CN114062722B - Unmanned aerial vehicle electroscope - Google Patents
Unmanned aerial vehicle electroscope Download PDFInfo
- Publication number
- CN114062722B CN114062722B CN202111351556.1A CN202111351556A CN114062722B CN 114062722 B CN114062722 B CN 114062722B CN 202111351556 A CN202111351556 A CN 202111351556A CN 114062722 B CN114062722 B CN 114062722B
- Authority
- CN
- China
- Prior art keywords
- electroscope
- aerial vehicle
- unmanned aerial
- guide
- net
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 239000004033 plastic Substances 0.000 claims abstract description 67
- 229920003023 plastic Polymers 0.000 claims abstract description 67
- 238000001514 detection method Methods 0.000 claims description 27
- 238000012360 testing method Methods 0.000 claims description 13
- 239000003381 stabilizer Substances 0.000 claims description 8
- 230000005611 electricity Effects 0.000 description 18
- 238000007689 inspection Methods 0.000 description 6
- 238000000034 method Methods 0.000 description 4
- 230000009194 climbing Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000013508 migration Methods 0.000 description 1
- 230000005012 migration Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R1/00—Details of instruments or arrangements of the types included in groups G01R5/00 - G01R13/00 and G01R31/00
- G01R1/02—General constructional details
- G01R1/04—Housings; Supporting members; Arrangements of terminals
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R19/00—Arrangements for measuring currents or voltages or for indicating presence or sign thereof
- G01R19/145—Indicating the presence of current or voltage
Abstract
The unmanned aerial vehicle electroscope comprises an unmanned aerial vehicle, wherein a light plastic net cage is arranged on the unmanned aerial vehicle, and is of a box body structure formed by light plastic rods.
Description
Technical Field
The invention relates to an electroscope, in particular to an unmanned aerial vehicle electroscope.
Background
The traditional electricity testing mode is that a worker carries an electroscope on a tower, and the steps of firstly low-voltage and then high-voltage, firstly lower and then upper and secondly near and then far are carried out on the line phase by phase. In the method, operators need to bear the electroscope to go on the tower, so that the method is inconvenient, the danger coefficient of climbing the tower and working at high positions is increased, and a certain threat is formed to safe production work; secondly, the operation personnel need take out in the high altitude and expand and put the longer telescopic electroscope back and can carry out the electricity test, and after the electroscope is expanded and is put and accomplish, the operation personnel need guarantee that the electroscope is contacted with the wire steadily and just can accurately judge whether the circuit does not have voltage, has increased the electricity test time by a wide margin. In sum, the traditional electricity checking method needs longer electricity checking time, and the danger coefficient is higher when the operator works at a high place, so that the work efficiency of power failure overhaul is affected to a certain extent. At present, in the electricity test work of ultra-high voltage transmission lines, no reliable method exists yet, and the electricity test can be effectively and quickly performed under the condition that an operator is not required to climb a tower.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle electroscope, which can be combined with an electroscope body by using an unmanned aerial vehicle, and the electroscope body is driven to fly above a guide wire by using the unmanned aerial vehicle, so that the electroscope is realized, the operations of climbing a tower and working at a high place by workers are omitted, the electroscope safety is improved, and the burden of the workers is lightened.
The invention aims to achieve the aim, and the aim is achieved by the following technical scheme:
unmanned aerial vehicle electroscope, including unmanned aerial vehicle, install light plastics box with a net on the unmanned aerial vehicle, the box structure that light plastics box with a net constitutes for light plastics pole, unmanned aerial vehicle sets up in the inside of light plastics box with a net, and electroscope body is connected to unmanned aerial vehicle's bottom, and electroscope detection end is connected to electroscope body's test end, and auxiliary electroscope guiding device is connected to light plastics box with a net's bottom, auxiliary electroscope guiding device includes two guide bars, and two guide bars can constitute the structure of falling the V font, and electroscope detection end can be located the tip inboard of V font structure.
In order to further achieve the purpose of the present invention, the following technical solutions may also be adopted: one side of the inside of the light plastic net cage is connected with a fixing rod, and one end of the fixing rod is connected with the shell of the unmanned aerial vehicle.
The utility model discloses a self-locking elastic rope, including two guide bars, the even light plastic net cage of one end of two guide bars articulates, the end connection gear of guide bar, the center pin of gear and guide bar, the articulated shaft collineation of light plastic net cage, two gears intermesh, the gear on two guide bars articulates each other, the self-locking bounce-back ware locking end is connected to the one end of guide bar, the self-locking bounce-back ware is locked spherical end is connected to the bottom of light plastic net cage, self-locking bounce-back ware locking end can be locked the self-locking bounce-back ware by locking spherical end, install the elastic rope between two guide bars, the both ends of elastic rope are connected with the middle part of two guide bars respectively, the elastic rope is in tensile state.
The utility model discloses a motor, including the even light plastic net cage of one end of two guide bars, the end connection gear of guide bar, the center pin of gear and guide bar, the articulated shaft collineation of light plastic net cage, two gears intermesh, the gear on two guide bars articulates each other, install the elastic rope between two guide bars, the both ends of elastic rope are connected with the middle part of two guide bars respectively, the elastic rope is in tensile state, the motor is connected to unmanned aerial vehicle's bottom, the output shaft of motor is the reel, the traction rope is connected to one side of reel, the one end and the middle part of guide bar of traction rope are connected.
The four corners of the bottom of the light plastic net cage are connected with one supporting leg. The lower extreme of stabilizer blade is connected the protection rope, and the one end and the stabilizer blade cooperation of protection rope, the other end and the unmanned aerial vehicle's of protection rope bottom are connected, and the protection rope is in the state of tightening.
One side of the guide rod is connected with an L-shaped rod, two ends of the L-shaped rod are connected with the guide rod, the corner of the L-shaped rod can be matched with the detection end of the electroscope, and the L-shaped rod is an insulating rod.
The invention has the advantages that: according to the invention, the unmanned aerial vehicle is combined with the electroscope body, and the unmanned aerial vehicle is used for driving the electroscope body to fly above the lead, so that electricity inspection is realized, operations of workers on towers and high-place operation are omitted, the electricity inspection safety is improved, and the burden of workers is reduced. The light plastic net cage is combined with the unmanned aerial vehicle, and a box structure formed by a light plastic net can be formed around the unmanned aerial vehicle, so that the unmanned aerial vehicle is protected, the fan blades of the unmanned aerial vehicle are prevented from being collided with the lead, and the box structure formed by the light plastic rod can be prevented from hooking the lead in comparison with the existing rod-shaped protection structure. When electricity is tested, the unmanned aerial vehicle drives the electroscope detection end to fly to the wire top, because the control unmanned aerial vehicle drives electroscope detection end and wire cooperation degree of difficulty great, when the electricity is tested, the inverted V font structure that two guide bars constitute can lead the wire to make things convenient for electroscope detection end and wire complex success rate.
Drawings
The accompanying drawings are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate the invention and together with the embodiments of the invention, serve to explain the invention. In the drawings:
FIG. 1 is a schematic diagram of the structure of the present invention;
FIG. 2 is a second schematic diagram of the structure of the present invention;
FIG. 3 is a schematic view of a garment structure of a lightweight plastic cage;
FIG. 4 is a third schematic diagram of the structure of the present invention.
Detailed Description
Preferred embodiments of the present invention will be described below with reference to the accompanying drawings.
Example 1:
unmanned aerial vehicle electroscope, as shown in fig. 1-4, including unmanned aerial vehicle 2, install light plastics box with a net 1 on the unmanned aerial vehicle 2, light plastics box with a net 1 is the box structure that light plastics pole constitutes, and unmanned aerial vehicle 2 sets up in the inside of light plastics box with a net 1, and electroscope body 5 is connected to unmanned aerial vehicle 2's bottom, and electroscope detection end 9 is connected to electroscope body 5's test end, and auxiliary electroscope guiding device is connected to light plastics box with a net 1's bottom, auxiliary electroscope guiding device includes two guide bars 7, and two guide bars 7 can constitute the structure of falling the V font, and electroscope detection end 9 can be located the tip inboard of V font structure.
According to the invention, the unmanned aerial vehicle 2 is combined with the electroscope body 5, and the unmanned aerial vehicle is used for driving the electroscope body 5 to fly above the guide line, so that electricity is tested, the operations of climbing a tower and working at a high place by workers are omitted, the electricity testing safety is improved, and the burden of the workers is reduced. The light plastic net cage 1 is combined with the unmanned aerial vehicle 2, and a box body structure formed by a light plastic net can be formed around the unmanned aerial vehicle 2, so that the unmanned aerial vehicle 2 is protected, the fan blades of the unmanned aerial vehicle 2 are prevented from being collided with the wires easily, and the light plastic net cage can be prevented from hooking the wires by the box body structure formed by the light plastic rods in the existing rod-shaped protection structure. When electricity is tested, the unmanned aerial vehicle 2 drives the electroscope detection end 9 to fly above the lead, and the control unmanned aerial vehicle 2 drives the electroscope detection end 9 to be matched with the lead, so that the lead can be guided by the inverted V-shaped structure formed by the two guide rods 7 when electricity is tested, and the success rate of the electroscope detection end 9 and the lead is convenient.
And (3) material selection and feasibility analysis of the application range implementation: the practical manufacturing sample is implemented according to the proportion and the matching mode of all parts in the specification drawing by taking the specification drawing as the drawing, the connection is a common connection mode such as a strong adhesive connection, welding and riveting flange connection integrated connection and the like, and the thickness and the strength of the connection point of the corresponding connection mode can be selected without creative need according to the practical connection strength during practical manufacturing. During specific operation, unmanned aerial vehicle 2 drives electroscope detection end 9 to fly to the wire top, then operating personnel control unmanned aerial vehicle 2 whereabouts, lets the wire get into the inboard of the reverse V font structure that two guide bars 7 constitute, then slowly controls unmanned aerial vehicle 2 whereabouts, and the reverse V font structure that two guide bars 7 constitute can drive unmanned aerial vehicle 2 and produce horizontal migration under the wire effect this moment to let electroscope detection end 9 and wire cooperation.
Example 2:
unmanned aerial vehicle electroscope, as shown in fig. 1-3, including unmanned aerial vehicle 2, install light plastics box with a net 1 on the unmanned aerial vehicle 2, light plastics box with a net 1 is the box structure that light plastics pole constitutes, and unmanned aerial vehicle 2 sets up in the inside of light plastics box with a net 1, and electroscope body 5 is connected to unmanned aerial vehicle 2's bottom, and electroscope detection end 9 is connected to electroscope body 5's test end, and auxiliary electroscope guiding device is connected to light plastics box with a net 1's bottom, auxiliary electroscope guiding device includes two guide bars 7, and two guide bars 7 can constitute the structure of falling the V font, and electroscope detection end 9 can be located the tip inboard of V font structure.
One side of the inside of the light plastic net cage 1 is connected with a fixing rod 11, and one end of the fixing rod 11 is connected with the shell of the unmanned aerial vehicle 2.
The fixing rod 11 can facilitate the connection of the light plastic net cage 1 and the unmanned aerial vehicle 2, and prevent the fan blades of the unmanned aerial vehicle 2 from colliding with the light plastic net cage 1.
Example 3:
unmanned aerial vehicle electroscope, as shown in fig. 1-3, including unmanned aerial vehicle 2, install light plastics box with a net 1 on the unmanned aerial vehicle 2, light plastics box with a net 1 is the box structure that light plastics pole constitutes, and unmanned aerial vehicle 2 sets up in the inside of light plastics box with a net 1, and electroscope body 5 is connected to unmanned aerial vehicle 2's bottom, and electroscope detection end 9 is connected to electroscope body 5's test end, and auxiliary electroscope guiding device is connected to light plastics box with a net 1's bottom, auxiliary electroscope guiding device includes two guide bars 7, and two guide bars 7 can constitute the structure of falling the V font, and electroscope detection end 9 can be located the tip inboard of V font structure. The utility model discloses a light plastic net cage 1 is evenly articulated to the one end of two guide bars 7, the end connection gear 6 of guide bar 7, the center pin of gear 6 and guide bar 7, the articulated shaft collineation of light plastic net cage 1, two gears 6 intermeshing, the gear 6 on two guide bars 7 articulates each other, self-locking rebound ware locking end 13 is connected to the one end of guide bar 7, self-locking rebound ware is locked spherical end 12 is connected to the bottom of light plastic net cage 1, self-locking rebound ware locking end 13 can be locked self-locking rebound ware by locking spherical end 12, install elastic rope 8 between two guide bars 7, the both ends of elastic rope 8 are connected with the middle part of two guide bars 7 respectively, elastic rope 8 is in tensile state.
Before taking off, an operator can release the locking end 13 of the self-locking rebound device from the locked spherical end 12 of the self-locking rebound device, and at the moment, the elastic rope 8 drives the two guide rods 7 to be converted into an inverted V-shaped structure so as to provide guidance for the detection end 9 of the electroscope, when the device is required to be transported and stored, the user can fold and retract the guide rods 7, and the locked spherical end 12 of the self-locking rebound device is locked by the locking end 13 of the self-locking rebound device, so that the guide rods 7 are kept in a retracted state.
Example 4:
unmanned aerial vehicle electroscope, as shown in fig. 1-3, including unmanned aerial vehicle 2, install light plastics box with a net 1 on the unmanned aerial vehicle 2, light plastics box with a net 1 is the box structure that light plastics pole constitutes, and unmanned aerial vehicle 2 sets up in the inside of light plastics box with a net 1, and electroscope body 5 is connected to unmanned aerial vehicle 2's bottom, and electroscope detection end 9 is connected to electroscope body 5's test end, and auxiliary electroscope guiding device is connected to light plastics box with a net 1's bottom, auxiliary electroscope guiding device includes two guide bars 7, and two guide bars 7 can constitute the structure of falling the V font, and electroscope detection end 9 can be located the tip inboard of V font structure.
The even light plastic net cage 1 of one end of two guide bars 7 articulates, the end connection gear 6 of guide bar 7, the center pin of gear 6 and guide bar 7, the articulated shaft collineation of light plastic net cage 1, two gears 6 intermeshing, gear 6 on two guide bars 7 articulates each other, install elastic rope 8 between two guide bars 7, elastic rope 8's both ends are connected with the middle part of two guide bars 7 respectively, elastic rope 8 is in tensile state, motor 3 is connected to the bottom of unmanned aerial vehicle 2, motor 3's output shaft connection reel 14, traction rope 4 is connected to one side of reel 14, traction rope 4's one end is connected with the middle part of guide bar 7.
When the two guide rods 7 are used for electricity inspection, the motor 3 is used for releasing the traction rope 4, so that the two guide rods 7 are converted into an inverted V-shaped structure to guide the inspection end 9 of the electricity inspection, and after the electricity inspection is finished, the motor 3 can retract the traction rope 4, so that the two guide rods 7 are converted into a state shown in fig. 2, and the influence of the guide rods 7 on the landing of the unmanned aerial vehicle 2 is avoided.
Example 5:
unmanned aerial vehicle electroscope, as shown in fig. 1-3, including unmanned aerial vehicle 2, install light plastics box with a net 1 on the unmanned aerial vehicle 2, light plastics box with a net 1 is the box structure that light plastics pole constitutes, and unmanned aerial vehicle 2 sets up in the inside of light plastics box with a net 1, and electroscope body 5 is connected to unmanned aerial vehicle 2's bottom, and electroscope detection end 9 is connected to electroscope body 5's test end, and auxiliary electroscope guiding device is connected to light plastics box with a net 1's bottom, auxiliary electroscope guiding device includes two guide bars 7, and two guide bars 7 can constitute the structure of falling the V font, and electroscope detection end 9 can be located the tip inboard of V font structure. The stabilizer blade 10 is all connected in the bottom four corners of light plastics box with a net 1, and protection rope 16 is connected to the lower extreme of stabilizer blade 10, and the one end and the stabilizer blade 10 cooperation of protection rope 16, the other end and the bottom of unmanned aerial vehicle 2 of protection rope 16 are connected, and protection rope 16 is in the state of tightening.
The support leg 10 of the present invention can prevent the guide bar 7 folded and retracted from easily contacting the ground. The protective cord 16 prevents the feet 10 from catching on the wire.
One side of the guide rod 7 is connected with an L-shaped rod 15, two ends of the L-shaped rod 15 are connected with the guide rod 7, corners of the L-shaped rod 15 can be matched with the electroscope detection end 9, and the L-shaped rod 15 is an insulating rod.
The L-shaped rod 15 can fill the gap between the guide rod 7 and the electroscope detection end 9 after the guide rod 7 is unfolded, so that the lead is convenient to be matched with the electroscope detection end 9.
The foregoing description is only of the preferred embodiments of the invention and is not intended to limit the invention.
Claims (3)
1. Unmanned aerial vehicle electroscope, its characterized in that: including unmanned aerial vehicle (2), install light plastics box with a net (1) on unmanned aerial vehicle (2), light plastics box with a net (1) is the box structure that light plastics pole constitutes, unmanned aerial vehicle (2) set up in the inside of light plastics box with a net (1), electroscope body (5) are connected to the bottom of unmanned aerial vehicle (2), electroscope detection end (9) are connected to the test end of electroscope body (5), auxiliary electroscope electric conduction device is connected to the bottom of light plastics box with a net (1), auxiliary electroscope electric conduction device includes two guide bars (7), and two guide bars (7) can constitute the structure of falling the V font, and electroscope detection end (9) can be located the tip inboard of V font structure, one side of the inside of light plastics box with a net (1) is connected dead lever (11), and the one end of dead lever (11) is connected with the shell of unmanned aerial vehicle (2), L shape pole (15) are connected to one side of guide bar (7), and the both ends of L shape pole (15) all are connected with guide bar (7), and L shape pole (15) can be the corner of detecting and the pole (9) is the insulating tip of electroscope;
the utility model discloses a self-locking elastic rope device, including two guide rods (7), a self-locking rebound device locking spherical end (12) and an elastic rope (8), wherein one end of each guide rod (7) is evenly hinged to one end of each light plastic net box (1), the end of each guide rod (7) is connected with a gear (6), the central shaft of each gear (6) is collinear with the corresponding guide rod (7) and the hinging shaft of each light plastic net box (1), the gears (6) are meshed with each other, one end of each guide rod (7) is connected with a self-locking rebound device locking end (13), the self-locking rebound device is locked by the locking spherical end (12) through the self-locking rebound device locking end (13), the elastic rope (8) is installed between the two guide rods (7), and two ends of the elastic rope (8) are respectively connected with the middle parts of the two guide rods (7) and are in a stretching state.
2. The unmanned aerial vehicle electroscope of claim 1, wherein: even light plastic net cage (1) of one end of two guide bars (7) is articulated, end connection gear (6) of guide bar (7), the center pin of gear (6) and guide bar (7), the articulated shaft collineation of light plastic net cage (1), two gears (6) intermeshing, gear (6) on two guide bars (7) are articulated each other, install elastic rope (8) between two guide bars (7), the both ends of elastic rope (8) are connected with the middle part of two guide bars (7) respectively, elastic rope (8) are in tensile state, motor (3) are connected to the bottom of unmanned aerial vehicle (2), output shaft connection reel (14) of motor (3), traction rope (4) are connected to one side of reel (14), the one end and the middle part of guide bar (7) of traction rope (4) are connected.
3. The unmanned aerial vehicle electroscope of claim 1, wherein: the bottom four corners of light plastics box with a net (1) all are connected a stabilizer blade (10), and protection rope (16) are connected to the lower extreme of stabilizer blade (10), and the one end and the stabilizer blade (10) cooperation of protection rope (16), the other end and the bottom of unmanned aerial vehicle (2) of protection rope (16) are connected, and protection rope (16) are in the state of tightening.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111351556.1A CN114062722B (en) | 2021-11-15 | 2021-11-15 | Unmanned aerial vehicle electroscope |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111351556.1A CN114062722B (en) | 2021-11-15 | 2021-11-15 | Unmanned aerial vehicle electroscope |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN114062722A CN114062722A (en) | 2022-02-18 |
| CN114062722B true CN114062722B (en) | 2024-04-02 |
Family
ID=80272772
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202111351556.1A Active CN114062722B (en) | 2021-11-15 | 2021-11-15 | Unmanned aerial vehicle electroscope |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN114062722B (en) |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108599007A (en) * | 2018-03-29 | 2018-09-28 | 武汉大学 | A kind of apparatus and method of high-tension line unmanned plane installation pulley insulating cord |
| CN109398702A (en) * | 2018-11-06 | 2019-03-01 | 广东电网有限责任公司 | A kind of line of fall device and its line of fall method dropproof based on unmanned plane |
| CN109459603A (en) * | 2018-06-21 | 2019-03-12 | 国网浙江江山市供电有限公司 | Distribution overhead line unmanned plane electroscopic device |
| CN209375014U (en) * | 2019-03-15 | 2019-09-10 | 国网安徽省电力有限公司宣城供电公司 | A kind of distribution line inspection device |
| CN110854739A (en) * | 2019-11-29 | 2020-02-28 | 国网福建省电力有限公司厦门供电公司 | Overhead transmission line electricity testing grounding method based on unmanned aerial vehicle |
| CN111879995A (en) * | 2020-08-14 | 2020-11-03 | 广东电网有限责任公司 | Electricity testing device and electricity testing method |
| CN112490928A (en) * | 2020-11-12 | 2021-03-12 | 叶飞 | High-altitude power distribution overhead line live working method and platform based on unmanned aerial vehicle technology |
| CN112550708A (en) * | 2020-12-10 | 2021-03-26 | 国网浙江省电力有限公司江山市供电公司 | Unmanned aerial vehicle tests electrical equipment |
| CN216956163U (en) * | 2021-11-15 | 2022-07-12 | 国家电网有限公司 | Unmanned aerial vehicle electroscope |
| JP2022140959A (en) * | 2021-03-15 | 2022-09-29 | 中部電力株式会社 | Conduction confirmation method of conductor |
-
2021
- 2021-11-15 CN CN202111351556.1A patent/CN114062722B/en active Active
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108599007A (en) * | 2018-03-29 | 2018-09-28 | 武汉大学 | A kind of apparatus and method of high-tension line unmanned plane installation pulley insulating cord |
| CN109459603A (en) * | 2018-06-21 | 2019-03-12 | 国网浙江江山市供电有限公司 | Distribution overhead line unmanned plane electroscopic device |
| CN109398702A (en) * | 2018-11-06 | 2019-03-01 | 广东电网有限责任公司 | A kind of line of fall device and its line of fall method dropproof based on unmanned plane |
| CN209375014U (en) * | 2019-03-15 | 2019-09-10 | 国网安徽省电力有限公司宣城供电公司 | A kind of distribution line inspection device |
| CN110854739A (en) * | 2019-11-29 | 2020-02-28 | 国网福建省电力有限公司厦门供电公司 | Overhead transmission line electricity testing grounding method based on unmanned aerial vehicle |
| CN111879995A (en) * | 2020-08-14 | 2020-11-03 | 广东电网有限责任公司 | Electricity testing device and electricity testing method |
| CN112490928A (en) * | 2020-11-12 | 2021-03-12 | 叶飞 | High-altitude power distribution overhead line live working method and platform based on unmanned aerial vehicle technology |
| CN112550708A (en) * | 2020-12-10 | 2021-03-26 | 国网浙江省电力有限公司江山市供电公司 | Unmanned aerial vehicle tests electrical equipment |
| JP2022140959A (en) * | 2021-03-15 | 2022-09-29 | 中部電力株式会社 | Conduction confirmation method of conductor |
| CN216956163U (en) * | 2021-11-15 | 2022-07-12 | 国家电网有限公司 | Unmanned aerial vehicle electroscope |
Non-Patent Citations (2)
| Title |
|---|
| 新型输电线路无人机验电装置研究;刘博迪;《电气工艺》(第21期);130-131 * |
| 无人机非接触式验电装置系统的开发与应用;熊猛;《河南科技》(第29期);72-74 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN114062722A (en) | 2022-02-18 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN110412059B (en) | Live radiation detection device for power transmission line hardware fitting and application method thereof | |
| CN103336153B (en) | High-voltage test junction pole | |
| CN205049690U (en) | Cable terminal partial discharge test auxiliary device | |
| CN206362918U (en) | Remote control termination for altitude test wiring unmanned aerial vehicle platform | |
| CN216956163U (en) | Unmanned aerial vehicle electroscope | |
| CN112563965B (en) | Power transmission line inspection robot and method | |
| CN114062722B (en) | Unmanned aerial vehicle electroscope | |
| CN106494640A (en) | A kind of multi-rotor unmanned aerial vehicle test and training unified platform | |
| CN110912018A (en) | Folding insulation shielding device on rod | |
| CN106556538B (en) | Multi-angle tensile test structure | |
| CN105811307A (en) | Full-automatic inspection robot applicable to power transmission line insulator string | |
| CN113071676A (en) | Unmanned aerial vehicle suspension test pencil electricity testing device and method | |
| US20220355930A1 (en) | Payload support frame for unmanned aerial system | |
| CN106501748A (en) | A kind of altitude test mode of connection based on unmanned air vehicle technique | |
| CN215645838U (en) | Electric wire netting overhauls spacing umbrella of insulation | |
| CN210707885U (en) | Unmanned aerial vehicle is patrolled and examined to electric power | |
| CN218298368U (en) | Unmanned aerial vehicle inspection device | |
| CN209258388U (en) | A kind of high-tension apparatus electrical verification unmanned plane | |
| CN106094814A (en) | A kind of full-automatic lightning arrester live-line test dolly | |
| CN207142720U (en) | A kind of unmanned plane special guide pulley and its jettison system | |
| CN211348324U (en) | High altitude test point quick termination | |
| CN219533307U (en) | Portable wireless test device for partial discharge test | |
| CN103437698A (en) | Retractable insulating ladder for overhaul at high altitude | |
| CN208242696U (en) | A kind of high-tension line bird-scaring unit installation tool | |
| CN217334840U (en) | Electric operating rod is tested to integral type pull rod |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |