotating shaft, the lower end of the third connecting plate (103) is fixedly connected with an extrusion disc (104), the upper end of the second rotating rod (101) penetrates through the second connecting plate (8) and is fixedly connected to the output end of a motor (9) to swing the extrusion device (10) and the motor (9) and are movably connected together.
4. The unmanned aerial vehicle with high power line danger elimination of claim 1, wherein: the main structure of the rapping crushing device (12) is provided with a third rotating rod (121) and a crushing plate (122), the crushing plate (122) is fixedly arranged on the front portion of the outer surface of the third rotating rod (121), a balance plate (123) is fixedly connected to the upper portions of the left end and the right end of the crushing plate (122), a fourth connecting plate (124) is fixedly connected to the left portion and the right portion of the upper ends of the two sets of balance plates (123), and the third rotating rod (121) is inserted and connected to the lower portion of the front end of the second fixing plate (11) to rap the crushing device (12) and the second fixing plate (11) in a penetrating mode.
5. The unmanned aerial vehicle with high power line danger elimination of claim 1, wherein: the right part of the first connecting plate (7) is connected with a limiting rod (13) in an inserting mode, and the lower end of the limiting rod (13) is fixedly connected to the lower wall of the right U-shaped frame (4).
6. The unmanned aerial vehicle with high power line danger elimination of claim 1, wherein: the lower part of the swinging extrusion device (10) is positioned in the middle of the beating and crushing device (12).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921707246.7U CN210761311U (en) | 2019-10-12 | 2019-10-12 | Unmanned aerial vehicle for eliminating risks of high-altitude power line in electrified mode |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921707246.7U CN210761311U (en) | 2019-10-12 | 2019-10-12 | Unmanned aerial vehicle for eliminating risks of high-altitude power line in electrified mode |
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| Publication Number | Publication Date |
|---|---|
| CN210761311U true CN210761311U (en) | 2020-06-16 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921707246.7U Expired - Fee Related CN210761311U (en) | 2019-10-12 | 2019-10-12 | Unmanned aerial vehicle for eliminating risks of high-altitude power line in electrified mode |
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| Country | Link |
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| CN (1) | CN210761311U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112398070A (en) * | 2021-01-06 | 2021-02-23 | 南京家洁馨商贸有限公司 | Landslide prevention data cable protection device in mountain area |
-
2019
- 2019-10-12 CN CN201921707246.7U patent/CN210761311U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112398070A (en) * | 2021-01-06 | 2021-02-23 | 南京家洁馨商贸有限公司 | Landslide prevention data cable protection device in mountain area |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200616 Termination date: 20211012 |
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| CF01 | Termination of patent right due to non-payment of annual fee |