CN209844408U - Unmanned aerial vehicle clearance system based on electric wire netting foreign matter - Google Patents
Unmanned aerial vehicle clearance system based on electric wire netting foreign matter Download PDFInfo
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- CN209844408U CN209844408U CN201920414695.6U CN201920414695U CN209844408U CN 209844408 U CN209844408 U CN 209844408U CN 201920414695 U CN201920414695 U CN 201920414695U CN 209844408 U CN209844408 U CN 209844408U
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Abstract
The utility model discloses an unmanned aerial vehicle cleaning system based on foreign matters in an electric network, which structurally comprises an unmanned aerial vehicle device, a ground control station, a self-checking device, an alarm module, a flaming device, a shearing device, an infrared recognition device and a protective device, the utility model discloses an unmanned aerial vehicle cleaning system based on foreign matters in an electric network, the design provides the design of the flaming device, the shearing device and the infrared recognition device, solves the problems that some foreign matters are easy to cause atmospheric pollution and are not suitable for wide-range popularization due to the adoption of a combustion mode, the infrared recognition device is used for recognizing the foreign matters on the cable, when the foreign matters are in a belt shape or are easy to be cleaned through shearing operation, the shearing device is preferably used for cleaning, when the recognized foreign matters are wound on the cable, the foreign matters are cleaned through the flaming device, and the aim of cleaning the foreign matters under the electrified state is achieved, safe operation, high efficiency and the beneficial effect of effectively reducing the pollution to the environment.
Description
Technical Field
The utility model relates to a power grid maintenance equipment technical field, concretely relates to unmanned aerial vehicle clearance system based on electric wire netting foreign matter.
Background
The power transmission line runs in a natural environment for a long time, foreign matters such as plastic of an agricultural greenhouse, a sunshade net, a woven belt, advertising cloth for advertisement, kites, kite pull ropes and the like are easy to be wound on the power transmission line due to wind blowing, and the like, the foreign matters are poor in insulating property after being drenched or affected by damp, accidents such as tripping and short circuit of the power transmission line are easy to happen, and power supply safety of a power grid is seriously affected, the traditional method for removing the foreign matters of the power transmission line is that an operator hangs a flying vehicle on a power transmission line on the premise that the power of the line is cut off, then the operator sits on the flying vehicle and moves to the foreign matters to take off the foreign matters, power supply is affected, the operator on a pole wastes time and has danger, along with the rapid development of the unmanned aerial vehicle technology, fire is sprayed by a remote control unmanned vehicle device at present, the foreign matters wound on the cable are burnt, and therefore, the unmanned aerial vehicle removing system, however, in the prior art, some foreign matters adopt a combustion mode, so that the air pollution is easily caused, the popularization is not suitable in a large range, and the unmanned aerial vehicle easily causes wing damage when colliding with hard objects and cannot fly.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
In order to overcome the prior art not enough, the unmanned aerial vehicle clearance system based on electric wire netting foreign matter has now been proposed, some foreign matters have been solved and have been adopted the mode of burning, easily cause the atmosphere pollution, the unsuitable problem of promoting on a large scale, unmanned aerial vehicle hits hard thing and easily causes the wing to damage, the problem that can't fly has been reached and can be realized cleaing away the foreign matter under the electrified state, the operation is safe, and efficient, can effectively reduce the pollution to the environment, and effectively prevent that the wing from directly hitting the beneficial effect that the foreign matter caused the damage.
(II) technical scheme
The utility model discloses a following technical scheme realizes: the utility model provides an unmanned aerial vehicle clearance system based on electric wire netting foreign matter, including unmanned aerial vehicle device, ground control station, self-checking device, alarm module, flaming device, shearing mechanism, infrared recognition device and protector, ground control station and unmanned aerial vehicle device alternate segregation, flaming device top right side and unmanned aerial vehicle device bottom rotation portion right side fixed connection, shearing mechanism top right side and unmanned aerial vehicle device bottom rotation portion left side fixed connection, flaming device and shearing mechanism position symmetry each other, infrared recognition device sets up the right-hand member in unmanned aerial vehicle device inside, self-checking device bottom and unmanned aerial vehicle device inside bottom rear side fixed connection, alarm module sets up at the self-checking device right-hand member and with the unmanned aerial vehicle device inside bottom fixed connection, protector sets up in unmanned aerial vehicle device top, unmanned aerial vehicle device comprises driving motor, visual image acquisition equipment, visual image transmission equipment, main control unit and machine carries the tracker, driving motor sets up at unmanned aerial vehicle device outside wing lower extreme, visual image acquisition equipment bottom and unmanned aerial vehicle device rotation portion outside right-hand member, visual image transmission equipment sets up at visual image acquisition equipment left end and with the inside bottom fixed connection of unmanned aerial vehicle device, main control unit bottom and the inside bottom middle part fixed connection of unmanned aerial vehicle device, machine carries the tracker setting in unmanned aerial vehicle device bottom left side, infrared identification equipment comprises infrared identification equipment and clearance selection equipment, infrared identification equipment sets up in visual image acquisition equipment upper end, clear away the selection equipment setting at infrared identification equipment left end, protector is by support column, urceolus, bracing piece, The device comprises a buffer spring, a support ring and a buffer ring, wherein the bottom end of the support column is fixedly connected with the middle part of the top end of the unmanned aerial vehicle device, the left end of the outer cylinder is fixedly connected with the upper side of the right end of the support column, the left end of the support rod is slidably connected with the right end of the inner side of the outer cylinder, the left end of the buffer spring is fixedly connected with the left end of the inner side of the outer cylinder, the right end of the buffer spring is fixedly connected with the left end of the support rod, the right end of the support rod is fixedly connected with the inner side of the support ring, the inner side of the buffer ring is fixedly connected with the inner part of the support ring, the flaming device, the shearing device, the clearing and selecting device, the airborne tracker, the self-checking device, the alarm module, the driving motor, the visual image acquisition device, the flaming device and the shearing device are both electrically connected with the clearing selection equipment, and the self-checking device is electrically connected with the alarm module.
Further, the infrared identification equipment can clearly distinguish heating faults at a distance of 10m, the resolution is not lower than 640 multiplied by 480, and the thermal sensitivity is not lower than 50 mk; the temperature measurement precision is not lower than 2k, the temperature measurement range is-20 ℃ to +150 ℃, and the infrared identification equipment has an automatic focusing function.
Furthermore, the visual image acquisition equipment is a visible light sensor camera, and meets the requirement of clearly distinguishing the pin-level target at a distance of not less than 10m, the effective pixels are not less than 1200 thousands, the remote control zooming function is realized, the continuous adjustment is realized, and the automatic focusing function is realized.
Further, the self-inspection apparatus at least includes: flight control module, battery voltage, motor, and telemetry signals.
Further, the unmanned aerial vehicle device is an eight-rotor unmanned aerial vehicle.
Further, the diameter of the outermost side of the protection device is smaller than the total length of the flaming device and the shearing device.
Furthermore, a supporting structure is formed by the outer cylinder, the supporting rods and the buffer springs, four groups of supporting structures are arranged, and the supporting structures are arranged between the supporting columns and the supporting rings at equal intervals.
Further, the model of the visual image acquisition equipment is LLKP-01.
Further, the type of the driving motor is 5008.
Further, the visual image transmission device model is 13SG-HDS 1000A.
Further, the onboard tracker is of a type GT 21.
(III) advantageous effects
Compared with the prior art, the utility model, following beneficial effect has:
1) in order to solve the problems that some foreign matters are easy to cause air pollution and are not suitable for large-scale popularization due to the adoption of a combustion mode, the design provides the design of the flaming device, the shearing device and the infrared recognition device, the problems that some foreign matters are easy to cause air pollution and are not suitable for large-scale popularization due to the adoption of the combustion mode are solved, the foreign matters on the cable are recognized through the infrared recognition device, when the foreign matter is in a band shape or easily removed by a cutting operation, it is preferably removed by using a cutting device, and when the recognized foreign matter is wound around the cable, it is removed by using a flaming device, thereby combine shearing mechanism and flaming device two kinds of modes to carry out the most suitable selection of cleaing away to the foreign matter on the cable, reach and to realize cleaing away the foreign matter under the electrified state, the operation is safe, and efficient, can effectively reduce the beneficial effect to the pollution of environment.
2) The utility model discloses a unmanned aerial vehicle, including unmanned aerial vehicle, supporting rod, buffer ring, the utility model discloses a protection device design is proposed in this design, it easily causes the wing to damage to have solved unmanned aerial vehicle and hit hard thing, the problem of unable flight, the buffering circle on the supporting rod is at first can touch to the foreign object, the buffering circle has elasticity, the impact force that receives can be tentatively reduced, and can the wing that the unmanned aerial vehicle device was touched to the foreign object directness, in the bracing piece indentation urceolus simultaneously, buffer spring in the urceolus flicks, further carry out the shock attenuation buffering, so protect, reach and effectively prevent that the wing direct impact from causing the beneficial effect of damage to the foreign object.
Drawings
Other features, objects and advantages of the invention will become more apparent upon reading of the detailed description of non-limiting embodiments with reference to the following drawings:
fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a block diagram of the present invention;
fig. 3 is a schematic view of the interior overlooking structure of the unmanned aerial vehicle device body of the present invention;
fig. 4 is a schematic view of the interior of the protection device according to the present invention;
in the figure: the device comprises an unmanned aerial vehicle device-1, a ground control station-2, a flaming device-3, a shearing device-4, an infrared recognition device-5, a self-checking device-6, an alarm module-7, a protective device-8, a driving motor-11, a visual image acquisition device-12, a visual image transmission device-13, a main controller-14, an infrared recognition device-51, a clearing selection device-52, an airborne tracker-15, a support column-81, an outer cylinder-82, a support rod-83, a buffer spring-84, a support ring-85 and a buffer ring-86.
Detailed Description
In the technical scheme:
flaming device 3, shearing mechanism 4, infrared recognition device 5, protector 8, infrared identification equipment 51, clear away selection equipment 52, support column 81, urceolus 82, bracing piece 83, buffer spring 84, lock ring 85, buffer ring 86 do the utility model discloses contain the essential innovative component.
Unmanned aerial vehicle device 1, ground control station 2, self-checking device 6, alarm module 7, driving motor 11, visual image acquisition equipment 12, visual image transmission equipment 13, main control unit 14, machine carry tracker 15 and be the realization the utility model discloses the necessary connectivity component of technical scheme.
In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
Referring to fig. 1, fig. 2, fig. 3 and fig. 4, the utility model provides an unmanned aerial vehicle clearance system based on electric wire netting foreign matter: the automatic fire-extinguishing device comprises an unmanned aerial vehicle device 1, a ground control station 2, a self-checking device 6, an alarm module 7, a fire-spraying device 3, a shearing device 4, an infrared recognition device 5 and a protection device 8, wherein the ground control station 2 is separated from the unmanned aerial vehicle device 1, the right side of the top end of the fire-spraying device 3 is fixedly connected with the right side of the bottom rotating part of the unmanned aerial vehicle device 1, the right side of the top end of the shearing device 4 is fixedly connected with the left side of the bottom rotating part of the unmanned aerial vehicle device 1, the fire-spraying device 3 is symmetrical to the shearing device 4 in position, the infrared recognition device 5 is arranged at the right end inside the unmanned aerial vehicle device 1, the bottom end of the self-checking device 6 is fixedly connected with the rear side of the bottom inside the unmanned aerial vehicle device 1, the alarm module 7 is arranged at the right end of the self-checking device 6 and is fixedly connected with, The visual image transmission device 13, the main controller 14 and the airborne tracker 15, the driving motor 11 is arranged at the lower end of the outer wing of the unmanned aerial vehicle device 1, the bottom end of the visual image acquisition device 12 is fixedly connected with the outer right end of the rotating part of the unmanned aerial vehicle device 1, the visual image transmission device 13 is arranged at the left end of the visual image acquisition device 12 and is fixedly connected with the inner bottom end of the unmanned aerial vehicle device 1, the bottom end of the main controller 14 is fixedly connected with the middle part of the inner bottom end of the unmanned aerial vehicle device 1, the airborne tracker 15 is arranged at the left side of the bottom end of the unmanned aerial vehicle device 1, the infrared recognition device 5 comprises an infrared recognition device 51 and a clearing selection device 52, the infrared recognition device 51 is arranged at the upper end of the visual image acquisition device 12, the clearing selection device 52 is arranged at the left end of the infrared recognition device 51, the protection device 8 comprises, the bottom end of a supporting column 81 is fixedly connected with the middle part of the top end of the unmanned aerial vehicle device 1, the left end of an outer cylinder 82 is fixedly connected with the upper side of the right end of the supporting column 81, the left end of a supporting rod 83 is slidably connected with the right end of the inner side of the outer cylinder 82, the left end of a buffer spring 84 is fixedly connected with the left end of the inner side of the outer cylinder 82, the right end of the buffer spring 84 is fixedly connected with the left end of the supporting rod 83, the right end of the supporting rod 83 is fixedly connected with the inner side of a supporting ring 85, the inner side of the buffer ring 86 is fixedly connected with the inner part of the supporting ring 85, a flaming device 3, a shearing device 4, a clearing and selecting device 52, an onboard tracker 15, a self-checking device 6, an alarm module 7, a driving motor 11, a visual image acquisition device 12 and a visual image transmission, the flaming device 3 and the shearing device 4 are both electrically connected with the clearing selection equipment 52, and the self-checking device 6 is electrically connected with the alarm module 7.
Wherein, the infrared recognition device 51 can clearly distinguish the heating fault at a distance of 10m, the resolution is not lower than 640 multiplied by 480, and the thermal sensitivity is not lower than 50 mk; the temperature measurement precision is not lower than 2k, the temperature measurement range is-20 ℃ to +150 ℃, and the infrared identification device 51 has an automatic focusing function and can effectively judge whether foreign matters exist on the induction network and whether the induction network works.
The visual image acquisition equipment 12 is a visible light sensor camera, meets the requirement of clearly distinguishing a pin-level target at a distance of not less than 10m, has an effective pixel of not less than 1200 ten thousand, has a remote control zooming function, is continuously adjustable, has an automatic focusing function, can effectively observe foreign matters on a cable, and is convenient for workers to recognize.
Wherein, the self-test device 6 at least comprises: the flight control module, the battery voltage, the motor and the remote control and remote measurement signals are conveniently connected with the alarm module, when any one of the flight control module, the battery voltage, the motor and the remote control and remote measurement signals breaks down, the alarm module can perform sound (light) alarm prompting at the ground control station, and the system is locked and cannot be released.
Wherein, unmanned aerial vehicle device 1 is eight rotor unmanned aerial vehicle, and flight stability is good, and the precision of hovering is high.
The diameter of the outermost side of the protective device 8 is smaller than the total length of the flaming device 3 and the shearing device 4, so that the wings of the unmanned aerial vehicle device 1 can be effectively protected, and the operation of the flaming device 3 and the shearing device 4 is not hindered.
Wherein, a bearing structure is formed by the outer cylinder 82, the support rods 83 and the buffer springs 84, and four groups of the bearing structure are arranged, and the equal distances are arranged between the support columns 81 and the support rings 85, so that a supporting function can be effectively played, and a damping function can be played.
The model of the visual image acquisition equipment 12 is LLKP-01, the image is clear, and the energy consumption is low.
The type of the driving motor 11 is 5008, the rotating speed is high, the noise is low, and the size is small.
The model of the visual image transmission device 13 is 13SG-HDS1000A, the signal is stable, and the transmission speed is high.
The model of the airborne tracker 15 is GT21, the information transmission is fast, and the positioning is accurate.
The material of the buffer ring 86 is polystyrene foam plastic, the polystyrene foam plastic is prepared by taking polystyrene resin as a main body and adding additives such as foaming agent and the like, the buffer ring is the most used buffer material at present, and the buffer ring has a closed-cell structure, small water absorption and excellent water resistance; the density is small, generally 0.015-0.03; the mechanical strength is good, the buffering performance is excellent, the processability is good, and the molding forming is easy; good colorability, strong temperature adaptability, excellent radiation resistance and the like, but can emit styrene gas which pollutes the environment when in combustion.
The working principle is as follows: at first unmanned aerial vehicle device 1 is eight rotor unmanned aerial vehicle, and driving motor 11's number is no less than 4, its aim at, eight rotor unmanned aerial vehicle flight stability is good, the precision of hovering is high, can realize better that the foreign matter clears away, this unmanned aerial vehicle device 1 bottom is equipped with rotates the rotation portion of being connected with unmanned aerial vehicle device 1 bottom, rotation portion is controlled by main control ware 14, rotation portion can rotate relative unmanned aerial vehicle device 1 after certain angle around the specified direction and lock, there are two kinds of circumstances about rotation portion: firstly, the method comprises the following steps: the flaming devices 3 and the shearing devices 4 are symmetrically arranged on the rotating portion in the horizontal direction respectively, the visual image acquisition equipment 12 and the infrared recognition equipment 51 are fixedly arranged on the unmanned aerial vehicle device 1, foreign matters on cables are observed and recognized by the visual image acquisition equipment 12 and the infrared recognition equipment 51, and when the cleaning selection equipment 52 selects the shearing devices 4 or the flaming devices 3 to clean the foreign matters, the main controller 14 controls the rotating portion to rotate, so that the selected shearing devices 4 or the flaming devices 3 rotate to the foreign matters, and the foreign matters are sheared or burnt; secondly, the method comprises the following steps: the visual image acquisition equipment 12 and the infrared recognition equipment 51 are arranged on the rotating part, the flaming device 3 and the shearing device 4 are respectively and symmetrically arranged at the bottom of the unmanned aerial vehicle device 1 along the horizontal direction, when the visual image acquisition equipment 12 and the infrared recognition equipment 51 observe foreign matters on a power grid, the main controller 14 controls the unmanned aerial vehicle device 1 to rotate relative to the rotating part, so that the shearing device 4 or the flaming device 3 selected by the removal selection equipment 52 rotates to the foreign matters, and the foreign matters are removed; it should be noted that, in this embodiment, the shearing apparatus 4 and the flaming device 3 are prior art, and refer to the disclosed structures of chinese patent CN201621353050.9, and the like, and therefore no description is given herein, the detachable airborne tracker 15 is further fixedly disposed on the unmanned aerial vehicle apparatus 1, and the airborne tracker 15 is connected with the main controller 14 of the unmanned aerial vehicle apparatus 1, when an accident occurs, the airborne tracker 15 can automatically send position information to the ground control station 2, thereby avoiding that the signal of the unmanned aerial vehicle apparatus 1 is lost during the fault, and the unmanned aerial vehicle cleaning system further includes the self-checking apparatus 6 and the alarm module 7, and the self-checking apparatus 6 at least includes: the system comprises a flight control module, a battery voltage, a motor and a remote control and remote measurement signal; when any one of the components of the flight control module, the battery voltage, the motor and the remote control and remote measurement signals is in fault, the alarm module 7 can perform sound (light) alarm prompt on the ground control station 2, the system is locked and cannot be released, and it needs to be explained that the alarm prompt comprises position information of the fault, so that the fault position can be conveniently and quickly found out, the unmanned aerial vehicle device 1 also supports one-key return, no matter what flight state the unmanned aerial vehicle device 1 is in, as long as an operator starts the one-key return function through a specific function key (button) on the ground control station 2 or a remote control handle, the unmanned aerial vehicle cleaning system should stop the current task and return according to a preset strategy; the unmanned aerial vehicle cleaning system has an automatic return function after losing link signals, no matter what flight state the unmanned aerial vehicle cleaning system is in, as long as the remote-measuring remote-control signals are interrupted, the unmanned aerial vehicle cleaning system should return according to a preset strategy, the protective device 8 is arranged on the unmanned aerial vehicle device 1, when the unmanned aerial vehicle cleaning system touches foreign objects, the buffer ring 86 on the support ring 85 is touched at first, the buffer ring 86 has elasticity, the received impact force can be reduced preliminarily, the foreign objects can directly touch the wings of the unmanned aerial vehicle device 1, meanwhile, the support rod 83 is retracted into the outer barrel 82, the buffer spring 84 in the outer barrel 82 flicks to further perform damping and buffering, and the protection is performed in such a way, the design provides the design of the flame spraying device 3, the shearing device 4 and the infrared recognition device 5, the problem that some foreign objects adopt a combustion mode is solved, the atmosphere pollution is easily caused, and the unmanned aerial vehicle cleaning, the infrared recognition device 5 is used for recognizing the foreign matters on the cable, when the foreign matters are in a belt shape or are easy to be removed through shearing operation, the shearing device 4 is preferably used for removing, when the recognized foreign matters are wound on the cable, the flaming device 3 is used for removing, so that the foreign matters on the cable are most properly removed and selected by combining the two modes of the shearing device 4 and the flaming device 3, the beneficial effects that the foreign matters can be removed under a charged state, the operation is safe, the efficiency is high, and the pollution to the environment can be effectively reduced are achieved, the design provides the design of the protection device 8, the problems that the wings of the unmanned aerial vehicle are easy to damage and cannot fly when the unmanned aerial vehicle collides with hard objects are solved, the foreign objects firstly touch the buffer ring 86 on the support ring 85, the buffer ring 86 has elasticity, the received impact force can be reduced, and the foreign objects can directly touch the primary wings of the unmanned aerial vehicle device 1, meanwhile, the supporting rod 83 retracts into the outer cylinder 82, the buffer spring 84 in the outer cylinder 82 bounces, and further shock absorption and buffering are carried out, so that protection is carried out, and the beneficial effect that the wings are effectively prevented from directly impacting foreign objects to cause damage is achieved.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above, it will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, but that the invention may be embodied in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (7)
1. The utility model provides an unmanned aerial vehicle clearance system based on electric wire netting foreign matter, includes unmanned aerial vehicle device (1), ground control station (2), self-checking device (6) and alarm module (7), its characterized in that: the ground control station is characterized by further comprising a flaming device (3), a shearing device (4), an infrared recognition device (5) and a protection device (8), wherein the ground control station (2) is separated from the unmanned aerial vehicle device (1), the right side of the top end of the flaming device (3) is fixedly connected with the right side of the bottom rotating part of the unmanned aerial vehicle device (1), the right side of the top end of the shearing device (4) is fixedly connected with the left side of the bottom rotating part of the unmanned aerial vehicle device (1), the flaming device (3) is symmetrical to the shearing device (4) in position, the infrared recognition device (5) is arranged at the right end inside the unmanned aerial vehicle device (1), the bottom end of the self-checking device (6) is fixedly connected with the rear side of the bottom inside the unmanned aerial vehicle device (1), an alarm module (7) is arranged at the right end of the self-checking device (6) and is fixedly connected with the bottom inside the unmanned aerial vehicle device (1), the protection device, the unmanned aerial vehicle device (1) consists of a driving motor (11), a visual image acquisition device (12), a visual image transmission device (13), a main controller (14) and an airborne tracker (15), wherein the driving motor (11) is arranged at the lower end of an outer wing of the unmanned aerial vehicle device (1), the bottom end of the visual image acquisition device (12) is fixedly connected with the right end of the outer side of a rotating part of the unmanned aerial vehicle device (1), the visual image transmission device (13) is arranged at the left end of the visual image acquisition device (12) and is fixedly connected with the inner bottom end of the unmanned aerial vehicle device (1), the bottom end of the main controller (14) is fixedly connected with the middle part of the inner bottom end of the unmanned aerial vehicle device (1), the airborne tracker (15) is arranged at the left side of the bottom end of the unmanned aerial vehicle device (1), and the infrared recognition device (5) consists of an infrared recognition device (51) and a clearing selection, the infrared recognition equipment (51) is arranged at the upper end of the visual image acquisition equipment (12), the clearing and selecting equipment (52) is arranged at the left end of the infrared recognition equipment (51), the protection device (8) consists of a support column (81), an outer barrel (82), a support rod (83), a buffer spring (84), a support ring (85) and a buffer ring (86), the bottom end of the support column (81) is fixedly connected with the middle part of the top end of the unmanned aerial vehicle device (1), the left end of the outer barrel (82) is fixedly connected with the upper side of the right end of the support column (81), the left end of the support rod (83) is slidably connected with the right end of the inner side of the outer barrel (82), the left end of the buffer spring (84) is fixedly connected with the left end of the inner barrel (82), the right end of the buffer spring (84) is fixedly connected with the left end of the support rod (83), and the right, buffer ring (86) inboard and the inside fixed connection of lock ring (85), flame projecting device (3), shearing mechanism (4), clear away selection equipment (52), machine carry tracker (15), self-checking device (6), alarm module (7), driving motor (11), visual image collection equipment (12), visual image transmission equipment (13) all are connected with main control unit (14) electricity, visual image transmission equipment (13) and main control unit (14) all with ground control station (2) wireless connection, visual image collection equipment (12) are connected with visual image transmission equipment (13) electricity, flame projecting device (3) and shearing mechanism (4) all with clear away selection equipment (52) electricity and be connected self-checking device (6) and alarm module (7) electricity.
2. The power grid foreign matter based unmanned aerial vehicle cleaning system of claim 1, wherein: the infrared identification equipment (51) can clearly distinguish heating faults at a distance of 10m, the resolution is not lower than 640 multiplied by 480, and the thermal sensitivity is not lower than 50 mk; the temperature measurement precision is not lower than 2k, the temperature measurement range is-20 ℃ to +150 ℃, and the infrared identification equipment (51) has an automatic focusing function.
3. The power grid foreign matter based unmanned aerial vehicle cleaning system of claim 1, wherein: the visual image acquisition equipment (12) is a visible light sensor camera, the requirement of clearly distinguishing a pin-level target at a distance of not less than 10m is met, effective pixels are not less than 1200 thousands, the remote control zoom function is realized, the continuous adjustment is realized, and the automatic focusing function is realized.
4. The power grid foreign matter based unmanned aerial vehicle cleaning system of claim 1, wherein: the self-test device (6) comprises at least: flight control module, battery voltage, motor, and telemetry signals.
5. The power grid foreign matter based unmanned aerial vehicle cleaning system of claim 1, wherein: unmanned aerial vehicle device (1) is eight rotor unmanned aerial vehicle.
6. The power grid foreign matter based unmanned aerial vehicle cleaning system of claim 1, wherein: the diameter of the outermost side of the protective device (8) is smaller than the total length of the flaming device (3) and the shearing device (4).
7. The power grid foreign matter based unmanned aerial vehicle cleaning system of claim 1, wherein: the outer cylinder (82), the support rods (83) and the buffer springs (84) form a support structure, four groups of support structures are arranged, and the support structures are arranged between the support columns (81) and the support rings (85) at equal intervals.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920414695.6U CN209844408U (en) | 2019-03-29 | 2019-03-29 | Unmanned aerial vehicle clearance system based on electric wire netting foreign matter |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201920414695.6U CN209844408U (en) | 2019-03-29 | 2019-03-29 | Unmanned aerial vehicle clearance system based on electric wire netting foreign matter |
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| CN209844408U true CN209844408U (en) | 2019-12-24 |
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| CN201920414695.6U Expired - Fee Related CN209844408U (en) | 2019-03-29 | 2019-03-29 | Unmanned aerial vehicle clearance system based on electric wire netting foreign matter |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113178813A (en) * | 2021-04-25 | 2021-07-27 | 温州市森脉电力设备有限公司 | High-altitude power supply line maintenance method |
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2019
- 2019-03-29 CN CN201920414695.6U patent/CN209844408U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113178813A (en) * | 2021-04-25 | 2021-07-27 | 温州市森脉电力设备有限公司 | High-altitude power supply line maintenance method |
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Granted publication date: 20191224 Termination date: 20200329 |