CN219172686U - Remote control patrol aircraft for low-altitude cable - Google Patents
Remote control patrol aircraft for low-altitude cable Download PDFInfo
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- CN219172686U CN219172686U CN202223535246.8U CN202223535246U CN219172686U CN 219172686 U CN219172686 U CN 219172686U CN 202223535246 U CN202223535246 U CN 202223535246U CN 219172686 U CN219172686 U CN 219172686U
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Abstract
The utility model provides a remote control patrol aircraft for a low-altitude cable, which belongs to the technical field of cable patrol equipment and aims to solve the problems that the existing patrol aircraft can only mark the approximate position of a target cable, so that maintenance personnel need to search for a damaged point again and the overhaul efficiency is low, and the remote control patrol aircraft comprises an unmanned body, a supporting fixed column, a cleaning fixed box and a patrol marking mechanism; the four groups of support fixing columns are respectively in a cylindrical structure and are fixedly connected below the support bottom plate; the cleaning fixing box is fixedly connected below the supporting bottom plate, and the lower end of the cleaning fixing box is provided with a rectangular groove structure; the inspection marking mechanism is fixedly connected to the lower portion of the unmanned aerial vehicle body, so that the cleaning and maintenance of the surface of the cable are realized, the temporary leak repairing of the cable damage is realized, the cable damage point is marked, the cable damage point is conveniently searched by a maintainer, and the cable maintenance efficiency is improved.
Description
Technical Field
The utility model belongs to the technical field of cable inspection equipment, and particularly relates to a remote control inspection aircraft for a low-altitude cable.
Background
The safe operation and maintenance of low-altitude cable is whether steady safety of power supply system is related to, in low-altitude cable's use, needs to monitor low-altitude cable's running condition, and current low-altitude cable inspection mode is generally for the personnel of inspecting use remote control unmanned aerial vehicle to inspect low-altitude cable, and current low-altitude cable remote control inspection aircraft generally includes: unmanned aerial vehicle body, remote controller, camera etc..
The prior application number is: the utility model discloses a distribution line inspection device with a current transformer, which comprises an aircraft, wherein a rudder servo machine, an elevating servo machine, a propeller motor and a battery are arranged in the body of the aircraft. The machine body is internally provided with a current transformer and a controller. The current transformer is connected with a gripping clamp, the gripping clamp is used as the primary side of the current transformer for gripping a cable of a power distribution line to be inspected, and the gripping clamp is arranged at the end part of the machine body. The controller is provided with a wireless communication module, the wireless communication module is used for communicating with the remote controller, and the controller is respectively connected with the rudder servo machine, the lifting servo machine, the propeller motor and the current transformer. The operation handle of the remote controller is used for controlling the aircraft to start, lift, turn and hover at the cable of the distribution line, controlling the grasping forceps to grasp the cable, measuring the current value and transmitting the current value to the display screen of the remote controller for display. The distribution line current is conveniently detected by the inspection personnel.
Based on the above, when the existing remote control patrol aircraft for the low-altitude cable is in use, when the cable is damaged on the outer surface, a signal is generally sent to the control center directly, and the control center sends a maintenance personnel to the target position for maintenance, but the general patrol aircraft can only mark the approximate position of the target cable, so that the maintenance personnel needs to search for a damaged point again, the maintenance efficiency is lower, and the damaged point is easy to break down by the current of the cable during waiting for maintenance, so that economic loss is caused.
Disclosure of Invention
In order to solve the technical problems, the utility model provides the remote control patrol aircraft of the low-altitude cable, which aims to solve the problems that when the existing remote control patrol aircraft of the low-altitude cable is in use, when the cable is damaged in appearance, the control center generally directly sends a signal to the control center, and the control center sends maintenance personnel to a target position for maintenance, but the general patrol aircraft only marks the approximate position of the target cable, so that the maintenance personnel needs to search for a damaged point again, the maintenance efficiency is lower, and the damaged point is easy to break down by the current of the cable during waiting for maintenance, thereby causing economic loss.
The utility model discloses a remote control patrol aircraft of a low-altitude cable, which is characterized by comprising the following specific technical means:
the remote control inspection aircraft for the low-altitude cable comprises an unmanned body, a supporting bottom plate, a camera, supporting fixed columns, a cleaning fixed box and an inspection marking mechanism;
the two groups of supporting bottom plates are arranged in total and are fixedly connected below the unmanned aerial vehicle body;
the camera is arranged below the unmanned aerial vehicle body;
the four groups of support fixing columns are respectively in a cylindrical structure and are fixedly connected below the support bottom plate;
the cleaning fixing box is fixedly connected below the supporting bottom plate, and the lower end of the cleaning fixing box is provided with a rectangular groove structure;
the inspection marking mechanism is fixedly connected below the unmanned aerial vehicle body.
Further, the support fixed column includes: a supporting sliding piece, a sucker base and a buffer spring;
the four groups of support sliding parts are respectively in a cylindrical structure and are all connected below the support fixing columns in a sliding manner;
the four groups of sucker bases are respectively fixedly connected below the supporting sliding piece, and the sucker bases are respectively of sucker structures;
the buffer springs are arranged in four groups, the upper ends of the four groups of buffer springs are fixedly connected with the inside of the supporting fixed column, and the lower ends of the four groups of buffer springs are fixedly connected with the inside of the supporting sliding piece.
Further, clean fixed case is including: the cleaning device comprises a cleaning driving motor, a cleaning driving screw rod, a cleaning sliding block and a cleaning plate;
the cleaning driving motor is fixedly connected to the left side of the cleaning fixing box;
the cleaning driving screw rod is rotationally connected in the cleaning fixing box, the left end of the cleaning driving screw rod is fixedly connected with the rotating shaft of the cleaning driving motor in a coaxial manner, and threads with different rotation directions are respectively arranged at the left end and the right end of the cleaning driving screw rod;
the two groups of cleaning sliding blocks are arranged in total and are respectively connected with the periphery of the cleaning driving screw rod in a threaded manner;
the cleaning plates are arranged in two groups, the two groups of cleaning plates are respectively in a semicircular structure, and the cleaning plates are respectively and fixedly connected below the cleaning sliding blocks.
Further, the cleaning fixing box further comprises: a flexible cleaning member;
the flexible cleaning pieces are arranged in two groups, the two groups of flexible cleaning pieces are respectively and fixedly connected to the inner periphery of the cleaning plate, and the flexible cleaning pieces are respectively of a semicircular rubber structure.
Further, the inspection marking mechanism comprises: the device comprises a marking driving box, a marking driving motor, a marking limiting plate, a marking lead screw and a marking sliding plate;
the marking driving box is fixedly connected below the unmanned aerial vehicle body;
the marking driving motor is fixedly connected to the upper end of the inside of the marking driving box;
the marking limiting plates are respectively fixedly connected to the front side and the rear side of the inside of the marking driving box, and are respectively provided with a rectangular groove structure;
the marking screw rod is rotationally connected in the marking driving box, and the upper end of the marking screw rod is coaxially and fixedly connected with the rotating shaft of the marking driving motor;
the marking slide plate is in threaded connection with the periphery of the marking screw rod, and the front end and the rear end of the marking slide plate are respectively in sliding connection with the inside of the rectangular groove of the marking limiting plate.
Further, the inspection marking mechanism further comprises: a marker ring and a fixing ball;
the marking rings are provided with a plurality of groups, the marking rings are all connected in the marking driving box in a sliding way, the lower ends of the two sides of the action of the marking rings are respectively provided with a circular groove structure, the marking rings are all arranged at the lower ends of the marking sliding plates, and the marking rings are all of semicircular annular plastic structures;
the four groups of fixing balls are respectively and fixedly connected in the marking driving box.
Compared with the prior art, the utility model has the following beneficial effects:
according to the utility model, through the arrangement of the supporting sliding piece, when the whole aircraft falls, the sucker base can enable the contact between the unmanned aerial vehicle body and the ground to be more stable, and meanwhile, the buffer spring realizes the buffer function of the unmanned aerial vehicle body and realizes the buffer protection of the unmanned aerial vehicle body.
According to the utility model, through the arrangement of the cleaning plates, when the inspection of the low-altitude cable is carried out, the unmanned aerial vehicle body is remotely controlled to the upper part of the cable, then the cleaning driving motor is turned on, the cleaning driving motor rotates to drive the cleaning driving screw to rotate, the cleaning driving screw rotates to drive the cleaning sliding block to move oppositely, the cleaning sliding block moves oppositely to drive the cleaning plates to move oppositely, the cable is wrapped by the cleaning plates which move oppositely at the moment, and when the unmanned aerial vehicle body flies for inspection, the two groups of cleaning plates realize cleaning and maintenance on the surface of the cable, so that the service life of the cable is prolonged.
According to the utility model, through the arrangement of the inspection marking mechanism, when an operator of an unmanned aerial vehicle finds a broken position of a cable, the operator can turn on the marking driving motor to rotate the marking screw rod so as to drive the marking sliding plate to move downwards through the rotation of the marking screw rod, and the marking sliding plate moves downwards so as to drive the marking ring to move downwards, so that the marking ring moves downwards to be clamped to the broken position of the cable, the temporary leakage of the broken position of the cable is realized, the broken point of the cable is marked, the cable is conveniently searched by subsequent maintenance personnel, and the maintenance efficiency is accelerated.
The utility model realizes the buffer protection of the unmanned aerial vehicle body, realizes the cleaning and maintenance of the surface of the cable, prolongs the service life of the cable, realizes the temporary leak repair of the damaged part of the cable, marks the damaged point of the cable, facilitates the maintenance personnel to find the damaged point of the cable and improves the maintenance efficiency of the cable.
Drawings
Fig. 1 is a schematic view of the overall structure of the present utility model.
Fig. 2 is a schematic view of the structure of the flexible cleaning member of the present utility model.
Fig. 3 is a schematic view of the structure of the cleaning driving motor of the present utility model.
Fig. 4 is a schematic structural view of the inspection marking mechanism of the present utility model.
FIG. 5 is a schematic cross-sectional view of the inspection marking mechanism of the present utility model.
Fig. 6 is a schematic view of the internal structure of the cleaning and fixing case of the present utility model.
In the figure, the correspondence between the component names and the drawing numbers is:
1. an unmanned body; 2. a support base plate; 3. a camera; 4. supporting the fixed column; 401. a support slider; 402. a sucker base; 403. a buffer spring; 5. cleaning the fixed box; 501. a cleaning drive motor; 502. cleaning a driving screw; 503. cleaning the sliding block; 504. a cleaning plate; 505. a flexible cleaning member; 6. a patrol marking mechanism; 601. a marking drive box; 602. a marking driving motor; 603. marking a limiting plate; 604. marking a lead screw; 605. marking a slide plate; 606. a marker ring; 607. and fixing the ball.
Embodiments of the present utility model are described in further detail below with reference to the accompanying drawings and examples.
Examples:
as shown in fig. 1 to 6:
the utility model provides a remote control patrol aircraft of a low-altitude cable, which comprises an unmanned aerial vehicle body 1, a supporting bottom plate 2, a camera 3, a supporting fixed column 4, a cleaning fixed box 5 and a patrol marking mechanism 6;
the two groups of supporting bottom plates 2 are arranged in total, and the two groups of supporting bottom plates 2 are fixedly connected below the unmanned aerial vehicle body 1;
the camera 3 is arranged below the unmanned body 1;
the four groups of support fixing columns 4 are respectively in a cylindrical structure, and the support fixing columns 4 are fixedly connected below the support bottom plate 2;
the cleaning fixing box 5 is fixedly connected below the supporting bottom plate 2, and the lower end of the cleaning fixing box 5 is provided with a rectangular groove structure;
the inspection marking mechanism 6 is fixedly connected below the unmanned aerial vehicle body 1.
Wherein, support fixed column 4 is including: a support slider 401, a suction cup base 402, and a buffer spring 403;
the four groups of support sliding pieces 401 are arranged in total, the four groups of support sliding pieces 401 are respectively in a cylindrical structure, and the support sliding pieces 401 are all connected below the support fixing columns 4 in a sliding manner;
four groups of sucker bases 402 are arranged, the four groups of sucker bases 402 are respectively and fixedly connected below the supporting sliding piece 401, and the sucker bases 402 are respectively in a sucker structure;
the buffer springs 403 are arranged in four groups, the upper ends of the four groups of buffer springs 403 are fixedly connected with the inside of the supporting fixed column 4, the lower ends of the four groups of buffer springs 403 are fixedly connected with the inside of the supporting sliding part 401, when the whole aircraft falls in use, the sucker base 402 can enable the contact between the unmanned aerial vehicle body 1 and the ground to be more stable, and meanwhile, the buffer springs 403 realize the buffer function of the unmanned aerial vehicle body 1 and realize buffer protection of the unmanned aerial vehicle body 1.
Wherein, clean fixed box 5 is including: a cleaning drive motor 501, a cleaning drive screw 502, a cleaning slider 503, and a cleaning plate 504;
the cleaning driving motor 501 is fixedly connected to the left side of the cleaning fixing case 5;
the cleaning driving screw rod 502 is rotationally connected in the cleaning fixing box 5, the left end of the cleaning driving screw rod 502 is fixedly connected with the rotating shaft of the cleaning driving motor 501 in a coaxial manner, and threads with different rotation directions are respectively arranged at the left end and the right end of the cleaning driving screw rod 502;
two groups of cleaning sliding blocks 503 are arranged, and the two groups of cleaning sliding blocks 503 are respectively connected with the periphery of the cleaning driving screw rod 502 in a threaded manner;
the cleaning plates 504 are arranged in two groups, the two groups of cleaning plates 504 are respectively in a semicircular structure, the cleaning plates 504 are respectively and fixedly connected to the lower portion of the cleaning sliding blocks 503, in use, when the unmanned aerial vehicle body 1 is remotely controlled to the upper portion of the cable when the unmanned aerial vehicle body 1 flies and inspects the cable, then the cleaning driving motor 501 is opened, the cleaning driving motor 501 rotates to drive the cleaning driving screw 502 to rotate, the cleaning driving screw 502 rotates to drive the cleaning sliding blocks 503 to move in opposite directions, the cleaning sliding blocks 503 move in opposite directions to drive the cleaning plates 504 to move in opposite directions, the cable is wrapped by the cleaning plates 504 at the moment, and when the unmanned aerial vehicle body 1 flies and inspects the cable, the two groups of cleaning plates 504 realize cleaning maintenance on the surface of the cable, so that the service life of the cable is prolonged.
Wherein, clean fixed box 5 still includes: a flexible cleaning member 505;
the two groups of the flexible cleaning elements 505 are arranged, the two groups of the flexible cleaning elements 505 are respectively and fixedly connected to the inner periphery of the cleaning plate 504, the flexible cleaning elements 505 are respectively of semicircular rubber structures, and in use, the flexible cleaning elements 505 realize the protection function on the outer surface of a cable.
Wherein, patrol and mark mechanism 6 includes: a marking driving case 601, a marking driving motor 602, a marking limiting plate 603, a marking lead screw 604, and a marking sled 605;
the marking driving box 601 is fixedly connected below the unmanned aerial vehicle body 1;
the marking driving motor 602 is fixedly connected to the inner upper end of the marking driving case 601;
the marking limiting plates 603 are provided with two groups, the two groups of marking limiting plates 603 are respectively fixedly connected to the front side and the rear side of the interior of the marking driving box 601, and the two groups of marking limiting plates 603 are respectively provided with a rectangular groove structure;
the marking screw 604 is rotatably connected inside the marking driving case 601, and the upper end of the marking screw 604 is fixedly connected coaxially with the rotating shaft of the marking driving motor 602;
the marking slide plate 605 is in threaded connection with the periphery of the marking lead screw 604, and the front end and the rear end of the marking slide plate 605 are respectively in sliding connection with the inside of the rectangular groove of the marking limiting plate 603, when an operator of the unmanned aerial vehicle 1 finds a broken position of a cable, the operator can turn on the marking driving motor 602 at this time, the marking driving motor 602 rotates to drive the marking lead screw 604 to rotate, the marking lead screw 604 rotates to drive the marking slide plate 605 to move downwards, and the marking slide plate 605 moves downwards to realize the driving function.
Wherein, inspection marking mechanism 6 still includes: a marker ring 606 and a securing ball 607;
the marking rings 606 are provided with a plurality of groups, the marking rings 606 are all connected in the marking driving box 601 in a sliding way, the lower ends of the two sides of the action of the plurality of groups of marking rings 606 are respectively provided with a circular groove structure, the marking rings 606 are all arranged at the lower end of the marking slide plate 605, and the marking rings 606 are all of a semicircular annular plastic structure;
the four groups of fixing balls 607 are respectively and fixedly connected in the marking driving box 601, when an operator of the unmanned aerial vehicle body 1 finds that a cable has a broken position in use, the operator can turn on the marking driving motor 602 at this time, the marking driving motor 602 rotates to drive the marking screw 604 to rotate, the marking screw 604 rotates to drive the marking sliding plate 605 to move downwards, the marking sliding plate 605 moves downwards to drive the marking ring 606 to move downwards, the marking ring 606 moves downwards to be clamped to the broken position of the cable, the cable breakage point can be found by subsequent maintenance personnel, and the maintenance efficiency can be accelerated.
Specific use and action of the embodiment:
firstly, when the inspection of low-altitude cables is carried out, the unmanned aerial vehicle body 1 is remotely controlled to the upper part of the cables, then the cleaning driving motor 501 is turned on, the cleaning driving motor 501 rotates to drive the cleaning driving screw 502 to rotate, the cleaning driving screw 502 rotates to drive the cleaning sliding block 503 to move oppositely, the cleaning sliding block 503 moves oppositely to drive the cleaning plate 504 to move oppositely, the cables are wrapped by the cleaning plate 504 moving oppositely at the moment, and when the unmanned aerial vehicle body 1 flies and inspects, the two groups of cleaning plates 504 realize cleaning maintenance on the surfaces of the cables, so that the service life of the cables is prolonged.
Then, when the operator of unmanned aerial vehicle body 1 finds that the cable line has broken position, the operator can open mark driving motor 602 this moment, and mark driving motor 602 rotates and drives mark lead screw 604 rotation, and mark lead screw 604 rotates and drives mark slide 605 downwardly moving, and mark slide 605 downwardly moving drives mark ring 606 downwardly moving, and mark ring 606 downwardly moving joint is to the position of broken cable line, has made things convenient for follow-up maintenance personnel to look for the cable line broken point for the efficiency of maintenance.
Finally, when the whole aircraft falls, the sucker base 402 can enable the contact between the unmanned aerial vehicle body 1 and the ground to be more stable, and meanwhile, the buffer spring 403 achieves a buffer function for the unmanned aerial vehicle body 1 and achieves buffer protection for the unmanned aerial vehicle body 1.
Claims (6)
1. The utility model provides a low altitude cable's remote control aircraft of patrolling and examining which characterized in that: the device comprises an unmanned aerial vehicle body (1), a supporting bottom plate (2), a camera (3), supporting fixed columns (4), a cleaning fixed box (5) and a patrol marking mechanism (6); two groups of supporting bottom plates (2) are arranged in total, and the two groups of supporting bottom plates (2) are fixedly connected below the unmanned aerial vehicle body (1); the camera (3) is arranged below the unmanned aerial vehicle body (1); the four groups of support fixing columns (4) are respectively in a cylindrical structure, and the support fixing columns (4) are fixedly connected below the support bottom plate (2); the cleaning fixing box (5) is fixedly connected below the supporting bottom plate (2), and a rectangular groove structure is arranged at the lower end of the cleaning fixing box (5); the inspection marking mechanism (6) is fixedly connected below the unmanned aerial vehicle body (1).
2. The remotely controlled, patrol aircraft for low-altitude cables according to claim 1, wherein: the support fixing column (4) comprises: a support slider (401), a suction cup base (402) and a buffer spring (403); the four groups of support sliding pieces (401) are arranged in total, the four groups of support sliding pieces (401) are respectively of cylindrical structures, and the support sliding pieces (401) are all connected below the support fixing columns (4) in a sliding manner; four groups of sucker bases (402) are arranged in total, the four groups of sucker bases (402) are respectively and fixedly connected below the supporting sliding piece (401), and the sucker bases (402) are respectively of sucker structures; the buffer springs (403) are provided with four groups, the upper ends of the four groups of buffer springs (403) are fixedly connected with the inside of the support fixing column (4), and the lower ends of the four groups of buffer springs (403) are fixedly connected with the inside of the support sliding piece (401).
3. The remotely controlled, patrol aircraft for low-altitude cables according to claim 1, wherein: the cleaning fixing box (5) comprises: a cleaning drive motor (501), a cleaning drive screw (502), a cleaning slider (503), and a cleaning plate (504); the cleaning driving motor (501) is fixedly connected to the left side of the cleaning fixing box (5); the cleaning driving screw rod (502) is rotationally connected in the cleaning fixing box (5), the left end of the cleaning driving screw rod (502) is fixedly connected with the rotating shaft of the cleaning driving motor (501) in a coaxial way, and threads with different rotation directions are respectively arranged at the left end and the right end of the cleaning driving screw rod (502); two groups of cleaning sliding blocks (503) are arranged in total, and the two groups of cleaning sliding blocks (503) are respectively connected with the periphery of the cleaning driving screw rod (502) in a threaded manner; the cleaning plates (504) are arranged in two groups, the two groups of cleaning plates (504) are respectively in a semicircular structure, and the cleaning plates (504) are respectively and fixedly connected below the cleaning sliding blocks (503).
4. A remotely controlled, patrol aircraft for low-altitude cables according to claim 3, wherein: the cleaning fixing box (5) further comprises: a flexible cleaning member (505); the two groups of flexible cleaning elements (505) are arranged in total, the two groups of flexible cleaning elements (505) are respectively and fixedly connected to the inner periphery of the cleaning plate (504), and the flexible cleaning elements (505) are respectively of a semicircular rubber structure.
5. The remotely controlled, patrol aircraft for low-altitude cables according to claim 1, wherein: the inspection marking mechanism (6) comprises: a marking driving box (601), a marking driving motor (602), a marking limiting plate (603), a marking lead screw (604) and a marking sliding plate (605); the marking driving box (601) is fixedly connected below the unmanned aerial vehicle body (1); the marking driving motor (602) is fixedly connected to the upper end of the inside of the marking driving box (601); the marking limiting plates (603) are arranged in two groups, the two groups of marking limiting plates (603) are respectively and fixedly connected to the front side and the rear side of the inside of the marking driving box (601), and the two groups of marking limiting plates (603) are respectively provided with a rectangular groove structure; the marking screw rod (604) is rotatably connected in the marking driving box (601), and the upper end of the marking screw rod (604) is fixedly connected with the rotating shaft of the marking driving motor (602) in a coaxial way; the marking slide plate (605) is in threaded connection with the periphery of the marking screw rod (604), and the front end and the rear end of the marking slide plate (605) are respectively in sliding connection with the inside of the rectangular groove of the marking limiting plate (603).
6. The remotely controlled, patrolling aircraft for low-altitude cables of claim 5, wherein: the inspection marking mechanism (6) further comprises: a marker ring (606) and a securing ball (607); the marking rings (606) are provided with a plurality of groups, the marking rings (606) are all connected in the marking driving box (601) in a sliding way, the lower ends of the two sides of the action of the marking rings (606) are respectively provided with a circular groove structure, the marking rings (606) are all arranged at the lower end of the marking sliding plate (605), and the marking rings (606) are all of a semicircular plastic structure; the four groups of fixing balls (607) are respectively fixedly connected in the marking driving box (601).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223535246.8U CN219172686U (en) | 2022-12-29 | 2022-12-29 | Remote control patrol aircraft for low-altitude cable |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223535246.8U CN219172686U (en) | 2022-12-29 | 2022-12-29 | Remote control patrol aircraft for low-altitude cable |
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| Publication Number | Publication Date |
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| CN219172686U true CN219172686U (en) | 2023-06-13 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202223535246.8U Active CN219172686U (en) | 2022-12-29 | 2022-12-29 | Remote control patrol aircraft for low-altitude cable |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116654308A (en) * | 2023-07-31 | 2023-08-29 | 国电投山西能源服务有限公司 | Maintenance robot for electric power facilities |
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2022
- 2022-12-29 CN CN202223535246.8U patent/CN219172686U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116654308A (en) * | 2023-07-31 | 2023-08-29 | 国电投山西能源服务有限公司 | Maintenance robot for electric power facilities |
| CN116654308B (en) * | 2023-07-31 | 2023-09-29 | 国电投山西能源服务有限公司 | Maintenance robot for electric power facilities |
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