CN202815124U - Insulator detecting device by using multi-rotor unmanned aerial vehicle - Google Patents
Insulator detecting device by using multi-rotor unmanned aerial vehicle Download PDFInfo
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Abstract
The utility model relates to an insulator detecting device by using a multi-rotor unmanned aerial vehicle. The device comprises a multi-rotor unmanned aerial vehicle, wherein a flight control system airborne computer thereon is connected with a positioning device, an unmanned aerial vehicle steering engine controller, a height measuring device, a speed measuring device, a high-definition camera, an unmanned aerial vehicle PCM remote-controlled receiver, an airborne wireless communication unit and a lifting device; the lifting device drives a detecting lower electrode to move, and the airborne wireless communication unit communicates with a ground station; and the unmanned aerial vehicle steering engine controller controls a servo steering engine, the servo steering engine controls a multi-rotor module, a detecting upper electrode and the detecting lower electrode are respectively connected with respective voltage sensor, and the two voltage sensors are connected with an A/D conversion unit, a DSP processing unit, and the flight control system airborne computer. The insulator detecting device can know and master the running conditions of the line insulators timely, can avoid the danger that is caused when the detecting personnel climb to carry out short-distance live operation, and can improve the detection efficiency.
Description
Technical field
The utility model relates to a kind of unmanned plane and detects insulator arrangement, and particularly a kind of many rotor wing unmanned aerial vehicles detect insulator arrangement.
Background technology
In recent years, the sustained and rapid development of Chinese national economy has proposed more and more higher requirement to China's power industry.China formed at present North China, northeast, East China, Central China, northwest and south electric network totally 6 distinguish electrical network transprovincially, 500 KVs become the skeleton of each large power system and transprovincially, trans-regional interconnection, the contradiction that power network development lags behind is eased substantially.Because China territory is vast, with a varied topography, for safety and reliably power supply, line walking safeguards that robotization and modernization demonstrate its urgency day by day.
Insulator is the insulator of supporting conductor, and insulator can guarantee that the electrified bodys such as cross-arm, shaft tower and bus have enough insulation.It is in operation needs to bear the loading of wire vertical direction and the pulling force of horizontal direction, the corrosion of climate change and the chemical substance such as also need stand Exposure to Sunlight, drench with rain.Therefore, insulator should have good electric property, and enough physical strengths are arranged again.All be unable to do without the use of insulator in the processes such as generating, power transformation, transmission of electricity, the quality of Insulators Used plays vital effect to the safe operation of electrical network.Insulator can be divided into support insulator, suspended insulator and bushing insulator etc. by structure, presses the dielectric substance classification, and porcelain, glass, composite organic insulator three types are arranged.Long-term in service, the impact of the environmental factors such as insulator can be struck by lightning, filth, bird pest, ice and snow, high humidity, the temperature difference; The effect that will bear highfield, lightning impulse current, power frequency arc electric current on electric; Mechanically to bear the effect of the mechanical forces such as long-term work load, comprehensive load, conductor galloping, these factors are progressive processes to the destruction of Insulators Used, therefore need to check the aerial Insulators Used of height in the situation of the normal operation of power circuit.
At present the detection method of insulator mainly contained direct observational method, ultraviolet imagery method, infrared imaging method, ultrasonic Detection Method, the equivalent salt density method, potential measurement method, electric-resistivity method, electric field method, leakage current method and pulse current method.The direct observational method error is larger, and can't detect the interior insulating property of insulator; The ultraviolet imagery method can only be used when shelf depreciation occurs, and influenced by environmental temperature; Infrared imaging method lacks effectively detection to early stage insulation defect, and detection and location are inaccurate, are subject to simultaneously the impact of environment temperature; Ultrasonic Detection Method is not suitable for Site Detection because of its coupling and decay and ultrasonic transducer performance issue; Equivalent salt density method elapsed time is long, and the conclusion that draws only is the whole filthy average level of insulator, can not truly reflect the insulating property of insulator; Electric-resistivity method is only applicable to low-voltage circuit; Electric field method is not high on the insulation harm sensitivity that some does not affect Electric Field Distribution, restricted application; The leakage current method need to be installed corresponding equipment at every insulator string string, and is subjected to a lot of other factor affecting, and data accuracy is limited; The detection resolution of pulse current method depends on resistance, position, the sheet number of insulator chain and the parameters such as corona inception voltage of normal insulation of poor insulator in string of poor insulator, and the method is full maturity not, is all doing further exploration both at home and abroad at present.The potential measurement method is very simple a kind of detection method, and its ultimate principle is namely by detecting electric potential difference between the insulator two ends, compares with the regularity of each voltage distribution of insulator on the insulator chain, can judge whether insulator dielectric is good.The method is simple to operation and the data accuracy rate high, and application is more extensive in the quite a long period in the past, but because it needs the testing staff to climb and carries out the close-range electrified operation, danger is higher and efficient is low.
Therefore, can seek a kind of method, can either utilize the simple and reliable property of potential measurement method, can avoid again needing the testing staff to climb and carry out the danger that close-range electrified operates, improve simultaneously detection efficiency.Along with utilizing reaching its maturity of unmanned plane line walking technology, consider the efficient means of utilizing this safety and stability of unmanned plane, carry out detection for insulator in conjunction with the potential measurement method.
The equipment of existing multiple on-line monitoring insulator, be 01102273.6 " high-voltage transmission line insulator live intelligent detector apparatus " such as the patent No., the patent No. be 92242814.X's " suspending insulator detector " etc., this type of patent has obtained certain beneficial effect, but still existent defect is as follows:
This kind equipment is irremovable monitoring equipment, namely need to install for each insulator chain or insulator sheet, perhaps still utilize the testing staff to carry this equipment and climb and carry out close-range electrified operation, workload is huge, and can not solve personal security and efficiency fully.
The existing robot that utilizes carries out the technology that insulator detects, and is 200810230387.4 " a kind of insulator detecting robot " such as the patent No., and this patent has obtained certain beneficial effect, but still existent defect is as follows:
(1) this robot still needs manually to be transported to the enterprising enforcement usefulness of shaft tower by ground, can't avoid the operation of personnel's close-range electrified fully;
(2) this robot does not possess the function of crossing pole or circuit item spacing walking, namely can only patrol and examine the insulator chain of S.C. single-pole tower junction at every turn, if want the insulator chain of patrolling different conductor or different shaft towers junction, still need manually carry out position movement.
The existing unmanned plane that utilizes carries out the technology that insulator detects, be 200810224172.1 " a kind of flying robot for detection of electric transmission line isolator " such as the patent No., and the patent No. is 201020138974.3 " novel detection device of Insulators Used ", these two patents have obtained certain beneficial effect, but still existent defect is as follows:
(1) system that described in the patent " a kind of flying robot for detection of electric transmission line isolator " insulator is detected is target identification system, only adopt visual manner to judge from the insulator outward appearance whether it is normal, it is low that the method detects accuracy, can't detect outward appearance without the defective of significant change;
(2) insulator detector does not load apparatus capable of fluctuating described in the patent " novel detection device of Insulators Used ", the two detection probe spacings that are insulator detector are a fixed value, the insulator that is not practicable for multiple spacing detects restricted application;
(3) equal not mentioned command set that flicks that detects behind the reliable signal in above-mentioned two patents, because many rotor wing unmanned aerial vehicles are when carrying out the insulator detection, be generally and do not hinder the circuit normal power supply, mostly be the band electro-detection, unmanned plane should reduce closely and even detection time of connect insulator as far as possible, detects security to improve.
The utility model content
The purpose of this utility model is exactly for addressing the above problem, provide a kind of many rotor wing unmanned aerial vehicles to detect insulator arrangement, it mainly utilizes the efficient means of this safety and stability of many rotor wing unmanned aerial vehicles, by measuring method realization that insulator two ends electromotive force compares with normal value to the detection of insulator state.Utilize this apparatus and method, not only can be used as a kind of monitoring means, in time understand and grasp the ruuning situation of line insulator, whether have potential safety hazard, for effective decision-making provides foundation; Can also avoid the testing staff to climb and carry out the danger that close-range electrified operates, improve simultaneously detection efficiency.The security of transmission line of electricity and unmanned plane patrolled and examined to utilize the extension of scope to have a great deal of practical meanings.
For achieving the above object, the utility model adopts following technical scheme:
A kind of many rotor wing unmanned aerial vehicles detect insulator arrangement, it comprises rotor wing unmanned aerial vehicle more than, be provided with the flight control system airborne control computer at many rotor wing unmanned aerial vehicles, the flight control system airborne control computer is connected with locating device, steering engine for unmanned plane controller, height measuring device, velocity measuring device, unmanned plane PCM remote-control receiver and airborne wireless communication unit, and the airborne wireless communication unit is communicated by letter with land station; Steering engine for unmanned plane controller control Servo-controller, Servo-controller is then controlled many rotor module of many rotor wing unmanned aerial vehicles, and described flight control system airborne control computer is connected with high-definition camera; In the detection utmost point be connected down the utmost point and be connected with separately voltage sensor respectively, two voltage sensors all are connected with the A/D conversion unit, the A/D conversion unit is connected with the DSP processing unit, the DSP processing unit is connected with the flight control system airborne control computer; The flight control system airborne control computer also is connected with jacking gear simultaneously, and Ghandler motion was moving under jacking gear drove and surveys.
Described locating device comprises unmanned plane satellite positioning module, unmanned plane digital compass and unmanned plane three-axis gyroscope, unmanned plane three axis accelerometer, and they all are connected with the flight control system airborne control computer.
Described jacking gear comprises a lifting unit, and it is moving that lifting unit drives the lower Ghandler motion of detection by lifting structure.It is lifting device structure described in 200580010899.4 that this lifting structure adopts number of patent application.
Described land station comprises land station's information handling system, and it is communicated by letter with the airborne wireless communication unit by land station's radio communication unit.
A kind of detection method that adopts many rotor wing unmanned aerial vehicles to detect insulator arrangement, step is:
Step 1: in the flight control system airborne control computer, arrange and flick the performed circuit of order and distance;
Step 2: the typical curve that in land station's information handling system, sets the insulator electric potential difference;
Step 3: choose many rotor wing unmanned aerial vehicles place of taking off, and flying height is set;
Step 4: after lift-launch insulator pick-up unit takes off on many rotor wing unmanned aerial vehicles, slowly regulate in real time the position of hovering according to high-definition image, finally guarantee to survey the upper and lower utmost point and touch respectively up and down two ends of insulator, then by voltage sensor, A/D conversion unit, DSP processing unit measured data are inputted the flight control system airborne control computer;
Step 5: after the flight control system airborne control computer obtains electric potential difference data, to flick immediately order and export to the steering engine for unmanned plane controller, and then by steering engine for unmanned plane controller control Servo-controller, command many rotor module actions, many rotor wing unmanned aerial vehicles will be according to the route of a kind of setting of step with apart from speeding away detected insulator;
Step 6: repeating step four, five, extremely all insulators detect complete on the whole insulator chain;
Step 7: after the insulator chain detection is complete, namely generate the insulator numbering report of doubtful non-normal working in land station's information process unit, this is numbered according to GPS, height and detects the insulator particular location that order information is judged.
In the described step 1, the described circuit that flicks command execution and distance need to arrange according to the direction of whole insulator chain with relative position, the distance of shaft tower, wire, when avoiding carrying out this order and the collision of insulator chain, tower and conductor.
In the described step 2, typical curve exchanges the spread voltage setting of aerial power transmission line insulator chain with reference to power industry standard DL/T 487-2000 330kV and 500kV; Because insulator chain voltage respectively also can be slightly variant in varying environment, the region, also can select not arrange typical curve, only in final analysis as a result the time, potential difference values curve plotting with each insulator detection on the whole insulator chain, find the corresponding insulator of the inconsistent point of variation tendency and other each points, be doubtful non-normal working insulator.
In the described step 3, selected place and the flying height of taking off should make insulator chain be in the visual field of high-definition camera under the prerequisite that guarantees safe flight as far as possible, is convenient to the carrying out of step 4.
In the described step 4, should be from the insulator sheet of the nearlyer side of distance of wire during detection.
In institute's step 7, the doubtful non-normal working insulator numbering report that generates should be sent to line attendant, carry out on this basis the insulator emphasis and change.
Principle of work of the present utility model is:
Survey the respectively insulator two ends of contact electrification operation of upper and lower level, after the electric signal that obtains becomes voltage signal respectively by two voltage sensors, by the A/D conversion unit voltage analog signal is converted into digital signal, input DSP processing unit carries out data to be processed, and the insulator two ends potential difference values that will obtain after then will processing is inputted the flight control system airborne control computer of many rotor wing unmanned aerial vehicles.The flight control system airborne control computer is accepted the much information of many rotor wing unmanned aerial vehicles state of flight and all parts working condition simultaneously, after the GPS value of many rotor wing unmanned aerial vehicles wherein and elevation information extracted, after mating one by one with potential difference values, pass to land station by wireless transmission and carry out the data processing, judge whether the insulator and the particular location thereof that work; Simultaneously, high-definition camera also with the video that gathers by passing to land station with the flight control system airborne control computer by wireless transmission, but the state of flight of the many rotor wing unmanned aerial vehicles of the personnel of land station Real Time Monitoring, also can regulate flying height near the image operation control flight control system airborne control computer that relies on high-definition camera to pass back in real time in the process of insulator and survey the distance between the utmost point under the utmost point and the detection at many rotor wing unmanned aerial vehicles, the utmost point can be distinguished the connect insulator two ends under making the upper utmost point of detection and surveying, and records respectively potential value.After the flight control system airborne control computer receives the upper utmost point of land station's adjusting detection and surveys the signal of the distance between the lower utmost point by wireless telecommunications, send instruction to lifting unit, change the distance of surveying between the upper utmost point and the lower utmost point of detection thereby regulate lifting structure by lifting unit.In addition, the flight control system airborne control computer is after the potential difference values that obtains the input of DSP processing unit, for reduce the detection time of connect insulator as far as possible, improve and detect security, can export to one of steering engine for unmanned plane controller and flick order, and then by steering engine for unmanned plane controller control Servo-controller, command many rotor module actions, leave insulator according to predefined route rapidly.
The beneficial effects of the utility model:
1. the utility model has designed the method and apparatus that a kind of many rotor wing unmanned aerial vehicles detect insulator, utilize this system, can realize the real-time band electro-detection to insulator state, utilize this apparatus and method, not only can be used as a kind of monitoring means, in time understand and grasp the ruuning situation of line insulator, whether have potential safety hazard, for effective decision-making provides foundation; Can also avoid the testing staff to climb and carry out the danger that close-range electrified operates, improve simultaneously detection efficiency.The security of transmission line of electricity and unmanned plane patrolled and examined to utilize the extension of scope to have a great deal of practical meanings.
2. above-mentioned many rotor wing unmanned aerial vehicles detect the method and apparatus of insulator, both utilized the simple and reliable property of potential measurement method, customer service the deficiency of other insulator detection methods such as visual manner, utilized again the efficient means of this safety and stability of unmanned plane, can avoid needing the testing staff to climb and carry out the danger that close-range electrified operates, have simultaneously and control performance simple, applied widely, that needn't install on a large scale, greatly improved detection efficiency.
3. above-mentioned many rotor wing unmanned aerial vehicles detect in the device of insulator, added lifting unit, thereby pass through to regulate lifting structure by it and change the distance of surveying between the upper utmost point and the lower utmost point of detection, saved the step of before detection, measuring first the insulator spacing, the insulator that makes this device be applicable to more kinds of spacings detects, and has greatly increased usable range.
4. above-mentioned many rotor wing unmanned aerial vehicles detect in the device of insulator, have adopted to flick command set.The flight control system airborne control computer is after the potential difference values that obtains the input of DSP processing unit, for reduce the detection time of connect insulator as far as possible, improve and detect security, can export to one of steering engine for unmanned plane controller and flick order, and then by steering engine for unmanned plane controller control Servo-controller, command many rotor module actions, leave insulator according to predefined route rapidly.
Description of drawings
Fig. 1 is structure and the data flowchart that many rotor wing unmanned aerial vehicles detect insulator arrangement.
Fig. 2 is the schematic appearance that many rotor wing unmanned aerial vehicles detect insulator arrangement.
Fig. 3 is the lifting structure synoptic diagram.
Among the figure, 1 surveys the upper utmost point, and 2 survey the lower utmost point, 3 voltage sensors, 4A/D conversion unit, 5DSP processing unit, 6 flight control system airborne control computers, 7 unmanned plane satellite positioning module, 8 unmanned plane digital compass, 9 unmanned plane three-axis gyroscopes, 10 unmanned plane three axis accelerometers, 11 steering engine for unmanned plane controllers, 12 unmanned plane barometric altimeters, 13 unmanned plane rotating speed measuring sensors, 14 unmanned plane PCM remote-control receivers, 15 airborne wireless communication units, 16 Servo-controllers, rotor module more than 17,18 land station's radio communication units, 19 land station's information process units, 20 high-definition cameras, 21 lifting units, 22 lifting structures.
Embodiment
Below in conjunction with accompanying drawing and embodiment the utility model is described further.
Among Fig. 1, a kind of many rotor wing unmanned aerial vehicles detect the device of insulator, it comprises many rotor wing unmanned aerial vehicles, be provided with the insulator pick-up unit at many rotor wing unmanned aerial vehicles, this device comprises surveys the upper utmost point 1, survey the lower utmost point 2, connect respectively voltage sensor 3, after two voltage sensors 3 will be surveyed the upper and lower utmost point 1,2 voltage analog signals that obtain and be converted into digital signal by A/D conversion unit 4, input DSP processing unit 5 carries out data to be processed, and DSP processing unit 5 input ends also are connected with the flight control system airborne control computer 6 of many rotor wing unmanned aerial vehicles.
Many rotor wing unmanned aerial vehicles comprise flight control system airborne control computer 6, and coupled have unmanned plane satellite positioning module 7, unmanned plane digital compass 8, unmanned plane three-axis gyroscope 9, unmanned plane three axis accelerometer 10, steering engine for unmanned plane controller 11, unmanned plane barometric altimeter 12, unmanned plane rotating speed measuring sensor 13, unmanned plane PCM remote-control receiver 14, an airborne wireless communication unit 15; Wherein the unmanned plane satellite positioning module 7, unmanned plane digital compass 8, unmanned plane three-axis gyroscope 9, unmanned plane three axis accelerometer 10, unmanned plane barometric altimeter 12, unmanned plane rotating speed measuring sensor 13, unmanned plane PCM remote-control receiver 14 is all analyzed the data input flight control system airborne control computer 6 that gathers, many rotor wing unmanned aerial vehicles that flight control system airborne control computer 6 collects unmanned plane satellite positioning module 7 and unmanned plane barometric altimeter 12 when detecting the GPS value and after the potential difference values inputted of height value and detected DSP processing unit 5 is complementary, transfer data to land station's radio communication unit 18 by airborne wireless communication unit 15, thereby land station's signal conditioning package 19 can be with sense potential difference data analyzing and processing, and in conjunction with GPS value and height value, the insulator sheet that can judge non-normal working belongs to which sheet with the position insulator chain.
Also carry high-definition camera 20 on many rotor wing unmanned aerial vehicles, high-definition camera 20 links to each other with flight control system airborne control computer 6, not only can send the collection video to land station's radio communication unit 18 by airborne wireless communication unit 15, but by the state of flight of the many rotor wing unmanned aerial vehicles of the personnel of land station Real Time Monitoring; Simultaneously, can be at many rotor wing unmanned aerial vehicles near the image that relies on high-definition camera 20 to pass back in real time in the process of insulator, can control flight control system airborne control computer 6 regulates flying height and surveys the distance between the utmost point 2 under the upper utmost point 1 and the detection, the utmost point 2 can be distinguished the connect insulator two ends under making the upper utmost point 1 of detection and surveying, and records respectively potential value.
Flight control system airborne control computer 6 is after receiving land station's information handling system upper utmost point 1 of 19 adjusting detections and survey the signal of the distance between the lower utmost point 2 by airborne wireless communication unit 15, send instruction to lifting unit 21, change the distance of surveying between the upper utmost point 1 and the lower utmost point 2 of detection thereby regulate lifting structure 22 by lifting unit 21.Wherein, lifting unit 21 is a programmable single chip computer, and it is connected with electric-motor drive unit in the lifting structure 22, and the distance signal that mainly flight control system airborne control computer 6 is sent is converted into motor drive signal, to regulate lifting structure 22.
Flight control system airborne control computer 6 is after the potential difference values that obtains 5 inputs of DSP processing unit, for reduce the detection time of connect insulator as far as possible, improve and detect security, can export to 11 1 of steering engine for unmanned plane controllers and flick order, and then by steering engine for unmanned plane controller 11 control Servo-controllers 16, command many rotor module actions 17, leave insulator according to predefined route rapidly.
Such as Fig. 2, detect the schematic appearance of insulator arrangement for many rotor wing unmanned aerial vehicles.The utmost point 1 in the detection, and two metal rings about surveying the lower utmost point 2 and be are connected with all adopting the Carbon Hollow Fiber pipe insulation between body and the rotor; The wire that voltage sensor 3 and two ends thereof link to each other all is in carbon fiber pipe inside; The rotor wire that links to each other with steering wheel also is in carbon fiber pipe inside; Remaining part all is in fixed installation in many rotor wing unmanned aerial vehicles agent structure, and wherein high-definition camera 20 is toward the outer side fixed installation; Need satisfy rotor wing unmanned aerial vehicle counterweigh requirement during installation, for each component locations and order no requirement (NR).
The step of the utility model barrier-avoiding method is:
Step 1: in the flight control system airborne control computer, arrange and flick the performed circuit of order and distance;
Step 2: the typical curve that in land station's information handling system, sets the insulator electric potential difference;
Step 3: tentatively choose many rotor wing unmanned aerial vehicles place of taking off, and flying height is set;
Step 4: after lift-launch insulator pick-up unit takes off on many rotor wing unmanned aerial vehicles, slowly regulate in real time the position of hovering according to high-definition image, finally guarantee to survey the upper and lower utmost point and touch respectively up and down two ends of insulator, then by voltage sensor, A/D conversion unit, DSP processing unit measured data are inputted the flight control system airborne control computer;
Step 5: after the flight control system airborne control computer obtains electric potential difference data, to flick immediately order and export to the steering engine for unmanned plane controller, and then by steering engine for unmanned plane controller control Servo-controller, command many rotor module actions, many rotor wing unmanned aerial vehicles will be according to the route of a kind of setting of step with apart from speeding away detected insulator;
Step 6: repeating step four, five, extremely all insulators detect complete on the whole insulator chain;
Step 7: after the insulator chain detection is complete, namely generate insulator numbering (judging insulator particular location and numbering according to GPS, height and detection sequential scheduling information) report of doubtful non-normal working in land station's information process unit.
Described in the coding rule of insulator can arrange referring to the spread voltage of power industry standard DL/T 487-2000 330kV and 500kV interchange aerial power transmission line insulator chain.
In the above-mentioned steps one, the described circuit that flicks command execution and distance need to arrange according to the direction of whole insulator chain with relative position, the distance of shaft tower, wire, when avoiding carrying out this order and the collision of insulator chain, tower and conductor; In addition, also can set the route that flicks namely returns on the former road of route along near this insulator the time.
In the above-mentioned steps two, described typical curve can be with reference to the spread voltage setting of power industry standard DL/T 487-2000 330kV and 500kV interchange aerial power transmission line insulator chain; Because insulator chain voltage respectively also can be slightly variant in varying environment, the region, also can select not arrange typical curve, only in final analysis as a result the time, potential difference values curve plotting with each insulator detection on the whole insulator chain, find the corresponding insulator of the inconsistent point of variation tendency and other each points, be doubtful non-normal working insulator.The method can be referring to the described content of periodical " power equipment " the 8th volume the 3rd phase article March in 2007 " the charged detection technique research of 500kV DC line poor insulator ".
In the above-mentioned steps three, selected place and the flying height of taking off should make insulator chain be in the visual field of high-definition camera under the prerequisite that guarantees safe flight as far as possible, is convenient to the carrying out of step 4.
In the above-mentioned steps four, should be from the insulator sheet of the nearlyer side of distance of wire (with reference to the order of insulator numbering) during detection.
In the above-mentioned steps seven, namely finish the detection of insulator, the doubtful non-normal working insulator numbering report that generates should be sent to line attendant, carry out on this basis the insulator emphasis and change.
Claims (4)
1. rotor wing unmanned aerial vehicle more than a kind detects insulator arrangement, it comprises rotor wing unmanned aerial vehicle more than, be provided with the flight control system airborne control computer at many rotor wing unmanned aerial vehicles, the flight control system airborne control computer is connected with locating device, steering engine for unmanned plane controller, height measuring device, velocity measuring device, unmanned plane PCM remote-control receiver and airborne wireless communication unit, and the airborne wireless communication unit is communicated by letter with land station; Steering engine for unmanned plane controller control Servo-controller, Servo-controller is then controlled many rotor module of many rotor wing unmanned aerial vehicles, it is characterized in that, and described flight control system airborne control computer is connected with high-definition camera; In the detection utmost point be connected down the utmost point and be connected with separately voltage sensor respectively, two voltage sensors all are connected with the A/D conversion unit, the A/D conversion unit is connected with the DSP processing unit, the DSP processing unit is connected with the flight control system airborne control computer; The flight control system airborne control computer also is connected with jacking gear simultaneously, and Ghandler motion was moving under jacking gear drove and surveys.
2. many rotor wing unmanned aerial vehicles as claimed in claim 1 detect insulator arrangement, it is characterized in that, described locating device comprises unmanned plane satellite positioning module, unmanned plane digital compass and unmanned plane three-axis gyroscope, unmanned plane three axis accelerometer, and they all are connected with the flight control system airborne control computer.
3. many rotor wing unmanned aerial vehicles as claimed in claim 1 detect insulator arrangement, it is characterized in that described jacking gear comprises a lifting unit, and it is moving that lifting unit drives the lower Ghandler motion of detection by lifting structure; Two metal rings are connected with many rotor wing unmanned aerial vehicles by the hollow carbon fiber pipe utmost point with being connected down very up and down in the described detection, and the wire that voltage sensor and two ends thereof link to each other all is in carbon fiber pipe inside; Many rotor module wire that links to each other with Servo-controller also is in carbon fiber pipe inside; High-definition camera is toward the outer side fixed installation.
4. many rotor wing unmanned aerial vehicles as claimed in claim 1 detect insulator arrangement, it is characterized in that described land station comprises land station's information handling system, and it is communicated by letter with the airborne wireless communication unit by land station's radio communication unit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220527954 CN202815124U (en) | 2012-10-16 | 2012-10-16 | Insulator detecting device by using multi-rotor unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220527954 CN202815124U (en) | 2012-10-16 | 2012-10-16 | Insulator detecting device by using multi-rotor unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN202815124U true CN202815124U (en) | 2013-03-20 |
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Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102879692A (en) * | 2012-10-16 | 2013-01-16 | 山东电力集团公司电力科学研究院 | Method and device for detecting insulator through multi-rotor unmanned aerial vehicle |
| CN105301463A (en) * | 2015-11-30 | 2016-02-03 | 国网山西省电力公司临汾供电公司 | Unmanned plane insulator zero measurement device |
| CN105492985A (en) * | 2014-09-05 | 2016-04-13 | 深圳市大疆创新科技有限公司 | Multi-sensor environment map building |
| CN107765134A (en) * | 2017-10-24 | 2018-03-06 | 深圳供电局有限公司 | A kind of method and unmanned plane of the lightning arrester live-line test for carrying out transmission line of electricity |
| US10001778B2 (en) | 2014-09-05 | 2018-06-19 | SZ DJI Technology Co., Ltd | Velocity control for an unmanned aerial vehicle |
| US10029789B2 (en) | 2014-09-05 | 2018-07-24 | SZ DJI Technology Co., Ltd | Context-based flight mode selection |
| CN108508335A (en) * | 2018-04-02 | 2018-09-07 | 中铁第四勘察设计院集团有限公司 | A kind of insulating padding block for dry type transformer environmental suitability evaluation method and equipment |
| US10240930B2 (en) | 2013-12-10 | 2019-03-26 | SZ DJI Technology Co., Ltd. | Sensor fusion |
| CN113013783A (en) * | 2021-02-24 | 2021-06-22 | 苏玉凤 | Power insulator maintenance construction system and construction method |
| CN113156274A (en) * | 2021-01-27 | 2021-07-23 | 南京工程学院 | Degraded insulator non-contact detection system and method based on unmanned aerial vehicle |
| US11368002B2 (en) | 2016-11-22 | 2022-06-21 | Hydro-Quebec | Unmanned aerial vehicle for monitoring an electrical line |
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2012
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| CN102879692A (en) * | 2012-10-16 | 2013-01-16 | 山东电力集团公司电力科学研究院 | Method and device for detecting insulator through multi-rotor unmanned aerial vehicle |
| US10240930B2 (en) | 2013-12-10 | 2019-03-26 | SZ DJI Technology Co., Ltd. | Sensor fusion |
| US10421543B2 (en) | 2014-09-05 | 2019-09-24 | SZ DJI Technology Co., Ltd. | Context-based flight mode selection |
| US10901419B2 (en) | 2014-09-05 | 2021-01-26 | SZ DJI Technology Co., Ltd. | Multi-sensor environmental mapping |
| US10001778B2 (en) | 2014-09-05 | 2018-06-19 | SZ DJI Technology Co., Ltd | Velocity control for an unmanned aerial vehicle |
| US10029789B2 (en) | 2014-09-05 | 2018-07-24 | SZ DJI Technology Co., Ltd | Context-based flight mode selection |
| US11914369B2 (en) | 2014-09-05 | 2024-02-27 | SZ DJI Technology Co., Ltd. | Multi-sensor environmental mapping |
| CN105492985A (en) * | 2014-09-05 | 2016-04-13 | 深圳市大疆创新科技有限公司 | Multi-sensor environment map building |
| US11370540B2 (en) | 2014-09-05 | 2022-06-28 | SZ DJI Technology Co., Ltd. | Context-based flight mode selection |
| US10429839B2 (en) | 2014-09-05 | 2019-10-01 | SZ DJI Technology Co., Ltd. | Multi-sensor environmental mapping |
| US10845805B2 (en) | 2014-09-05 | 2020-11-24 | SZ DJI Technology Co., Ltd. | Velocity control for an unmanned aerial vehicle |
| CN105301463A (en) * | 2015-11-30 | 2016-02-03 | 国网山西省电力公司临汾供电公司 | Unmanned plane insulator zero measurement device |
| US11368002B2 (en) | 2016-11-22 | 2022-06-21 | Hydro-Quebec | Unmanned aerial vehicle for monitoring an electrical line |
| CN107765134A (en) * | 2017-10-24 | 2018-03-06 | 深圳供电局有限公司 | A kind of method and unmanned plane of the lightning arrester live-line test for carrying out transmission line of electricity |
| CN107765134B (en) * | 2017-10-24 | 2023-11-14 | 深圳供电局有限公司 | Method for carrying out live test on lightning arrester of power transmission line and unmanned aerial vehicle |
| CN108508335A (en) * | 2018-04-02 | 2018-09-07 | 中铁第四勘察设计院集团有限公司 | A kind of insulating padding block for dry type transformer environmental suitability evaluation method and equipment |
| CN113156274A (en) * | 2021-01-27 | 2021-07-23 | 南京工程学院 | Degraded insulator non-contact detection system and method based on unmanned aerial vehicle |
| CN113013783A (en) * | 2021-02-24 | 2021-06-22 | 苏玉凤 | Power insulator maintenance construction system and construction method |
| CN113013783B (en) * | 2021-02-24 | 2022-11-04 | 国网甘肃省电力公司陇南供电公司 | Power insulator maintenance construction system and construction method |
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Address after: 250002, No. 1, South Second Ring Road, Shizhong District, Shandong, Ji'nan Co-patentee after: STATE GRID CORPORATION OF CHINA Patentee after: ELECTRIC POWER RESEARCH INSTITUTE OF STATE GRID SHANDONG ELECTRIC POWER Co. Address before: 250002, No. 1, South Second Ring Road, Shizhong District, Shandong, Ji'nan Co-patentee before: State Grid Corporation of China Patentee before: ELECTRIC POWER RESEARCH INSTITUTE OF SHANDONG ELECTRIC POWER Corp. |
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Assignee: National Network Intelligent Technology Co.,Ltd. Assignor: ELECTRIC POWER RESEARCH INSTITUTE OF STATE GRID SHANDONG ELECTRIC POWER Co. Contract record no.: X2019370000006 Denomination of utility model: Insulator detecting device by using multi-rotor unmanned aerial vehicle Granted publication date: 20130320 License type: Exclusive License Record date: 20191014 |
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